阅读说明：本技术 纤维增强3d打印 (Fiber-reinforced 3D printing ) 是由 米可·胡托宁 简妮·皮拉贾玛基 于 2018-01-18 设计创作，主要内容包括：一种3D打印机包括用于供应预浸渍纤维复合长丝(800)的打印头(500),预浸渍纤维复合长丝包括在热塑性基体材料之内的非弹性轴向纤维股线。在长丝供应器与加热喷嘴(2)之间的第一加热区(1)能够加热到基体的熔化温度之上。喷嘴之后的固结元件(9)将固结力施加到长丝,以使长丝附着到部件上。喷嘴能够加热到至少基体的熔化温度。长丝被驱动通过第一加热区进入喷嘴中。第一加热区之前的冷区(6)使长丝的温度保持低于基体的熔化温度。第一加热区与喷嘴之间的热断区(7)在第一加热区与喷嘴之间产生温度间隙。打印头/固结元件能够在三个自由度上移动。本申请进一步涉及一种部件的增材制造的方法。(A 3D printer includes a print head (500) for supplying pre-impregnated fiber composite filaments (800) including inelastic axial fiber strands within a thermoplastic matrix material. A first heating zone (1) between the thread supply and the heating nozzle (2) can be heated above the melting temperature of the substrate. A consolidation element (9) after the nozzle applies a consolidation force to the filaments to adhere the filaments to the part. The nozzle is capable of being heated to at least the melting temperature of the substrate. The filaments are driven through a first heating zone into a nozzle. A cold zone (6) preceding the first heating zone maintains the temperature of the filaments below the melting temperature of the substrate. A thermal break zone (7) between the first heating zone and the nozzle creates a temperature gap between the first heating zone and the nozzle. The print head/solid element is capable of movement in three degrees of freedom. The application further relates to a method of additive manufacturing of a component.)

1. A three-dimensional printer (300), the three-dimensional printer (300) for additive manufacturing of a part (700), the three-dimensional printer (300) comprising:

a build platen (100) for supporting the component (700) to be manufactured; and

a print head (500) comprising or connected to a fibre composite filament supply loaded with a thermoplastic pre-impregnated fibre composite filament (800) comprising one or more non-elastic axial fibre strands extending within a thermoplastic matrix material of the filament (800);

wherein the print head (500) comprises:

a first heating zone (1) between the fibre composite filament supply and the heating nozzle (2), the first heating zone (1) being heatable by a first heater above the melting temperature of the thermoplastic matrix material to preheat the pre-impregnated fibre composite filaments (800);

A consolidation element (9) located after the heating nozzle (2) to apply a consolidation and/or compaction force to the fiber composite filament (800) to affix the fiber composite filament (800) to the component (700), wherein the consolidation element (9) opposes at least one of the build platen and a previously printed structure of the component, the heating nozzle (2) is heatable by a second heater to at least a melting temperature of the matrix material to heat the fiber composite filament (800);

a filament drive (4) driving a fibre composite filament (800) comprising one or more inelastic axial fibre strands through the first heating zone (1) into the heating nozzle (2) at a selected feed rate,

a cold feed zone (6) between the filament drive (4) and the first heating zone (1) to maintain the temperature of the fiber composite filaments (800) below the melting temperature of the matrix material;

a non-heated thermal break zone (7) between the first heating zone (1) and the heating nozzle (2) to create a temperature gap between the first heating zone (1) and the heating nozzle (2);

Wherein the three-dimensional printer (300) comprises a plurality of actuators to move at least a print head (500) comprising the consolidation element (9) in three degrees of freedom relative to the build platen (100).

2. The three-dimensional printer of claim 1, wherein:

-the print head (500) comprising the consolidation element (9) is movable about its selected axis;

-the print head (500) comprising the consolidation element (9) is rotatable in a selected rotation thereof;

the build platen (100) is movable about a selected axis thereof; and/or

The build platen (100) is rotatable in a selected rotation thereof.

3. The three-dimensional printer according to claim 1 or 2, wherein it further comprises a controller (200) operatively connected to the first and second heaters, the filament driver (4), the print head (500) comprising the consolidation element (9) and the plurality of actuators, wherein the controller (200) is configured to execute instructions causing the composite filament (800) to extrude to form the component (700).

4. The three-dimensional printer according to claim 1, 2 or 3, wherein it further comprises

A polymer driver configured to feed polymer filaments into a polymer extrusion nozzle;

a polymer heater configured to heat the polymer filaments to a temperature above a melting temperature of the polymer;

wherein the polymer extrusion nozzle is configured to extrude the polymer filaments to form the part.

5. The three-dimensional printer according to any one of the preceding claims, wherein it further comprises:

a support material driver configured to feed support material into a support material extrusion nozzle;

a support material heater configured to heat the support material to a temperature above a melting temperature of the support material;

wherein the support material extrusion nozzle is configured to extrude the support material filament to form a support structure for the component (700).

6. The three-dimensional printer according to any one of the preceding claims, wherein the controller (200) executes instructions to additively manufacture a layered structure of support material, polymer and the composite filament (800).

