CN212908306U - Easily install fastening formula aviation connector - Google Patents
Easily install fastening formula aviation connector Download PDFInfo
- Publication number
- CN212908306U CN212908306U CN202022397911.6U CN202022397911U CN212908306U CN 212908306 U CN212908306 U CN 212908306U CN 202022397911 U CN202022397911 U CN 202022397911U CN 212908306 U CN212908306 U CN 212908306U
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- CN
- China
- Prior art keywords
- public
- female
- mounting
- head
- left part
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- 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
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- 238000009434 installation Methods 0.000 claims abstract description 9
- 230000002742 anti-folding effect Effects 0.000 claims description 7
- 238000007789 sealing Methods 0.000 claims description 7
- 229920000715 Mucilage Polymers 0.000 claims 1
- 239000000853 adhesive Substances 0.000 claims 1
- 238000005096 rolling process Methods 0.000 claims 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 4
- 241001391944 Commicarpus scandens Species 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- Connector Housings Or Holding Contact Members (AREA)
Abstract
The utility model relates to an easily install fastening formula aviation connector, cooperate, two including public head and female head size public head passes through the sinle silk connection, two female head passes through the pencil and connects, public overhead left part and the mounting of being provided with, be provided with the kerve on the left part, the mounting passes through kerve and left part swing joint, be provided with inside groove and round hole on the mounting, female overhead right part including, be provided with the locating piece on the right part, mounting and left part and right part size cooperate, the sinle silk link up two public heads, the pencil link up two female heads. The utility model provides an easily install fastening formula aviation connector has practiced thrift installation time, and the installation is succinct convenient, has promoted the steadiness to inserting the port, reduces cracked risk after connector afterbody wire is bent many times, promotes the life of whole subassembly, and reinforcing connector public female head is joined in marriage and is inserted the leakproofness, satisfies the customer and to dustproof and waterproof's requirement.
Description
Technical Field
The utility model relates to a plug field, concretely relates to easily install fastening formula aviation connector.
Background
The aviation plug is one of connectors and is named after the military industry, namely aviation plug for short; the aviation plug comprises a male head and a female head; the adapter is a common adapter component in the circuit connection process, and has high requirements on stability and convenience.
The common connection mode of the male head and the female head of the plug at present is generally as follows: the plug-in connection, the threaded connection or the matching of the plug-in connection and the threaded connection are poor in stability, and the connection modes of the threaded connection, the plug-in connection and the threaded matching are troublesome and inconvenient to install; and the lead is easy to break off when being bent for many times, and the poor sealing property of the joint of the male head and the female head is easy to damp.
SUMMERY OF THE UTILITY MODEL
The utility model aims at: the fastening type aviation connector easy to install is provided, and the problems are solved.
In order to achieve the above object, the present invention provides the following technical solutions:
the utility model provides an easily install fastening formula aviation connector, cooperatees including public head and female head size, two public head passes through the sinle silk connection, two female head passes through the pencil and connects, public overhead left part and the mounting of being provided with, be provided with the kerve on the left part, the mounting passes through kerve and left part swing joint, be provided with inside groove and round hole on the mounting, female overhead right part including, be provided with the locating piece on the right part, the mounting cooperatees with left part and right part size, the sinle silk link up two public heads, the pencil link up two female heads.
Further, the outer groove is located the outside of a left part, public overhead being provided with prevents a piece, be provided with plug-in components on the sinle silk, the sinle silk and pencil outside all are connected with public head and female head respectively through the cementing piece, the mounting is located the outside of a left part.
Furthermore, prevent that a specifically is located the outside of sinle silk, the plug-in components have a plurality ofly, the sinle silk passes through plug-in components and pencil electric connection, be provided with the card limit on the mounting, inside groove and round hole intercommunication on the mounting, be provided with on the left part and prevent slow-witted.
Furthermore, prevent that a book is connected with public head and keeps away from the one end of preventing slow-witted piece, be provided with the slot on the pencil, the mounting passes through card limit and urceolus and a left part swing joint, the inside groove specifically is the heliciform, inside groove and round hole all have a plurality ofly.
Further, the anti-folding piece is specifically a spring, the wiring harness is electrically connected with the plug-in through the slot, and the male head is provided with a sealing piece; the inner grooves and the round holes are matched with the sizes of the positioning blocks and are corresponding in position.
