CN205376953U - Fixed aviation connector device - Google Patents
Fixed aviation connector device Download PDFInfo
- Publication number
- CN205376953U CN205376953U CN201521111826.1U CN201521111826U CN205376953U CN 205376953 U CN205376953 U CN 205376953U CN 201521111826 U CN201521111826 U CN 201521111826U CN 205376953 U CN205376953 U CN 205376953U
- Authority
- CN
- China
- Prior art keywords
- contact pin
- electric wire
- sleeve
- hole
- dividing plate
- 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
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- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
The utility model discloses a fixed aviation connector device, including casing, contact pin and electric wire, contact pin and electric wire in the casing, the baffle that the level that is fixed with in the casing set up, a plurality of jacks have on the baffle, the contact pin plug bush is in the jack, the lower part of contact pin is in the below of baffle, outside radial extension limit of extending has on the lower part lateral wall of contact pin, it presses on the bottom surface of baffle to extend the limit, the bottom middle part of contact pin has connecting insertion hole, the bottom lateral wall of contact pin has the external screw thread, the tip of electric wire has the connector, the middle part of connector has the spiro union hole, the bottom surface in spiro union hole has the protruding post in middle part, middle part protruding stake pocket cover and card are put in connecting insertion hole, the bottom spiro union of contact pin is in the spiro union hole. It is compact that it makes electric wire and contact pin be connected, can not become flexible, guarantees normal use.
Description
Technical field:
This utility model relates to electric elements technical field, more specifically to a kind of fixed Aviation Connector device.
Background technology:
Aviation plug is the electromechanical compo connecting electric wiring.The connected mode of its contact pin of currently the majority aviation plug and electric wire often adopts welding manner, adopt human weld's efficiency low and the technical merit of workman is required height, labor intensity is big, quality is wayward, easily causing that not prison welding is solid, rosin joint, the problem such as loosen, severe patient occurs that sealing-off phenomenon causes open circuit in use.
Utility model content:
The purpose of this utility model is to overcome the deficiencies in the prior art, it is provided that a kind of fixed Aviation Connector device, it is compact that it makes electric wire be connected with contact pin, will not loosen, it is ensured that normally use.
This utility model solves the scheme of described technical problem:
A kind of fixed Aviation Connector device, including housing, contact pin and electric wire, contact pin and electric wire are in housing, described housing is fixed with horizontally disposed dividing plate, dividing plate has multiple jack, contact pin sleeve is in jack, the bottom of contact pin is in the lower section of dividing plate, the lower outside wall of contact pin has the extension edge extended radially outwards, extension edge is pressed against on the bottom surface of dividing plate, the center bottom of contact pin has connection jack, the Basolateral wall of contact pin has external screw thread, the end of electric wire has union joint, the middle part of union joint has bolt apertures, the bottom surface of bolt apertures has the protruding post in middle part, the protruding post sleeve in middle part holding are in connecting jack, the bottom of contact pin is screwed onto in bolt apertures.
There is in the middle part of the bottom surface of described dividing plate the joint pin downwardly extended, the middle part of bottom resilient holding block has through hole, the medial wall of through hole has holding shrinkage pool, the bottom sidewall of joint pin has lobe, joint pin sleeve holding are in through-holes, the lobe holding of joint pin is in corresponding holding shrinkage pool, and the upper surface of bottom resilient holding block is pressed against on the bottom surface of dividing plate.
The end face of described bottom resilient holding block has the bottom sleeve of connecting groove, union joint and contact pin in corresponding connecting groove, and the bottom face of union joint is pressed against on the bottom surface of connecting groove.
The bottom surface of described connecting groove has electric wire through-hole, and electric wire sleeve is in electric wire through-hole.
The bottom inside wall of the electric wire through-hole of described bottom resilient holding block has the main groove of connection, and annular sleeve holding is in connecting main groove, and electric wire sleeve is in annular sleeve.
Prominent effect of the present utility model is:
Compared with prior art, it is compact that it makes electric wire be connected with contact pin, will not loosen, it is ensured that normally use.
Accompanying drawing illustrates:
Fig. 1 is structural representation of the present utility model；
Fig. 2 is partial enlarged drawing of the present utility model.