7. A method for additive manufacturing of a component, comprising:

Supplying a thermoplastic pre-impregnated fiber composite filament comprising one or more inelastic axial fiber strands extending within a thermoplastic matrix material of the filament;

supporting a component to be manufactured on a build platen;

preheating the pre-impregnated fiber composite filaments at a first heating zone (1) between the fiber composite filament supply and a heating nozzle (2), wherein the temperature of the first heating zone (1) is set above the melting temperature of the thermoplastic matrix material;

heating the fiber composite filaments in the heating nozzle (2), wherein the temperature of the heating nozzle is set above the melting temperature of the matrix material;

applying a consolidation force and/or a compaction force to the fiber composite filaments (800) by means of a consolidation element (9) attached to the heating nozzle (2) to attach the fiber composite filaments (800) to the component (700);

moving a print head (500) comprising the consolidation element (9) in three degrees of freedom relative to the build platen by a plurality of actuators;

driving the fibrous composite filaments comprising one or more inelastic axial fiber strands through the first heating zone (1) into the heating nozzle (2) at a selected feed rate,

Maintaining the temperature below the melting temperature of the matrix material at a cold feed zone (6) extending between the filament drive (4) and the first heating zone (1);

interrupting the heating of the fiber composite filament (800) at a non-heated thermal break zone (7) between the first heating zone (1) and the heating nozzle (2) to create a temperature gap between the first heating zone (1) and the heating nozzle (2).

8. The method of claim 7, comprising: extruding the composite filament to form the part.

9. The method according to claim 7 or 8, comprising: extruding polymer filaments through a polymer extrusion nozzle to form the part.

10. The method of claim 7, 8 or 9, comprising: extruding a support material through a support material extrusion nozzle to form the component.

11. The method according to any of the preceding claims 7 to 10, comprising: performing additive manufacturing of a layered structure of a support material, a polymer, and the composite filament.

12. The method according to any of the preceding claims 7 to 11, comprising: additive manufacturing of a layered structure of support material, polymer and the composite filaments is performed by varying the layer thicknesses of the support layer, the polymer layer and the composite fibre material layer.

13. The method according to any of the preceding claims 7 to 12, comprising: performing additive manufacturing of a freely arranged 3D structure of a support material, a polymer and the composite filament.

14. The method according to any of the preceding claims 7 to 13, comprising: performing additive manufacturing of a freely arranged 3D structure of support material, polymer and the composite filament, wherein the structure has a selected area thickness of support material, polymer material and composite fibre material.

15. The three-dimensional printer according to any one of the preceding claims 1 to 6 or the method according to any one of the preceding claims 7 to 14, wherein the consolidation element (9) is a consolidation ring (9).

Technical Field

The present invention relates to additive manufacturing of components, and more particularly to a method and three-dimensional printer for additive manufacturing of fibre reinforced components.

Background

The following background description may include insights, discoveries, understandings or disclosures, or relevant content along with disclosures not known to the relevant art prior to the present invention but provided by the present disclosure. Some such contributions disclosed herein may be specifically pointed out below, while other such contributions encompassed by the present disclosure are apparent from their context.

Automated Fiber Placement (AFP) refers to an additive manufacturing process for composite structures in which continuous fibers are aligned layer-by-layer on a predetermined path to form the structure. Automated fiber placement of thermoplastic composites is known in the art. AFP technology is useful for thermoset polymers and thermoplastic polymers with continuous reinforcing fibers (carbon fibers, glass fibers, etc.). In AFP, the thermoplastic polymer feedstock is in the form of impregnated, preformed and cured fibre bundles. The fiber bundle is fed through a print head where the fiber bundle is heated above the melting temperature of the matrix polymer (i.e., thermoplastic polymer). The print head is connected to a robot arranged to perform printing of the fibres in a predetermined three-dimensional (X-Y-Z) path to form the desired configuration of the final part.

Fuse Fabrication (FFF) is a three-dimensional (3D) printing technique in which continuous filaments of thermoplastic material are used. The mechanical properties of 3D printed objects manufactured by using fuse manufacturing techniques are limited, as these objects typically consist only of polymers. This limitation can be mitigated by adding chopped (short) fiber reinforcement to the polymer to print the filaments, but this does not significantly improve the mechanical properties of the 3D printed object.

Continuous fiber reinforcement can be used in plastic composites to provide high strength. However, to date, the commercial experience of using continuous fiber reinforcement in fuse manufacturing has been very limited.

US5936861A discloses a technique of Fused Filament Fabrication (FFF) using pre-impregnated continuous fibre reinforcement raw material to extrude a continuous fibre reinforcement through a single nozzle, wherein during printing the reinforcement fibres are impregnated on an external impregnation tank linked to the printing device. During 3D printing, the fiber reinforcement is impregnated in an external impregnation device located in front of the printing device. Alternatively, a co-milled fiber bundle is used, where both the matrix and the reinforcement fibers are in the form of fibers in the same fiber bundle, which is fed through a 3D printing nozzle where the matrix fibers melt and cause the fibers to be impregnated.

"Three-dimensional printing of connecting-fibers by in-nozzle impregnation" (scientific report 6, article No. 23058(2016), doi:10.1038/srep23058, 2016, 11.3.11.h. online (http:// www.nature.com/articules/srep 23058)) published by Ryosuke Matsuzaki et al discloses a device using an impregnation nozzle in which fibers are impregnated with a thermoplastic polymer during printing.

US 14491439 and US 9327453B 2 disclose the use of a twin extruder to print the polymer matrix and continuous fiber reinforcement. They disclose the use of FFF, where 3D printing of continuous fibers is performed using pre-impregnated, pre-formed and cured fiber filaments that are impregnated with a thermoplastic polymer and heated in a fiber printing nozzle. The 3D printer further comprises another printing nozzle for printing only the base material. The fiber printing nozzle applies a flattening/ironing force to the molten fiber reinforcement filaments within the nozzle. In the automated fiber placement technique, the flattening/ironing force is equal to the consolidation force.

