[go: up one dir, main page]

CN106450822A - Miniature magnetic latching relay ground structure for geosynchronous orbit - Google Patents

Miniature magnetic latching relay ground structure for geosynchronous orbit Download PDF

Info

Publication number
CN106450822A
CN106450822A CN201611055723.7A CN201611055723A CN106450822A CN 106450822 A CN106450822 A CN 106450822A CN 201611055723 A CN201611055723 A CN 201611055723A CN 106450822 A CN106450822 A CN 106450822A
Authority
CN
China
Prior art keywords
latching relay
magnetic latching
miniature magnetic
metal
gasket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201611055723.7A
Other languages
Chinese (zh)
Other versions
CN106450822B (en
Inventor
王凤丽
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Institute of Technical Physics of CAS
Original Assignee
Shanghai Institute of Technical Physics of CAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shanghai Institute of Technical Physics of CAS filed Critical Shanghai Institute of Technical Physics of CAS
Priority to CN201611055723.7A priority Critical patent/CN106450822B/en
Publication of CN106450822A publication Critical patent/CN106450822A/en
Application granted granted Critical
Publication of CN106450822B publication Critical patent/CN106450822B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01RELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
    • H01R4/00Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation
    • H01R4/58Electrically-conductive connections between two or more conductive members in direct contact, i.e. touching one another; Means for effecting or maintaining such contact; Electrically-conductive connections having two or more spaced connecting locations for conductors and using contact members penetrating insulation characterised by the form or material of the contacting members
    • H01R4/64Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail

Landscapes

  • Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)

Abstract

本发明公开了一种地球同步轨道用微型磁保持继电器接地结构。接地结构包括导通接地和绝缘安装两部分:金属垫片与微型磁保持继电器紧配合安装,通过焊接在金属垫片上的接地线将微型磁保持继电器金属外壳与机壳导通;在金属垫片外侧安装绝缘垫片,绝缘垫片与电路板贴合,实现微型磁保持继电器金属外壳与电路板绝缘安装。该结构从根本上解决了该类型继电器金属外壳与机壳接地,同时在电路板上绝缘安装的问题。该结构具有重量轻,操作方便,可靠性高,可以经受空间环境的考验。

The invention discloses a grounding structure of a miniature magnetic latching relay for a geosynchronous orbit. The grounding structure includes two parts: conduction grounding and insulation installation: the metal gasket and the miniature magnetic latching relay are installed tightly, and the metal shell of the miniature magnetic latching relay is connected to the chassis through the ground wire welded on the metal gasket; An insulating gasket is installed on the outside of the chip, and the insulating gasket is attached to the circuit board to realize the insulation installation of the metal case of the miniature magnetic latching relay and the circuit board. This structure fundamentally solves the problem of grounding the metal shell and the casing of this type of relay, and at the same time insulating and installing on the circuit board. The structure has the advantages of light weight, convenient operation, high reliability, and can withstand the test of space environment.

Description

一种地球同步轨道用微型磁保持继电器接地结构A Grounding Structure of Miniature Magnetic Latching Relay Used in Geosynchronous Orbit

技术领域technical field

本发明涉及一种地球同步轨道用微型磁保持继电器接地结构,具体涉及结构形式和材料,它主要应用于地球同步轨道空间遥感器。从根本上解决了微型磁保持继电器金属外壳与机壳接地,同时在电路板上绝缘安装的问题。The invention relates to a grounding structure of a miniature magnetic holding relay for a geosynchronous orbit, in particular to a structure form and a material, and is mainly applied to a space remote sensor of the geosynchronous orbit. It fundamentally solves the problem of grounding the metal casing of the miniature magnetic latching relay and the casing, and at the same time insulating and installing on the circuit board.