The utility model has the advantages that: the utility model provides an easily install fastening formula aviation connector, through public head, female head, the mounting, the outer tank, left part, right side spare and prevent a piece and mutually support the use, realize spiral preventing slow-witted bayonet sealing connection, and the installation on the wire prevents the effect of a piece, the installation time has been practiced thrift, the installation is succinct convenient, the steadiness to inserting the port has been promoted, reduce cracked risk after connector afterbody wire is bent many times, promote the life of whole subassembly, strengthen the public female head of connector and join in marriage and insert the leakproofness, satisfy the customer and to dustproof and waterproof requirement.
Drawings
Figure 1 is the utility model relates to an easily install overall structure axonometric drawing of fastening formula aviation connector.
Figure 2 is the utility model relates to an easily install fastening formula aviation connector's partial structure axonometric drawing.
Fig. 3 is an axonometric view of another part of the structure of the fastening type aviation connector easy to install of the present invention.
Fig. 4 is another partial structural axonometric view of the fastening type aviation connector easy to install of the present invention.
Figure 5 is the utility model discloses a still partly structural axonometric drawing of easy installation fastening formula aviation connector.
In the figure: 1. a male head; 2. a wire core; 3. a plug-in; 4. a left part; 5. a fool-proof piece; 6. an outer tank; 7. a fixing member; 71. edge clamping; 72. an inner tank; 73. a circular hole; 8. a female head; 9. a right piece; 10. positioning blocks; 11. a wire harness; 12. a slot; 13. a seal member; 14. an anti-folding piece.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention will be further described in detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are for purposes of illustration only and are not intended to limit the invention.
Referring to fig. 1 to 5, an easy-to-install fastening type aviation connector comprises a male connector 1 and a female connector 8, and is characterized in that: the sizes of the male heads 1 are matched with those of the female heads 8, the two male heads 1 are connected through the wire core 2, the two female heads 8 are connected through the wire harness 11, the male head 1 is provided with a left part 4 and a fixing part 7, the left part 4 is provided with an outer groove 6, is used for being movably connected with a fixed part 7, the fixed part 7 is movably connected with the left part 4 through an outer groove 6, the fixing member 7 is provided with an inner groove 72 and a round hole 73 for mutually matching and installing and positioning the positioning block 10, thereby realizing convenient installation, stability and fixed connection of the male head 1 and the female head 8, the female head 8 comprises a right piece 9, the right piece 9 is provided with a positioning block 10, for inserting in round hole 73, thoroughly fix a position public head 1 and female head 8, mounting 7 cooperatees with left part 4 and right part 9 size, sinle silk 2 link up two public heads 1, pencil 11 link up two female heads 8.
The anti-bending piece 14 is specifically located on the outer side of the wire core 2 and used for preventing the wire core 2 from being broken after being bent for multiple times, the plug-in pieces 3 are multiple, the wire core 2 is electrically connected with the wire harness 11 through the plug-in pieces 3, the fixing piece 7 is provided with a clamping edge 71, an inner groove 72 and a round hole 73 in the fixing piece 7 are communicated, and the left piece 4 is provided with the fool-proof piece 5.
The anti-folding part 14 is connected with one end of the male head 1 far away from the fool-proof part 5, the wiring harness 11 is provided with a slot 12, the fixing part 7 is movably connected with the left part 4 through a clamping edge and an outer groove 6, the inner groove 72 is spiral, and the inner groove 72 and the round hole 73 are multiple.
The anti-folding piece 14 is specifically a spring, the wiring harness 11 is electrically connected with the plug-in 3 through the slot 12 and is used as a circuit, and the male head 1 is provided with a sealing piece 13 which is used for ensuring that the joint of the male head 1 and the female head 8 is sealed and cannot be damaged due to damp; the inner groove 72 and the round hole 73 are matched with the positioning block 10 in size and corresponding in position.
