阅读说明：本技术 一种具有双绕组的单层磁极电磁作动器 (Single-layer magnetic pole electromagnetic actuator with double windings ) 是由 岳洪浩 赵勇 杨飞 陆一凡 吴君 阮琪 于 2021-07-02 设计创作，主要内容包括：本发明提出了一种具有双绕组的单层磁极电磁作动器,属于航空航天领域。解决了现有电磁作动器推力小的问题。它包括定子和动子,所述定子包括定子框架、外磁结构和内磁结构,所述外磁结构包括外磁轭、外磁环、外后磁环、外前磁环、换向导磁环、外顺磁轭和外前磁轭,所述动子设置在定子内部。可实现纳卫星低成本高效率在轨释放。采用双气隙双绕组结构,内绕组电流方向和外绕组电流方向相反,抑制了电枢反应,提高了能量转换率。它主要用于电磁作动器。(The invention provides a single-layer magnetic pole electromagnetic actuator with double windings, and belongs to the field of aerospace. The problem of current electromagnetic actuator thrust little is solved. The magnetic motor comprises a stator and a rotor, wherein the stator comprises a stator frame, an outer magnetic structure and an inner magnetic structure, the outer magnetic structure comprises an outer yoke, an outer magnetic ring, an outer rear magnetic ring, an outer front magnetic ring, a reversing magnetic conductive ring, an outer sequential magnetic yoke and an outer front magnetic yoke, and the rotor is arranged inside the stator. The on-orbit release of the nano-satellite with low cost and high efficiency can be realized. By adopting a double-air-gap double-winding structure, the current direction of the inner winding is opposite to that of the outer winding, so that the armature reaction is inhibited, and the energy conversion rate is improved. The electromagnetic actuator is mainly used for the electromagnetic actuator.)

1. A single-layer magnetic pole electromagnetic actuator having a double winding, comprising: the magnetic field generator comprises a stator and a rotor, wherein the stator comprises a stator frame (1), an outer magnetic structure and an inner magnetic structure, the outer magnetic structure comprises an outer yoke (2), an outer magnetic ring (3), an outer rear magnetic ring (4A), an outer front magnetic ring (4B), a reversing magnetic ring (5), an outer sequential magnetic yoke (6) and an outer front magnetic yoke (7), the outer yoke (2) is positioned at the radial inner side center position of the outer wall of a groove of the stator frame (1), the outer magnetic ring (3) is positioned at the radial inner side center position of the outer yoke (2), the outer rear magnetic ring (4A) is positioned at the axial rear end of the outer magnetic ring (3), the outer front magnetic ring (4B) is positioned at the axial front end of the outer magnetic ring (3), the reversing magnetic ring (5) is positioned at the axial rear ends of the outer yoke (2) and the outer rear magnetic ring (4A), the outer sequential magnetic ring (6) is positioned at the radial inner side of the outer magnetic ring (3), the outer front magnetic yoke (7) is positioned at the axial front end of the outer sequential magnetic yoke (6), the outer magnetic structure is fixedly arranged on the stator frame (1) through an outer lock nut (8), the inner magnetic structure comprises an inner magnetic yoke (9), an inner magnetic ring (10), an inner rear magnetic ring (11A), an inner front magnetic ring (11B), an inner paramagnetic ring (12) and an inner front magnetic yoke (13), the inner magnetic yoke (9) is positioned at the radial outer side center position of the inner wall of the groove of the stator frame (1), the inner magnetic ring (10) is positioned at the radial outer side center position of the inner magnetic yoke (9), the inner rear magnetic ring (11A) is positioned at the axial rear end of the inner magnetic ring (10), the inner front magnetic ring (11B) is positioned at the axial front end of the inner magnetic ring (10), the inner sequential magnetic ring (12) is positioned at the radial outer side of the inner magnetic ring (10), the inner front magnetic yoke (13) is positioned at the axial front end of the inner sequential magnetic ring (12), the internal magnetic structure is fixedly arranged on the stator frame (1) through an internal lock nut (14), and the rotor is arranged inside the stator.

2. The single layer magnetic pole electromagnetic actuator of claim 1, wherein: the rotor comprises an inner rotor frame (15), an inner coil (16), an outer rotor frame (17) and an outer coil (18), wherein the inner rotor frame (15) is located on the radial outer side of the inner magnetic structure, the outer rotor frame (17) is located on the radial inner side of the outer magnetic structure, the inner coil (16) surrounds and is fixed at the rear end of the inner rotor frame (15), the outer coil (18) surrounds and is fixed at the rear end of the outer rotor frame (17), and the inner rotor frame (15) is fixedly connected with the outer rotor frame (17).

