CN216085525U - Install straight-through aviation connector fast - Google Patents
Install straight-through aviation connector fast Download PDFInfo
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- CN216085525U CN216085525U CN202122810449.2U CN202122810449U CN216085525U CN 216085525 U CN216085525 U CN 216085525U CN 202122810449 U CN202122810449 U CN 202122810449U CN 216085525 U CN216085525 U CN 216085525U
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- butt joint
- connecting pipe
- clamping
- joint part
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Abstract
The utility model provides a rapid installation straight-through aviation connector which comprises a rubber core, wherein a first connecting pipe and a second connecting pipe are respectively installed at two ends of the rubber core; the rubber core comprises a middle body part, and a first butt joint part and a second butt joint part are respectively arranged on two sides of the middle body part; the periphery of the first butt joint part is provided with a plurality of first protruding clamping point parts, the middle body part is provided with a first clamping part, the inner side of one end, butted with the first butt joint part, of the first connecting pipe is provided with a plurality of first guide grooves, and the butted end of the first connecting pipe extends outwards to form a first clamping groove part; the periphery of the second butt joint part is provided with a plurality of second protruding clamping point parts, the middle body part is provided with a second clamping part, the inner side of one end, butted with the second butt joint part, of the second connecting pipe is provided with a plurality of second guide grooves, and the butted end of the second connecting pipe extends outwards to form a second clamping groove part. The quick-installation straight-through aviation connector has the advantages of being quick and convenient to install, free of loosening problems after installation and the like.
Description
Technical Field
The utility model relates to a connector, in particular to a quick-mounting straight-through aviation connector.
Background
At present, all the straight-through connectors are connected by threads, and the installation efficiency is low during installation; and the screw thread has the hidden trouble of not tightly twisting, so that certain potential safety hazard exists when the screw is used.
There is therefore a need for a new quick-install feedthrough aerospace connector that overcomes the above-mentioned problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome the defects of the prior art and provides a quick-mounting straight-through aviation connector which is quick and convenient to mount and free of loosening after mounting.
The utility model is realized by the following steps:
the utility model provides a rapid installation straight-through aviation connector which comprises a rubber core, wherein a first connecting pipe and a second connecting pipe are respectively installed at two ends of the rubber core;
an elastic terminal is arranged in the rubber core, a first cable and a second cable are respectively connected to the elastic terminal, the first cable penetrates out of the first connecting pipe, and the second cable penetrates out of the second connecting pipe;
the rubber core comprises a middle body part, a first butt joint part and a second butt joint part are respectively arranged on two sides of the middle body part, and the middle body part, the first butt joint part and the second butt joint part are coaxially arranged;
a plurality of first protruding clamping point parts are arranged on the periphery of the first butt joint part, a first clamping part is arranged on one side, facing the first butt joint part, of the middle body part, a plurality of first guide grooves are formed in the inner side of one butt joint end of the first connecting pipe and the first butt joint part, and a first clamping groove part extends outwards from the butt joint end of the first connecting pipe; the first guide grooves and the first protruding clamping point parts are arranged in a one-to-one correspondence mode, and the first clamping groove parts are fixed with the first clamping parts;
a plurality of second protruding clamping point parts are arranged on the periphery of the second butt joint part, a second clamping part is arranged on one side, facing the second butt joint part, of the middle body part, a plurality of second guide grooves are formed in the inner side of one end, butted with the second butt joint part, of the second connecting pipe, and a second clamping groove part extends outwards from the butted end of the second connecting pipe; the second guide groove and the second protruding clamping point part are arranged in a one-to-one correspondence mode, and the second clamping groove part is fixed with the second clamping part.
Further, install first waterproof circle and second waterproof circle on the first butt joint portion, install third waterproof circle and fourth waterproof circle on the second butt joint portion.
Furthermore, a first clamping plate extends outwards from the butt joint end of the first connecting pipe, and the first clamping groove is positioned on the first clamping plate; and a second clamping plate extends outwards from the butt joint end of the second connecting pipe, and the second clamping groove is positioned on the second clamping plate.
Furthermore, a first tail cover is arranged on the rear side of the first connecting pipe, and the first cable sequentially penetrates through the first connecting pipe and the first tail cover; the rear side of the second connecting pipe is provided with a second tail cover, and the second cable sequentially penetrates through the second connecting pipe and the second tail cover.
Further, the number of the first protruding clamping point parts and the number of the first guide grooves are three, and the three first protruding clamping point parts are uniformly distributed on the same annular outer peripheral side of the first butt joint part.
Further, the number of the second protruding clamping point parts and the number of the second guide grooves are three, and the three second protruding clamping point parts are uniformly distributed on the same annular outer peripheral side of the second butt joint part.
The utility model has the following beneficial effects:
the rapid installation straight-through aviation connector provided by the utility model is matched with the protruding clamping point part through the arrangement of the guide groove, and the clamping groove part is matched with the clamping part, so that the connection and fixation of the rubber core, the first connecting pipe and the second structure are realized, the installation is rapid and convenient, and the phenomenon of loosening cannot easily occur after the installation.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
FIG. 1 is an exploded view of a quick-install feedthrough aerospace connector provided by embodiments of the present invention;
fig. 2 is a perspective view of a first connection pipe according to an embodiment of the present invention;
FIG. 3 is a perspective view of a rubber core provided in an embodiment of the present invention;
FIG. 4 is a schematic structural diagram illustrating a first installation step of a quick-install feedthrough aviation connector provided in accordance with an embodiment of the present invention;
FIG. 5 is a schematic structural diagram of a second installation step of a quick installation feedthrough aviation connector provided in an embodiment of the present invention;
FIG. 6 is a perspective view of a quick-install feedthrough aviation connector provided in accordance with an embodiment of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the description of the present embodiment, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, or orientations or positional relationships which are conventionally placed when the products of the present invention are used, and are only for convenience of describing the present invention and simplifying the description, but do not indicate or imply that the device or element to be referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal", "vertical", "overhang" and the like do not imply that the components are required to be absolutely horizontal or overhang, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present embodiment, it should also be noted that, unless explicitly stated or limited otherwise, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in this particular embodiment may be specifically understood by those of ordinary skill in the art.
As shown in fig. 1 to 6, the utility model provides a quick-installation straight-through aircraft connector, which comprises a rubber core, wherein a first connecting pipe 4 and a second connecting pipe 5 are respectively installed at two ends of the rubber core, and the first connecting pipe 4 and the second connecting pipe 5 have the same structure.
An elastic terminal is arranged in the rubber core, a first cable 6 and a second cable 7 are respectively connected to the elastic terminal, the first cable 6 penetrates out of the first connecting pipe 4, and the second cable 7 penetrates out of the second connecting pipe 5. The elastic terminal is provided with two elastic contact parts for respectively connecting and fixing the first cable 6 and the second cable 7, thereby realizing electric conduction.
The rubber core comprises a middle body part 1, a first butt joint part 2 and a second butt joint part 3 are respectively arranged on two sides of the middle body part 1, and the middle body part 1, the first butt joint part 2 and the second butt joint part 3 are coaxially arranged. The first butt joint part 2 is used for being connected with the first adapter 4, and the second butt joint part 3 is used for being connected with the second adapter 5. In the preferred embodiment, the first butt joint portion 2 is mounted with a first waterproof ring 13 and a second waterproof ring 14, and the second butt joint portion 3 is mounted with a third waterproof ring 15 and a fourth waterproof ring 16. After two takeover and two butt joint portions are connected the completion respectively, first waterproof circle 13 with second waterproof circle 14 all butt extremely the inside of first takeover 4, third waterproof circle 15 with fourth waterproof circle 16 all butt extremely the inside of second takeover 5 to have good water-proof effects.
As shown in fig. 1 to 6, the first butt joint portion 2 is provided at an outer periphery thereof with a plurality of first protruding click portions 21. A first buckling part 11 is arranged on one side of the middle body part 1 facing the first butt joint part 2, a plurality of first guide grooves 42 are arranged on the inner side of one end of the first connecting pipe 4 in butt joint with the first butt joint part 2, and a first clamping groove part 41 extends outwards from the butt joint end of the first connecting pipe 4; the first guide grooves 42 and the first protruding click portions 21 are arranged in a one-to-one correspondence manner, specifically, the number of the first protruding click portions 21 and the number of the first guide grooves 42 are three, the three first protruding click portions 21 are uniformly distributed on the same annular outer peripheral side of the first butt-joint portion 2, that is, the three first protruding click portions 21 are concentrically arranged, and the first click portion 41 is fixed with the first click portion 11; in the preferred embodiment, a first locking plate 43 extends outward from the abutting end of the first adapter 4, and the first locking groove portion 41 is located on the first locking plate 43. During the installation, correspond protrusion stuck point portion and guide way, then make butt joint portion and takeover butt joint, rotatory certain angle then makes the bayonet catch portion and buckle looks buckle fixed, can make butt joint portion and takeover firm the linking together, can not take place the phenomenon that the pine takes off.
The periphery of the second docking portion 3 is provided with a plurality of second protruding click portions 31. A second buckling part 12 is arranged on one side of the middle body part 1 facing the second butt joint part 3, a plurality of second guide grooves are arranged on the inner side of one end, butted with the second butt joint part 3, of the second connecting pipe 5, and a second clamping groove part extends outwards from the butted end of the second connecting pipe 5; the second guide grooves and the second protruding click portions 31 are arranged in a one-to-one correspondence manner, specifically, the number of the second protruding click portions 31 and the number of the second guide grooves are three, the three second protruding click portions 31 are uniformly distributed on the same annular peripheral side of the second butt joint portion 3, that is, the three second protruding click portions 31 are arranged concentrically. The second locking groove portion is fixed to the second locking portion 12. In the preferred embodiment, a second clamping plate extends outwards from the abutting end of the second adapter tube 5, and the second clamping groove is located on the second clamping plate.
