阅读说明：本技术 通过快速扰动可变光束特性光纤产生暂时的视在强度分布 (Temporary apparent intensity profile generation by rapidly perturbing a variable beam characteristic fiber ) 是由 A·W·布朗 D·A·V·克莱尔 R·L·法罗 于 2018-03-28 设计创作，主要内容包括：本发明公开了一种光束传送装置、系统和方法,用于关于一组限制区域中的成员依次调整传播路径,以建立可控的、暂时的视在强度分布。所公开的技术需要对可变光束特性(VBC)光纤施加不同的扰动状态,以改变传播路径和该组限制区域中的经调整的光束的被限制部分从中传播通过的成员,从而在VBC光纤的输出端建立可控的、暂时的视在强度分布。(A beam delivery apparatus, system and method are disclosed for sequentially adjusting the propagation path with respect to members of a set of confined areas to establish a controllable, temporary apparent intensity profile. The disclosed technique entails applying different perturbation states to a Variable Beam Characteristic (VBC) fiber to alter the propagation path and the members of the set of confined regions through which the confined portion of the modified beam propagates to establish a controllable, temporary apparent intensity profile at the output end of the VBC fiber.)

1. An optical beam delivery apparatus configured to sequentially adjust a propagation path with respect to members of a set of confinement regions for establishing a controllable, temporary apparent intensity distribution, the optical beam delivery apparatus comprising:

a first length of optical fibre having a first Refractive Index Profile (RIP) for propagation of an optical beam, the first RIP being capable of modifying the optical beam in response to an applied perturbation to form an adapted optical beam which is movable to propagate along different propagation paths in response to different states of the applied perturbation; and

a second length of optical fibre coupled to the first length of optical fibre and having a second RIP different from the first RIP, defining the set of confinement regions in which different members of the set occupy different positions to provide different intensity profiles at the output end of the second length of optical fibre, such that, in response to sequentially applying different perturbation conditions, different members of the set through which the confined portion of the set propagates establish the controllable, temporary apparent intensity profile at the output end of the second length of optical fibre.

2. The optical beam delivery device of claim 1, wherein the set of confinement regions comprises coaxial confinement regions.

3. The optical beam delivery device of claim 1 or 2, wherein the controllable, temporary apparent intensity profile has a temporary apparent intensity profile selected from the group of apparent intensity profiles comprising gaussian, saddle, annular, elongated and substantially flat-topped.

4. An optical beam delivery device according to claim 1, wherein the first RIP comprises a gradient index RIP.

5. The optical beam delivery apparatus of claim 1, wherein the different perturbation states comprise mechanical oscillations configured to move the propagation path of the adjusted optical beam between two or more members of the set of confinement regions.

6. The optical beam delivery device of claim 1, wherein the optical beam delivery device further comprises a perturbation device comprising a voice coil or a piezoelectric device.

7. The optical beam delivery device of claim 1, wherein the second length of optical fiber comprises a multi-core optical fiber.

8. An optical power sequencer for generating a controllable, temporary apparent intensity profile, the optical power sequencer comprising:

a laser source for providing a beam of light;

a Variable Beam Characteristic (VBC) optical fibre comprising first and second lengths of optical fibre coupled to one another, the first and second lengths of optical fibre having respective first and second Refractive Index Profiles (RIP) that are different from one another, the first RIP being capable of modifying the optical beam in response to a perturbation applied to the VBC optical fibre to form an adjusted optical beam exhibiting an intensity profile at an input end of the second length of optical fibre, the intensity profile being adjustable based on different perturbation conditions, and the second RIP being defined by a plurality of confinement regions arranged to confine at least a portion of the adjusted optical beam corresponding to the intensity profile; and

a controller operatively coupled to the VBC fiber and configured to control a perturbation device that applies the different perturbation states based on a signal from the controller, the signal being indicative of which member or members of the set of confinement regions the confined portion should propagate through in order to establish a controllable, temporary apparent intensity profile at the output end of the second length of fiber.

9. The optical power sequencer of claim 8, wherein the signal is configured to cause the perturbation device to generate a fast mechanical oscillation applied to the VBC fiber.

10. The optical power sequencer of claim 8, wherein the optical power sequencer further comprises a perturbation device, and the perturbation device comprises a voice coil or a piezoelectric device.

11. The optical power sequencer of claim 8, wherein the controller is configured to cause the perturbation device to alter beam dwell time when altering one or more members of the set of confinement regions through which the confined portion should propagate.

12. The optical power sequencer of claim 8, wherein the set of confinement regions comprises coaxial confinement regions.

13. The optical power sequencer of claim 8, wherein the set of confinement regions comprises a non-coaxial confinement core.

14. A method of laser machining a material by sequentially adjusting a propagation path for establishing a controllable, temporary apparent intensity distribution with respect to members of a set of confinement regions, the method comprising:

receiving an optical beam at a Variable Beam Characteristic (VBC) optical fibre comprising first and second lengths of optical fibre having respective first and second Refractive Index Profiles (RIP) different from one another, the first RIP being capable of modifying the optical beam in response to perturbations applied to the VBC optical fibre to form an adjusted optical beam, and the second RIP being defined by a set of confinement regions arranged to confine at least a portion of the adjusted optical beam corresponding to a condition of the perturbations applied to the VBC optical fibre; and is

Applying different perturbation states to the VBC fiber to alter the propagation path and members of the set of confinement regions through which the confined portion of the modified beam propagates, thereby establishing the controllable, temporary apparent intensity profile at the output end of the second length of fiber.

15. The method of claim 14, wherein the set of confinement regions includes a first region and a second region coaxially surrounding the first region, and the applying includes dithering light intensity between the first region and the second region.

16. The method of claim 14, wherein the set of confinement regions includes a first core and a second core spaced apart from the first core, and the applying includes dithering light intensity between the first core and the second core.

17. The method of claim 14, wherein the applying comprises:

applying a first perturbation state for a first duration; and

the second perturbation state is applied for a second duration different from the first duration.

18. The method of claim 17, wherein the first state comprises an unperturbed state of the first length of optical fiber.

19. The method of claim 14, wherein the different perturbation states correspond to repeatable patterns of different propagation paths.

20. The method of claim 14, wherein the first RIP comprises a gradient index RIP.

Technical Field

The technology disclosed herein relates to fiber lasers and fiber coupled lasers. More particularly, the disclosed technology relates to methods, apparatus and systems for adjusting and maintaining adjusted beam characteristics (spot size, divergence profile, spatial profile or beam shape, etc., or any combination thereof) at the output of a fiber laser or fiber coupled laser.

RELATED APPLICATIONS

The present application is a partial continuation of each of the following applications filed on 26/5/2017: U.S. patent application No.15/607,399; no.15/607,410 and No.15/607,411; and international application PCT/US 2017/034848. Each of these applications claims the benefit of U.S. provisional patent application No.62/401,650 filed on 29/9/2016. All of these applications are incorporated herein by reference in their entirety.

Background

The use of high power fiber coupled lasers continues to be popular in various applications, such as material processing, cutting, welding, and/or additive manufacturing. These include, for example, fiber lasers, disk lasers, diode pumped solid state lasers, and lamp pumped solid state lasers. In these systems, optical power is transmitted from a laser to a workpiece via an optical fiber.

Various fiber-coupled laser material processing tasks require different beam characteristics (e.g., spatial profile and/or divergence profile). For example, cutting thick metal and welding typically requires a larger spot size than cutting thin metal. Ideally, the characteristics of the laser beam are adjustable to achieve optimal processing for these different tasks. Conventionally, there are two options for the user: (1) with a laser system with fixed beam characteristics, which can be used for different tasks, but is not optimal for most tasks (i.e. a trade-off between performance and flexibility); or (2) purchase of laser systems or accessories that provide variable beam characteristics, but add significant cost, size, weight, complexity, and may result in reduced performance (e.g., optical loss) or reduced reliability (e.g., reduced robustness or reduced operational time). Currently available laser systems capable of changing beam characteristics require the use of free-space optics or other complex and expensive additional mechanisms (e.g., zoom lenses, mirrors, translatable or motorized lenses, combiners, etc.) to change the beam characteristics. None of the solutions provide the required adjustability of beam characteristics to minimize or eliminate the need to use free-space optics or other additional components that incur substantial losses in cost, complexity, performance, and/or reliability. What is needed is an in-fiber device for providing varying beam characteristics that does not require or minimize the use of free-space optics and that can avoid significant cost, complexity, performance trade-offs, and/or reliability reductions.

Goppold et al, Fraunhofer IWS, describes attempts to improve laser cutting of thick steel plates using a technique they call "dynamic Beam shaping" (DBS). As described in Industrial Photonics volume 4, pages 18 and 19 and other locations in phase 3 (7 months 2017), DBS needs to synchronize the following two mobile phases. The first stage is the movement of the laser cutter relative to the laser beam, which is defined by the feed speed and workpiece geometry. The second stage is an additional high frequency galvanometer controlled oscillation of the laser beam within the cut kerf. With respect to the second stage, Goppold et al describe figure 8, side to side, front to back and other types of beam movement that are intended to improve the quality of the cut (e.g., reduce dross adhesion and oxidation) by distributing light energy evenly within the cut material to optimize the cut. However, these attempts use expensive free space optics and rely on scanning techniques.

Disclosure of Invention

The disclosure is summarized by the following example embodiments. Further aspects and advantages will become apparent from the following detailed description of embodiments, which proceeds with reference to the accompanying drawings.

Exemplary embodiment 1: an optical beam delivery apparatus configured to sequentially adjust a propagation path with respect to members of a set of confinement regions to establish a controllable, temporary apparent intensity distribution, the optical beam delivery apparatus comprising: a first length of optical fibre having a first Refractive Index Profile (RIP) for propagation of an optical beam, the first RIP being capable of modifying the optical beam in response to an applied perturbation to form an adapted optical beam which is movable to propagate along different propagation paths in response to different states of the applied perturbation; and a second length of optical fibre coupled to the first length of optical fibre and having a second RIP different from the first RIP, defining the set of confinement regions in which different members of the set occupy different positions to provide different intensity profiles at the output end of the second length of optical fibre, such that, in response to sequentially applying different perturbation conditions, different members of the set through which the confined portion propagates establish the controllable, temporary apparent intensity profile at the output end of the second length of optical fibre.

Example embodiment 2: the optical beam delivery apparatus of previous example 1, wherein the set of confinement regions comprises coaxial confinement regions.

Exemplary embodiment 3: the optical beam delivery device of the preceding example 1 or 2, wherein the controllable, temporary apparent intensity profile has a temporary apparent intensity profile selected from the group of apparent intensity profiles comprising gaussian, saddle, annular, elongated and substantially flat-topped.

Example embodiment 4: an optical beam delivery device according to preceding example 1, wherein the first RIP comprises a gradient index RIP.

Example embodiment 5: the optical beam delivery apparatus of the preceding example 1, wherein the different perturbation states comprise mechanical oscillations configured to move the propagation path of the adjusted optical beam between two or more members of the set of confinement regions.

Example embodiment 6: the optical beam delivery device of the preceding example 1, wherein the optical beam delivery device further comprises a perturbation device comprising a voice coil or a piezoelectric device.

Example embodiment 7: the optical beam delivery apparatus of the foregoing example 1, wherein the second length of optical fiber comprises a multi-core optical fiber.

