CN106401891A - Annular magnetic steel installation structure of ion thruster - Google Patents
Annular magnetic steel installation structure of ion thruster Download PDFInfo
- Publication number
- CN106401891A CN106401891A CN201611118157.XA CN201611118157A CN106401891A CN 106401891 A CN106401891 A CN 106401891A CN 201611118157 A CN201611118157 A CN 201611118157A CN 106401891 A CN106401891 A CN 106401891A
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- magnetic steel
- ion thruster
- installation structure
- thruster
- box
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H1/00—Using plasma to produce a reactive propulsive thrust
- F03H1/0081—Electromagnetic plasma thrusters
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F7/00—Magnets
- H01F7/02—Permanent magnets [PM]
- H01F7/0205—Magnetic circuits with PM in general
- H01F7/0221—Mounting means for PM, supporting, coating, encapsulating PM
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- Physics & Mathematics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- Plasma & Fusion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Plasma Technology (AREA)
Abstract
Description
技术领域technical field
本发明公开了一种离子推力器环形磁钢安装结构,属于航天技术和真空技术领域。The invention discloses an annular magnetic steel installation structure of an ion thruster, which belongs to the fields of aerospace technology and vacuum technology.
背景技术Background technique
电推进技术作为一种先进空间推进技术,已经在空间各个应用领域得到了广泛应用,包括姿态控制、南北位置保持、轨道转移、大气阻尼补偿、深空探测主推进等。尤其在深空探测任务中,电推进技术以其高比冲、长寿命等特点,可以大大节省推进剂携带量,增加航天器有效载荷比例,具有很强的优势。As an advanced space propulsion technology, electric propulsion technology has been widely used in various space application fields, including attitude control, north-south position keeping, orbit transfer, atmospheric damping compensation, deep space exploration main propulsion, etc. Especially in deep space exploration missions, electric propulsion technology, with its high specific impulse and long life, can greatly save the amount of propellant carried and increase the payload ratio of the spacecraft, which has strong advantages.
环切场离子推力器放电室具有放电效率高、束流平直度好、所需永磁体磁感应强度弱的优点。大直径环形磁钢不易加工和充磁,通常采用小块磁钢拼接的方法制备磁钢环,这种方法存在因磁钢间的排斥难易紧密排列,装配困难。同时,离子推力器工作时产生的高温,对磁钢耐温提出了较高要求。本发明解决了由多个小块磁钢组装成环形磁钢过程中相互排斥难以紧密排布问题和环形磁钢在推力器上的装配问题,降低了离子推力器对磁钢的高温使用性要求。The discharge chamber of the tangential field ion thruster has the advantages of high discharge efficiency, good beam straightness, and weak magnetic induction intensity of the required permanent magnet. Large-diameter ring magnets are not easy to process and magnetize. Usually, the method of splicing small pieces of magnets is used to prepare magnet rings. This method is difficult to arrange closely because of the repulsion between magnets, and assembly is difficult. At the same time, the high temperature generated by the ion thruster puts forward higher requirements on the temperature resistance of the magnetic steel. The invention solves the problem of mutual repulsion in the process of assembling a plurality of small pieces of magnetic steel into ring-shaped magnets and the problem of assembling the ring-shaped magnets on the thruster, and reduces the high-temperature usability requirements of the ion thruster on the magnets .
发明内容Contents of the invention
本发明所要解决的技术问题是针对现有技术中的问题而提供一种离子推力器环形磁钢安装结构,本发明解决了由多个小块磁钢组装成环形磁钢过程中相互排斥难以紧密排布安装问题,通过磁钢安装位置的设计降低了离子推力器对磁钢的高温使用性要求。The technical problem to be solved by the present invention is to provide an ion thruster annular magnetic steel installation structure for the problems in the prior art. Arrangement and installation problems, through the design of the installation position of the magnetic steel, the high-temperature usability requirements of the ion thruster for the magnetic steel are reduced.