背景技术Background technique

地球同步轨道空间等离子体温度高、密度小伴随着地磁亚暴活动,遥感器面临着严重的表面充放电问题,同时该轨道位于外辐射带的中心高度边缘,高能电子具有通量大、能量高等特点。为了避免遥感器严重的深层充放电危险,减轻空间静电放电对遥感器的影响,满足电磁兼容性的要求,须对遥感器进行相应的防护设计。产生深层充放电的源头为高能电子(100keV~10MeV),发生深层充放电效应的对象为孤立导体和介质材料。介质材料如电路板,电缆外皮、胶等,这些介质材料已经有成熟的工艺进行静电控制。而孤立导体,面积超过3cm2或长度超过25cm的导体,如DC-DC、继电器等金属封装的元器件,已经有规范的工艺要求接地,屏蔽等。但如微型磁保持继电器2JB0.5-1器件,表面金属封装,无接地管脚,表面积为7.34cm2,不能按常规的方法接地,因此需要特别的接地处理方法。The high temperature and low density of space plasma in geosynchronous orbit is accompanied by geomagnetic substorm activities, and remote sensors are faced with serious surface charging and discharging problems. features. In order to avoid the serious danger of deep charge and discharge of the remote sensor, reduce the impact of space electrostatic discharge on the remote sensor, and meet the requirements of electromagnetic compatibility, the corresponding protection design must be carried out for the remote sensor. The source of deep charge and discharge is high-energy electrons (100keV ~ 10MeV), and the objects of deep charge and discharge effect are isolated conductors and dielectric materials. Dielectric materials such as circuit boards, cable sheaths, glue, etc., these dielectric materials have mature technology for electrostatic control. For isolated conductors, conductors with an area of more than 3cm2 or a length of more than 25cm, such as DC-DC, relays and other metal-encapsulated components, there are already standardized processes that require grounding and shielding. However, such as the miniature magnetic latching relay 2JB0.5-1 device, the surface metal package, no grounding pin, the surface area is 7.34cm 2 , it cannot be grounded in a conventional way, so a special grounding treatment method is required.

发明内容Contents of the invention

为了解决现有技术中存在的问题,本发明提供了一种地球同步轨道用微型磁保持继电器接地结构,该结构形式操作简单,对元器件不造成任何损伤,从根本上解决了微型磁保持继电器金属外壳与机壳接地,同时在电路板上绝缘安装的问题。In order to solve the problems existing in the prior art, the present invention provides a grounding structure of miniature magnetic latching relays for geosynchronous orbits. This structure is easy to operate, does not cause any damage to components, and fundamentally solves the problem of The metal shell and the chassis are grounded, and the problem of insulating and installing on the circuit board at the same time.

本发明解决技术问题所采用的技术方案如下:The technical solution adopted by the present invention to solve technical problems is as follows:

本发明微型磁保持继电器接地结构包括微型磁保持继电器1、金属垫片2和绝缘垫片3,所述的微型磁保持继电器1嵌套安装在金属垫片1上,金属垫片1安装在管脚一侧,与微型磁保持继电器1外壳接触的尺寸为紧配合,避让管脚,同时预留焊盘位置;所述的绝缘垫片3嵌套安装在金属垫片2外侧,绝缘垫片3与金属垫片2之间为间隙配合,并避让微型磁保持继电器1管脚;微型磁保持继电器1的金属外壳通过金属垫片1及接地引线与机壳导通,微型磁保持继电器1的金属外壳通过绝缘垫片3的隔离与电路板实现绝缘安装。The grounding structure of the miniature magnetic latching relay of the present invention includes a miniature magnetic latching relay 1, a metal gasket 2 and an insulating gasket 3. The miniature magnetic latching relay 1 is nested and installed on the metal gasket 1, and the metal gasket 1 is installed on the tube On one side of the foot, the size of the contact with the shell of the miniature magnetic latching relay 1 is a tight fit, avoiding the pins, and at the same time reserving the position of the pad; the insulating gasket 3 is nested and installed on the outside of the metal gasket 2, and the insulating gasket 3 There is a gap between the metal gasket 2 and the pins of the miniature latching relay 1 are avoided; the metal case of the miniature latching relay 1 is connected to the casing through the metal gasket 1 and the grounding lead, and the metal case of the miniature latching relay 1 The shell is isolated from the circuit board by the insulating gasket 3 to realize insulated installation.