Example embodiment 8: an optical power sequencer for generating a controllable, temporary apparent intensity profile, the optical power sequencer comprising: a laser source for providing a beam of light; a Variable Beam Characteristic (VBC) optical fibre comprising first and second lengths of optical fibre coupled to one another, the first and second lengths of optical fibre having respective first and second Refractive Index Profiles (RIP) that are different from one another, the first RIP being capable of modifying the optical beam in response to a perturbation applied to the VBC optical fibre to form an adjusted optical beam exhibiting an intensity profile at an input end of the second length of optical fibre, the intensity profile being adjustable based on different perturbation conditions, and the second RIP being defined by a plurality of confinement regions arranged to confine at least a portion of the adjusted optical beam corresponding to the intensity profile; and a controller operatively coupled to the VBC fiber and configured to control a perturbation device that applies different perturbation states based on signals from the controller, the signals being indicative of which member or members of the set of confinement regions the confined portion should propagate through in order to establish a controllable, temporary apparent intensity profile at the output end of the second length of fiber.

Example embodiment 9: the optical power sequencer of the preceding example 8, wherein the signal is configured to cause the perturbation device to generate a fast mechanical oscillation applied to the VBC fiber.

Example embodiment 10: the optical power sequencer of the previous example 8, wherein the optical power sequencer further comprises a perturbation device comprising a voice coil or a piezoelectric device.

Example embodiment 11: the optical power sequencer of preceding example 8, wherein the controller is configured to cause the perturbation device to alter beam dwell time when altering the one or more members of the set of confinement regions through which the confined portion should propagate.

Example embodiment 12: the optical power sequencer of previous example 8, wherein the set of confinement regions includes coaxial confinement regions.

Example embodiment 13: the optical power sequencer of previous example 8, wherein the set of confinement regions includes a non-coaxial confinement core.

Exemplary embodiment 14: a method of laser machining a material by sequentially adjusting a propagation path with respect to members of a set of confinement regions to establish a controllable, temporary apparent intensity distribution, the method comprising: receiving an optical beam at a Variable Beam Characteristic (VBC) optical fibre comprising first and second lengths of optical fibre having respective first and second Refractive Index Profiles (RIP) different from one another, the first RIP being capable of modifying the optical beam in response to perturbations applied to the VBC optical fibre to form an adjusted optical beam, and the second RIP being defined by a set of confinement regions arranged to confine at least a portion of the adjusted optical beam corresponding to a condition of the perturbations applied to the VBC optical fibre; and applying different perturbation states to the VBC fiber to alter the propagation path and members of the set of confinement regions through which the confined portion of the modified beam propagates, thereby establishing the controllable, temporary apparent intensity profile at the output end of the second length of fiber.

Example embodiment 15: the method of preceding example 14, wherein the set of confinement regions includes a first region and a second region coaxially surrounding the first region, and the applying includes dithering light intensity between the first region and the second region.

Example embodiment 16: the method of preceding example 14, wherein the set of confinement regions includes a first core and a second core spaced apart from the first core, and the applying includes dithering light intensity between the first core and the second core.

Example embodiment 17: the method of the preceding example 14, wherein the applying comprises: applying a first perturbation state for a first duration; and applying a second perturbation state for a second duration different from the first duration.

Example embodiment 18: the method of preceding example 17, wherein the first state comprises an unperturbed state of the first length of optical fiber.

Example embodiment 19: the method of the preceding example 14, wherein the different perturbation states correspond to repeatable patterns of different propagation paths.

Example embodiment 20: the method of preceding example 14, wherein the first RIP comprises a gradient index RIP.

Further exemplary embodiments: a computer or machine readable medium to implement a device, system or apparatus, or to store thereon instructions for a processor, which when executed, performs any of the example methods.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments of the present disclosure and, together with the description, serve to explain the advantages and principles of the presently disclosed technology. In the drawings, there is shown in the drawings,

FIG. 1 illustrates an exemplary fiber configuration for providing a laser beam with variable beam characteristics;

FIG. 2 depicts a cross-sectional view of an exemplary optical fiber structure for transmitting a light beam having variable beam characteristics;

FIG. 3 illustrates an example method of perturbing an optical fiber structure used to provide a light beam having variable beam characteristics;

FIG. 4 is a graph showing the lowest order modes (LP) calculated for a first length of fiber at different fiber bend radii₀₁) A graph of the spatial profile of (a);

fig. 5 shows an example of a two-dimensional intensity distribution at a junction (junction) when an optical fiber for changing a beam characteristic is almost straight;

FIG. 6 shows an example of a two-dimensional intensity distribution at a junction when an optical fiber for changing beam characteristics is bent at a selected radius to preferentially excite a particular confinement region of a second length of optical fiber;

7-10 plot experimental results to illustrate additional output beams of various bend radii for optical fibers used to change the beam characteristics shown in FIG. 2;

11-16 illustrate cross-sectional views of exemplary first lengths of optical fiber for effecting beam characteristic adjustment in an optical fiber assembly;

FIGS. 17-19 show cross-sectional views of exemplary second lengths of optical fiber ("limiting fiber") for limiting adjusted beam characteristics in a fiber optic assembly;

FIGS. 20 and 21 illustrate cross-sectional views of exemplary second lengths of optical fiber for varying the divergence angle of and confining an adjusted optical beam in a fiber optic assembly configured to provide variable beam characteristics;

FIG. 22A illustrates an exemplary laser system including a fiber optic assembly configured to provide variable beam characteristics between a feed fiber and a processing head;

FIG. 22B illustrates an exemplary laser system including a fiber optic assembly configured to provide variable beam characteristics between a feed fiber and a processing head;

FIG. 23 illustrates an exemplary laser system including a fiber optic assembly configured to provide variable beam characteristics between a feed fiber and a plurality of processing fibers;

FIG. 24 illustrates examples of various perturbation components for providing variable beam characteristics according to various examples provided herein;

FIG. 25 illustrates an exemplary process for adjusting and maintaining a modified characteristic of a light beam;

26-28 are cross-sectional views illustrating exemplary second lengths of optical fiber ("limiting fiber") for limiting an adjusted beam characteristic in a fiber optic assembly;

FIGS. 29, 30 and 31 show sequential output beams of three different perturbation states of an optical fiber for varying the characteristics of the beam shown in FIG. 2;

FIGS. 32A, 32B and 32C show the resulting flat-topped, saddle-shaped and stepped temporal apparent intensity profiles of the output beams according to the different time-weighted sequences shown in FIGS. 29, 30 and 31, respectively;

FIG. 33 is a block diagram of an optical power sequencer for generating a temporal apparent intensity profile, according to one embodiment;

FIGS. 34 and 35 illustrate multi-core fibers used to generate the temporary apparent intensity profiles shown in FIGS. 33, 36A, 36B, 36C, and 36D; and

FIGS. 36A, 36B, 36C and 36D are magnified views of the temporary apparent intensity distribution shown in FIG. 33.

Detailed Description

As used throughout this disclosure and in the claims, the singular forms "a," "an," and "the" include the plural forms unless the context clearly dictates otherwise. In addition, the term "comprising" means "including". Furthermore, the term "coupled" does not exclude the presence of intermediate elements between the coupled items. Furthermore, the terms "modify" and "adjust" are used interchangeably to mean "change".

The systems, devices, and methods described herein should not be construed as limiting in any way. Rather, the present disclosure is directed to all novel and non-obvious features and aspects of the various disclosed embodiments, alone and in various combinations and sub-combinations with each other. The disclosed systems, methods, and apparatus are not limited to any specific aspect or feature or combination thereof, nor do the disclosed systems, methods, and apparatus require that any one or more specific advantages be present or problems be solved. Any theory of operation is for ease of explanation, but the disclosed systems, methods, and apparatus are not limited to these theories of operation.

Although the operations of some of the disclosed methods are described in a particular order for convenient presentation, it should be understood that this manner of description encompasses rearrangement, unless a particular order is required by specific language set forth below. For example, operations described sequentially may in some cases be rearranged or performed concurrently. Moreover, for the sake of simplicity, the attached figures may not show the various ways in which the disclosed systems, methods, and apparatus can be used in conjunction with other systems, methods, and apparatus. Further, the specification sometimes uses terms such as "producing" and "providing" to describe the disclosed methods. These terms are high-level abstractions of the actual operations that are performed. The actual operations that correspond to these terms will vary depending on the particular implementation and are readily discernible by one of ordinary skill in the art.

In some examples, a value, process, or device is referred to as "lowest," "best," "smallest," or the like. It should be understood that such description is intended to indicate that a selection may be made among many alternatives of functions used, and that such a selection need not be better, smaller, or more optimal than others. Examples are described with reference to directions indicated as "above," "below," "upper," "lower," etc. These terms are used for convenience of description and do not imply any particular spatial orientation.

Definition of

Definitions of words and terms used herein:

1. the term "beam characteristic" means one or more of the following terms used to describe a beam. In general, the beam characteristics of most interest depend on the application or the specifics of the optical system.

2. The term "beam diameter" is defined as the distance across the center of the beam along the axis for which the irradiance (intensity) is equal to 1/e of the maximum irradiance². Although it is used hereinThe disclosed examples typically use beams propagating in azimuthally symmetric modes, but an ellipse or other beam shape may be used, and the beam diameter may vary along different axes. A circular beam is characterized by a single beam diameter. Other beam shapes may have different beam diameters along different axes.

3. The term "spot size" is from the center point of maximum irradiance to 1/e²Radial distance (radius) of points.

4. The term "beam divergence distribution" is power versus full cone angle. This quantity is sometimes referred to as the "angular distribution" or "NA distribution".

5. The term "beam parameter product" (BPP) of a laser beam is defined as the product of the beam radius (measured at the beam waist) and the beam divergence half-angle (measured in the far field). The unit of BPP is usually mm-mrad.

"confinement fiber" is defined as a fiber having one or more confinement regions, wherein the confinement region comprises a high index region (core region) surrounded by a low index region (cladding region). The RIP of the confinement fiber may comprise one or more high index regions (core regions) surrounded by a low index region (cladding region), wherein light is guided in the high index region. Each confinement region and each cladding region may have any RIP including, but not limited to, step index and gradient index. The confinement regions may or may not be concentric and may be of various shapes, such as circular, annular, polygonal, arcuate, elliptical, irregular, or the like, or any combination thereof. The confinement regions in a particular confinement fiber may all have the same shape or may be different shapes. Further, the confinement regions may be coaxial or may have axes that are offset with respect to each other. The restricted area may have a uniform thickness in the longitudinal direction about the central axis, or the thickness may vary in the longitudinal direction about the central axis.

7. The term "intensity distribution" refers to the intensity of light as a function of position along a line (one-dimensional profile) or on a plane (two-dimensional profile). The line or plane is generally perpendicular to the direction of propagation of the light. This is a quantitative attribute.

"brightness" is a photometric measurement of luminous intensity per unit area of light propagating in a given direction.

9.“M²The factor "(also referred to as" beam quality factor "or" beam propagation factor ") is a dimensionless parameter for quantifying the beam quality of a laser beam, M²1 is a diffraction limited beam, larger M²The value corresponds to a lower beam quality. M²Equal to BPP divided by λ/π, where λ is the wavelength of the light beam in microns (if BPP is expressed in mm-mrad).

10. The term "numerical aperture" or "NA" of an optical system is a dimensionless number that characterizes the angular range of light that the system can accept or emit.