为解决本发明的技术问题采用如下技术方案:Adopt following technical scheme for solving technical problem of the present invention:
一种离子推力器环形磁钢安装结构,包括磁钢、极靴,所述极靴和磁钢置于磁钢盒内,所述磁钢装配到磁钢盒时利用极靴对磁钢的吸引力实现小块磁钢的紧密排列,所述磁钢盒用磁钢盖封装,所述磁钢盒和磁钢盖通过连接螺钉组件安装在推力器外壳上。An ion thruster ring-shaped magnetic steel installation structure, including magnetic steel and pole shoes, the pole shoes and the magnetic steel are placed in the magnetic steel box, and the magnetic steel is attracted by the pole shoes to the magnetic steel when the magnetic steel is assembled into the magnetic steel box The compact arrangement of small pieces of magnetic steel is realized by force, and the magnetic steel box is sealed with a magnetic steel cover, and the magnetic steel box and the magnetic steel cover are installed on the thruster shell through a connecting screw assembly.
所述磁钢盒和磁钢盖材质为硬铝或钛合金无磁材料。The magnetic steel box and the magnetic steel cover are made of duralumin or titanium alloy non-magnetic material.
所述极靴材质为精密合金或电工纯铁导磁材料。The material of the pole shoe is precision alloy or electric pure iron magnetic material.
所述磁钢盖靠近离子推力器阳极侧厚度小于1.5mm。The thickness of the magnetic steel cover near the anode side of the ion thruster is less than 1.5mm.
所述磁钢盖外表面等离子体喷涂氧化铝涂层。The outer surface of the magnetic steel cover is plasma-sprayed with aluminum oxide coating.
所述磁钢与离子推力器阳极间的距离小于4mm。The distance between the magnetic steel and the anode of the ion thruster is less than 4mm.
本发明的离子推力器环形磁钢安装结构,在不影响磁场的强度和分布的前提下,通过设计极靴,解决了由多个小块磁钢组装成环形磁钢过程中相互排斥难以紧密排布安装困难问题。利用将磁钢环安装于外壳上的设计降低了离子推力器对磁钢的高温使用性要求。The ring magnet installation structure of the ion thruster of the present invention, on the premise of not affecting the strength and distribution of the magnetic field, through the design of the pole shoe, solves the problem of mutual repulsion and tight arrangement in the process of assembling ring magnets from multiple small pieces of magnets. Difficulty in cloth installation. The design of installing the magnetic steel ring on the casing reduces the high temperature usability requirements of the ion thruster on the magnetic steel.
附图说明Description of drawings
图1 为本发明离子推力器环形磁钢安装结构示意图;Figure 1 is a schematic diagram of the installation structure of the ion thruster ring magnet of the present invention;
图中:1-磁钢盖、2-磁钢盒、3-磁钢、4-极靴、5-螺钉组件、6-推力器外壳、7-离子推力器阳极。In the figure: 1-magnetic steel cover, 2-magnetic steel box, 3-magnetic steel, 4-pole shoe, 5-screw assembly, 6-thruster shell, 7-ion thruster anode.
具体实施方式detailed description
以下结合附图和具体实施方式进一步说明本发明,但不限于此。The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments, but is not limited thereto.