3. The single layer magnetic pole electromagnetic actuator having dual windings as claimed in claim 2, wherein: the inner rotor frame (15) and the outer rotor frame (17) are fixedly connected through thread matching at the bottom end.

4. The single layer magnetic pole electromagnetic actuator having dual windings as claimed in claim 2, wherein: the energizing current directions of the inner coil (16) and the outer coil (18) are opposite.

5. The single layer magnetic pole electromagnetic actuator of claim 1, wherein: the external locking nut (8) is fixed with the stator frame (1) in a thread fit mode, and the internal locking nut (14) is fixed with the stator frame (1) in a thread fit mode.

6. The single layer magnetic pole electromagnetic actuator of claim 1, wherein: the outer yoke (2), the reversing magnetic conductive ring (5), the outer forward yoke (6), the outer front yoke (7), the inner yoke (9), the inner forward magnetic ring (12) and the inner front yoke (13) are all made of soft magnetic alloy 1J50 materials.

7. The single layer magnetic pole electromagnetic actuator of claim 1, wherein: the outer magnetic ring (3), the outer rear magnetic ring (4A), the outer front magnetic ring (4B), the inner magnetic ring (10), the inner rear magnetic ring (11A) and the inner front magnetic ring (11B) are all made of neodymium iron boron alloy hard magnetic materials.

8. The single layer magnetic pole electromagnetic actuator of claim 1, wherein: the magnetizing directions of the outer magnetic ring (3), the outer rear magnetic ring (4A), the outer front magnetic ring (4B), the inner magnetic ring (10), the inner rear magnetic ring (11A) and the inner front magnetic ring (11B) are as follows in sequence: inner N outer S, right S left N, right N outer S, inner S outer N, right S left N, right N left S.

9. The single layer magnetic pole electromagnetic actuator of claim 1, wherein: the magnetizing directions of the outer magnetic ring (3), the outer rear magnetic ring (4A), the outer front magnetic ring (4B), the inner magnetic ring (10), the inner rear magnetic ring (11A) and the inner front magnetic ring (11B) are as follows in sequence: inner S outer N, right N left S, right S left N, inner N outer S, right N left S, right S left N.

Technical Field

The invention belongs to the field of aerospace, and particularly relates to a single-layer magnetic pole electromagnetic actuator with double windings.

Background

The cooperative work of a plurality of satellites to complete complex space exploration tasks becomes a research hotspot in the international aerospace field, such as formation, clustering and the like. Particularly, the nano-satellite has the advantages of short development period, low cost and the like, and the formed cluster has high flexibility and good robustness and can complete tasks which cannot be independently completed by a large satellite or have high required cost.

To save cost, often in one rocket launch lift-off mission, a large number of nano-satellites are stored and released on a predetermined orbit by using a deployer. The nanosatellite has weak orbit control capability and carries limited fuel, so that the separation speed of the nanosatellites can be adjusted when the nanosatellites are ejected and separated, and the nanosatellites naturally form stable relative motion with each other. This requires the on-track deployer to implement a timed release of the nano-satellites at a particular time, allowing the nano-satellites of different masses to separate at a predetermined speed. And the traditional deployer mostly adopts a compression spring, so that the release speed is difficult to accurately adjust for different types of nano-satellites.

The electromagnetic actuator utilizes the electrified coil to generate ampere force in a permanent magnetic field to push and release the nano-satellite, and the separation speed is accurate and adjustable. In order to reduce the cost of aerospace applications, it is often desirable that an electromagnetic actuator has a small volume, a light weight, a high thrust density, and a high energy conversion rate. However, in the current conventional electromagnetic actuator, the electromagnetic field generated by the coil weakens the original permanent magnetic field generated by the magnetic ring, the armature reaction is obvious, the energy conversion rate is low, and the thrust of the electromagnetic actuator is small.

Disclosure of Invention

The invention provides a single-layer magnetic pole electromagnetic actuator with double windings, which aims to solve the problems in the prior art.