11. The term "light intensity" is not an official (SI) unit, but is used to denote the incident power per unit area on a surface or through a plane.

12. The term "power density" refers to the optical power per unit area, although this is also referred to as "light intensity".

13. The term "radial beam position" refers to the position of the beam in the optical fiber measured relative to the center of the fiber core in a direction perpendicular to the fiber axis.

"radiance" is the radiation emitted per unit solid angle per unit area of a light source (e.g., a laser) in a given direction. Radiance may be varied by changing the beam intensity distribution and/or beam divergence profile or distribution. The ability to change the radiance profile of the laser beam means the ability to change the BPP.

15. The term "refractive index profile" or "RIP" refers to the refractive index as a function of position along a line (1D) perpendicular to the optical fiber axis or in a plane (2D) perpendicular to the optical fiber axis. Many optical fibers are azimuthally symmetric, in which case the 1D RIP is the same at any azimuthal angle.

"step index fiber" has a RIP that is flat (index of refraction independent of position) within the fiber core.

A "gradient index optical fibre" has a RIP in which the refractive index decreases with increasing radial position (i.e. with increasing distance from the centre of the fibre core).

"parabolic index fiber" is a special case of a gradient index fiber, where the refractive index decreases quadratically with increasing distance from the center of the fiber core.

Optical fiber for changing beam characteristics

Methods, systems, and apparatus are disclosed herein that are configured to provide an optical fiber operable to provide a laser beam having a Variable Beam Characteristic (VBC) that may reduce the cost, complexity, optical loss, or other disadvantages of the above-described conventional approaches. Such VBC fibers are configured to change various beam characteristics. The VBC fiber can be used to control these beam characteristics, allowing the user to adjust various beam characteristics to suit the particular requirements of various laser processing applications. For example, VBC fiber can be used to adjust: beam diameter, beam divergence profile, BPP, intensity profile, M²Factor, NA, light intensity, power density, radial beam position, radiance, spot size, etc., or any combination thereof.

In general, the disclosed techniques entail coupling a laser beam into an optical fiber, wherein the characteristics of the laser beam in the fiber may be adjusted by perturbing the laser beam and/or perturbing a first length of the fiber (e.g., bending the fiber or introducing one or more other perturbations) in any of a variety of ways, and maintaining the adjusted beam characteristics, in whole or in part, in a second length of the fiber. The second length of optical fiber is specifically configured to maintain and/or further modify the adjusted beam characteristic. In some cases, the second length of fiber maintains the adjusted beam characteristics by transmitting the laser beam to its end use (e.g., material processing). The first length of optical fiber and the second length of optical fiber may comprise the same or different optical fibers.

The disclosed technology is compatible with fiber lasers and fiber coupled lasers. Fiber coupled lasers typically transmit output via a delivery fiber having a step index profile (RIP), i.e., having a flat or constant index of refraction within the fiber core. In fact, depending on the design of the optical fiber, the RIP of the transport fiber may not be possibleIs completely flat. The important parameter is the core diameter (d) of the fiber_core) And NA. The core diameter is typically in the range of 10-1000 microns (although other values are possible) and the NA is typically in the range of 0.06-0.22 (although other values are possible). The delivery fiber from the laser may be routed directly to the processing head or workpiece, or may be routed to a fiber-to-fiber coupler (FFC) or fiber-to-fiber switch (FFS) that couples light from the delivery fiber into a processing fiber that transmits the beam to the processing head or workpiece.

Most material processing tools (especially those with high power: (>1 kW)) using multimode (MM) optical fiber, but some material processing tools use Single Mode (SM) optical fiber located at d_coreAnd the low end of the NA range. The beam characteristics of SM fibers are uniquely determined by the fiber parameters. However, the beam characteristics from MM fibers may vary (unit to unit and/or in terms of laser power and time) depending on the beam characteristics from the laser source coupled into the fiber, the launch or splice conditions of the fiber, the fiber RIP, and the static and dynamic geometry of the fiber (bend, twist, motion, microbend, etc.). For SM and MM delivery fibers, the beam characteristics may not be optimal for a given material processing task, nor may they be optimal for a range of tasks, which motivates the desire to systematically vary the beam characteristics to customize or optimize for a particular processing task.

In one example, the VBC optical fiber may have a first length and a second length, and may be configured to be interposed as an in-fiber device between the delivery fiber and the processing head to provide the adjustability required for the beam characteristics. In order to be able to adjust the optical beam, a perturbation device and/or assembly is provided adjacent to and/or coupled to the VBC fiber and is responsible for perturbing the optical beam of the first length such that a characteristic of the optical beam is altered in the first length of fiber and the altered characteristic is maintained or further altered as the optical beam propagates in the second length of fiber. The perturbed beam is launched into a second length of VBC fiber configured to maintain the adjusted beam characteristic. The first length of optical fiber and the second length of optical fiber may be the sameOr a different optical fiber and/or the second length of optical fiber may include a limiting fiber. The beam characteristics maintained by the second length of VBC fiber may include any of: beam diameter, beam divergence profile, BPP, intensity profile, brightness, M²Factor, NA, light intensity, power density, radial beam position, radiance, spot size, etc., or any combination thereof.

FIG. 1 illustrates an exemplary VBC optical fiber 100 for providing a laser beam with variable beam characteristics without the need for using free-space optics to change the beam characteristics. The VBC fiber 100 includes a first length of fiber 104 and a second length of fiber 108. The first length of optical fiber 104 and the second length of optical fiber 108 may be the same or different optical fibers and may have the same or different RIPs. The first length of optical fiber 104 and the second length of optical fiber 108 may be connected together by a splice. The first length of optical fiber 104 and the second length of optical fiber 108 may be otherwise coupled, may be spaced apart, or may be connected via an intervening component, such as another length of optical fiber, free space optics, glue, index matching material, or the like, or any combination thereof.

The perturbation device 110 is disposed near the perturbation region 106 and/or surrounds the perturbation region 106. Perturbation device 110 may be a device, component, structure within a fiber, and/or other feature. The perturbation device 110 perturbs at least the optical beam 102 in the first length of optical fiber 104 or the second length of optical fiber 108, or a combination thereof, to adjust one or more beam characteristics of the optical beam 102. The adjustment of the optical beam 102 may occur in the first length of optical fiber 104 or the second length of optical fiber 108, or a combination thereof, in response to a perturbation by the perturbation device 110. The perturbation regions 106 may extend over various widths and may or may not extend into a portion of the second length of optical fiber 108. As the optical beam 102 propagates in the VBC fiber 100, the perturbation device 110 can physically act on the VBC fiber 100 to perturb the fiber and adjust the characteristics of the optical beam 102. Alternatively, perturbation device 110 may act directly on beam 102 to alter its beam characteristics. After the adjustment, the perturbed beam 112 has beam characteristics that are different from the beam characteristics of the beam 102, which will be fully or partially maintained in the second length of optical fiber 108. In another example, perturbation device 110 need not be positioned near the joint. Furthermore, no splice is required at all, e.g., the VBC fiber 100 may be a single fiber, and the first and second lengths of fiber may be spaced apart or fixed with a small gap (air space or filled with an optical material, e.g., optical cement or index matching material).

The perturbed beam 112 is launched into the second length of optical fiber 108, wherein the characteristics of the perturbed beam 112 are largely maintained or continue to develop as the perturbed beam 112 propagates, thereby producing adjusted beam characteristics at the output end of the second length of optical fiber 108. In one example, the new beam characteristics may include an adjusted intensity profile. In one example, the altered beam intensity profile will remain within the various structurally bounded confinement regions of the second length of optical fiber 108. Thus, the beam intensity profile can be adjusted to a desired beam intensity profile optimized for a particular laser machining task. In general, the intensity distribution of the perturbed beam 112 will evolve as it propagates in the second length of optical fiber 108 to fill the confinement region into which the perturbed beam 112 is launched in response to conditions in the first length of optical fiber 104 and the perturbation caused by the perturbing means 110. Furthermore, depending on the emission conditions and the fiber properties, the angular distribution may evolve as the light beam propagates in the second fiber. Typically, the input divergence profile is largely preserved by the fiber, but if the input divergence profile is narrow and/or if the fiber has irregularities or intentional features that disturb the divergence profile, the profile may be widened. Various confinement regions, perturbations, and fiber characteristics of the second length of optical fiber 108 will be described in more detail below. The beams 102 and 112 are conceptual abstractions intended to show how the beams propagate through the VBC fiber 100 to provide variable beam characteristics, and are not intended to accurately simulate the behavior of a particular beam.

The VBC fiber 100 can be fabricated by a variety of methods, including PCVD (plasma chemical vapor deposition), OVD (outside vapor deposition), VAD (vapor axial deposition), MOCVD (metal-organic chemical vapor deposition), and/or DND (direct nanoparticle deposition). The VBC fiber 100 may comprise a variety of materials. For example, VBC fiber 100 may comprise SiO₂Doped with GeO₂SiO of (2)₂Germanosilicate, phosphorus pentoxide, phosphosilicate, Al₂O₃Aluminosilicate, and the like, or any combination thereof. The confinement region may be defined by a cladding layer doped with fluorine, boron, or the like, or any combination thereof. Other dopants may be added to the active fiber, including rare earth ions, e.g., Er³⁺(erbium) and Yb³⁺(ytterbium) and Nd³⁺(Neodymium), Tm³⁺(Thulium) Ho³⁺(holmium), and the like, or any combination thereof. The confinement region may be defined by a cladding layer having a refractive index lower than that of the fluorine or boron doped confinement region. Alternatively, the VBC fiber 100 can comprise a photonic crystal fiber or a microstructured fiber.

The VBC fiber 100 is suitable for use in any of a variety of fiber, fiber optic or fiber laser devices, including continuous and pulsed fiber lasers, disc lasers, solid state lasers or diode lasers (pulse rate is not limited except by physical limitations). Furthermore, implementations in planar waveguides or other types of waveguides (rather than just optical fibers) are within the scope of the claimed technology.

FIG. 2 depicts a cross-sectional view of an exemplary VBC fiber 200 for adjusting beam characteristics of a light beam. In one example, the VBC fiber 200 may be a processing fiber in that a beam may be transmitted to a processing head for material processing. The VBC fiber 200 includes a first length of fiber 204 spliced to a second length of fiber 208 at a junction 206. Perturbing member 210 is disposed proximate to node 206. The perturbation component 210 may be any of a variety of devices configured to be able to adjust the beam characteristics of the optical beam 202 propagating in the VBC fiber 200. In one example, the disturbance assembly 210 can be a mandrel and/or another device that can provide a way to change the bend radius and/or bend length of the VBC fiber 200 near the joint. Other examples of perturbation devices will be discussed below with reference to FIG. 24.

In one example, the first length of optical fiber 204 has a parabolic refractive index RIP 212, as shown in the left RIP diagram. When the fiber 204 is straight or nearly straight, most of the intensity distribution of the beam 202 is concentrated in the center of the fiber 204. The second length of optical fibre 208 is a constraint fibre having a RIP 214, as shown in the right RIP diagram. The second length of optical fiber 208 includes confinement regions 216, 218, and 220. Confinement region 216 is a central core surrounded by two annular (or ring-shaped) confinement regions 218 and 220. Layers 222 and 224 are structural barriers of low index material between confinement regions (216, 218, and 220), commonly referred to as "cladding" regions. In one example, layers 222 and 224 may include fluorosilicate rings; in some embodiments, the fluorosilicate cladding is relatively thin. Other materials may also be used, and claimed subject matter is not so limited.