The utility model discloses a theory of operation does: when the use is started: firstly, inserting the fool-proof piece 5 into a fool-proof hole on the right piece 9 of the female head 8, completing the positioning of the male head 1 and the female head 8 at the moment, inserting the plug-in piece 3 on the wire core 2 into the slot 12 on the wire harness 11 in the process, and completing the electrical connection of the aviation plug at the moment; then the fixing element 7 is rotated manually to move towards the female head 8, in the process, the positioning block 10 on the right element 9 enters the inner groove 72, the positioning block 10 continuously moves in the inner groove 72 along with the continuous rotation of the fixing element 7, in the process, the fixing element 7 continuously approaches the female head 8 and reaches the outer side of the right element 9, finally the positioning block 10 is inserted into the round hole 73, the left element 4 tightly pushes the sealing element 13 in the female head 8, the sealing of the joint of the male head 1 and the female head 8 is completed, and the connection of the male head 1 and the female head 8 is completed.
The above examples are provided for further illustration of the present invention, but do not limit the present invention to these specific embodiments. Any modification, equivalent replacement, and improvement made within the spirit and principle of the present invention should be understood as being within the protection scope of the present invention.
Claims (5)
1. The utility model provides an easy installation fastening formula aviation connector, includes public head (1) and female head (8), its characterized in that: public first (1) and female first (8) size cooperate, two public first (1) is connected, two through sinle silk (2), female first (8) are connected through pencil (11), be provided with left part (4) and mounting (7) on public first (1), be provided with on the left side part (4) outer groove (6), mounting (7) are through outer groove (6) and left part (4) swing joint, be provided with inside groove (72) and round hole (73) on mounting (7), including right part (9) on female first (8), be provided with on the right side part (9) locating piece (10), mounting (7) cooperate with left part (4) and right part (9) size, sinle silk (2) link up two public first (1), two female first (8) are link up in 11).
2. An easy-to-install fastening aviation connector as claimed in claim 1, wherein: outer groove (6) are located the outside of left part (4), be provided with on public head (1) and prevent rolling over piece (14), be provided with plug-in components (3) on sinle silk (2), sinle silk (2) and pencil (11) outside all are connected with public head (1) and female head (8) respectively through the mucilage binding piece, mounting (7) are located the outside of left part (4).
3. An easy-to-install fastening aviation connector as claimed in claim 2, wherein: the anti-folding wire is characterized in that the anti-folding part (14) is specifically located on the outer side of the wire core (2), the plug-in part (3) is multiple, the wire core (2) is electrically connected with the wire harness (11) through the plug-in part (3), a clamping edge (71) is arranged on the fixing part (7), an inner groove (72) in the fixing part (7) is communicated with the round hole (73), and a fool-proof part (5) is arranged on the left part (4).
4. An easy-to-install fastening aviation connector as claimed in claim 3, wherein: prevent folding piece (14) and public head (1) and keep away from the one end of preventing slow-witted piece (5) and be connected, be provided with slot (12) on pencil (11), mounting (7) are through card limit and outer tank (6) and left part (4) swing joint, inside groove (72) specifically are the heliciform, inside groove (72) and round hole (73) all have a plurality ofly.
5. An easy-to-install fastening aviation connector as claimed in claim 4, wherein: the anti-folding piece (14) is specifically a spring, the wiring harness (11) is electrically connected with the plug-in piece (3) through a slot (12), and a sealing piece (13) is arranged on the male head (1); the inner groove (72) and the round hole (73) are matched with the positioning block (10) in size and correspond to each other in position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022397911.6U CN212908306U (en) | 2020-10-26 | 2020-10-26 | Easily install fastening formula aviation connector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022397911.6U CN212908306U (en) | 2020-10-26 | 2020-10-26 | Easily install fastening formula aviation connector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212908306U true CN212908306U (en) | 2021-04-06 |
Family
ID=75260943
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022397911.6U Expired - Fee Related CN212908306U (en) | 2020-10-26 | 2020-10-26 | Easily install fastening formula aviation connector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212908306U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113178757A (en) * | 2021-04-14 | 2021-07-27 | 镇江南方电子有限公司 | Multi-core radio frequency coaxial connector with fool-proof structure |
-
2020
- 2020-10-26 CN CN202022397911.6U patent/CN212908306U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113178757A (en) * | 2021-04-14 | 2021-07-27 | 镇江南方电子有限公司 | Multi-core radio frequency coaxial connector with fool-proof structure |
| CN113178757B (en) * | 2021-04-14 | 2022-04-15 | 镇江南方电子有限公司 | Multi-core radio frequency coaxial connector with fool-proof structure |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210406 |