Using the FFF method and AFP method of printing continuous fibers, 3D structures are created layer-by-layer by applying continuous fiber reinforcement to form the final structure. In FFF and AFP, continuous fibers embedded in a thermoplastic or thermoset polymer matrix are extruded through a print head to form a continuous fiber reinforced 3D structure. The AFP and FFF of continuous fibers differ in the size and form of the printed object. In AFP, very large objects are typically generated, whereas AFP is typically used (but not limited to) to form hollow structures. On the other hand, the FFF of continuous fibers can be used to generate smaller objects of any shape.

In both continuous fiber FFF and thermoplastic polymer AFP technologies, the raw materials are in the form of impregnated, preformed and cured fiber reinforcement tows. In the FFF of continuous fibers and AFP technology of thermoplastic polymers, a raw tow is fed through a print head where the tow is heated above the melting temperature of the matrix polymer, after which the fibers are laid layer by layer on a printing surface. In both FFF for continuous fibers and AFP for thermoplastic polymers, the molten fibers are subjected to compaction forces (i.e., consolidation forces and/or flattening/ironing forces) that adhere the fibers to the part being fabricated. In AFP, the compaction/consolidation force is applied by a consolidation roller, while in FFF of continuous fibers, the compaction/consolidation force is applied by the external geometry of a heated fiber printing nozzle (ironing edge). In the AFP technique, this force is referred to as a compaction/consolidation force, while in the FFF of continuous fibers, this force is referred to as a flattening/ironing force. FFF and AFP can be used to extrude continuous fibers embedded in thermoplastic polymers or thermoset polymers and create objects from these materials by additive manufacturing (i.e., 3D printing). Existing 3D printing technology differs from automated fiber placement technology that prints continuous fibers in the size and form of the printed object.

In FFF and AFP, fibers are compacted onto printed parts by melt bonding of the polymer surface. Fusion bonding comprises three stages: intimate contact, molecular diffusion (reattachment or self-adhesion), and consolidation. The intimate contact stage comprises: the two surfaces are bonded together under heat and pressure such that the polymer matrix of each surface is in direct contact with each other. Once intimate contact is achieved, the polymer chains diffuse between the two layers (surfaces) by thermal vibration and entangle to form a bond. Finally, the bonded area is cooled under pressure and a cohesive bond (bond) is formed.

Other techniques include devices using impregnation nozzles in which the fibers are impregnated with a thermosetting photocurable polymer in specially designed impregnation nozzles during printing, or in which fiber layers are stacked together.

Despite the above methods, there is still a need to provide a more advanced 3D printing technique of continuous fiber reinforcement.

Disclosure of Invention

The following presents a simplified summary of the features disclosed herein in order to provide a basic understanding of some example aspects of the invention. This summary is not an extensive overview of the invention. It is not intended to identify key/critical elements of the invention or to delineate the scope of the invention. Its sole purpose is to present some concepts disclosed herein in a simplified form as a prelude to the more detailed description.

According to one aspect, the subject matter of the independent claims is provided. Embodiments are defined in the dependent claims.

Examples of one or more implementations are set forth in more detail in the accompanying drawings and the description below. Other features will be apparent from the description and drawings, and from the claims.

Drawings

In the following, the invention will be described in more detail by means of preferred embodiments with reference to the accompanying drawings, in which

FIG. 1 is a schematic diagram illustrating a 3D printer according to an exemplary embodiment;

fig. 2 is a schematic diagram illustrating a prior art 3D printing unit;

fig. 3 is a schematic diagram illustrating a 3D printing unit according to an exemplary embodiment;

fig. 4 is a flowchart illustrating a 3D printing process according to an exemplary embodiment;

FIG. 5 is a schematic diagram illustrating a fiber printing unit according to an exemplary embodiment;

fig. 6A is a schematic diagram illustrating a 3D printing component according to an exemplary embodiment;

fig. 6B is a schematic diagram illustrating a 3D printing component according to an exemplary embodiment;

fig. 7A and 7B are schematic views illustrating a 3D printing structure according to an exemplary embodiment;

fig. 8A, 8B, 8C, and 8D are schematic views illustrating an exemplary structure of the print head.

Detailed Description

The following embodiments are exemplary. Although the specification may refer to "an", "one", or "some" embodiment(s), this does not necessarily mean that each such reference is to the same embodiment, or that the feature applies to only a single embodiment. Individual features of different embodiments may also be combined to provide further embodiments. Furthermore, the words "comprise", "comprises" and "comprising" should be understood as meaning: the described embodiments are not limited to only those features which have been mentioned, but they may also contain features/structures which are not specifically mentioned.

One embodiment discloses a structure of a 3D printed object consisting of a polymer and a continuous/semi-continuous fiber reinforcement embedded in a polymer matrix and a method for additive manufacturing of such a structure.

Fig. 1 shows an exemplary 3D printer 300, which includes three separate 3D printing units (i.e., printheads): a first printing unit 400 for 3D printing the support material, a second printing unit 600 for 3D printing the polymer filaments, and a third printing unit 500 for 3D printing the composite fiber reinforcement filaments 800. First printing unit 400, second printing unit 600, and third printing unit 500 are free to move in the X/Y/Z dimension and in each possible 3D rotation about the X/Y/Z axis (i.e., each printhead 400, 500, 600 is controllable and programmable, and is capable of operating on three-dimensional spatial axes, and further optionally rotates about 3 rotational axes, however, the number of printing units is not limited to three, other embodiments may include two or more printing units to 3D print, for example, polymer, composite fiber filaments, and/or support materials, the 3D printer 300 further includes: a movable or fixed build platen 100 that, for supporting a part 700 to be manufactured; and a controller 200 operatively connected to the first printing unit 400, the second printing unit 500, and the third printing unit 600.

