CN204361398U - A kind of combining structure realizing electrical connector and reliably pull away - Google Patents

A kind of combining structure realizing electrical connector and reliably pull away Download PDF

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Publication number
CN204361398U
CN204361398U CN201420643120.9U CN201420643120U CN204361398U CN 204361398 U CN204361398 U CN 204361398U CN 201420643120 U CN201420643120 U CN 201420643120U CN 204361398 U CN204361398 U CN 204361398U
Authority
CN
China
Prior art keywords
keyset
breakaway plug
socket
lock bracket
electrical connector
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.)
Expired - Fee Related
Application number
CN201420643120.9U
Other languages
Chinese (zh)
Inventor
李京苑
吴学森
刘宁
周人歌
何芸香
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.)
China Academy of Launch Vehicle Technology CALT
Beijing Aerospace Changzheng Aircraft Institute
Original Assignee
China Academy of Launch Vehicle Technology CALT
Beijing Aerospace Changzheng Aircraft Institute
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 China Academy of Launch Vehicle Technology CALT, Beijing Aerospace Changzheng Aircraft Institute filed Critical China Academy of Launch Vehicle Technology CALT
Priority to CN201420643120.9U priority Critical patent/CN204361398U/en
Application granted granted Critical
Publication of CN204361398U publication Critical patent/CN204361398U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of combining structure realizing electrical connector and reliably pull away, comprise breakaway plug, lock bracket, keyset, separation socket, switching bearing, solidus plate; Wherein one end of breakaway plug one end and lock bracket is connected, the breakaway plug other end be separated socket grafting, the other end of lock bracket passes the through hole in the middle part of solidus plate and connects, and is separated on socket and is provided with keyset, and keyset is fixedly connected with bearing of transferring.The utility model can stop rocket projectile before receiving cutting and separating signal, and breakaway plug is unexpected major hidden danger of throwing off under the flight environment of vehicle of shock and vibration, thus guarantees a body cutting and separating control command reliable delivery.

Description

A kind of combining structure realizing electrical connector and reliably pull away
Technical field
The utility model relates to a kind of combining structure realizing electrical connector and reliably pull away, and belongs to aircraft field.
Background technology
In aircraft flight process, guarantee that a body cutting and separating control command reliable delivery is the key link being related to aircraft success or failure.In order to ensure that rocket projectile is before the signal receiving cutting and separating, breakaway plug is not thrown off under the flight environment of vehicle of shock and vibration, structurally needs to take safeguard.In existing point of slotting operation technique, common way is in the stay column hole of breakaway plug, penetrate steel wire, reserve certain rich length, the other end of steel wire is fixed in another different from being separated socket place housing after isolation shell sections, its weak point is: for the electrical connector that separating force is less, installs, test or in flight environment of vehicle, there is point slotting unexpected hidden danger pulled away on ground.
Utility model content
Technical problem to be solved in the utility model is: for overcoming the deficiencies in the prior art, provides a kind of combining structure realizing electrical connector and reliably pull away.
Technical solution of the present utility model is:
Realize the combining structure that electrical connector reliably pulls away, comprise breakaway plug, lock bracket, keyset, separation socket, switching bearing, solidus plate; Wherein one end of breakaway plug one end and lock bracket is connected, the breakaway plug other end be separated socket grafting, the other end of lock bracket passes the through hole in the middle part of solidus plate and connects, and is separated on socket and is provided with keyset, and keyset is fixedly connected with bearing of transferring.
Breakaway plug one end is provided with radial through hole, keyset is provided with the through hole be connected with bearing of transferring.
The utility model advantage is compared with prior art:
The utility model can stop rocket projectile before receiving cutting and separating signal, and breakaway plug is unexpected major hidden danger of throwing off under the flight environment of vehicle of shock and vibration, thus guarantees a body cutting and separating control command reliable delivery.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the connection layout of the utility model breakaway plug;
Fig. 3 is the utility model assembling assumption diagram.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described in detail.
Realize the combining structure that electrical connector reliably pulls away, comprise breakaway plug 1, lock bracket 2, keyset 3, separation socket 4, switching bearing 5, solidus plate 6; Wherein breakaway plug 1 one end is provided with radial through hole, be connected with one end of lock bracket 2, breakaway plug 1 other end be separated socket 4 grafting, the other end of lock bracket 2 passes through hole also the two connection in the middle part of solidus plate 6, be separated on socket 4 and be provided with keyset 3, keyset 3 is provided with the through hole be connected with bearing 5 of transferring, keyset 3 is fixedly connected with switching bearing 5.
Part mounting means of the present utility model is: to be arranged at by separation socket 4 in the middle part of switching bearing 5 in endoporus, by first separation socket 4 being fixed on after on keyset 3, again by breakaway plug 1 be separated socket 4 grafting (see Fig. 1), then breakaway plug 1 and other connectors and cable are passed by bearing 5 endoporus of transferring, keyset 3 is connected (see Fig. 3) with switching bearing 5 front end, again switching bearing 5 is fixed on bottom, solidus plate 6 is fixed on housing rear end frame, regulate lock bracket 2, its front end and breakaway plug 1 stay column end face are fitted, lock bracket 2 rear end passes by solidus plate 6 mesopore, by nut and bullet plain cushion locking positioning (see Fig. 2), ensure that breakaway plug 1 is not thrown off before separation signal sends.
By optimizing the fit dimension between each coherent element, rationally determine the axial installation site of breakaway plug 1 and diameter of bore dimensional accuracy, can make the aerodynamic configuration that the rear end face after rocket projectile cutting and separating keeps good, mounting structure is simple to operate, plugs and unplugs conveniently.
The unexposed technology of the utility model belongs to general knowledge as well known to those skilled in the art.

