CN207320554U - A kind of reliable erecting device of built-in type aviation plug - Google Patents

A kind of reliable erecting device of built-in type aviation plug Download PDF

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Publication number
CN207320554U
CN207320554U CN201721120471.1U CN201721120471U CN207320554U CN 207320554 U CN207320554 U CN 207320554U CN 201721120471 U CN201721120471 U CN 201721120471U CN 207320554 U CN207320554 U CN 207320554U
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CN
China
Prior art keywords
built
socket
aviation plug
claw
type
Prior art date
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Active
Application number
CN201721120471.1U
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Chinese (zh)
Inventor
陈昊
杨俊国
孙岳炜
张洁琼
马浩
秦文滨
包婧
徐芬
孟新功
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.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
Original Assignee
Jiangxi Hongdu Aviation Industry Group Co Ltd
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Application filed by Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201721120471.1U priority Critical patent/CN207320554U/en
Application granted granted Critical
Publication of CN207320554U publication Critical patent/CN207320554U/en
Active legal-status Critical Current
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Abstract

A kind of reliable erecting device of built-in type aviation plug provided by the utility model, including base, base lower section are equipped with claw, and claw is used for fixedly separated socket fixing nut;Six side's boss are equipped with above base, six side's boss are used for fast quick-detach separation socket;Six side's boss centers are equipped with four square grooves, and four square grooves are used for mounting torque spanner.A kind of reliable erecting device of built-in type aviation plug disclosed in the utility model, by the design of claw, conveniently screws separation socket fixing nut, and accurately control separates pretightning force when socket is fixedly mounted, to ensure the reliability and uniformity of installation;It when dismounting separates socket, a variety of spanners can be used to back out separation socket fixing nut by the way that six side's boss force is quick, will be that separation socket base is removed.Separation socket is being installed with that can avoid instrument improper use damage separation socket and built-in type mounting groove in disassembly process.

Description

A kind of reliable erecting device of built-in type aviation plug
Technical field
The utility model belongs to aviation type electric connector mounting technology field, and in particular to a kind of built-in type aviation plug Reliable erecting device.
Background technology
During existing separation socket installation, needs are buried because in, operate mounting groove narrow space, installation need to be grasped by man-hour manually hand-held With reference to nipper plier clamping built-in type separation socket fixing nut, it is difficult to control in installation process to screwing degree, installs and dismantle During when being screwed using nipper plier easily to fixing nut and it is interior bury the damage of groove inner wall, so as to influence to separate socket installation matter Amount.
The content of the invention
To be solved in the utility model is that existing separation socket installation process is difficult to control, and influences socket installation quality Technical problem, there is provided a kind of reliable erecting device of built-in type aviation plug, for the reliable consistent peace of built-in type separation socket Dress and quick and convenient dismounting.
In order to solve the technical problem of the utility model, the utility model is achieved through the following technical solutions:It is a kind of The reliable erecting device of built-in type aviation plug, for installing built-in type aviation plug, the built-in type aviation plug is installed on In built-in type mounting groove, the built-in type aviation plug includes separation socket fixing nut and separation socket base, its feature exists In:Including base 1, the lower section of the base 1 is equipped with claw 2, and the claw is used for fixedly separated socket fixing nut, avoids point From the contact at six angles of socket fixing nut, the crush injury to separating socket fixing nut hexagonal is eliminated;The top of base 1 Equipped with six side's boss 3, the six sides boss 3 is used for fast quick-detach separation socket;Six sides boss, 3 center is equipped with four square grooves 4, Four square groove 4 is used for mounting torque spanner.
Preferably, the claw 2 is three.
Preferably, 2 width of claw is less than separation socket fixing nut edge lengths, prevents damage separation socket from fixing spiral shell The insurance bore portion of female hexagon apex.
Preferably, 2 outside diameter of claw is less than built-in type mounting groove outside diameter, and claw 2 gos deep into built-in type mounting groove and energy Enough block separation socket fixing nut.
Preferably, 2 extension elongation of claw is more than built-in type installation groove depth, ensures that separation socket fixing nut is being twisted When tightly will be in place, claw 2 not be collided with separating socket.
Compared with prior art, the beneficial effect of the utility model acquisition is:
A kind of reliable erecting device of built-in type aviation plug disclosed in the utility model, it is convenient by the design of claw Separation socket fixing nut is screwed, and accurately control separates pretightning force when socket is fixedly mounted, to ensure the reliability of installation And uniformity;When dismounting separates socket, a variety of spanners can be used to be fixed by the quick separation socket of backing out of six side's boss force Nut, will be that separation socket base is removed.Separation socket is being installed with that can avoid instrument improper use damage point in disassembly process From socket and built-in type mounting groove.
Brief description of the drawings
Fig. 1 is a kind of reliable erecting device structure diagram of built-in type aviation plug.
Fig. 2 is that a kind of reliable erecting device of built-in type aviation plug uses figure.
Reference numeral:1st, base;2nd, claw;3rd, six side's boss;4th, four square groove;5th, built-in type mounting groove;6th, socket is separated Fixing nut;7th, socket base is separated;10th, a kind of reliable erecting device of built-in type aviation plug.
Embodiment
Below in conjunction with the accompanying drawings, embodiment is described in detail.
Referring to attached drawing 1 and attached drawing 2, a kind of reliable erecting device 10 of built-in type aviation plug, for installing built-in type boat Blind plug, the built-in type aviation plug are installed in built-in type mounting groove 5, and the built-in type aviation plug includes separation socket Fixing nut 6 and separation socket base 7, including base 1, the lower section of base 1 are equipped with claw 2, and the claw is used for fixed point From socket fixing nut 6, the contact at 6 six angles of separation socket fixing nut is avoided, is eliminated to separating socket fixing nut 6 six The crush injury at angle;The top of base 1 is equipped with six side's boss 3, and the six sides boss 3 is used for fast quick-detach separation socket;Institute State six side's boss, 3 center and be equipped with four square grooves 4, four square groove 4 is used for mounting torque spanner.
Preferably, the claw 2 is three.
Preferably, 2 width of claw is less than 6 edge lengths of separation socket fixing nut, prevents damage separation socket from fixing The insurance bore portion of the hexagon apex of nut 6.
Preferably, 2 outside diameter of claw is less than built-in type mounting groove 5, and claw 2 gos deep into built-in type mounting groove 5 and can Block separation socket fixing nut 6.
Preferably, 2 extension elongation of claw is more than 5 depth of built-in type mounting groove, ensures that separation socket fixing nut 6 exists Tighten when will be in place, claw 2 is not collided with separating socket.
During installation separation socket, separation socket base 7 is penetrated in built-in type mounting groove 5, and dismantling device screws separation socket Fixing nut 6,6 installation pretightening force of separation socket fixing nut is controlled using torque spanner;During dismounting separation socket, according to installation Method reverse operating, separation socket can be pulled down quickly, efficiency of assembling can be improved using the fixture out of built-in type mounting groove 5 And quality.
Listed above is only one of specific embodiment of the utility model.Obviously, the utility model is not limited to above reality Example is applied, there can also be many similar reshapings.Those of ordinary skill in the art can be direct from the utility model disclosure All deformations for exporting or associating, are considered as the utility model scope of the claimed.