所述的金属垫片1采用导电性好且可焊接的铜材质。The metal gasket 1 is made of copper material with good conductivity and weldability.

所述的绝缘垫片3材质选择空间性能稳定、绝缘性能良好的聚酰亚胺。The insulating gasket 3 is made of polyimide with stable space performance and good insulation performance.

本发明的有益效果是:解决了无接地管脚,需静电防护的孤立导体元器件的接地问题。接地方式安全可靠,且操作便利。The beneficial effect of the invention is that it solves the grounding problem of the isolated conductor components which have no grounding pin and need electrostatic protection. The grounding method is safe and reliable, and the operation is convenient.

附图说明Description of drawings

图1为继电器接地结构图,图中:1微型磁保持继电器2JB0.5-1,2金属垫片,3绝缘垫片。Figure 1 is a relay grounding structure diagram, in the figure: 1 miniature magnetic latching relay 2JB0.5-1, 2 metal gaskets, 3 insulating gaskets.

图2为金属垫片结构图,图(1)是主视图,图(2)A-A剖面图。Fig. 2 is a structural diagram of a metal gasket, Fig. (1) is a front view, Fig. (2) A-A sectional view.

图3为绝缘垫片结构图,图(1)是主视图,图(2)是A-A剖面图。Figure 3 is a structural diagram of an insulating gasket, Figure (1) is a front view, and Figure (2) is a cross-sectional view of A-A.

具体实施方式detailed description

将金属垫片2卡在微型磁保持继继电器1上,金属垫片2与绝缘垫片3胶结,并在金属垫片2与微型磁保持继继电器1上点少许胶,待胶固化后,三个元件组成一体,再焊接到电路板上,绝缘垫片3与电路板紧密贴合。焊接完成后在金属垫片2在图1指示的位置点焊一根接地导线,再将导线引导机壳固定。即完成接地操作流程。Put the metal gasket 2 on the miniature magnetic latching relay 1, glue the metal gasket 2 and the insulating gasket 3, and put a little glue on the metal gasket 2 and the miniature magnetic latching relay 1, after the glue is cured, three The components are formed into one, and then welded to the circuit board, and the insulating gasket 3 is closely attached to the circuit board. After the welding is completed, spot-weld a ground wire on the metal gasket 2 at the position indicated in Figure 1, and then guide the wire to the casing and fix it. That is, the grounding operation process is completed.

Claims (3)

1. a kind of geostationary orbit is with miniature magnetic latching relay ground structure, including miniature magnetic latching relay (1), metal Pad (2) and insulation spacer (3), it is characterised in that:
Described miniature magnetic latching relay (1) is nested on metallic gasket (1), and metallic gasket (1) is arranged on pin one Side, the size for contacting with miniature magnetic latching relay (1) shell is tight fit, avoids pin, while reserving pad locations;Described Insulation spacer (3) nested on the outside of metallic gasket (2), join for gap between insulation spacer (3) and metallic gasket (2) Close, and avoid miniature magnetic latching relay (1) pin;The metal shell of miniature magnetic latching relay (1) passes through metallic gasket (1) And ground lead is turned on casing, the metal shell of miniature magnetic latching relay (1) passes through isolation and the circuit of insulation spacer (3) Insulating mounting realized by plate.
2. a kind of geostationary orbit according to claim 1 is with miniature magnetic latching relay ground structure, and its feature exists In:Described metallic gasket (1) adopts good conductivity and welding copper material.
3. a kind of geostationary orbit according to claim 1 is with miniature magnetic latching relay ground structure, and its feature exists In:Described insulation spacer (3) material selects the good polyimides of space stable performance, insulating properties.
CN201611055723.7A 2016-11-25 2016-11-25 A kind of miniature magnetic latching relay ground structure of geostationary orbit Active CN106450822B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611055723.7A CN106450822B (en) 2016-11-25 2016-11-25 A kind of miniature magnetic latching relay ground structure of geostationary orbit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611055723.7A CN106450822B (en) 2016-11-25 2016-11-25 A kind of miniature magnetic latching relay ground structure of geostationary orbit