如图所示,一种离子推力器环形磁钢安装结构,包括磁钢3、极靴4,极靴4和磁钢3置于磁钢盒2内,其中极靴4安装在磁钢盒2内远离离子推力器阳极的一侧,磁钢3装配到磁钢盒2时利用极靴4对磁钢3的吸引力实现小块磁钢3的紧密排列,利用磁钢盒2的盒式安装结构将小块磁钢3拼接成磁钢环,解决了由多个小块磁钢组装成环形磁钢过程中相互排斥难以紧密排布问题。磁钢盒2用磁钢盖3封装,磁钢盒2和磁钢盖1通过连接螺钉组件5安装在推力器外壳6上,解决了环形磁钢在推力器上的装配问题。其中磁钢盒2和磁钢盖1材质为硬铝或钛合金无磁材料。极靴4材质为精密合金或电工纯铁导磁材料。磁钢盖1靠近离子推力器阳极7侧厚度小于1.5mm。磁钢盖1外表面等离子体喷涂氧化铝涂层,氧化铝涂层不仅提高了磁钢盖的表面发射率,并确保磁钢盖1与离子推力器阳极7间的电绝缘;磁钢3与离子推力器阳极7间的距离小于4mm。As shown in the figure, an ion thruster annular magnetic steel installation structure includes a magnetic steel 3, a pole piece 4, the pole piece 4 and the magnetic steel 3 are placed in the magnetic steel box 2, and the pole shoe 4 is installed in the magnetic steel box 2 On the side far away from the anode of the ion thruster, when the magnetic steel 3 is assembled to the magnetic steel box 2, the attraction force of the pole piece 4 to the magnetic steel 3 is used to realize the close arrangement of small pieces of magnetic steel 3, and the box-type installation of the magnetic steel box 2 is used. The structure splices small pieces of magnetic steel 3 into a magnetic steel ring, which solves the problem of mutual repulsion and difficulty in tight arrangement during the process of assembling a ring-shaped magnetic steel from multiple small pieces of magnetic steel. The magnetic steel box 2 is packaged with a magnetic steel cover 3, and the magnetic steel box 2 and the magnetic steel cover 1 are installed on the thruster shell 6 through the connecting screw assembly 5, which solves the assembly problem of the ring magnet on the thruster. Wherein the magnetic steel box 2 and the magnetic steel cover 1 are made of duralumin or titanium alloy non-magnetic material. The pole shoe 4 is made of precision alloy or electric pure iron magnetic material. The thickness of the magnetic steel cover 1 near the anode 7 of the ion thruster is less than 1.5 mm. The outer surface of the magnetic steel cover 1 is plasma-sprayed with aluminum oxide coating, and the aluminum oxide coating not only improves the surface emissivity of the magnetic steel cover, but also ensures the electrical insulation between the magnetic steel cover 1 and the ion thruster anode 7; The distance between the anodes 7 of the ion thruster is less than 4mm.
本发明结构的环形磁钢3组件通过螺钉组件5固定到推力器外壳6上,并与离子推力器阳极7隔离;其安装结构将离子推力器阳极7与磁钢3间的热传导由传统推力器的导热传导转变为辐射传导,将推力器外壳6与磁钢3间的热传导由传统推力器的辐射传导转变为导热传导。在推力器外壳6温度低于离子推力器阳极7条件,利用这种传导方式的转变降低了离子推力器对磁钢3的高温使用性要求。The ring-shaped magnetic steel 3 assembly of the structure of the present invention is fixed on the thruster shell 6 by the screw assembly 5, and is isolated from the ion thruster anode 7; its installation structure transfers the heat conduction between the ion thruster anode 7 and the magnetic steel 3 by the traditional thruster The heat conduction of the thruster is converted into radiation conduction, and the heat conduction between the thruster shell 6 and the magnetic steel 3 is changed from the radiation conduction of the traditional thruster to the heat conduction. When the temperature of the thruster casing 6 is lower than that of the ion thruster anode 7, the transformation of the conduction mode reduces the high-temperature usability requirements of the ion thruster on the magnetic steel 3 .
本发明包括但不限于以上实施例,凡是在本发明精神的原则之下进行的任何等同替换或局部改进,都将视为在本发明的保护范围之内。The present invention includes but is not limited to the above embodiments, and any equivalent replacement or partial improvement under the principle of the spirit of the present invention will be considered within the protection scope of the present invention.