Claims (2)

1. the combining structure realizing electrical connector and reliably pull away, it is characterized in that, comprise breakaway plug (1), lock bracket (2), keyset (3), be separated socket (4), switching bearing (5), solidus plate (6); Wherein one end of breakaway plug (1) one end and lock bracket (2) is connected, breakaway plug (1) other end be separated socket (4) grafting, the other end of lock bracket (2) passes through hole also the two connection at solidus plate (6) middle part, be separated on socket (4) and be provided with keyset (3), keyset (3) is fixedly connected with switching bearing (5).
2. a kind of combining structure realizing electrical connector and reliably pull away as claimed in claim 1, it is characterized in that, breakaway plug (4) one end is provided with radial through hole, keyset (3) is provided with the through hole be connected with bearing of transferring (5).
CN201420643120.9U 2014-10-31 2014-10-31 A kind of combining structure realizing electrical connector and reliably pull away Expired - Fee Related CN204361398U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420643120.9U CN204361398U (en) 2014-10-31 2014-10-31 A kind of combining structure realizing electrical connector and reliably pull away

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420643120.9U CN204361398U (en) 2014-10-31 2014-10-31 A kind of combining structure realizing electrical connector and reliably pull away

Publications (1)

Publication Number Publication Date
CN204361398U true CN204361398U (en) 2015-05-27

Family

ID=53262846

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420643120.9U Expired - Fee Related CN204361398U (en) 2014-10-31 2014-10-31 A kind of combining structure realizing electrical connector and reliably pull away

Country Status (1)

Country Link
CN (1) CN204361398U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105226469A (en) * 2015-09-15 2016-01-06 北京航天发射技术研究所 Plug-in connector docks the adaptive motion system that comes off
CN112762777A (en) * 2020-11-16 2021-05-07 中国运载火箭技术研究院 Separating mechanism and aircraft
CN112985194A (en) * 2021-05-06 2021-06-18 中国科学院力学研究所 Connecting and unlocking device and carrier rocket

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105226469A (en) * 2015-09-15 2016-01-06 北京航天发射技术研究所 Plug-in connector docks the adaptive motion system that comes off
CN112762777A (en) * 2020-11-16 2021-05-07 中国运载火箭技术研究院 Separating mechanism and aircraft
CN112985194A (en) * 2021-05-06 2021-06-18 中国科学院力学研究所 Connecting and unlocking device and carrier rocket
CN112985194B (en) * 2021-05-06 2021-08-06 中国科学院力学研究所 Connecting and unlocking device and carrier rocket

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20150527

Termination date: 20171031