In one example, the perturbation component 210 may physically act on the optical fiber 204 and/or the optical beam 202 to adjust its beam characteristics and generate an adjusted optical beam 226 as the optical beam 202 propagates along the VBC optical fiber 200. In the present example, the intensity distribution of the light beam 202 is modified by the perturbation component 210. After adjusting the beam 202, the intensity distribution of the adjusted beam 226 may be concentrated in the outer confinement regions 218 and 220, where the intensity is relatively small in the central confinement region 216. Because each of the confinement regions 216, 218, and/or 220 is isolated by a thin layer of lower index of refraction material in barrier layers 222 and 224, the second length of optical fiber 208 may substantially maintain the adjusted intensity profile of the adjusted optical beam 226. The beam will typically be azimuthally distributed within a given confinement region, but will not (significantly) transition between confinement regions as it propagates along the second length of fiber 208. Thus, the adjusted beam characteristics of the adjusted beam 226 remain largely within the isolated confinement regions 216, 218, and/or 220. In some cases, it may be desirable to divide the power of the light beam 226 between the confinement regions 216, 218, and/or 220, rather than concentrating in a single region, and this state may be achieved by generating an appropriately adjusted light beam 226.

In one example, the core confinement region 216 and the annular confinement regions 218 and 220 may be composed of fused silica glass, and the cladding layers 222 and 224 defining the confinement regions may be composed of fluorosilicate glass. Other materials may be used to form the various confinement regions (216, 218, and 220), including germanosilicates, phosphosilicates, aluminosilicates, and the like, or combinations thereof, and claimed subject matter is not so limited. Other materials may be used to form barrier rings (222 and 224), including fused silica, borosilicate, or the like, or combinations thereof, and claimed subject matter is not so limited. In other embodiments, the optical fiber or waveguide comprises or consists of various polymers or plastics or crystalline materials. Typically, the refractive index of the core confinement region is greater than the refractive index of the adjacent barrier/cladding region.

In some examples, it may be desirable to increase the number of confinement regions in the second length of fiber to increase the granularity of beam steering over beam displacement to fine tune the beam profile. For example, the confinement region may be configured to provide a gradual beam displacement.

FIG. 3 illustrates an exemplary method of perturbing an optical fiber 200 to provide a variable beam characteristic of an optical beam. Changing the bend radius of the optical fiber may change the radial beam position, divergence angle, and/or radiance profile of the beam within the optical fiber. The bend radius of the VBC optical fiber 200 can be varied from a first bend radius R around the splice joint 206 by using a stepped mandrel or taper as the perturbation assembly 210₁Reduced to a second radius of curvature R₂. Additionally or alternatively, the engagement length on the mandrel or cone may vary. A roller 250 may be used to engage the VBC fiber 200 across the perturbation assembly 210. In one example, the amount of engagement of the roller 250 with the optical fiber 200 has been shown to shift the distribution of the intensity profile to the outer confinement regions 218 and 220 of the optical fiber 200 having a fixed mandrel radius. There are a variety of other methods for changing the bend radius of optical fiber 200, such as using a clamping assembly, a flexible tube, or the like, or combinations thereof, and claimed subject matter is not so limited. In another example, the length of the VBC fiber 200 bend can also change the beam characteristics in a controllable and reproducible manner for a particular bend radius. In an example, changing the bend radius and/or length over which the optical fiber is bent at a particular bend radius also modifies the intensity profile of the beam such that one or more modes may be radially offset from the center of the fiber core.

Maintaining the bend radius of the fiber at the junction 206 ensures that the adjusted beam characteristics (e.g., the radial beam position and radiance profile of the beam 202) do not return to their undisturbed state prior to launch into the second length of fiber 208. Further, the adjusted radial beam characteristics of the adjusted beam 226, including location, divergence angle, and/or intensity distribution, may be varied based on the degree of reduction in the bend radius and/or bend length of the VBC fiber 200. Thus, specific beam characteristics can be obtained using this method.

In the present example, a first length of optical fiber 204 with a first RIP 212 is spliced at a junction 206 to a second length of optical fiber 208 with a second RIP 214. However, a single fiber may be used with a single RIP formed to be able to perturb (e.g. by microbending) the beam characteristics of the beam 202 and to maintain the modified beam. Such a RIP may be similar to the RIP shown in the fibre shown in figures 17, 18 and/or 19.

Fig. 7-10 provide experimental results of the VBC fiber 200 (shown in fig. 2 and 3) and further illustrate the beam response to the perturbation of the VBC fiber 200 when the perturbation assembly 210 acts on the VBC fiber 200 to bend the fiber. Fig. 4-6 are simulations and fig. 7-10 are experimental results in which a light beam from an SM 1050nm light source is launched into an input fiber (not shown) having a core diameter of 40 microns. The input fiber is spliced to a first length of fiber 204.

FIG. 4 is a graph showing the lowest order mode (LP) of a first length of optical fiber 204 at different fiber bend radii 402₀₁) Wherein the perturbation component 210 involves bending the VBC fiber 200. As the fiber bend radius decreases, the beam propagating in the VBC fiber 200 is adjusted so that the mode is radially offset from the center 404 of the core of the VBC fiber 200 (r-0 microns), towards the core/cladding interface (located at r-100 microns in this example). High order mode (LP)_In) Also shifts with bending. Thus, for straight or nearly straight fibers (very large bend radii), LP₀₁Is centered at or near the center of the VBC fiber 200. At a bend radius of about 6cm, LP₀₁Is offset from the center 406 of the VBC fiber 200 to a radial position of about 40 μm. At a bend radius of about 5cm, LP₀₁Is offset from the center 406 of the VBC fiber 200 to a radial position of about 50 μm.At a bend radius of about 4cm, LP₀₁Is offset from the center 406 of the VBC fiber 200 to a radial position of about 60 μm. At a bend radius of about 3cm, LP₀₁Is offset from the center 406 of the VBC fiber 200 to a radial position of about 80 μm. At a bend radius of about 2.5cm, LP₀₁Curve 416 is offset from the center 406 of the VBC fiber 200 to a radial position of about 85 μm. Note that the shape of the pattern remains relatively constant (up to near the edge of the core), which is a particular property of the parabolic RIP. This attribute is not required by the VBC function, and other RIPs may be used, although in some cases this attribute may be desirable.

In one example, if the VBC fiber 200 is straightened, the LP₀₁The mode will move back to the center of the fiber. Thus, the purpose of the second length of fiber 208 is to "capture" or confine the adjusted intensity profile of the beam in a confined region that is offset from the center of the VBC fiber 200. The joint between the fibers 204 and 208 is included in the bend region, so the shifted mode profile will be preferentially launched into one of the annular confinement regions 218 and 220, or distributed in the confinement region. Fig. 5 and 6 illustrate this effect.

FIG. 5 shows an exemplary two-dimensional intensity distribution at a junction 206 within a second length of fiber 208 when the VBC fiber 200 is nearly straight. Most of the LP₀₁And LP_InWithin the confinement region 216 of the optical fiber 208. FIG. 6 shows a two-dimensional intensity distribution at a junction 206 within the second length of fiber 208 when the VBC fiber 200 is bent at a selected radius to preferentially excite a confinement region 220 (the outermost confinement region) of the second length of fiber 208. Most of the LP₀₁And LP_InWithin the confinement region 220 of the optical fiber 208.

In one example, the confinement region 216 of the second length of optical fiber 208 has a diameter of 100 microns, the confinement region 218 has a diameter between 120 microns and 200 microns, and the confinement region 220 has a diameter between 220 microns and 300 microns. Confinement regions 216, 218 and 220 are separated by 10 μm thick rings of fluorosilicate, providing 0.22 NA for the confinement regions. Other inner and outer diameters of the confinement regions, the thickness of the rings separating the confinement regions, the NA value of the confinement regions, and the number of confinement regions may be used.

Referring again to FIG. 5, with the parameters described, when VBC fiber 200 is straight, approximately 90% of the power is contained within central confinement region 216, and approximately 100% of the power is contained within confinement regions 216 and 218. Referring now to FIG. 6, when fiber 200 is bent to preferentially excite second annular confinement region 220, approximately 75% of the power is contained within confinement region 220 and more than 95% of the power is contained within confinement regions 218 and 220. These calculations include LP₀₁And two higher order modes, which are typical in some 2-4kW fiber lasers.

As is apparent from FIGS. 5 and 6, in the case where the perturbation assembly 210 acts on the VBC fiber 200 to bend the fiber, the bend radius determines the spatial overlap of the modal intensity distribution of the first length of fiber 204 with the different guiding confinement regions (216, 218, and 220) of the second length of fiber 208. Thus, changing the bend radius can change the intensity distribution at the output end of the second length of fiber 208, thereby changing the diameter or spot size of the beam and thus its radiance and BPP value. Such adjustment of spot size can be achieved in an all-fiber configuration, thereby eliminating the involvement of free-space optics, and thus reducing or eliminating the disadvantages of free-space optics described above. Such adjustments may also be made by other perturbation components that change the bend radius, bend length, fiber tension, temperature, or other perturbations discussed below.

In a typical material processing system (e.g., a cutting or welding tool), the output of the processed optical fiber is imaged by the processing head at or near the workpiece. Thus, changing the intensity profile as shown in fig. 5 and 6 can change the beam profile at the workpiece in order to adjust and/or optimize the process as desired. For purposes of the above calculations, a particular RIP of two fibers is assumed, but other RIPs are possible, and claimed subject matter is not so limited.

7-10 plot experimental results (measured intensity profiles) to illustrate additional output beams for various bend radii of the VBC fiber 200 shown in FIG. 2.

In FIG. 7, when the VBC fiber 200 is straight, the beam is almost entirely confined to the confinement region 216. As the bend radius decreases, the intensity distribution of the output end moves to a larger diameter of the confinement regions 218 and 220 that are further away from the confinement region 216, see, for example, this movement seen in fig. 8-10. FIG. 8 depicts the intensity distribution when the bend radius of the VBC fiber 200 is selected to preferentially shift the intensity distribution toward the confinement region 218. Fig. 9 depicts experimental results when the bend radius is further reduced and selected to move the intensity distribution outward to the confinement region 220 and the confinement region 218. In fig. 10, at the minimum bend radius, the beam is almost in "ring mode", with most of the intensity in the outermost confinement region 220.

Although the confined region is excited from one side at the splice node 206, the intensity distribution is nearly symmetric in azimuth due to the scrambling within the confined region as the beam propagates within the VBC fiber 200. While the optical beam typically scrambles azimuthally as it propagates, various structures or perturbations (e.g., coils) can be included to facilitate this process.

For the fiber parameters used in the experiments shown in fig. 7-10, a particular confinement region was not fully excited because there was some intensity in the multiple confinement regions. This feature may enable advantageous material processing applications that are optimized by having a flatter or distributed beam intensity profile. In applications where cleaner excitation of a given restricted area is required, different fiber RIPs may be used to achieve this feature.

The results shown in fig. 7-10 relate to the particular optical fiber used in this experiment, and the details will vary depending on the implementation details. In particular, the spatial profile and divergence distribution of the output beam and its dependence on the bend radius will depend on the particular RIP employed, the splicing parameters and the characteristics of the laser source launched into the first optical fibre.