In order to achieve the purpose, the invention adopts the following technical scheme: a single-layer magnetic pole electromagnetic actuator with double windings comprises a stator and a rotor, wherein the stator comprises a stator frame, an outer magnetic structure and an inner magnetic structure, the outer magnetic structure comprises an outer yoke, an outer magnetic ring, an outer rear magnetic ring, an outer front magnetic ring, a reversing magnetic conductive ring, an outer sequential magnetic yoke and an outer front magnetic yoke, the outer yoke is located at the radial inner center position of the outer wall of a groove of the stator frame, the outer magnetic ring is located at the radial inner center position of the outer yoke, the outer rear magnetic ring is located at the axial rear end of the outer magnetic ring, the outer front magnetic ring is located at the axial front end of the outer magnetic ring, the reversing magnetic conductive ring is located at the axial rear end of the outer yoke and the outer rear magnetic ring, the outer paramagnetic yoke is located at the radial inner side of the outer magnetic ring, the outer front magnetic yoke is located at the axial front end of the outer sequential magnetic yoke, the outer magnetic structure is fixedly installed on the stator frame through an outer lock nut, and the inner magnetic structure comprises an inner yoke, an outer magnetic structure and an inner magnetic structure, The inner magnet ring is positioned at the radial outer side center position of the inner groove wall of the stator frame, the inner magnet ring is positioned at the radial outer side center position of the inner magnet yoke, the inner rear magnet ring is positioned at the axial rear end of the inner magnet ring, the inner front magnet ring is positioned at the axial front end of the inner magnet ring, the inner paramagnetic ring is positioned at the radial outer side of the inner magnet ring, the inner front magnet yoke is positioned at the axial front end of the inner paramagnetic ring, the inner magnetic structure is fixedly installed on the stator frame through an inner lock nut, and the rotor is arranged inside the stator.

Furthermore, the rotor comprises an inner rotor frame, an inner coil, an outer rotor frame and an outer coil, the inner rotor frame is located on the radial outer side of the inner magnetic structure, the outer rotor frame is located on the radial inner side of the outer magnetic structure, the inner coil is wound and fixed at the rear end of the inner rotor frame, the outer coil is wound and fixed at the rear end of the outer rotor frame, and the inner rotor frame is fixedly connected with the outer rotor frame.

Furthermore, the inner rotor frame and the outer rotor frame are fixedly connected through thread matching at the bottom end.

Furthermore, the energizing current directions of the inner coil and the outer coil are opposite.

Furthermore, the outer lock nut is fixed with the stator frame in a thread fit mode, and the inner lock nut is fixed with the stator frame in a thread fit mode.

Furthermore, the outer yoke, the reversing magnetic conductive ring, the outer forward magnetic yoke, the outer front magnetic yoke, the inner forward magnetic ring and the inner front magnetic yoke are all made of 1J50 materials.

Furthermore, the outer magnetic ring, the outer rear magnetic ring, the outer front magnetic ring, the inner rear magnetic ring and the inner front magnetic ring are made of neodymium iron boron alloy hard magnetic materials.

Furthermore, the magnetizing directions of the outer magnetic ring, the outer rear magnetic ring, the outer front magnetic ring, the inner rear magnetic ring and the inner front magnetic ring are as follows in sequence: inner N outer S, right S left N, right N outer S, inner S outer N, right S left N, right N left S.

Furthermore, the magnetizing directions of the outer magnetic ring, the outer rear magnetic ring, the outer front magnetic ring, the inner rear magnetic ring and the inner front magnetic ring are as follows in sequence: inner S outer N, right N left S, right S left N, inner N outer S, right N left S, right S left N.

Compared with the prior art, the invention has the beneficial effects that: the invention solves the problem of small thrust of the existing electromagnetic actuator, has the advantages of high and stable thrust density and high energy conversion rate, and can realize the low-cost high-efficiency on-orbit release of the nano-satellite. By adopting a double-air-gap double-winding structure, the current direction of the inner winding is opposite to that of the outer winding, so that the armature reaction is inhibited, and the energy conversion rate is improved. The reversing magnetic conduction rings are utilized to solve the problem of magnetic field cancellation caused by opposite magnetic circuits, guide different branch magnetic flows is realized, magnetic leakage is reduced, air gap magnetic field intensity is improved, the axial size of the actuator is effectively reduced by the single-layer magnetic poles and the single-layer coil structure, and the actuator is convenient to mount and carry. The invention has the advantages of repeated use, high thrust density, high energy conversion rate, small volume and light weight, can realize the in-orbit time-sharing speed regulation and release of the nano-satellites with different masses, and can meet the actual requirements of the aerospace application at the present stage.

Compared with the prior art, the method has the advantages that:

1. in the double-air-gap double-winding structure, the current direction of the inner winding is opposite to that of the outer winding, and the generated electromagnetic fields are mutually counteracted, so that the influence of the electromagnetic fields on the original permanent magnetic field is inhibited, and the energy conversion rate is improved.

2. The reversing magnetic conduction rings are utilized to solve the problem of magnetic field cancellation caused by opposite magnetic circuits, realize the guidance of different branch magnetic fluxes, reduce the magnetic leakage and improve the air gap magnetic field intensity, and have the advantages of compact structure, small volume, light weight and high thrust density.

3. The axial size of the actuator is effectively reduced by the single-layer magnetic pole and the single-layer coil structure, and the actuator is convenient to mount and carry.

Drawings

FIG. 1 is a schematic radial cross-sectional view of a single-layer magnetic pole electromagnetic actuator with dual windings according to the present invention;

FIG. 2 is a schematic cross-sectional view of a stator according to the present invention;

FIG. 3 is a schematic cross-sectional view of a mover according to the present invention;

FIG. 4 is a schematic cross-sectional structural view of an inner mover frame according to the present invention;

FIG. 5 is a schematic perspective view of an inner mover frame according to the present invention;

FIG. 6 is a schematic cross-sectional view of the outer rotor frame according to the present invention;

fig. 7 is a schematic perspective view of the outer rotor frame according to the present invention.

1-stator frame, 2-outer yoke, 3-outer magnet ring, 4A-outer rear magnet ring, 4B-outer front magnet ring, 5-reversing magnetic conductive ring, 6-outer consequent magnet ring, 7-outer front magnet ring, 8-outer lock nut, 9-inner yoke, 10-inner magnet ring, 11A-inner rear magnet ring, 11B-inner front magnet ring, 12-inner consequent magnet ring, 13-inner front magnet ring, 14-inner lock nut, 15-inner rotor frame, 16-inner coil, 17-outer rotor frame, 18-outer coil, 19-nano satellite.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely explained below with reference to the drawings in the embodiments of the present invention.

Referring to fig. 1-7 to illustrate the present embodiment, a single-layer magnetic pole electromagnetic actuator with double windings comprises a stator and a rotor, wherein the stator comprises a stator frame 1, an outer magnetic structure and an inner magnetic structure, the outer magnetic structure comprises an outer yoke 2, an outer magnetic ring 3, an outer rear magnetic ring 4A, an outer front magnetic ring 4B, a commutation magnetic ring 5, an outer sequential magnetic yoke 6 and an outer front magnetic yoke 7, the outer yoke 2 is located at a radial inner center position of an outer wall of a groove of the stator frame 1, the outer magnetic ring 3 is located at a radial inner center position of the outer yoke 2, the outer rear magnetic ring 4A is located at an axial rear end of the outer magnetic ring 3, the outer forward magnetic ring 4B is located at an axial front end of the outer magnetic ring 3, the commutation magnetic ring 5 is located at an axial rear end of the outer yoke 2 and the outer rear magnetic ring 4A, the outer paramagnetic yoke 6 is located at a radial inner side of the outer magnetic ring 3, the outer forward magnetic yoke 7 is located at an axial front end of the outer paramagnetic yoke 6, the outer magnetic structure is fixedly installed at a rear inner magnetic structure comprising a yoke 9, a magnetic structure is installed at a rear end of the stator frame 1, and a magnetic structure, The inner magnetic ring 10, the inner rear magnetic ring 11A, the inner front magnetic ring 11B, the inner paramagnetic ring 12 and the inner front magnetic yoke 13 are arranged at the center position of the radial outer side of the inner wall of the groove of the stator frame 1, the inner magnetic ring 10 is arranged at the center position of the radial outer side of the inner magnetic yoke 9, the inner rear magnetic ring 11A is arranged at the axial rear end of the inner magnetic ring 10, the inner front magnetic ring 11B is arranged at the axial front end of the inner magnetic ring 10, the inner paramagnetic ring 12 is arranged at the radial outer side of the inner magnetic ring 10, the inner front magnetic yoke 13 is arranged at the axial front end of the inner paramagnetic ring 12, the inner magnetic structure is fixedly arranged on the stator frame 1 through an inner lock nut 14, and the rotor is arranged in the stator.

The rotor of the present embodiment includes an inner rotor frame 15, an inner coil 16, an outer rotor frame 17 and an outer coil 18, the inner rotor frame 15 is located at the radial outer side of the inner magnetic structure, the outer rotor frame 17 is located at the radial inner side of the outer magnetic structure, the inner coil 16 surrounds and is fixed at the rear end of the inner rotor frame 15, the outer coil 18 surrounds and is fixed at the rear end of the outer rotor frame 17, the inner rotor frame 15 and the outer rotor frame 17 are fixedly connected through the thread fit at the bottom end, the directions of the current passing through the inner coil 16 and the outer coil 18 are opposite, the outer locknut 8 and the stator frame 1 are fixedly fixed through the thread fit, the inner locknut 14 and the stator frame 1 are fixedly fixed through the thread fit, the outer yoke 2, the commutating magnetic conductive ring 5, the outer sequential yoke 6, the outer front yoke 7, the inner yoke 9, the inner paramagnetic ring 12 and the inner front yoke 13 are all made of 1J50 material, the outer magnetic ring 3, the outer rear magnetic ring 4A, the outer front magnetic ring 4B, the inner magnetic ring 10, the inner rear magnetic ring 11A and the inner front magnetic ring 11B are made of neodymium-iron-boron alloy hard magnetic materials, and the magnetizing directions of the outer magnetic ring 3, the outer rear magnetic ring 4A, the outer front magnetic ring 4B, the inner magnetic ring 10, the inner rear magnetic ring 11A and the inner front magnetic ring 11B are as follows in sequence: inner N outer S, right S left N, right N outer S, inner S outer N, right S left N, right N left S or inner S outer N, right N left S, right S left N, inner N outer S, right N left S, right S left N.

The principle of the embodiment is as follows: the magnetic flux generated by the outer magnetic ring 3, the outer rear magnetic ring 4A and the outer front magnetic ring 4B forms an outer rear permanent magnetic loop and an outer front permanent magnetic loop, a larger permanent magnetic field is generated in an outer air gap, the magnetic flux generated by the inner magnetic ring 10, the inner rear magnetic ring 11A and the inner front magnetic ring 11B forms an inner rear permanent magnetic loop and an inner front permanent magnetic loop, a larger inner permanent magnetic field is formed in an inner air gap, the directions of the outer permanent magnetic field and the inner permanent magnetic field are opposite, the outer coil 18 is positioned in the outer permanent magnetic field, the inner coil 16 is positioned in the inner permanent magnetic field, and currents in opposite directions are introduced into the inner coil 16 and the outer coil 18 to generate the same-direction electromagnetic force so as to push the nano-satellite 19 to release. The outer rear permanent magnetic circuit is: the outer back magnetic flux starts from the N pole of the outer magnetic ring 3, passes through the outer paramagnetic yoke 6, the outer coil 18, the rear part of the reversing magnetic conductive ring 5 and the rear part of the outer yoke 2 and returns to the S pole of the outer magnetic ring 3; the outer front permanent magnetic circuit is as follows: the outer front magnetic flux starts from the N pole of the outer magnetic ring 3, passes through the outer paramagnetic yoke 6, the outer coil 18, the front part of the reversing magnetic conductive ring 5, the outer front magnetic yoke 7 and the front part of the outer magnetic yoke 2 and returns to the S pole of the outer magnetic ring 3; the internal back magnetic flux starts from the N pole of the internal magnetic ring 10 and returns to the S pole of the internal magnetic ring 10 through the internal paramagnetic ring 12, the internal rotor frame 15, the internal coil 16, the rear part of the reversing magnetic conductive ring 5 and the rear part of the internal yoke 9; the inner front magnetic flux starts from the N pole of the inner magnetic ring 10, passes through the inner paramagnetic ring 12, the inner rotor frame 15, the inner coil 16, the front part of the reversing magnetic conductive ring 5 and the front part of the inner yoke 9 and returns to the S pole of the inner magnetic ring 10. The magnetic flux generated by the outer rear magnetic ring 4A, the outer front magnetic ring 4B, the inner rear magnetic ring 11A and the inner front magnetic ring 11B has the function of converging the magnetic flux generated by the outer magnetic ring 3 and the inner magnetic ring 10, so that the air gap magnetic field is increased and the magnetic field distribution of the local areas at the front end and the rear end of the coil is improved.

The single-layer magnetic pole electromagnetic actuator with double windings provided by the invention is described in detail above, and the principle and the implementation mode of the invention are explained in the present document by applying specific examples, and the description of the above examples is only used to help understanding the method and the core idea of the invention; meanwhile, for a person skilled in the art, according to the idea of the present invention, there may be variations in the specific embodiments and the application scope, and in summary, the content of the present specification should not be construed as a limitation to the present invention.