CN106714536A - Plasma shielding protection method of electric thruster power supply line in vacuum chamber - Google Patents

Plasma shielding protection method of electric thruster power supply line in vacuum chamber Download PDF

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Publication number
CN106714536A
CN106714536A CN201611117616.2A CN201611117616A CN106714536A CN 106714536 A CN106714536 A CN 106714536A CN 201611117616 A CN201611117616 A CN 201611117616A CN 106714536 A CN106714536 A CN 106714536A
Authority
CN
China
Prior art keywords
supply line
plasma
vacuum chamber
power supply
electric
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.)
Pending
Application number
CN201611117616.2A
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Chinese (zh)
Inventor
崔强
江豪成
李达
赵蓁
黄骁
马彦坤
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.)
Lanzhou Institute of Physics of Chinese Academy of Space Technology
Original Assignee
Lanzhou Institute of Physics of Chinese Academy of Space Technology
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 Lanzhou Institute of Physics of Chinese Academy of Space Technology filed Critical Lanzhou Institute of Physics of Chinese Academy of Space Technology
Priority to CN201611117616.2A priority Critical patent/CN106714536A/en
Publication of CN106714536A publication Critical patent/CN106714536A/en
Pending legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K9/00Screening of apparatus or components against electric or magnetic fields
    • H05K9/0007Casings
    • H05K9/0018Casings with provisions to reduce aperture leakages in walls, e.g. terminals, connectors, cables

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  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Plasma Technology (AREA)

Abstract

The invention discloses a plasma shielding protection method of an electric thruster power supply line in a vacuum chamber. The plasma shielding protection method comprises steps that (1) shielding protection of a flange plate opening of a binding post in the chamber is carried out; (2) a power supply cable in the chamber is wrapped; (3) wrapping protection of an electric connector is carried out; (4) small holes having diameters in a range from 0.5 to 1mm are disposed in a shielding wrapping layer on the opening part of the flange plate and an electric connector wrapping layer, and the number of the small holes is not less than 1/cm3. The electric thruster power supply line in the vacuum chamber is protected by using non-adhesive metal foil, polyimide adhesive tapes, and other materials, and an object of shielding the plasma is achieved. The plasma shielding protection method is advantageous in that the safety performance and the reliability of the power supply line in the narrow space of the chamber are obviously improved, and the short circuit condition of the flange part and the electric connector in the chamber caused by the entrance of the plasma is eliminated, and therefore the service lifetime of the electric connector is prolonged, and the normal power supply of the electric thruster is guaranteed.

