CN205666387U - Aviation plug locking tool - Google Patents
Aviation plug locking tool Download PDFInfo
- Publication number
- CN205666387U CN205666387U CN201620527776.3U CN201620527776U CN205666387U CN 205666387 U CN205666387 U CN 205666387U CN 201620527776 U CN201620527776 U CN 201620527776U CN 205666387 U CN205666387 U CN 205666387U
- Authority
- CN
- China
- Prior art keywords
- aviation plug
- frock body
- notch
- aviation
- tool body
- 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
Links
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 abstract description 4
- 238000005253 cladding Methods 0.000 abstract 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
Landscapes
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The utility model provides an aviation plug locking tool, the structure of which comprises a tool body for connecting an aviation plug and a power-assisted wrench, the tool body is a sleeve structure with an open end and a closed end, a notch matched with the surface of the aviation plug is arranged on the end surface of the opening of the tool body, and the number of the notches arranged on the tool body is equal to the number of the protrusions on the surface of the aviation plug; when the aviation plug is inserted into the tool body, the aviation plug is in surface-to-surface contact with the tool body, the surface bulges of the aviation plug are inserted into the notches of the tool body in a one-to-one opposite mode, and the surfaces of the bulges do not exceed the outer surface of the tool body outwards; the closed end face of the tool body is further provided with a square hole matched with the power-assisted wrench for use. The notch side cladding of frock body has the protection pad, and the protruding side of aviation plug contacts with the protection pad of notch side. The utility model is used for add man-hour or when later maintenance quick locking or the dismantlement of aviation plug to pencil.
Description
Technical field
This utility model relates to aviation plug, specifically a kind of aviation plug locking fixture.
Background technology
Aviation plug is as connecting the adapter of electric wiring in current electronic circuit, the most wide use is to each electron-like
Product, particularly requires the fields such as higher vehicle-mounted product, military use product to connection reliability, based on its purposes, with reference to Fig. 4,
It is recognised that the surface of aviation plug has projection, the outside of aviation plug has aviation plug shell；Manufacturing enterprise is producing
When being furnished with the wire harness of aviation plug, owing to not locking the aid used, aviation plug for aviation plug on the market
Design structure is complicated, needs to use sharp object to be stuck in locking nut and lock in the middle of shell when producing or during later maintenance
Operation or demolition and maintenance, during often occur sharp object scratch the bad problem such as aviation plug or not tight.
Summary of the invention
Technical assignment of the present utility model is to solve the deficiencies in the prior art, does not has dedicated lock clamping tool for aviation plug
And lock problem that is bad or that be easily scratched during locking, it is provided that a kind of aviation plug locking fixture, it is achieved aviation plug
Quick locking.
This utility model solves its technical problem and be the technical scheme is that
A kind of aviation plug locking fixture, including the frock body for connecting aviation plug and Spanner with aid, frock is originally
Body is one end open, the tube-in-tube structure of one end closing, the open end of frock body offers and aviation plug rat
The notch matched, when aviation plug inserts frock body, aviation plug and frock body plane-plane contact, the table of aviation plug
Face male cooperation inserts in the notch of frock body, and convex surfaces is the most outwards beyond the outer surface of frock body；Frock body
Closed End be further opened with the square hole that is used in combination with Spanner with aid.
On the basis of said structure, in order to make frock body preferably be plugged on the outside of aviation plug, frock body
On offer the number of the notch protruding number equal to described aviation plug surface, the projection on described aviation plug surface is the most relative
Insert in the notch that frock body is offered.
On the basis of said structure, in order to avoid damaging the projection on its surface, frock during locking aviation plug
The notch side of body is coated with neonychium, and the protruding side of aviation plug contacts with the neonychium of notch side.
Preferably, frock body selects No. 45 steel.
For realizing quick locking aviation plug, on frock body, the degree of depth of notch is less than the protruding length on aviation plug surface
Degree.
For realizing quick locking aviation plug, the degree of depth of frock body is less than the length of aviation plug.
A kind of aviation plug locking fixture of the present utility model compared with prior art produced by provide the benefit that:
This utility model is reasonable in design, simple in construction, by connecting aviation plug and Spanner with aid, it is achieved add at wire harness
When man-hour or later maintenance, the quick locking of aviation plug or dismounting, make aviation plug can reach the locking degree of standard, simultaneously
The damage in locking aviation plug, aviation plug caused can be prevented effectively from, solve the problem that aviation plug locking is bad；
Whole processing efficient, quick, the time-saving quality the most also having ensured aviation plug.
Accompanying drawing explanation
Accompanying drawing 1 is the structural representation of this utility model open end；
Accompanying drawing 2 is the structure left view after Fig. 1 removes neonychium；
Accompanying drawing 3 is the structure right view after Fig. 1 removes neonychium；
Accompanying drawing 4 is the end face structure figure of existing aviation plug.
In figure, each label represents:
1, frock body, 2, notch, 3, square hole, 4, neonychium；
A, aviation plug, B, aviation plug shell, C, projection.
Detailed description of the invention
Below in conjunction with the accompanying drawings 1,2,3,4, a kind of aviation plug locking fixture of the present utility model is described in detail below.
Embodiment one:
With reference to accompanying drawing 4, being the end face structure figure of conventional aviation plug A, aviation plug A surface has protruding C, and aviation is inserted
It is additionally provided with aviation plug shell B, according to the aviation plug A of this kind of structure, in order to realize the quick of aviation plug A outside head A
Locking, so design a kind of auxiliary aviation plug A locking frock, its be arranged on aviation plug A and aviation plug shell B it
Between, and can match with the protruding C on aviation plug A surface, concrete structure is as follows.