The structure and operation of an exemplary printing unit 500 for 3D printing of composite fibre reinforcing filaments 800 will be described in more detail below, for example in connection with fig. 3, 4, 5 and 8A to 8C.

Fig. 2 shows a prior art solution for 3D printing, comprising an extruder for 3D printing of continuous fiber reinforced composite filaments pre-impregnated with thermoplastic resin. The fibre filaments 800 may be in the form of a fibre bundle 3 and the filament drive 4 is arranged to drive the fibre composite filaments 800 through the cold feed zone 6 into the heated nozzle 11. In the solution of fig. 2, the heating nozzle 11 has a geometric feature called "ironing lip" to apply an "ironing force" (i.e., a consolidation force) to the polymer matrix of the filament 800 being 3D printed during 3D printing. This "ironing force" exerted by the facet areas located in the tip of nozzle 11 is the same as the consolidation force exerted in the AFP technique using a separate compaction roller. Cutter 5 cuts the fiber-reinforced filaments 800 to form individual assemblies of components. In the case of fig. 2, the temperature between the fiber bundle 3 and the nozzle 11 in the extruder is kept below Tm (Tm ═ the melting temperature of the polymer matrix), and the cross-sectional area of the fiber-reinforced composite filament 800 is greater than 6.4 × 10 ^-3mm²And less than 1.3mm²。

The exemplary embodiment differs from prior art solutions for 3D printing of fibre-reinforced objects in that in the embodiment the fibre filament supply is realized in a different way. The exemplary embodiment further differs from prior art solutions for 3D printing of fiber reinforced objects in that in an embodiment the consolidation force is applied in a different way.

Fig. 3 shows a 3D printing arrangement according to an exemplary embodiment. In fig. 3, a printing unit 500 for 3D printing of composite fibre reinforced filaments 800 comprises an extruder for 3D printing of continuous fibre reinforced composite filaments pre-impregnated with a thermoplastic matrix material. The fibre filaments 800 may be in the form of a fibre bundle 3 and the filament drive 4 is arranged to drive the fibre composite filament 800 through the cold feed zone 6, the first heating zone 1 (heating zone 1) and the first heat break zone 7 (heat break 7) into the heating nozzle 2 (i.e. second heating zone 2, heating zone 2). The heating nozzle 2 is surrounded by a consolidation element 9 (which may be a consolidation ring 9) located behind the heating nozzle 2. The knot-ring 9 is arranged to apply (press) the filaments 800 gently onto the component 700. The consolidation ring 9 may or may not be heated.

The final attachment of the printed filament 800 to the underlying material occurs in the consolidation ring 9, which may be unheated and may protrude downward (closer to the printed part 700) than the heating nozzle 2. After compaction, the filaments 800 solidify in a cooling stage, which may include cooling of the part by an external cooling device (not shown in fig. 3).

The cutter 5 is arranged to cut the fibre-reinforced filaments 800, e.g. to form a separate assembly of the component 700.

As shown in fig. 3, the first heating zone 1 is located before the heating nozzle 2, wherein the pre-impregnated fiber composite filaments 800 are pre-heated in the first heating zone 1 and, thus, the temperature of the extruder is not kept below Tm (Tm ═ the melting temperature of the thermoplastic matrix material) between the fiber bundle 3 and the heating nozzle 2 (but the temperature of the first heating zone 1 before the heating nozzle 2 is above Tm).

The first heating zone 1 (heating zone 1) is a preheating zone at a temperature T ≧ Tm (Tm ═ the melting temperature of the polymer matrix). The first heating zone 1 is located before the heating nozzle 2 (heating zone 2), and the first thermal break zone 7 is between the first heating zone 1 and the heating nozzle 2. The heating nozzle 2 and the first heating region 1 may have separate heaters (not shown in fig. 3). For example, the temperature in the heating nozzle 2 may be higher than the temperature in the first heating zone 1, and vice versa. The first heating zone 1, which preheats the material (i.e. the polymer matrix) before it reaches the heating nozzle 2, may speed up the 3D printing process, as the material is preheated before entering the heating nozzle 2 (heating zone 2). Thus, the speed of the printing process can be increased.

The heating zone 1 (preheating zone) can further increase the compaction of the layer of filaments and at the same time increase the speed of the process. The increase in the degree of compaction is a result of the fiber filaments being heated for a longer time and/or in a longer size region. The degree of compaction is increased by ensuring better preheating of the matrix polymer around the fibers 800 in the heating zone 1 (preheat) before heating the nozzle 2.

A consolidation ring 9 may be arranged around the heating nozzle 2. The consolidation loops 9 compact the fiber filaments 800 onto the part 700 being 3D printed. The consolidation ring (or compaction ring) 9 may be a separate entity attached to the heating nozzle 2. The gap between the member 700 and the heating nozzle 2 may be larger than the gap between the fastening ring 9 and the member 700. The binder ring 9 may be formed of a heat insulating material (e.g., ceramic), and the binder ring 9 may not be heated. Alternatively, the fastening ring 9 may be formed of metal, and the fastening ring 9 may be heated by a (separate) heater (not shown in fig. 3).

The consolidation rings 9 may be arranged to act as a welding head to ultrasonically weld the preheated (or even unheated or cooled) fiber filaments 800 to the component 700.

Another thermal break 8 may be located between the heating zone 2 (i.e., heating nozzle 2) and the consolidation ring 9 (see fig. 5).