Publications (2)

Publication Number Publication Date
CN106450822A true CN106450822A (en) 2017-02-22
CN106450822B CN106450822B (en) 2018-10-19

Family

ID=58218630

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611055723.7A Active CN106450822B (en) 2016-11-25 2016-11-25 A kind of miniature magnetic latching relay ground structure of geostationary orbit

Country Status (1)

Country Link
CN (1) CN106450822B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2392273Y (en) * 1999-07-24 2000-08-16 莫列斯公司 Means for fixing connector
CN1567657A (en) * 2003-06-24 2005-01-19 纬创资通股份有限公司 Electrical connector with electromagnetic wave guiding function
US6945795B1 (en) * 2004-12-09 2005-09-20 Itt Manufacturing Enterprises, Inc. Quadrax interconnect grounding
CN203339420U (en) * 2013-06-05 2013-12-11 立讯精密工业(昆山)有限公司 Voice connector
CN204391417U (en) * 2014-07-15 2015-06-10 番禺得意精密电子工业有限公司 Shielded connector
CN206282979U (en) * 2016-11-25 2017-06-27 中国科学院上海技术物理研究所 Geostationary orbit is with miniature magnetic latching relay ground structure

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2392273Y (en) * 1999-07-24 2000-08-16 莫列斯公司 Means for fixing connector
CN1567657A (en) * 2003-06-24 2005-01-19 纬创资通股份有限公司 Electrical connector with electromagnetic wave guiding function
US6945795B1 (en) * 2004-12-09 2005-09-20 Itt Manufacturing Enterprises, Inc. Quadrax interconnect grounding
CN203339420U (en) * 2013-06-05 2013-12-11 立讯精密工业(昆山)有限公司 Voice connector
CN204391417U (en) * 2014-07-15 2015-06-10 番禺得意精密电子工业有限公司 Shielded connector
CN206282979U (en) * 2016-11-25 2017-06-27 中国科学院上海技术物理研究所 Geostationary orbit is with miniature magnetic latching relay ground structure

Also Published As

Publication number Publication date
CN106450822B (en) 2018-10-19

Similar Documents

Publication Publication Date Title
CN103809085B (en) Termination and cable voltage method of testing for cable voltage test
CN202978201U (en) Intelligent high-voltage cable joint of built-in partial discharge sensor
US20180153046A1 (en) Apparatus for installing high and low voltage conversion circuit, high and low voltage conversion system and power source
CN103235166B (en) Hand-hole type capacitive voltage divider
CN102121948A (en) System for measuring transient shell voltage of gas insulated switchgear
EP3333889A1 (en) Heat dissipating structure and electronic apparatus
CN206282979U (en) Geostationary orbit is with miniature magnetic latching relay ground structure
CN207651363U (en) A kind of gas-insulated high-voltage system with particle trap
US8903047B1 (en) High voltage circuit with arc protection
CN109074938B (en) Transformers with pluggable high voltage bushings
CN103411726B (en) A kind of pressure unit
CN106450822B (en) A kind of miniature magnetic latching relay ground structure of geostationary orbit
CN206281873U (en) Gas-insulated locking device for detecting high-voltage capacitor
CN204992464U (en) High pressure through -wall sleeve
CN209299657U (en) An anti-jamming device applied to power electronic technology
CN106707112B (en) Capacitor testing device
US10530137B2 (en) Coaxial motor power cable
Junge et al. Electromagnetic interference control techniques for spacecraft harness
CN114361892A (en) Coaxial cable adapter in cabin for high-vacuum-degree vacuum cabin
CN205196091U (en) Make things convenient for high -voltage insulation test's lightning grounding hole
CN101848599B (en) Flexible Printed Circuit Board
JP2020064012A (en) Partial discharge detection antenna
US3017485A (en) Means for electric vacuum furnaces
CN204315705U (en) Antenna and security device
CN105981487B (en) Electronic components for noise reduction

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant