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 PDFInfo
- 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
- Authority
- CN
- China
- Prior art keywords
- built
- socket
- aviation plug
- claw
- type
- 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.)
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Links
- 238000000926 separation method Methods 0.000 claims abstract description 38
- 210000000078 Claw Anatomy 0.000 claims abstract description 27
- 238000009434 installation Methods 0.000 claims abstract description 13
- 238000000034 method Methods 0.000 abstract description 4
- 208000004703 Crush Injury Diseases 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
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
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)
- 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.
- 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.
- 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.
- 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 describedClaw（2）Outside diameter is less than built-in type mounting groove outside diameter.
- 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 describedClaw（2）Extension elongation is more than built-in type installation groove depth.
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) |
-
2017
- 2017-09-04 CN CN201721120471.1U patent/CN207320554U/en active Active
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| GR01 | Patent grant | ||
| GR01 | Patent grant |