Fig. 5 further illustrates the nozzle system/nozzle arrangement/nozzle unit 500 (i.e., the printing unit 500) in more detail according to an embodiment. According to an embodiment, the 3D printing unit 500 shown in fig. 5 is configured to accomplish filament feeding, filament melting, filament 800 passing through the heated nozzle 2, and filament compaction in a compaction element (which may be a compaction ring or consolidation ring 9). The compacting ring 9 may be a geometrical component of the cover structure/housing 25 of the printing unit 500. Thus, the compaction ring may be a separate component that is attached to the cover structure/housing 25 or any suitable portion/component (see fig. 8A, 8B, 8C, 8D). The 3D printing unit shown in fig. 5 includes a consolidation ring 9 and a preheating zone (i.e., heating zone 1). The printing unit 500 may further include: thermal insulation 7, 8, 20 (i.e. thermal fuses 7, 8, 20 which can optionally be cooled, for example, by air or liquid), heating zone 2 (heating nozzle 2), thermocouple 21 for preheating zone 1 (surrounding heating zone 1), thermocouple 24 for heating nozzle 2, air gap 22 and cooling fins 23 which are cooled, for example, by air or liquid. The heat insulator 7 corresponds to a thermal cutoff 7 located between the preheating zone (i.e., heating zone 1) and the heating zone 2 (i.e., heating nozzle 2). The insulator 8 may be located between the heating zone 2 (i.e., the heating nozzle 2) and the consolidation ring 9. The insulation 20 is located at the cold feed zone 6 before the preheating zone, i.e. the heating zone 1.

One embodiment enables 3D printing of layered structures such that the fiber layer may have the same or different thickness compared to the polymer layer. The thickness of the individual fiber layers may be equal to one or more of the polymer layers. Preferably, a single fibrous layer is equal to several polymer layers. The fiber 800 may be printed into a groove formed by the polymer layer/layers.

In one embodiment, coarse fiber composite filaments (diameter ≧ 0.9mm) are used, and several polymer layers may be applied on top/under/around one fiber composite filament layer. More than 2 printing units/nozzles may be used (at least one of which is the printing unit 500 that 3D prints the composite fibre reinforcement filaments 800, i.e. the 3D printing arrangement of fig. 3). The diameter of the coarse fiber composite filaments may be 0.9mm or more.

In one embodiment, fine fiber composite filaments may be used. The diameter of the fine fiber composite filaments may be 0.1mm to 0.9 mm. The diameter of the fine fiber composite filaments may be the same as or greater than the diameter of the polymer layer. In the latter case, several polymer layers may be applied on top of/under/around one layer of fibre composite filaments.

In one embodiment, the fiber reinforced composite filaments are pre-impregnated with a thermoplastic matrix material. The matrix material of the composite fiber filaments (and the polymer filaments printed by the printing unit 6003D) is thermoplastic; therefore, no photocuring is required.

In one embodiment, the pre-impregnated fiber reinforced composite filaments 800 are heated in a first heating zone 1 in which the temperature is set above the melting temperature of the matrix material before the fiber reinforced composite filaments enter the heating nozzle 2. An additional heating zone 1 is therefore located before the heating nozzle 2. This additional heating zone 1 can speed up the 3D printing process, as the material is heated before entering the heating nozzle 2. The preheating in the additional heating zone 1 can also improve the consolidation of the printed fiber filaments with the previously printed material layer of the component as the heating of the fiber filaments improves. This may be beneficial, especially when higher printing speeds are used. The temperature in the additional heating zone 1 is above the melting temperature of the matrix polymer material.

In one exemplary method, the fiber-reinforced composite filament feed rate may be adjusted. The fiber-reinforced composite filament feed rate need not be linear and/or constant. The feed zone of the fiber-reinforced composite filaments is not kept completely below the melting temperature of the thermoplastic matrix material, since the heating zone 1, in which the matrix material is preheated, is located in the feed zone of the fiber-reinforced composite filaments 800. The feed zone of the fiber-reinforced composite filament 800 is not completely cold. The first thermal break 7 between the heating zone 1 and the heating zone 2 is unheated, and the temperature in the first thermal break 7 may be lower than the temperature in the heating zone 1 and the heating zone 2. The function of the thermal break zone 7 is to form a temperature gap between the heating zone 1 and the heating nozzle 2. The thermal break zone 7/the resulting temperature gap enables independent control of the temperature of the heating zone 1 and the heating nozzle 2.

In one embodiment, the printing unit 400 (see fig. 1) for the support material is arranged to 3D print the support material to be removed from the final 3D printed part. The printing unit 600 for polymer is arranged to 3D print the perimeter (surface), fine details and/or thin polymer filled structures of the 3D printed part. The printing unit 500 for composite fibre filaments is arranged to 3D print a continuous fibre reinforcement having a relatively high layer thickness (typically higher than the layer thickness of the polymer) and a relatively wide line width (typically wider than the line width of the polymer, but may also be the same or thinner than the polymer line width). The continuous fiber reinforcement is a composite fiber filament comprising fiber filaments pre-impregnated with a thermoplastic matrix material. The nozzles of the printing units 400, 500, 600 may be circular.

The heating nozzle 2 is surrounded by a compacting ring 9, which may be unheated and made of an insulator material. Alternatively, the compacting ring 9 may be heated and made of a material that is effectively thermally conductive, such as metal. The gap between the heating nozzle 2 and the print bed (build platen 100) or previously printed material layer (part 700) may be greater than or equal to the gap between the print bed 100 or previously printed material layer 700 and the compacting ring 9.