With reference to shown in accompanying drawing 1,2,3, a kind of aviation plug locking fixture of the present utility model, its structure includes for connecting
The frock body 1 of aviation plug A and Spanner with aid, frock body 1 selects No. 45 steel, frock body 1 to be one end open, one end
The tube-in-tube structure closed, the open end of frock body 1 offers the notch 2 matched with aviation plug A rat C,
And the number offering notch 2 on frock body 1 is equal to the protruding C number on aviation plug A surface, due to the convex of head plug surface of navigating
Playing C number is five, so also offering five notches 2 matched with protruding C on frock body 1.When aviation plug A inserts
During frock body 1, aviation plug A and frock body 1 plane-plane contact, the protruding C on aviation plug A surface inserts frock the most relatively
In the notch 2 that body 1 is offered, and protruding C Surface is the most outwards beyond the outer surface of frock body 1；The Closed End of frock body 1
It is further opened with the square hole 3 being used in combination with Spanner with aid.
In order to avoid damaging the protruding C on its surface during locking aviation plug A, the notch 2 side bag of frock body 1
Being covered with neonychium 4, the protruding C side of aviation plug A contacts with the neonychium 4 of notch 2 side.
Embodiment two:
On the architecture basics of embodiment one, for realizing quick locking aviation plug A, the degree of depth of notch 2 on frock body 1
Less than the protruding C length on aviation plug A surface, the degree of depth of frock body 1 length less than aviation plug A.Insert at aviation plug A
During entering frock body 1, the notch 2 that the protruding C on aviation plug A surface offers along frock body 1 slides into the most sliding
Till Dong, now, aviation plug A is not fully inserted in frock body 1, and the protruding C on aviation plug A surface is not the most entirely located in
In the notch 2 that frock body 1 is offered, when rotating Spanner with aid, the locking of aviation plug A can be realized very easily, and without
Adjust aviation plug A and stretch out the part of frock body 1, improve locking efficiency.
It should be noted that the number of notch 2 is not limited only to the number equal to aviation plug A rat C, notch 2
Number can also fewer of more than the protruding C number on aviation plug A surface, as long as aviation plug A insert frock body 1 and
Spanner with aid and frock body 1 with the use of and when inserting the square hole 3 of frock body 1, the protruding C on aviation plug A surface is positioned at
In the notch 2 of frock body 1.During use, under the effect of Spanner with aid, the notch 2 side extruding aviation of frock body 1
The protruding C on plug A surface, thus realize the locking of aviation plug A.
It should be noted that after use this utility model, cause during the most effectively avoiding locking aviation plug A
Scuffing, damage, the bad problem such as not tight, also improve work efficiency, the average time locking each aviation plug A is permissible
Saving five minutes, installation, dismounting operation to aviation plug A have the biggest practicality.
Last it should be noted that, above content is only in order to illustrate the technical solution of the utility model, rather than to this practicality
The restriction of novel protected scope, although this utility model has been made to explain by this detailed description of the invention part, this area
It is to be appreciated by one skilled in the art that the technical solution of the utility model can be modified or equivalent, without deviating from
The spirit and scope of technical solutions of the utility model.
Claims (6)
1. an aviation plug locking fixture, it is characterised in that include that the frock for connecting aviation plug and Spanner with aid is originally
Body, described frock body is one end open, the tube-in-tube structure of one end closing, and the open end of frock body offers and aviation
The notch that plug surface projection matches, when aviation plug inserts frock body, aviation plug and frock body plane-plane contact,
In the rat of aviation plug coordinates the notch inserting frock body, and convex surfaces is the most outwards beyond the appearance of frock body
Face；The Closed End of described frock body is further opened with the square hole being used in combination with Spanner with aid.
A kind of aviation plug locking fixture the most according to claim 1, it is characterised in that offer groove on described frock body
The number of mouth is equal to the protruding number on described aviation plug surface, and the projection on described aviation plug surface inserts frock the most relatively
In the notch that body is offered.
A kind of aviation plug locking fixture the most according to claim 1 and 2, it is characterised in that the groove of described frock body
Mouth side is coated with neonychium, and the protruding side of described aviation plug contacts with the neonychium of notch side.
A kind of aviation plug locking fixture the most according to claim 1 and 2, it is characterised in that described frock body is selected
No. 45 steel.
A kind of aviation plug locking fixture the most according to claim 1 and 2, it is characterised in that groove on described frock body
The degree of depth of mouth is less than the projection length on aviation plug surface.
A kind of aviation plug locking fixture the most according to claim 1 and 2, it is characterised in that described frock body deep
Degree is less than the length of aviation plug.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620527776.3U CN205666387U (en) | 2016-06-02 | 2016-06-02 | Aviation plug locking tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620527776.3U CN205666387U (en) | 2016-06-02 | 2016-06-02 | Aviation plug locking tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205666387U true CN205666387U (en) | 2016-10-26 |
Family
ID=57158450
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620527776.3U Expired - Fee Related CN205666387U (en) | 2016-06-02 | 2016-06-02 | Aviation plug locking tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205666387U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110581419A (en) * | 2019-09-24 | 2019-12-17 | 成都凯迪飞研科技有限责任公司 | High-reliability fastening device for rear accessory of aerial cable connector |
-
2016
- 2016-06-02 CN CN201620527776.3U patent/CN205666387U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110581419A (en) * | 2019-09-24 | 2019-12-17 | 成都凯迪飞研科技有限责任公司 | High-reliability fastening device for rear accessory of aerial cable connector |
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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: 20161026 Termination date: 20190602 |