Claims (5)

  1. A kind of 1. reliable erecting device of built-in type aviation plug, for installing built-in type aviation plug, the built-in type aviation Plug is installed in built-in type mounting groove, and the built-in type aviation plug includes separation socket fixing nut and separation socket seat Body, it is characterised in that:Including base(1), the base(1)Lower section is equipped with claw(2), the claw is used for fixedly separated socket Fixing nut;The base(1)Top is equipped with six side's boss(3), the six sides boss(3)Socket is separated for fast quick-detach; The six sides boss(3)Center is equipped with four square grooves(4), four square groove(4)For mounting torque spanner.
  2. A kind of 2. reliable erecting device of built-in type aviation plug as claimed in claim 1, it is characterised in that:The claw (2)For three.
  3. A kind of 3. reliable erecting device of built-in type aviation plug as claimed in claim 2, it is characterised in that:The claw (2)Width is less than separation socket fixing nut edge lengths.
  4. A kind of 4. reliable erecting device of built-in type aviation plug as claimed in claim 2, it is characterised in that:It is described
    Claw(2)Outside diameter is less than built-in type mounting groove outside diameter.
  5. A kind of 5. reliable erecting device of built-in type aviation plug as claimed in claim 2, it is characterised in that:It is described
    Claw(2)Extension elongation is more than built-in type installation groove depth.
CN201721120471.1U 2017-09-04 2017-09-04 A kind of reliable erecting device of built-in type aviation plug Active CN207320554U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721120471.1U CN207320554U (en) 2017-09-04 2017-09-04 A kind of reliable erecting device of built-in type aviation plug

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721120471.1U CN207320554U (en) 2017-09-04 2017-09-04 A kind of reliable erecting device of built-in type aviation plug

Publications (1)

Publication Number Publication Date
CN207320554U true CN207320554U (en) 2018-05-04

Family

ID=62385298

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721120471.1U Active CN207320554U (en) 2017-09-04 2017-09-04 A kind of reliable erecting device of built-in type aviation plug

Country Status (1)

Country Link
CN (1) CN207320554U (en)

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