In one embodiment, the polymer thread used for 3D printing of the polymer may be in the form of a continuous polymer filament having a diameter of 0.1mm to 5mm, the inner diameter of the nozzle for the polymer may be relatively small (typically 0.1mm to 3mm), and the 3D printing thread width of the polymer is very thin (typically 0.1mm to 5 mm). However, the raw material filaments may have a different geometry than the round wire. Any cross-sectional shape of the filaments is possible.

In one embodiment, the continuous fiber reinforcement for 3D printing is in the form of relatively thick fiber composite filaments having a thickness of 0.1 mm-10 mm. Thus, the inner diameter of the nozzle for the fibre composite filament is typically 0.1 mm-20 mm and the 3D printed line width of the fibre reinforcement is 0.2 mm-40 mm. However, the raw material filaments may have a different geometry than the round wire. Any cross-sectional shape of the filaments is possible.

Fig. 6A, 6B, 7A, and 7B are simplified diagrams illustrating a 3D printing part according to an exemplary embodiment.

In one embodiment, the layer thickness of the fiber reinforcement in the component 3D printed by using the heating nozzle 2 may be higher than the layer thickness of the polymer layer 3D printed by using the nozzle for the polymer. In the 3D printed object 700, there may be several thin polymer layers covered by a single composite fiber filament layer (see fig. 6A). The composite fiber filament layer may also be embedded within the interior of the 3D printed part (see fig. 6A). Since most of the 3D printing time is typically consumed by filling the part being 3D printed, the increase in composite filament layer thickness provided by the composite filament layer in the interior (or top) of the 3D printed part can enable a significant reduction in 3D printing time.

The line width of the 3D printed line depends on the diameter of the corresponding extruder nozzle, i.e. a smaller nozzle diameter enables a 3D printed line with a thinner line width, whereas a larger nozzle diameter enables a 3D printed line with a thicker line width.

The printing units 400, 600, nozzles for the polymer/polymer filament supply and nozzles for the support material/support material supply may be implemented by utilizing existing techniques and systems. Therefore, they need not be discussed in more detail herein.

The final 3D printed part 700 may contain a polymer portion, a continuous fiber reinforced portion, and additional filling and support structures.

In fiber filament printing, a nozzle refers to a device through which the fiber filament is ejected. In fiber filament printing, the speed of the fiber filaments ejected through the nozzle 2 may be the same as or slower or faster than the speed of the filaments fed from the fiber bundle 3, determined by the fiber drive 4. The nozzle 2 and/or the consolidation ring 9 do not limit the cross-sectional area.

In one embodiment, the filament feed rate out of the fiber bundle 3 (determined by the fiber driver 4) may be equal to the filament spray rate through the nozzle 2 for a short period of time, and then the fiber driver 4/fiber bundle 3 may be free to roll while the filaments 800 are sprayed through the nozzle 2.

In one embodiment, the filament feed rate out of the fiber bundle 3 (determined by the fiber driver 4) may be equal to the filament ejection rate through the nozzle 2 for a short period of time, and then the fiber driver 4/fiber bundle 3 may be pre-loaded with filaments 800 while they are ejected through the nozzle 2.

Filaments refer to the cross-sectional area of the wound build material, retaining the meaning of three-dimensional printing, and strands may refer to individual fibers, e.g., embedded in a matrix, that together form an entire composite filament.

In the 3D printing process, continuous reinforcing filaments are applied to build platen 100 to build layer 700 to form a three-dimensional structure. The position and orientation of the build platen 100 and/or the position and orientation of each nozzle are controlled by one or more controllers 200 to deposit continuous fiber reinforcing filaments in desired positions and directions. The direction and position of each 3D printed material (support material, polymer and fiber filaments) can be controlled in the X, Y and Z directions and all possible rotations around each of these directions. The position and orientation control mechanism may include a gantry system, robotic arm, and/or H-frame, which would be equipped with position and/or displacement sensors onto the controller 200 to monitor the relative position or velocity of the nozzle with respect to the build platen 100 and/or layer 700 of the part being constructed. The controller 200 may use the sensed X, Y and/or Z position and/or displacement and/or rotation about one or more of X, Y and the Z position/axis, or velocity vector, to control movement of the nozzle or platen 100.

The three-dimensional printer 300 may include a cutter 5 controlled by the controller 200 to cut the continuous fiber reinforcement filaments 800 to form individual components on the structure. For example, the cutter 5 may be a cutting blade or a laser.

The filament drive 4 feeds or pushes the unmelted filament 800 at a feed rate (which may or may not be variably controlled by the controller 200), after which the matrix material of the composite filament 800 may be heated, as described in connection with fig. 3.

The composite filaments 800 and thus the matrix material are heated in a heating zone 1, in which the temperature is set above the melting temperature of the matrix material and below the melting temperature of the continuous fiber reinforcement.

The controller 200 controls the position and movement of the nozzle 2, the feed rate, the printing rate, the cutter 5 and/or the temperature to accomplish the 3D printing.

When the part 700 is complete, the final part 700 may be removed from the build platen 100. Alternatively, a secondary print head may be used to deposit an optional coating on the part to provide a protective coating and/or to apply graphics or images on the final part.

The remaining space may either be left as a void or filled with a separate material such as a polymer.

The heating zones 1, 2 are thermally conductive, for example made of copper, stainless steel, brass or the like.

The nozzles may each have the same or different nozzle diameters.