Fiber parameters other than those shown in fig. 2 may be used and still be within the scope of the claimed subject matter. In particular, different RIP and core sizes and shapes may be used to facilitate compatibility with different input beam profiles and to achieve different output beam characteristics. In addition to the parabolic refractive index profile shown in fig. 2, example RIPs for the first length of fiber include other gradient index profiles, step refractive indices, pedestal designs (i.e., nested cores with gradually decreasing refractive index as the distance from the center of the fiber increases), and designs of nested cores having the same refractive index values but different NA values for the center core and the surrounding rings. In addition to the profiles shown in fig. 2, example RIPs for the second length of optical fiber include confinement fibers having different numbers of confinement regions, non-uniform confinement region thicknesses, different and/or non-uniform values of the thickness of the rings surrounding the confinement regions, different and/or non-uniform NA values of the confinement regions, different refractive index values of the high and low index portions of the RIP, non-circular confinement regions (e.g., elliptical, oval, polygonal, square, rectangular, or combinations thereof), and other designs, as discussed in more detail in fig. 26-28. Furthermore, the VBC fibers 200 and other examples of VBC fibers described herein are not limited to use of two fibers. In some examples, implementations may include using one optical fiber or more than two optical fibers. In some cases, the optical fiber may not be axially uniform; for example, a fiber bragg grating or a long period grating may be included, or the diameter may vary along the length of the fiber. Furthermore, the optical fiber need not be azimuthally symmetric, for example, the core may have a square or polygonal shape. Various fiber coatings (buffer layers) may be used, including high index or index matching coatings (which strip light at the glass-polymer interface) and low index coatings (which guide light by total internal reflection at the glass-polymer interface). In some examples, multiple fiber coatings may be used on the VBC fiber 200.

11-16 show cross-sectional views of examples of a first length of optical fiber for enabling adjustment of a characteristic of an optical beam in a VBC fiber in response to a disturbance of the optical beam propagating in the first length of optical fiber. Some examples of beam characteristics that may be adjusted in the first length of fiber are: beam diameter, beam divergence profile, BPP, intensity profile, brightness, M²Factor, NA, light intensity distribution, power density distribution, radial beam position, radiance, spot size, etc., or any combination thereof. In FIG. 11-The first length of fiber depicted in 16 and described below is merely an example and does not provide an exhaustive description of the variety of first lengths of fiber that may be used to adjust beam characteristics in a VBC fiber assembly. The choice of materials, suitable RIP and other variables for the first length of optical fibre shown in figures 11-16 depend at least on the desired beam output. A wide variety of fiber variables are contemplated and are within the scope of the claimed subject matter. Accordingly, the claimed subject matter is not limited by the examples provided herein.

In fig. 11, a first length of optical fiber 1100 includes a step index profile 1102. Fig. 12 shows a first length of optical fibre 1200 comprising a "pedestal RIP" (i.e. a core comprising a step index region surrounded by a larger step index region) 1202. Fig. 13 shows a first length of optical fibre 1300 comprising a multi-pedestal RIP 1302.

FIG. 14A shows a first length of optical fiber 1400 including a gradient index profile 1418 surrounded by an under-doped region 1404. When the fiber 1400 is perturbed, the modes may move radially outward in the fiber 1400 (e.g., during bending of the fiber 1400). The gradient index profile 1402 may be designed to facilitate maintaining or even compressing the modal shape. Such a design may facilitate adjusting the light beam propagating in the optical fiber 1400 to generate a light beam having a beam intensity distribution concentrated at the outer circumference of the optical fiber (i.e., in a portion of the fiber core that is offset from the fiber axis). As described above, when the conditioned beam is coupled into a second length of optical fiber having a confinement region, the intensity distribution of the conditioned beam may be confined to the outermost confinement region, thereby providing a ring-shaped intensity distribution. Beam spots with narrow outer confinement regions can be used to achieve certain material processing actions.

FIG. 14B shows a first length of optical fiber 1406 including a graded index profile 1414 surrounded by a lower doped region 1408, similar to that of the optical fiber 1400. However, the optical fiber 1406 includes a diverging structure 1410 (low index region), as shown by the profile 1412. The diverging structure 1410 is a region formed of a material having a lower refractive index than the surrounding core. When a light beam is launched into the first length of optical fiber 1406, refraction from the diverging structure 1410 causes the beam divergence to increase in the first length of optical fiber 1406. The amount of increase in divergence depends on the amount of spatial overlap of the light beam with the diverging structure 1410 and the magnitude of the refractive index difference between the diverging structure 1410 and the core material. The diverging structure 1410 may have a variety of shapes depending on the input divergence distribution and the desired output divergence distribution. In one example, the diverging structure 1410 has a triangular or gradient index shape.

FIG. 15 shows a first length of optical fiber 1500, including a parabolic index central region 1502 surrounded by a constant index region 1504. A low index annular layer (or low index annular ring or ring) 1506 surrounding the parabolic index center region 1502 is between the constant index region 1504 and the parabolic index center region 1502. Low index ring 1506 helps guide the light beam through fiber 1500. When the propagating beam is perturbed, the modes move radially outward in the fiber 1500 (e.g., during bending of the fiber 1500). The parabolic index region 1502 facilitates maintaining the mode shape as one or more modes move radially outward. When the mode reaches the constant index region 1504 in the outer portion of the RIP 1510, it will compress on the low index ring 1506, which (compared to the first fiber RIP shown in fig. 14A and 14B) may result in preferential excitation of the outermost confinement region in the second fiber. In one implementation, this fiber design works with a confinement fiber having a central step-index core and a single annular core. The parabolic index portion 1502 of RIP 1510 overlaps the central step index core of the confining fiber. The constant index portion 1504 overlaps the annular core of the confinement fiber. The constant index portion 1504 of the first fiber is intended to make it easier for the beam to move to overlap the annular core by bending. This fiber design is also applicable to other designs of constrained optical fibers.

FIG. 16 shows a first length of optical fiber 1600 including guiding regions 1604, 1606, 1608, and 1616 bounded by lower index layers 1610, 1612, and 1614, wherein the indices of refraction of the lower index layers 1610, 1612, and 1614 are stepped or, more generally, do not all have the same value. When perturbation component 210 (see FIG. 2) acts on fiber 1600, the step index layer may serve to confine the beam intensity to certain guiding regions (1604, 1606, 1608, and 1616). In this manner, the conditioned beam can be captured in the guiding region through a series of perturbation actions (e.g., through a series of bend radii, a series of bend lengths, a series of microbending pressures, and/or a series of acousto-optic signals), thereby allowing a degree of perturbation tolerance before the beam intensity distribution moves to a more distant radial position in the optical fiber 1600. Thus, the change in the beam characteristics can be controlled stepwise. The radial widths of guide regions 1604, 1606, 1608, and 1616 may be adjusted to achieve a desired loop width, as may be desired for an application. Furthermore, if desired, the guiding region may have a thicker radial width in order to capture a larger portion of the incident beam profile. Region 1606 is an example of such a design.

Fig. 17-21 depict examples of optical fibers configured to be capable of maintaining and/or limiting the adjusted beam characteristics in a second length of optical fiber (e.g., optical fiber 208). These fiber designs are referred to as "ring-limited fibers" because they contain a central core surrounded by a ring or annular core. These designs are merely examples and are not exhaustive of the various optical fiber RIP's that may be used to maintain and/or limit the adjusted beam characteristics within the optical fiber. Accordingly, the claimed subject matter is not limited to the examples provided herein. Further, any of the first lengths of optical fiber described above in fig. 11-16 may be combined with any of the second lengths of optical fiber described in fig. 17-21.

FIG. 17 illustrates a cross-sectional view of an exemplary second length of optical fiber for maintaining and/or limiting adjusted beam characteristics in a VBC fiber assembly. When a perturbed beam is coupled from a first length of optical fiber to a second length of optical fiber 1700, the second length of optical fiber 1700 may retain at least a portion of the beam characteristics adjusted in response to the perturbation in the first length of optical fiber within one or more confinement regions 1704, 1706, and/or 1708. Optical fiber 1700 has RIP 1702. Each of the confinement regions 1704, 1706, and/or 1708 is bounded by a lower index layer 1710 and/or 1712. This design enables the second length of optical fiber 1700 to maintain the adjusted beam characteristics. As a result, the beam output by the optical fiber 1700 will substantially maintain the received adjusted beam, as modified in the first length of optical fiber, thereby providing the output beam with adjusted beam characteristics, which may be customized for a processing task or other application.

Similarly, FIG. 18 depicts a cross-sectional view of an exemplary second length of optical fiber 1800 for maintaining and/or limiting beam characteristics that are adjusted in response to perturbations of the first length of optical fiber in the VBC fiber assembly. Optical fiber 1800 has RIP 1802. However, confinement regions 1808, 1810, and/or 1812 have a thickness that is different from the thickness of confinement regions 1704, 1706, and 1708. Each of the confinement regions 1808, 1810, and/or 1812 is bounded by a lower index layer 1804 and/or 1806. Varying the thickness of the confinement region (and/or the barrier region) can customize or optimize the confined adjusted emissivity profile by selecting a particular radial position at which to confine the adjusted beam.

Fig. 19 depicts a cross-sectional view of an exemplary second length of optical fiber 1900 having a RIP 1902 for maintaining and/or confining an adjusted beam configured to provide variable beam characteristics in a VBC fiber assembly. In this example, the number and thickness of confinement regions 1904, 1906, 1908, and 1910 are different than the number and thickness of optical fibers 1700 and 1800, and barrier layers 1912, 1914, and 1916 also have different thicknesses. In addition, confinement regions 1904, 1906, 1908, and 1910 have different refractive indices, and barrier layers 1912, 1914, and 1916 also have different refractive indices. Such a design may further enable finer or optimized customization to limit and/or maintain the adjusted beam radiation for a particular radial position within the optical fiber 1900. When a perturbed beam is launched from a first length of fiber to a second length of fiber 1900, the modified beam characteristics of the beam (with adjusted intensity profile, radial position and/or divergence angle, etc., or combinations thereof) are confined within a particular radius by one or more confinement regions 1904, 1906, 1908, and/or 1910 of the second length of fiber 1900.

As previously described, the divergence angle of the beam may be maintained or adjusted and then maintained in the second length of fiber. There are various ways to change the divergence angle of the light beam. The following are examples of optical fibers configured to enable adjustment of the divergence angle of a light beam propagating from a first length of optical fiber to a second length of optical fiber in a fiber optic assembly to change the characteristics of the light beam. However, these are merely examples and are not exhaustive of the various methods that may be used to adjust the divergence of the light beam. Accordingly, the claimed subject matter is not limited to the examples provided herein.