Description

A kind of plasma shield guard method of electric thruster supply line in vacuum chamber
Technical field
The invention belongs to electric thruster supply line technical field, and in particular to a kind of electric thruster supply line is in vacuum Plasma shield guard method in cabin.
Background technology
To electric thruster supply line in vacuum chamber part, such as do not carry out shielding protection, although generally also can Meet thruster power reguirements, but potential safety hazard is caused to whole thruster electric power system.Thruster in the normal mode of operation, Substantial amounts of plasma can be produced in narrow and small vacuum chamber, with the aggregation that increases of plasma, form plasma cloud cluster, When these plasmas enter cabin inner flange junction or electrical connector interior, a kind of conducting medium can be turned into, so as to occur short The situation on road.Other ion sputtering can cause to damage to power cable in cabin, while ion can also be attached to cabin inner flange wiring Terminal surfaces, so as to influence the electric conductivity of binding post, if implementing this kind of shielding protection, can greatly prolong cable and terminals The service life of son, excludes potential risk, effectively reduces experimentation cost.
The content of the invention
The technical problems to be solved by the invention are directed to shortcoming of the prior art and provide a kind of electric thruster and power Plasma shield guard method of the circuit in vacuum chamber, with solve cabin inner flange, electric connector and power cable short circuit and The shortcomings of damage.
Adopted the following technical scheme that to solve technical problem of the invention:
A kind of plasma shield guard method of electric thruster supply line in vacuum chamber, comprises the following steps:
(1) shielding protection will be carried out at the flange dish opening of cabin internal wiring terminal;
(2) power cable in cabin is wrapped up;
(3) electric connector is implemented into parcel protection;
(4) aperture that 0.5-1mm is opened on clad and electric connector clad, the quantity of aperture are shielded at flange dish opening It is not less than 1/cm3
The step(1)It is middle that region at the internal wiring terminal flange dish opening of cabin is covered with without glue metal foil, together When it is fixed with Kapton Tape.
The step(2)It is middle power cable in cabin is wrapped up with without glue metal foil, it is ensured that cable surface and without The tight attaching of glue metal foil.
The step(3)It is middle electric connector is protected with without glue metal foil, prevent plasma from entering inside it The phenomenon being short-circuited.
Compared with the prior art, the invention has the advantages that:(1)The present invention it is unique compared with other congenic methods and Practicality;(2)After the present invention, ion without being adhered to flange binding post surface, it is to avoid the electric conductivity of pair of wire connection terminals Have undesirable effect, while eliminating plasma accumulates in the short-circuit conditions occurred between each binding post;(3)Using this After invention, protect power cable from because of ion sputtering and caused by damage, it is to avoid the generation of short-circuit conditions;(4)Using this After invention, block plasma and enter electrical connector interior, it is to avoid the problem of short circuit, extend the use longevity of electric connector Life.
The present invention by electric thruster supply line in vacuum chamber, using without materials such as glue metal foil, Kapton Tapes Protected, reached the purpose of shielding plasma.This method significantly improves the security of Cang Nei small spaces supply line With reliability, eliminate at the inner flange of cabin and electric connector because plasma enter and caused by short-circuit conditions, extend and be electrically connected Connect the service life of device, it is ensured that the normal power supply of electric thruster.
Specific embodiment
The present invention is described in further detail below:
A kind of plasma shield guard method of electric thruster supply line in vacuum chamber, comprises the following steps:
(1) region at the flange dish opening of cabin internal wiring terminal is carried out into covering shielding protection with without glue metal foil, while with Kapton Tape is fixed.
(2) power cable in cabin is wrapped up with without glue metal foil, it is ensured that power cable surface and without glue metal The tight attaching of paper tinsel.
(3) electric connector is protected with without glue metal foil, prevents plasma from entering its short circuit occurred inside Phenomenon.
(4) aperture that 0.5-1mm is opened on clad and electric connector clad is shielded at flange dish opening, aperture Quantity is not less than 1/cm3.Because electric thruster is used as a kind of vacuum device, it is necessary under vacuum conditions just can normal work. When parcel operation is implemented, vacuum chamber exposes in an atmosphere, then just has gas in integument at two, in order to allow the gas can During vacuum chamber is vacuumized, timely and effectively release out it is necessary to perforate and to ensure certain density, to reach The vacuum environment of test requirements document.
The present invention is used in LIPS-300 thruster performance tests, to vacuum chamber inner flange, power cable and electric connector Many wheel performance tests have been carried out after carrying out shielding protection.All properties experiment demonstrate guard method of the present invention be it is effective, So as to eliminate a series of problems for protection being not carried out and bringing.Such as, shielding protection is not carried out at flange dish opening, on the one hand Plasma in vacuum chamber can be attached on binding post, and the electric conductivity of binding post will be influenceed in the course of time until cannot Normally use, another aspect plasma is gathered at flange binding post, the phenomenon being easily short-circuited.