One embodiment discloses an advanced 3D printer capable of 3D printing continuous fiber reinforcement. An advanced 3D printer and method for additive manufacturing of components is disclosed that enables alternative 3D printing of continuous fiber reinforcement compared to existing 3D printers and methods.

One embodiment can produce a 3D printed object that is stronger than a 3D printed object that is 3D printed using a conventional FFF printer. One embodiment also minimizes 3D printing time. In one embodiment, the 3D printed object is reinforced by fiber reinforcement. One embodiment enables the incorporation of continuous fiber reinforcement into the object to be 3D printed.

In one embodiment, the 3D printer 300 may include a printing unit 500 to 3D print the composite fiber reinforced filament 800 and a printing unit 600 to 3D print the polymer filament, but without the printing unit 400 to 3D print the support material.

In one embodiment, the 3D printer 300 may include a printing unit 500 to 3D print the composite fiber reinforced filament 800 and a printing unit 400 to 3D print the support material, but without the printing unit 600 to 3D print the polymer filament.

In one embodiment, the 3D printer 300 may include a printing unit 500 to 3D print the composite fiber reinforced filaments 800, but no printing unit 400 to 3D print the support material, and no printing unit 600 to 3D print the polymer filaments.

The composite fiber filaments are formed of a fiber reinforcement and a thermoplastic matrix polymer that bonds the filament bundles together. The fiber reinforcement may comprise one or more yarns containing glass fibers, carbon fibers, aramid fibers, natural fibers (e.g., kenaf, hemp, etc.), thermoplastic polymer fibers (e.g., polyamide, PLA, etc.), and/or hybrid fibers (two or more different fibers in a single composite fiber filament). Each yarn may contain from 1 to 1000000 individual fibers.

The matrix material used to bond the fiber reinforcement in the composite fiber filaments may comprise thermoplastic polymers such as, but not limited to: PLA, PGA, PLGA, PLDLA, PCL, TMC, PA, PE, PEEK, PEKK, copolymers of various monomers, and/or mixtures of various thermoplastic polymers/copolymers.

The polymeric filaments may comprise thermoplastic polymers such as, but not limited to: PLA, PGA, PLGA, PLDLA, PCL, TMC, PA, PE, PEEK, PEKK, copolymers of various monomers, and/or mixtures of various thermoplastic polymers/copolymers/additives.

The support material may comprise any thermoplastic polymer that is soluble in a solvent different from the solvent of the polymer used in the composite fiber filaments and polymer filaments. The solvent may include, but is not limited to, water, acetic acid, acetone, oil, and the like. Alternatively, the support material may comprise any thermoplastic polymer, copolymer, and/or mixture that may mechanically disintegrate from the 3D printed part after the printing process. In this case, there is no limitation or requirement on the solubility of the support material.

Fig. 4 is a flow chart illustrating an exemplary process of 3D printing of thermoplastic pre-impregnated fiber composite filaments 800. Referring to fig. 4, a method for additive manufacturing of a component 700 includes: a thermoplastic pre-impregnated fiber composite filament 800 is supplied 401, the filament 800 comprising one or more inelastic axial fiber strands extending within the thermoplastic matrix material of the filament 800. The part 700 to be manufactured is supported on a movable or fixed build platen 100. In the 3D printing unit 500, the pre-impregnated fiber composite filaments 800 are heated 402 at a first heating zone 1 extending between the fiber composite filament supply 3 and the heating nozzle 2 of the 3D printing unit 500. The temperature of the first heating zone 1 is set above the melting temperature of the thermoplastic matrix material. The method further comprises: the pre-impregnated fiber composite filaments 800 are heated 404 at the heating nozzle 2 to maintain the temperature of the fiber composite filaments 800 or to heat the fiber composite filaments 800 to a higher temperature. The temperature of the heating nozzle 2 is set above the melting temperature of the base material. Thermoplastic pre-impregnated fiber composite filaments are extruded from the heated nozzle 2 through the compaction ring 9, and the printing unit 500 and/or the compaction ring 9 and the build platen 100 are moved 405 relative to each other in three degrees of freedom by a plurality of actuators (e.g., the printing unit 500 and the build platen 100 may be moved 405 relative to each other in three degrees of freedom). Alternatively, the build platen 100 is fixed and the movements required to generate the part 700 are produced only by moving the printing unit 500 and/or the compaction ring 9 in the X, Y and Z directions and possibly with all possible rotations about these axes. The compaction ring 9 applies a compaction force to the extruded fiber filaments 800 and ensures that the fiber filaments 800 are firmly attached to the previously printed fiber/polymer/support layer 700. Following the compacting ring 9 is an additional cooler unit which cools the printed fibre layer and improves its solidification. The fibrous composite filament 800 comprising one or more inelastic axial fiber strands is driven 406 through the first heating zone 1 into the heated nozzle 2 at a selected feed rate, wherein the feed rate and/or the printing rate may be controlled. The heating of the fiber composite filaments 800 can be interrupted 403 at a non-heated thermal break 7 between the first heating zone 1 and the heating nozzle 2. The temperature of the thermal break zone 7 through which the fibrous composite filaments 800 travel during printing is not controlled; the first heating zone 1 and the heating nozzle 2 are thermally separated (isolated) from each other by a thermal break zone 7. To form the part 700, the filament 800 is adhered to the part 700 (e.g., to a previously printed fiber, polymer, or support layer) or to the build platen 100. The filaments 800 may be cut 408 by the cutter 5, for example, when the part 700 is completed 409, when the supplied material is changed to, for example, a polymer filament/support material, or when the design of the part 700 requires.

In one embodiment, solidification occurs in a cooling phase after heating the nozzle 2.