Fig. 20 depicts a cross-sectional view of an exemplary second length of optical fiber 2000 having a RIP 2002 for modifying, maintaining and/or limiting beam characteristics adjusted in response to perturbations of the first length of optical fiber. In this example, the second length of optical fiber 2000 is similar to the second length of optical fiber described previously and forms part of a VBC fiber assembly for conveying variable beam characteristics, as described above. There are three confinement regions 2004, 2006, and 2008 and three barrier layers 2010, 2012, and 2016. The second length of optical fiber 2000 also has a diverging structure 2014 located within a confinement region 2006. The divergence structure 2014 is a region formed of a material having a lower index of refraction than the surrounding confinement region. When the light beam is launched into the second length of optical fiber 2000, refraction from the diverging structure 2014 causes the divergence of the light beam to increase in the second length of optical fiber 2000. The amount of increase in divergence depends on the amount of spatial overlap of the light beam with the diverging structure 2014 and the magnitude of the refractive index difference between the diverging structure 2014 and the core material. By adjusting the radial position of the light beam near the emission point emitted to the second length of optical fiber 2000, the divergence distribution can be changed. The adjusted divergence of the light beam is maintained in an optical fiber 2000, the optical fiber 2000 configured to convey the adjusted light beam to a processing head, another optical system (e.g., a fiber-to-fiber coupler or a fiber-to-fiber switch), a workpiece, or the like, or a combination thereof. In one example, the divergent structure 2014 may have about 10 relative to the surrounding material^-5-3x10^-2The refractive index of (2) decreases. Other values of the refractive index drop may be used within the scope of the present disclosure, and claimed subject matter is not so limited.

Fig. 21 depicts a cross-sectional view of an exemplary second length of optical fiber 2100 having a RIP 2102 for modifying, maintaining and/or limiting beam characteristics adjusted in response to perturbations of the first length of optical fiber. The second length of optical fiber 2100 forms part of a VBC fiber assembly for transmitting an optical beam having variable characteristics. In this example, there are three confinement regions 2104, 2106 and 2108 and three barrier layers 2110, 2112 and 2116. The second length of optical fiber 2100 also has a plurality of diverging structures 2114 and 2118. The diverging structures 2114 and 2118 are regions formed of a gradient low index material. When the light beam is launched from the first length of fiber to the second length of fiber 2100, refraction from the diverging structures 2114 and 2118 causes the beam divergence to increase. The amount of increase in divergence depends on the amount of spatial overlap of the light beam with the diverging structures and the magnitude of the refractive index difference between diverging structures 2114 and/or 2118 and the surrounding core material of confinement regions 2106 and 2104, respectively. By adjusting the radial position of the light beam near the emission point emitted to the second length of optical fiber 2100, the divergence distribution can be varied. The design shown in fig. 21 allows the intensity distribution and divergence distribution to be varied somewhat independently by selecting a particular confinement region and the divergence distribution within that confinement region (as each confinement region may include a diverging structure). The adjusted divergence of the light beam is maintained in an optical fiber 2100, the optical fiber 2100 being configured to deliver the adjusted light beam to a processing head, another optical system, or a workpiece. Forming the diverging structures 2114 and 2118 with a gradient or non-constant refractive index enables adjustment of the divergence profile of the light beam propagating in the optical fiber 2100. The adjusted beam characteristics (e.g., radiance profile and/or divergence profile) may be maintained while being conveyed to the processing head by the second optical fiber. Alternatively, the adjusted beam characteristics, such as radiance profile and/or divergence profile, may be maintained or further adjusted as the second fiber is routed through a fiber-to-fiber coupler (FFC) and/or a fiber-to-fiber switch (FFS) to the processing fiber that delivers the beam to the processing head or workpiece.

Fig. 26-28 are cross-sectional views illustrating an example of an optical fiber and optical fiber RIP configured to be able to maintain and/or limit an adjusted beam characteristic of a light beam propagating in an azimuthally asymmetric second length of optical fiber, wherein the beam characteristic is adjusted in response to a perturbation of the light beam by a perturbation device 110 coupled to a perturbation of the first length of optical fiber of the second length of optical fiber. These azimuthally asymmetric designs are merely examples and are not exhaustive of the various fiber RIPs that may be used to maintain and/or limit the adjusted beam characteristics within an azimuthally asymmetric fiber. Accordingly, the claimed subject matter is not limited to the examples provided herein. Further, any of the various first length optical fibers (e.g., similar to those described above) may be combined with any azimuthally asymmetric second length optical fibers (e.g., similar to those described in fig. 26-28).

Fig. 26 shows RIP at different azimuthal angles across the cross-section of an elliptical optical fiber 2600. At a first azimuthal angle 2602, fiber 2600 has a first RIP 2604. At a second azimuth angle 2606, rotated 45 ° from first azimuth angle 2602, optical fiber 2600 has a second RIP 2608. At a third azimuth angle 2610 rotated another 45 ° from the second azimuth angle 2606, the optical fiber 2600 has a third RIP 2612. The first RIP 2604, the second RIP 2608, and the third RIP2612 are all different.

Fig. 27 shows RIP at different azimuthal angles across a cross section of a multi-core fiber (MCF) 2700. At a first azimuth angle 2702, the optical fiber 2700 has a first RIP 2704. At a second azimuth angle 2706, the optical fiber 2700 has a second RIP 2708. The first RIP 2704 and the second RIP2708 are different. In one example, perturbation device 110 may act in multiple planes to launch the adjusted beam into different regions of the azimuthally asymmetric second fiber.

Fig. 28 shows RIP at different azimuthal angles across a cross-section of an optical fiber 2800 having at least one crescent-shaped core. In some cases, the corners of the crescent shape may be rounded, flattened, or otherwise shaped, which may minimize optical losses. At a first azimuthal angle 2802, the fiber 2800 has a first RIP 2804. At a second azimuth angle 2806, the fiber 2800 has a second RIP 2808. The first RIP 2804 and the second RIP2808 are different.

Fig. 22A illustrates an example of a laser system 2200 that includes a VBC fiber assembly 2202, the VBC fiber assembly 2202 configured to provide variable beam characteristics. The VBC fiber assembly 2202 includes a first length of fiber 104, a second length of fiber 108, and a perturbation device 110. The VBC fiber assembly 2202 is disposed between a feed fiber 2212 (i.e., an output fiber from a laser source) and a VBC delivery fiber 2240. The VBC delivery fiber 2240 may include a second length of fiber 108 or an extension of the second length of fiber 108 that modifies, maintains, and/or restricts the adjusted beam characteristics. The light beam 2210 is coupled into the VBC fiber optic assembly 2202 via a feed fiber 2212. Fiber optic assembly 2202 is configured to change a characteristic of light beam 2210 according to the various examples described above. The output of the fiber optic assembly 2202 is the conditioned light beam 2214, which is coupled into the VBC delivery fiber 2240. The VBC delivery fiber 2240 delivers the conditioned beam 2214 to the free-space optical assembly 2208, which free-space optical assembly 2208 then couples the beam 2214 into the processing fiber 2204. The conditioned beam 2214 is then transmitted to the processing head 2206 by the processing fiber 2204. The processing head may include guided-wave optics (e.g., optical fibers and fiber couplers), free-space optics (e.g., lenses, mirrors, filters, diffraction gratings), and/or beam scanning components (e.g., galvanometer scanners, polygon mirror scanners), or other scanning systems for shaping beam 2214 and delivering the shaped beam to the workpiece.

In laser system 2200, one or more free-space optics of assembly 2208 may be disposed in an FFC or other beam coupler 2216 to perform various optical operations on conditioned beam 2214 (represented in fig. 22A by dashed lines other than dashed line of beam 2210). For example, the free-space optical assembly 2208 can maintain the adjusted beam characteristics of the light beam 2214. Processed optical fiber 2204 may have the same RIP as VBC delivery fiber 2240. Thus, the adjusted beam characteristic of the adjusted beam 2214 may be maintained up to the processing head 2206. The processed fiber 2204 may include a RIP similar to any of the second lengths of fiber described above, including a confinement region.

Alternatively, as shown in fig. 22B, free-space optical assembly 2208 can change the adjusted beam characteristic of light beam 2214 by, for example, increasing or decreasing the divergence and/or spot size of light beam 2214 (e.g., by enlarging or reducing light beam 2214) and/or otherwise further modifying adjusted light beam 2214. Further, processed fiber 2204 may have a different RIP than VBC delivery fiber 2240. Thus, the RIP of the processed fiber 2204 can be selected to maintain additional adjustments to the adjusted beam 2214 by the free-space optics of the assembly 2208 to generate a twice adjusted beam 2224 (represented in fig. 22B by a dashed line different from the dashed line of beam 2214).

Fig. 23 shows an example of a laser system 2300 including a VBC fiber assembly 2302 disposed between a feed fiber 2312 and a VBC delivery fiber 2340. During operation, the light beam 2310 is coupled into the VBC fiber assembly 2302 via the feed fiber 2312. The fiber assembly 2302 includes the first length of optical fiber 104, the second length of optical fiber 108, and the perturbation device 110, and is configured to alter the characteristics of the optical beam 2310 according to the various examples described above. The fiber assembly 2302 generates a conditioned light beam 2314 that is output by the VBC delivery fiber 2340. The VBC delivery fiber 2340 includes a second length of optical fiber 108 for modifying, maintaining, and/or limiting the adjusted beam characteristics in the fiber assembly 2302 according to the various examples described above (see, e.g., fig. 17-21). The VBC delivery fiber 2340 couples the conditioned beam 2314 into a beam switch (FFS)2332, which then couples its various output beams to one or more of the multiple processing fibers 2304, 2320 and 2322. Processing fibers 2304, 2320, and 2322 deliver conditioned beams 2314, 2328, and 2330 to respective processing heads 2306, 2324, and 2326.

In one example, beam switch 2332 includes one or more sets of free-space optics 2308, 2316, and 2318 configured to perform various optical operations of conditioned beam 2314. Free-space optics 2308, 2316, and 2318 can maintain or change the adjusted beam characteristics of beam 2314. Thus, the adjusted light beam 2314 may be held or further adjusted by free space optics. The processed fibers 2304, 2320 and 2322 may have the same or different RIP than the RIP of the VBC carrying fiber 2340, depending on whether it is desired to maintain or further modify the optical beams carried from the free-space optical assemblies 2308, 2316 and 2318 to the respective processed fibers 2304, 2320 and 2322. In other examples, one or more beam portions of the beam 2310 are coupled to the workpiece without adjustment, or different beam portions are coupled to respective VBC fiber optic assemblies, such that beam portions associated with multiple beam characteristics can be provided for simultaneous workpiece processing. Alternatively, the beam 2310 may be switched to one or more of a set of VBC fiber assemblies.

The conditioned beam 2314 is routed through any of the free-space optical assemblies 2308, 2316 and 2318 so that various additional conditioned beams can be delivered to the processing heads 2206, 2324 and 2326. Thus, the laser system 2300 provides additional degrees of freedom to alter the characteristics of the beam and switch the beam between processing heads ("time sharing") and/or deliver the beam to multiple processing heads simultaneously ("power sharing").

For example, free-space optics in beam switch 2332 may direct adjusted beam 2314 to free-space optics 2316 configured to maintain adjusted characteristics of beam 2314. The processed fiber 2304 may have the same RIP as the RIP of the VBC delivery fiber 2340. Thus, the beam delivered to processing head 2306 will be the maintained adjusted beam 2314.

In another example, beam switch 2332 can direct adjusted beam 2314 to free-space optical assembly 2318, which is configured to maintain adjusted characteristics of adjusted beam 2314. The processed fiber 2320 may have a RIP different from that of the VBC carrying fiber 2340 and the divergence-altering structures described in fig. 20 and 21 may be configured to provide additional adjustment to the divergence profile of the light beam 2314. Thus, the beam delivered to processing head 2324 will be twice conditioned beam 2328 with a beam divergence profile that is different from the beam emittance profile of conditioned beam 2314.

Processed optical fibers 2304, 2320, and/or 2322 may include RIPs similar to any of the second lengths of optical fiber described above, including confinement regions or various other RIPs, and claimed subject matter is not so limited.

In yet another example, free-space optical switch 2332 may direct adjusted light beam 2314 to free-space optical assembly 2308, which is configured to change the beam characteristics of adjusted light beam 2314. The processed optical fiber 2322 may have a RIP different from that of the VBC carrying optical fiber 2340 and may be configured to retain (or alternatively further modify) the new further adjusted characteristic of the light beam 2314. Thus, the beam delivered to processing head 2326 will be twice conditioned beam 2330 with beam characteristics (due to the conditioned divergence profile and/or intensity profile) that differ from those of conditioned beam 2314.

In fig. 22A, 22B, and 23, the optics in the FFC or FFS can adjust the spatial profile and/or divergence profile by magnifying or demagnifying the light beam 2214 before launching into the processed fiber. The spatial profile and/or divergence profile may also be adjusted via other optical transformations. The launch location to the processed fiber may also be adjusted. These methods may be used alone or in combination.

Fig. 22A, 22B, and 23 merely provide examples of combinations of adjustments to beam characteristics using free-space optics and various combinations of fiber RIPs to hold or modify adjusted beams 2214 and 2314. The examples provided above are not exhaustive and are for illustrative purposes only. Accordingly, claimed subject matter is not so limited.

FIG. 24 illustrates various examples of a perturbation device, assembly or method for perturbing the VBC fiber 200 and/or an optical beam propagating in the VBC fiber 200 (collectively referred to herein as "perturbation device 110" for simplicity) according to various examples provided herein. The perturbation device 110 may be any of a variety of devices, methods, and/or components configured to be capable of adjusting the beam characteristics of the optical beam propagating in the VBC fiber 200. Some examples of various disturbance states that may be applied to the VBC fiber 200 include, but are not limited to, the amount or direction of bending, lateral mechanical stress, mechanical pressure caused by acoustic oscillations, temperature changes, piezoelectric transducer displacement, and varying period or amplitude of the refraction grating. The change in one or more states creates a different perturbation state. To change one or more of these states, the perturbation device 110 can be a mandrel 2402, a microbend 2404 in a VBC fiber, a flex tube 2406, an acousto-optic transducer 2408, a thermal device 2410, a piezoelectric device 2412, a grating 2414, a clamp 2416 (or other fastener), the like, or any combination thereof. These are merely examples of perturbation devices 100 and are not an exhaustive list of perturbation devices 100, and claimed subject matter is not limited in this respect.

The mandrel 2402 can be used to perturb the VBC fiber 200 by providing a form in which the VBC fiber 200 can bend. As described above, reducing the bend radius of the VBC fiber 200 moves the intensity profile of the beam radially outward. In some examples, the mandrel 2402 may be stepped or conical to provide discrete levels of bend radius. Alternatively, the mandrel 2402 may include a taper without a step to provide a continuous bend radius to more precisely control the bend radius. The radius of curvature of the mandrel 2402 may be constant (e.g., cylindrical) or non-constant (e.g., elliptical). Similarly, a flexible tube 2406, clamp 2416 (or other type of fastener), or roller 250 may be used to guide and control the bending of the VBC fiber 200 around the mandrel 2402. Furthermore, changing the length of the fiber that is bent at a particular bend radius can also modify the intensity profile of the beam. The VBC fiber 200 and the mandrel 2402 can be configured to predictably alter the intensity profile within the first fiber (e.g., proportional to the length and/or bend radius of the fiber bend). The roller 250 can be moved up and down along a track 2442 on a platform 2434 to change the bend radius of the VBC fiber 200.

With or without the mandrel 2402, a clamp 2416 (or other fastener) may be used to guide and control bending of the VBC fiber 200. The clamp 2416 can move up and down along the track 2442 or the platform 2446. The clamp 2416 can also be rotated to change the bend radius, tension or direction of the VBC fiber 200. The controller 2448 may control the movement of the clamp 2416.

In another example, the perturbation device 110 can be a flexible tube 2406 and can guide the bending of the VBC fiber 200 with or without a mandrel 2402. The flexible tube 2406 may surround the VBC optical fiber 200. Tube 2406 may be made of a variety of materials and may be manipulated using a piezoelectric transducer controlled by controller 2444. In another example, a clamp or other fastener may be used to move the flexible tube 2406.

Microbends 2404 in VBC fibers are local perturbations caused by lateral mechanical stress on the fiber. Microbending can cause one or both of mode coupling and transition from one confinement region to another confinement region within the fiber, resulting in different beam characteristics of the beam propagating in the VBC fiber 200. The mechanical stress may be applied by an actuator 2436 controlled by a controller 2440. For example, the VBC perturbing means 110 can be configured to control the beam propagation path in the VBC fiber 200 in one or both axes by providing microbends 2404 to the VBC fiber 200 at selected radial positions. According to one embodiment, the actuator 2436 includes two actuator probes 2436a and 2436b positioned to apply mechanical stress to the VBC fiber 200 in orthogonal directions, thereby directing the beam propagating in the VBC fiber 200 to any location in two-dimensional space. In other embodiments, several azimuthally spaced probes are provided to apply forces at discrete angles around the perimeter to modify the beam propagation path. However, these are merely examples of methods of inducing mechanical stress in optical fiber 200 and claimed subject matter is not limited in these respects. The skilled person will appreciate that various other techniques for beam steering are also suitable.

An acousto-optic transducer (AOT)2408 may be used to induce perturbations in a beam propagating in a VBC fiber using acoustic waves. The perturbation is caused by the oscillating mechanical pressure of the acoustic wave modifying the refractive index of the optical fiber. The period and intensity of the acoustic wave is related to the frequency and amplitude of the acoustic wave, allowing dynamic control of the acoustic wave disturbance. Accordingly, perturbation assembly 110, including AOT 2408, may be configured to alter the beam characteristics of the optical beam propagating in the optical fiber. In one example, the piezoelectric transducer 2418 can generate sound waves and can be controlled by a controller or driver 2420. The acoustic waves induced in the AOT 2408 may be modulated to change and/or control the beam characteristics of the beam in the VBC 200 in real time. However, this is merely an example of a method for creating and controlling AOT 2408 and claimed subject matter is not limited in this respect.

The thermal device 2410 may be used to induce perturbations in the light beam propagating in the VBC fiber using heat. The perturbation is caused by modifying the RIP of the heat-induced fiber. The perturbation can be dynamically controlled by controlling the amount of heat delivered to the fiber and the length of heat applied. Accordingly, perturbing member 110, including thermal device 2410, may be configured to alter a range of beam characteristics. Thermal device 2410 may be controlled by controller 2450.

The piezoelectric transducer 2412 may be used to induce a perturbation of a light beam propagating in the VBC fiber using piezoelectric action. The perturbation is caused by modifying the RIP of the optical fibre induced by the piezoelectric material connected to the optical fibre. The piezoelectric material in the form of a jacket around the bare optical fiber can apply tension or compression to the optical fiber, thereby modifying its refractive index via the resulting density change. The perturbation may be dynamically controlled by controlling the voltage of the piezoelectric device 2412. Accordingly, the perturbation assembly 110 comprising the piezoelectric transducer 2412 may be configured to change the beam characteristics within a certain range.

In one example, the piezoelectric transducer 2412 can be configured to move the VBC fiber 200 in multiple directions (e.g., axially, radially, and/or laterally) depending on a variety of factors, including how the piezoelectric transducer 2412 is connected to the VBC fiber 200, the polarization direction of the piezoelectric material, the applied voltage, and the like. In addition, the VBC fiber 200 can be bent using the piezoelectric transducer 2412. For example, driving a length of piezoelectric material having multiple sections with opposing electrodes may cause the piezoelectric transducer 2412 to bend in a lateral direction. The voltage applied by the electrodes 2424 to the piezoelectric transducer 2412 can be controlled by the controller 2422 to control the displacement of the VBC fiber 200. The displacement may be modulated to change and/or control the beam characteristics of the beam in the VBC 200 in real time. However, this is merely an example of a method of controlling displacement of the VBC fiber 200 using the piezoelectric transducer 2412, and claimed subject matter is not limited thereto.

The grating 2414 may be used to induce perturbations in the beam propagating in the VBC fiber 200. The grating 2414 can be written into the fiber by noting the periodic changes in the refractive index into the core. The grating 2414 (e.g., a fiber bragg grating) may operate as a filter or reflector. Long period gratings may induce transitions between co-propagating fiber modes. Thus, a long period grating may be used to adjust the radiance, intensity profile, and/or divergence profile of a beam of one or more modes to couple one or more original modes to one or more different modes having different radiance and/or divergence profiles. The adjustment is achieved by changing the period or amplitude of the refractive index grating. For example, methods of changing the temperature, bend radius and/or length (e.g., stretching) of the fiber bragg grating may be used for such adjustment. The VBC fiber 200 with the grating 2414 can be coupled to a stage 2426. The table 2426 may be configured to perform any of a variety of functions and may be controlled by a controller 2428. For example, the table 2426 can be coupled to the VBC fiber 200 with a fastener 2430, and can be configured to use the fastener 2430 to stretch and/or bend the VBC fiber 200 to leverage. Stage 2426 can have an embedded thermal device and can change the temperature of the VBC fiber 200.

Fig. 25 illustrates an example process 2500 for adjusting and/or preserving beam characteristics within an optical fiber without using free-space optics to adjust the beam characteristics. In block 2502, the first length of optical fiber and/or the optical beam is perturbed to adjust one or more characteristics of the optical beam. Process 2500 moves to block 2504 where the light beam is launched into the second length of optical fiber. Process 2500 moves to block 2506 where the optical beam with the adjusted beam characteristic propagates in the second length of optical fiber. Process 2500 moves to block 2508 where at least a portion of one or more beam characteristics of the beam are maintained within one or more confinement regions of the second length of optical fiber. The first length of optical fiber and the second length of optical fiber may be comprised of the same optical fiber, or may be different optical fibers.

The present inventors have recognized that relatively high-speed perturbation actuation optimizes certain laser machining operations. In this case, relatively high speed perturbation means that due to material properties and heat dissipation mechanisms, the perturbation state is switched faster than the material temperature, and highly localized exposure intensity variations can be significantly simulated. Perturbation devices implemented with fast actuators (e.g., piezoelectric or voice coil actuators) can be used to simulate various alternative temporal and spatial effects. These effects rapidly change the adjusted beam position for limiting the beam according to a repeating sequence (i.e., pattern) of different limiting regions. In one embodiment, controlled oscillation of the dithered beam or other high speed programmable sequential adjustment rapidly changes the confinement of the beam to produce a temporary apparent intensity profile (also referred to simply as a temporal profile) at the output of the second length of fiber that improves the performance of the cut or weld.

In contrast to the purely spatial intensity distributions described previously with reference to fig. 7-10, the temporal apparent intensity distribution is based on the average or cumulative beam power delivered onto the area, for example, according to some repeatable sequence of delivered power at discrete locations in the area. In other words, time-weighted or time-averaged power means that the power of the beam does not need to be directly increased or decreased at any particular time to affect the area of the workpiece. Instead, the area of the effective beam front is subdivided into locations where the beams are incident, and the dwell time at certain locations is adjustable to vary the time-weighted power transmittable at the locations in the area.

Fig. 29, 30 and 31 show by way of example how a set of confinement regions constructed from the second length of optical fiber 208 serve as the aforementioned discrete locations. Fig. 29 shows the optical power 2900 delivered to the confinement region 216 for a controllable amount of time. Likewise, fig. 30 shows the optical power 3000 delivered to the confinement region 218 for a controllable amount of time. Fig. 31 shows the optical power 3100 delivered to the confinement region 220 for another controllable amount of time. However, the amount of time and sequence that the beam power is delivered to each of the confinement regions 216, 218, and 220 is controllable and can be dynamically varied to produce a selectable temporal apparent intensity profile. Thus, the beam power is distributed over two or more locations in the relevant area, not only spatially but also temporally, according to a repeatable sequence of locations and dwell times. Several examples of temporal apparent intensity distributions are presented in fig. 32A, 32B, and 32C, although one skilled in the art will appreciate that substantially any temporal distribution is possible. Note that the following letters "a", "B", "C", etc. represent different alternative time distributions.

Fig. 32A, 32B, and 32C show three different time-weighted configurations for forming temporal apparent intensity distributions for plateau 3210, saddle (or alternatively, ring) 3220, and step (i.e., high-granularity gaussian approximation) 3230, respectively. As previously described, these temporal apparent intensity profiles are formed as the sequence of intensities is transmitted to a set of different elements of the confined area, and the sequence is repeated according to a pattern. Thus, different sequences (i.e., a particular order of restricted area activity) may be repeated in the pattern that ultimately results in substantially the same final temporal distribution, although the sequences in the pattern are different.

However, in this example, there are at least two ways in which temporal distribution can be achieved. First, the beam dwells when different target locations (i.e., one or more members of the set of restricted areas) in the sequence can vary. Second, the dwell time may be equal for all target locations, but some target locations repeat with the sequence. (the word "sequence" need not imply that consecutive target locations are adjacent, although in some embodiments they may be, for example, dithered). Either technique enables time averaging or time weighting to effectively transform the static intensity distribution into various time distributions that do not need to be statically actuated by the inherent (e.g., static bending) perturbation states previously described. Thus, for ease of description, the intensity is described in terms of percentages, and the following examples are described in terms of variable residence times.

The residence time of the flat top distribution 3210 in each zone was approximately 33.33%. The dwell time of saddle shaped distribution 3220 is about 57.2% in region 220, about 28.6% in region 218, and about 14.2% in region 216. The residence time for the stepped profile 3230 is about 14.2% in region 220, about 28.6% in region 218, and about 57.2% in region 216. Various other percentages are possible, for example, 75/25%. In non-percent absolute terms, the skilled artisan will appreciate that the dwell time at a particular location is a function of the desired profile, the type of laser process, and the thermal material properties of the workpiece (e.g., thermal conductivity, thermal diffusivity, specific heat, melting point, or other properties).

The actuation speed for achieving the temporary apparent intensity profile may also depend on the type of workpiece material being processed. For example, to properly alias the time distribution (i.e., mitigate the effects of beam position transitions) in highly thermally conductive materials (e.g., copper or aluminum), a faster actuation rate is used. On the other hand, a slightly slower transition between beam positions may provide a time profile suitable for laser machining operations on materials with lower thermal conductivity (e.g., large steel plates that absorb a large amount of heat). For example, dwell times of about 20 milliseconds (ms) have been contemplated to improve results during laser perforation operations. However, the skilled person will appreciate that shorter residence times are possible.

Fig. 33 shows a beam shaper system 3300 implemented with a beam delivery device 3302 in the form of a VBC fiber 3306 constructed in accordance with the disclosed example represented by the example VBC fiber 100 (see, e.g., fig. 1 for more detail). Some of the previously described details of fig. 1 are further simplified for the sake of brevity and are therefore not reproduced in fig. 33.

The laser source 3010 emits an optical beam 102 (fig. 1) propagating in a first length of optical fiber 3312, the first length of optical fiber 3312 corresponding to the first length of optical fiber 104 (fig. 1). The beam 102 is incident on the VBC fiber 3306. The perturbation device 110 operates in conjunction with the VBC fiber 3306 and applies different perturbation conditions (e.g., different amounts or directions) to the VBC fiber 3306, the perturbation device 110 directing the fiber modes to different respective confinement regions of a second length of fiber 3320, the second length of fiber 3320 corresponding to the second length of fiber 108 (fig. 1). The second length of optical fiber 3320 is an MCF 3400 (fig. 34) constructed according to the disclosed example represented by example MCF2700 (see, e.g., fig. 27), but with multiple designer-selected cores, as described below.

As previously described with reference to fig. 24, using the example output results shown in fig. 29-31, controller 3330 enables beam shaper system 3300 to selectively move the fiber mode (i.e., intensity profile) of beam 102 to different regions at the input of second length of optical fiber 3320. In some embodiments, controller 3330 comprises a computer workstation having an input-output (I/O) device adapted to establish a signal interface with perturbation device 110 to signal a perturbation state corresponding to a desired beam shape indicated by, for example, a user input. The skilled person will appreciate that the controller 3330 may comprise a Central Processing Unit (CPU), a Field Programmable Gate Array (FPGA) or other control device adapted to perform logical operations. The controller 3330 may also include a non-transitory machine-readable storage medium having stored thereon instructions that, when executed, cause the controller 3330 to perform any of the methods or operations described in this disclosure.

In the first "A" configuration, the controller 3330 signals the perturbation device 110 to apply a first sequence (i.e., mode) of perturbation states to the VBC fiber 3306 to establish a first temporary apparent intensity distribution 3340 at the output of the second length of fiber 3320_A. Then, has a first selected intensity distribution 3340_AIs transmitted by the processing head 3350 to the workpiece 3360.

In a subsequent "B" configuration, the controller 3330 signals the perturbation device 110 to apply a second perturbation condition, different from the first condition, to the VBC fiber 3306 to establish a different selected intensity profile 3340 at the output of the second length of fiber 3320 than the first selected intensity profile 3340_ASecond selected intensity profile 3340_B. Thus, the perturbation device 110, in response to a control signal from the controller 3330, applies a selected amount or direction of rapid bending to the VBC fiber 3306, which in turn moves the fiber mode to a set of different target locations of the confined area, thereby providing a way to establish a different, selectable, temporary apparent intensity profile 3370 at the output end of the second length of fiber 3320. Will be described later with respect to intensity distribution 3340_B、3340_CAnd 3340_DAdditional details of the configuration of (a).

Just as each distribution 3370 has process-specific dwell time and spatial parameters, different temporal apparent intensity distribution 3370 selections are made based on different workpiece material properties. Thus, according to some embodiments, the change from one perturbation mode to another is configured indirectly, for example, in response to a selected change 3380 in the type of material to be machined or a selected change 3380 in calibration settings for an indirect correlation with a material of the same or different type as the workpiece 3360. In other embodiments, the change from one perturbation mode to another is configured directly, for example, by directly selecting 3390 the desired beam shape (i.e., potentially material independent). Thus, a user may simply select a material or beam shape through a selection interface 3396 provided by, for example, the controller 3330, in order to dynamically change the beam shape. Changes may also be made wholly or partly autonomously. For simplicity, the resulting intensity profile, which is selected directly or indirectly, is referred to simply as the selected intensity profile.

Although the intensity distribution 3340_A、3340_B、3340_CAnd 3340_DNot completely azimuthally symmetric, but those skilled in the art will appreciate that the selection of an azimuthally symmetric intensity distribution is sometimes understood to mean the selection of an intensity profile, since in an azimuthally symmetric set of confinement regions, a given intensity profile is generally the same at any radial cross-sectional location in the set of confinement regions.

Fig. 34 and 35 show MCF 3400. In fig. 34, the right core 3410 is the active member in a set of confined areas for producing the apparent distribution, as previously described. Also, in fig. 35, the left core 3510 is the active member of the group. However, the skilled person will appreciate that each core in MCF 3400 may be used to transfer optical power and, therefore, collectively provide an array of optical fibre pixels (or so-called optical fibre pixels) for generating the various modes, examples of which are shown in fig. 36A, 36B, 36C and 36D, respectively as intensity profile 3340 shown in fig. 33_A、3340_B、3340_CAnd 3340_DIs shown enlarged. Note that "top," "bottom," "left," "right," and the like are used as a frame of reference for one example to facilitate description. In practice, the actual direction may vary.

In contrast to the coaxial confinement region examples described above, fiber pixels are capable of achieving non-azimuthally symmetric power densities. For example, a bowtie-shaped intensity profile 3340 is established by avoiding resting on the top and bottom regions_A. Non-azimuthally symmetric power densities have many applications.

For example, when cutting, the non-azimuthally symmetric power density shown in fig. 36B may deliver a higher time-averaged power at the cut-out side of the cut and a lower time-averaged power at the center of the cut. A reverse configuration, not shown, is useful, for example, for melting previously cut sides or other aspects that improve the quality of the cut.

Fig. 36C shows an example that is useful when welding two different types of metals together. The non-azimuthally symmetric beam shape of fig. 36C delivers a higher time-weighted power to one type of metal with a first thermal response on one side of the beam. At the same time, the shape delivers a lower time-weighted power to another type of metal having a second thermal response different from the first thermal response on the other side of the beam.

Finally, fig. 36D shows an elongated strip 3340 of relatively high time-averaged power_D. This is useful for creating wider incisions. Further, according to some embodiments, the following updates are used to generate the stripe 3340_DThe ribbon may be rotated relatively slowly clockwise or counter-clockwise about the central core. Thus, the pattern comprises a longer sequence (i.e. a different sequence of stripes), which essentially results in a rotated stripe time distribution. More generally, any temporal distribution may be dynamically changed. For example, the time-weighted power may be dynamically changed to accommodate different layers or coatings during cutting, and the individual sequences or overall pattern may be changed in synchronization with the feed rate and workpiece geometry to optimize cutting. The modes can be rapidly switched to produce different, temporary apparent intensity profiles for different alloys, thicknesses or coatings.

The applicant presently believes that the above dynamic variations also contribute to the induction of thermally induced mechanical vibrations in the workpiece. Generally, vibrations induced at or near the resonant frequency of a structure are used to greatly amplify the vibration intensity. To facilitate material separation, this phenomenon can be exploited to rapidly propagate material defects (e.g., cracks). The vibrations may be the result of rapid changes in temperature experienced during operation of the described process. In these cases, the speed at which the sequence is performed is deliberately below the so-called aliasing speed, so that the temperature profile at a particular location oscillates significantly at the resonance frequency. These advantages can be more easily achieved by pulsed operation of the light source. Despite the above concepts, whether thermally-induced mechanical vibrations promote material separation will depend on the parameters of the particular application, such as the thermal performance of common materials, the actual conditions of use, and the actuation mechanism.

The disclosed fiber coupling techniques provide different, temporal apparent intensity profiles that can be tailored for different materials and optimize laser processing (i.e., cutting, welding, glazing, or other types of processing). Among other things, the disclosed technique solves the problem of beam profiles that are only spatially selectable with limited static intensity distribution settings. Thus, the disclosed techniques facilitate adjusting kerf size, melt jetting (edge quality), or other laser machining parameters.

Having described and illustrated the general principles and specific principles of examples of the presently disclosed technology, it should be apparent that these examples can be modified in arrangement and detail without departing from such principles. We claim all modifications and variations coming within the spirit and scope of the following claims.