Claims (4)

1. plasma shield guard method of a kind of electric thruster supply line in vacuum chamber, it is characterised in that including following Step:
(1) shielding protection will be carried out at the flange dish opening of cabin internal wiring terminal;
(2) power cable in cabin is wrapped up;
(3) electric connector is implemented into parcel protection;
(4) aperture that 0.5-1mm is opened on clad and electric connector clad, the quantity of aperture are shielded at flange dish opening It is not less than 1/cm3
2. plasma shield protection side of a kind of electric thruster supply line according to claim 1 in vacuum chamber Method, it is characterised in that:The step(1)It is middle that region at the flange dish opening of cabin internal wiring terminal is carried out with without glue metal foil Covering, while fixed with Kapton Tape.
3. plasma shield protection of a kind of electric thruster supply line according to claim 1 and 2 in vacuum chamber Method, it is characterised in that:The step(2)It is middle power cable in cabin is wrapped up with without glue metal foil, it is ensured that cable table Face and the tight attaching without glue metal foil.
4. plasma shield protection side of a kind of electric thruster supply line according to claim 3 in vacuum chamber Method, it is characterised in that:The step(3)It is middle electric connector is protected with without glue metal foil, prevent plasma from entering The phenomenon of its short circuit occurred inside.
CN201611117616.2A 2016-12-07 2016-12-07 Plasma shielding protection method of electric thruster power supply line in vacuum chamber Pending CN106714536A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201611117616.2A CN106714536A (en) 2016-12-07 2016-12-07 Plasma shielding protection method of electric thruster power supply line in vacuum chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201611117616.2A CN106714536A (en) 2016-12-07 2016-12-07 Plasma shielding protection method of electric thruster power supply line in vacuum chamber

Publications (1)

Publication Number Publication Date
CN106714536A true CN106714536A (en) 2017-05-24

Family

ID=58936278

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201611117616.2A Pending CN106714536A (en) 2016-12-07 2016-12-07 Plasma shielding protection method of electric thruster power supply line in vacuum chamber

Country Status (1)

Country Link
CN (1) CN106714536A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111005849A (en) * 2019-11-28 2020-04-14 兰州空间技术物理研究所 Plasma sealing structure of discharge chamber of annular magnetic steel circular cutting field ion thruster

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2767444A3 (en) * 1997-02-04 1999-02-19 Hsing Chau Ind Co Ltd Electrical shielding metal housing e.g. for computer signal transmission device
CN1550061A (en) * 2001-08-30 2004-11-24 Electrical machines for navy vessels based on superconducting technology,
CN102074924A (en) * 2009-11-24 2011-05-25 刘新月 Broken cable sealing device
CN102694299A (en) * 2012-06-11 2012-09-26 上海航天科工电器研究院有限公司 Metal wire clip of tail end fixing cable
CN202711793U (en) * 2012-07-16 2013-01-30 艾恩特精密工业股份有限公司 Shielding cable structure and combination thereof
CN105071142A (en) * 2015-07-28 2015-11-18 株洲南车时代电气股份有限公司 Cabinet capable of electromagnetic shielding
CN106286180A (en) * 2016-10-17 2017-01-04 哈尔滨工业大学 The magnetic field shielding case of cusped magnetic field thruster

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2767444A3 (en) * 1997-02-04 1999-02-19 Hsing Chau Ind Co Ltd Electrical shielding metal housing e.g. for computer signal transmission device
CN1550061A (en) * 2001-08-30 2004-11-24 Electrical machines for navy vessels based on superconducting technology,
CN102074924A (en) * 2009-11-24 2011-05-25 刘新月 Broken cable sealing device
CN102694299A (en) * 2012-06-11 2012-09-26 上海航天科工电器研究院有限公司 Metal wire clip of tail end fixing cable
CN202711793U (en) * 2012-07-16 2013-01-30 艾恩特精密工业股份有限公司 Shielding cable structure and combination thereof
CN105071142A (en) * 2015-07-28 2015-11-18 株洲南车时代电气股份有限公司 Cabinet capable of electromagnetic shielding
CN106286180A (en) * 2016-10-17 2017-01-04 哈尔滨工业大学 The magnetic field shielding case of cusped magnetic field thruster

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111005849A (en) * 2019-11-28 2020-04-14 兰州空间技术物理研究所 Plasma sealing structure of discharge chamber of annular magnetic steel circular cutting field ion thruster

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Application publication date: 20170524

RJ01 Rejection of invention patent application after publication