Claims (6)
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| Application Number | Priority Date | Filing Date | Title |
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| CN201611118157.XA CN106401891A (en) | 2016-12-07 | 2016-12-07 | Annular magnetic steel installation structure of ion thruster |
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| CN201611118157.XA CN106401891A (en) | 2016-12-07 | 2016-12-07 | Annular magnetic steel installation structure of ion thruster |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107729602A (en) * | 2017-09-01 | 2018-02-23 | 兰州空间技术物理研究所 | A kind of ion thruster working parameters Optimal Design Method |
| CN107795445A (en) * | 2017-09-01 | 2018-03-13 | 兰州空间技术物理研究所 | A kind of annular magnetic steel ring cutting field ion thruster structure and main support ring |
| CN111140453A (en) * | 2019-12-27 | 2020-05-12 | 兰州空间技术物理研究所 | An annular magnetic steel installation structure for the cone section of an ion thruster |
| CN115653860A (en) * | 2022-10-25 | 2023-01-31 | 兰州空间技术物理研究所 | Cathode pole shoe assembly of riveting divergent field ion thruster |
| CN118242245A (en) * | 2024-03-31 | 2024-06-25 | 兰州空间技术物理研究所 | A vibration reduction structure for an ion thruster optical system |
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| CN104269336A (en) * | 2014-09-04 | 2015-01-07 | 兰州空间技术物理研究所 | Ion thruster discharge chamber magnetic pole structure and design method thereof |
| EP2849204A1 (en) * | 2013-09-12 | 2015-03-18 | Roth & Rau AG | Plasma generating apparatus |
| CN105179191A (en) * | 2015-08-12 | 2015-12-23 | 兰州空间技术物理研究所 | Annular quadrupole permanent magnet ring cutting field magnetic circuit structure for ion thruster |
| CN205388924U (en) * | 2016-02-16 | 2016-07-20 | 兰州空间技术物理研究所 | Ring magnets's installation device |
-
2016
- 2016-12-07 CN CN201611118157.XA patent/CN106401891A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| EP2849204A1 (en) * | 2013-09-12 | 2015-03-18 | Roth & Rau AG | Plasma generating apparatus |
| CN104269336A (en) * | 2014-09-04 | 2015-01-07 | 兰州空间技术物理研究所 | Ion thruster discharge chamber magnetic pole structure and design method thereof |
| CN105179191A (en) * | 2015-08-12 | 2015-12-23 | 兰州空间技术物理研究所 | Annular quadrupole permanent magnet ring cutting field magnetic circuit structure for ion thruster |
| CN205388924U (en) * | 2016-02-16 | 2016-07-20 | 兰州空间技术物理研究所 | Ring magnets's installation device |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107729602A (en) * | 2017-09-01 | 2018-02-23 | 兰州空间技术物理研究所 | A kind of ion thruster working parameters Optimal Design Method |
| CN107795445A (en) * | 2017-09-01 | 2018-03-13 | 兰州空间技术物理研究所 | A kind of annular magnetic steel ring cutting field ion thruster structure and main support ring |
| CN107795445B (en) * | 2017-09-01 | 2019-08-23 | 兰州空间技术物理研究所 | An annular magnetic steel annular tangential field ion thruster structure and main support ring |
| CN111140453A (en) * | 2019-12-27 | 2020-05-12 | 兰州空间技术物理研究所 | An annular magnetic steel installation structure for the cone section of an ion thruster |
| CN111140453B (en) * | 2019-12-27 | 2021-09-24 | 兰州空间技术物理研究所 | An annular magnetic steel installation structure for the cone section of an ion thruster |
| CN115653860A (en) * | 2022-10-25 | 2023-01-31 | 兰州空间技术物理研究所 | Cathode pole shoe assembly of riveting divergent field ion thruster |
| CN115653860B (en) * | 2022-10-25 | 2023-09-22 | 兰州空间技术物理研究所 | A riveted divergent field ion thruster cathode shoe assembly |
| CN118242245A (en) * | 2024-03-31 | 2024-06-25 | 兰州空间技术物理研究所 | A vibration reduction structure for an ion thruster optical system |
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Application publication date: 20170215 |