Fig. 7A and 7B are schematic views (perspective, side, and top views) illustrating a 3D structure according to an exemplary embodiment.

In the printed structure according to embodiments (i.e. in the 3D printed part 700), the fiber reinforcement is present as filaments of 0.1 mm-10 mm thickness. In one embodiment, the inner diameter of the heating nozzle 2 (i.e., the second heating region 2) is typically 0.1mm to 20mm, and the width of the printed line is 0.2mm to 40 mm.

The thickness of the layer of individual fiber reinforcement (printed by using the fiber printing unit 500) may be greater than the thickness of an individual polymer layer (printed by using the polymer printing unit 600). Thus, in a part 700 printed by a method and a 3D printer according to embodiments, there may be several polymer layers at the same height covered by only one fibre layer. The fiber layer may be embedded in the interior of the 3D printed part 700. Since most of the printing time is typically consumed by filling the printing part 700, increasing the layer thickness by a thick fibrous layer in the interior of the part significantly reduces the printing time.

The component 700 may include four parts: a polymeric structure, continuous or semi-continuous fiber reinforcement, additional fillers, and support materials. To complete the 3D printing, the 3D model is loaded and printing parameters are set for each part of the part. Loading the 3D model and setting the parameters such that: as a result of printing, the polymer structure forms/defines the exterior and interior shape of the part, the support material forms the support structure for the part 700, the fiber reinforcement reinforces the part, and additional filler fills the empty spaces/regions in the fiber layer of the part 700 (i.e., between the printed fiber filaments 800) to complete the part. The printing parameters include, for example, the layer height of each layer.

Fig. 8A, 8B, 8C, and 8D are schematic diagrams illustrating an exemplary structure of a print head including the consolidation element 9 and the first heating region 1. A cross-section through line a-a is shown.

In FIG. 8A, the consolidation elements are fixed parts of the printhead cover structure. The printhead structure shown in fig. 8A is similar to that shown in fig. 5.

In FIG. 8B, the consolidation elements are not fixed parts of the printhead lid structure; instead, the consolidation elements are movable relative to the printhead cover structure.

In fig. 8C, the consolidation element is not a fixed part of the printhead cover structure (instead, the consolidation element is movable relative to the printhead cover structure), and there are additional components behind the consolidation element, e.g., heating unit 26, cooler ultrasonic bonding head 26, etc.

In fig. 8D, the consolidation element is a fixed part of the printhead cover structure, and there are additional components behind the consolidation element, e.g., heating unit 26, cooler ultrasonic bonding head 26, etc.

Otherwise, the printhead structure shown in fig. 8B, 8C, and 8D is largely similar to the printhead structure shown in fig. 5.

Example 1

Using custom software, G-code for fiber printing and polymer printing is generated from the 3D design of the object to be 3D printed. According to the generated G-code, the continuous fiber reinforcement is 3D printed in a groove generated by 3D printing the polymer material. Separate printing units/nozzles are used for the polymer material and the continuous fiber reinforcement. The diameter of the fiber filament used was 1.8 mm. The fiber filaments were 3D printed into grooves (0.6 mm in height and 4.2mm in width) that were 3D printed in the part being manufactured. The single fiber layer covers the entire groove (i.e., the height of the groove is equal to the height of the single fiber layer). Additional filling structures are 3D printed by using polymer nozzles to fill the area surrounded by the fiber layer. The polymer material was 3D printed in a 0.3mm layer thickness. Thus, the thickness of one fibrous layer is equal to the thickness of two polymer layers (see fig. 6A).

Example 2

Using custom software, G-code for fiber printing and polymer printing is generated from the 3D design of the object to be 3D printed. The continuous fiber reinforcement is 3D printed in the groove created by 3D printing of the polymer material according to the created G-code using separate printing units/nozzles for the polymer material and the continuous fiber reinforcement. The fiber filaments used had a diameter of 1.0 mm. The fiber filaments were 3D printed into grooves (0.3 mm in height and 2.6mm in width) that were 3D printed in the part being manufactured. The single fiber layer covers the entire groove (i.e., the height of the groove is equal to the height of the single fiber layer). Additional filling structures are 3D printed by using polymer nozzles to fill the area surrounded by the fibers. The polymer material was 3D printed in a 0.3mm layer thickness. Thus, the thickness of one fibrous layer is equal to the thickness of one polymeric layer (see fig. 6B).

Example 3

Using custom software, G-code for fiber printing and polymer printing is generated from a 3D design (3D model) of an object to be 3D printed (see fig. 7A, 7B). From the generated G-code, the fiber reinforcement, polymer and support material are 3D printed. The continuous fiber reinforcement is 3D printed in the groove created by 3D printing of the polymer material using separate printing units/nozzles for the polymer material, the continuous fiber reinforcement and the support material. The fiber filaments used had a diameter of 1.8 mm. The fiber filaments were 3D printed into grooves (0.6 mm in height and 4.2mm in width) that were 3D printed in the part being manufactured. A single fiber layer covers the entire groove. Additional filling structures are 3D printed by using polymer nozzles to fill the area surrounded by the fibers. The polymer material was 3D printed in a 0.3mm layer thickness. Thus, the thickness of one fibrous layer is equal to the thickness of two polymer layers (see fig. 6A). According to the G code, the support material is 3D printed on the selected area (see fig. 7A, 7B).

It will be clear to a person skilled in the art that with the advancement of technology, the inventive concept may be implemented in various ways. The invention and its embodiments are not limited to the examples described above but may vary within the scope of the claims.