Further, a first tail cover 8 is arranged at the rear side of the first connecting pipe 4, and the first cable 6 sequentially penetrates through the first connecting pipe 4 and the first tail cover 8; the rear side of the second connecting pipe 5 is provided with a second tail cover 9, and the second cable 7 sequentially penetrates through the second connecting pipe 5 and the second tail cover 9. The tail cap is provided for fixing the cable.
In the preferred embodiment, the second protruding click portion 31 has the same structure as the first protruding click portion 21, the second click portion has the same structure as the first click portion 41, the second click portion 12 has the same structure as the first click portion 11, and the second guide groove has the same structure as the first guide groove 42.
As shown in fig. 4 to 6, during installation, the second adapter tube 5 is fixed to the rubber core (step one shown in fig. 4), then the first adapter tube 4 is abutted to the rubber core, and then rotated by a certain angle (step two shown in fig. 5), so that the snap groove portion and the snap portion are fastened and fixed, the abutting portion and the adapter tube can be stably connected together, and the phenomenon of loosening is avoided (as shown in fig. 6, installation is completed).
In summary, the quickly-installed straight-through aviation connector provided by the utility model is provided with the guide groove matched with the protruding clamping point part, and the clamping groove part matched with the clamping part, so that the rubber core is connected and fixed with the first connecting pipe 4 and the second structure, the installation is quick and convenient, and the phenomenon of loosening cannot easily occur after the installation
The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the utility model, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.
Claims (6)
1. A quick-installation straight-through aviation connector is characterized by comprising a rubber core, wherein a first connecting pipe and a second connecting pipe are respectively installed at two ends of the rubber core;
an elastic terminal is arranged in the rubber core, a first cable and a second cable are respectively connected to the elastic terminal, the first cable penetrates out of the first connecting pipe, and the second cable penetrates out of the second connecting pipe;
the rubber core comprises a middle body part, a first butt joint part and a second butt joint part are respectively arranged on two sides of the middle body part, and the middle body part, the first butt joint part and the second butt joint part are coaxially arranged;
a plurality of first protruding clamping point parts are arranged on the periphery of the first butt joint part, a first clamping part is arranged on one side, facing the first butt joint part, of the middle body part, a plurality of first guide grooves are formed in the inner side of one butt joint end of the first connecting pipe and the first butt joint part, and a first clamping groove part extends outwards from the butt joint end of the first connecting pipe; the first guide grooves and the first protruding clamping point parts are arranged in a one-to-one correspondence mode, and the first clamping groove parts are fixed with the first clamping parts;
a plurality of second protruding clamping point parts are arranged on the periphery of the second butt joint part, a second clamping part is arranged on one side, facing the second butt joint part, of the middle body part, a plurality of second guide grooves are formed in the inner side of one end, butted with the second butt joint part, of the second connecting pipe, and a second clamping groove part extends outwards from the butted end of the second connecting pipe; the second guide groove and the second protruding clamping point part are arranged in a one-to-one correspondence mode, and the second clamping groove part is fixed with the second clamping part.
2. The quick-install pass-through aircraft connector of claim 1, wherein: install first waterproof circle and second waterproof circle on the first butt joint portion, install third waterproof circle and fourth waterproof circle on the second butt joint portion.
3. The quick-install pass-through aircraft connector of claim 1, wherein: a first clamping plate extends outwards from the butt joint end of the first connecting pipe, and the first clamping groove is positioned on the first clamping plate; and a second clamping plate extends outwards from the butt joint end of the second connecting pipe, and the second clamping groove is positioned on the second clamping plate.
4. The quick-install pass-through aircraft connector of claim 1, wherein: a first tail cover is arranged on the rear side of the first connecting pipe, and the first cable sequentially penetrates through the first connecting pipe and the first tail cover; the rear side of the second connecting pipe is provided with a second tail cover, and the second cable sequentially penetrates through the second connecting pipe and the second tail cover.
5. The quick-install pass-through aircraft connector of claim 1, wherein: the number of the first protruding clamping point parts and the number of the first guide grooves are three, and the three first protruding clamping point parts are uniformly distributed on the same annular peripheral side of the first butt joint part.
6. The quick-install pass-through aircraft connector of claim 1, wherein: the number of the second protruding clamping point parts and the number of the second guide grooves are three, and the three second protruding clamping point parts are uniformly distributed on the same annular peripheral side of the second butt joint part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122810449.2U CN216085525U (en) | 2021-11-17 | 2021-11-17 | Install straight-through aviation connector fast |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122810449.2U CN216085525U (en) | 2021-11-17 | 2021-11-17 | Install straight-through aviation connector fast |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216085525U true CN216085525U (en) | 2022-03-18 |
Family
ID=80661435
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122810449.2U Active CN216085525U (en) | 2021-11-17 | 2021-11-17 | Install straight-through aviation connector fast |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216085525U (en) |
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2021
- 2021-11-17 CN CN202122810449.2U patent/CN216085525U/en active Active
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