Detailed description of the invention:
nullEmbodiment，See as shown in Figure 1 to Figure 2，A kind of fixed Aviation Connector device，Including housing 100、Contact pin 1 and electric wire 2，Contact pin 1 and electric wire 2 are in housing 100，Described housing 100 is fixed with horizontally disposed dividing plate 10，Dividing plate 10 has multiple jack 11，Contact pin 1 sleeve is in jack 11，The bottom of contact pin 1 is in the lower section of dividing plate 10，The lower outside wall of contact pin 1 has the extension edge 121 extended radially outwards，Extension edge 121 is pressed against on the bottom surface of dividing plate 10，The center bottom of contact pin 1 has connection jack 122，The Basolateral wall of contact pin 1 has external screw thread，The end of electric wire 2 has union joint 21，The middle part of union joint 21 has bolt apertures 22，The bottom surface of bolt apertures 22 has the protruding post 23 in middle part，Protruding post 23 sleeve in middle part holding are in connecting jack 122，The bottom of contact pin 1 is screwed onto in bolt apertures 22.
Further, there is in the middle part of the bottom surface of described dividing plate 10 joint pin 13 downwardly extended, the middle part of bottom resilient holding block 3 has through hole 31, the medial wall of through hole 31 has holding shrinkage pool 32, the bottom sidewall of joint pin 13 has lobe 131, joint pin 13 sleeve holding are in through hole 31, and lobe 131 holding of joint pin 13 is in corresponding holding shrinkage pool 32, and the upper surface of bottom resilient holding block 3 is pressed against on the bottom surface of dividing plate 10.
Further, the end face of described bottom resilient holding block 3 has connecting groove 33, and the bottom sleeve of union joint 21 and contact pin 1 is in corresponding connecting groove 33, and the bottom face of union joint 21 is pressed against on the bottom surface of connecting groove 33.
Further, the bottom surface of described connecting groove 33 has electric wire through-hole 34, and electric wire 2 sleeve is in electric wire through-hole 34.
Further, the bottom inside wall of the electric wire through-hole 34 of described bottom resilient holding block 3 has the main groove 35 of connection, and annular sleeve 36 holding is in connecting main groove 35, and electric wire 2 sleeve is in annular sleeve 36.
Operation principle: being threadeded with contact pin 1 by union joint 21, it is connected firmly, meanwhile, the position realizing contact pin 1 by bottom resilient holding block 3 is fixed, thus ensureing that contact pin 1 is on dividing plate 10 and does not fall out, it is ensured that properly functioning during grafting.
Finally; embodiment of above is merely to illustrate this utility model; and be not limitation of the utility model; those of ordinary skill about technical field; when without departing from spirit and scope of the present utility model; can also making a variety of changes and modification, therefore all equivalent technical schemes fall within category of the present utility model, and scope of patent protection of the present utility model should be defined by the claims.
Claims (5)
- null1. a fixed Aviation Connector device，Including housing (100)、Contact pin (1) and electric wire (2)，Contact pin (1) and electric wire (2) are in housing (100)，It is characterized in that: described housing (100) is fixed with horizontally disposed dividing plate (10)，Dividing plate (10) has multiple jack (11)，Contact pin (1) sleeve is in jack (11)，The bottom of contact pin (1) is in the lower section of dividing plate (10)，The lower outside wall of contact pin (1) has the extension edge (121) extended radially outwards，Extension edge (121) is pressed against on the bottom surface of dividing plate (10)，The center bottom of contact pin (1) has connection jack (122)，The Basolateral wall of contact pin (1) has external screw thread，The end of electric wire (2) has union joint (21)，The middle part of union joint (21) has bolt apertures (22)，The bottom surface of bolt apertures (22) has the protruding post (23) in middle part，Protruding post (23) sleeve in middle part holding are in connecting jack (122)，The bottom of contact pin (1) is screwed onto in bolt apertures (22).
- 2. the fixed Aviation Connector device of one according to claim 1, it is characterized in that: there is in the middle part of the bottom surface of described dividing plate (10) joint pin (13) downwardly extended, the middle part of bottom resilient holding block (3) has through hole (31), the medial wall of through hole (31) has holding shrinkage pool (32), the bottom sidewall of joint pin (13) has lobe (131), joint pin (13) sleeve holding are in through hole (31), lobe (131) holding of joint pin (13) is in corresponding holding shrinkage pool (32), the upper surface of bottom resilient holding block (3) is pressed against on the bottom surface of dividing plate (10).
- 3. the fixed Aviation Connector device of one according to claim 2, it is characterized in that: the end face of described bottom resilient holding block (3) has connecting groove (33), the bottom sleeve of union joint (21) and contact pin (1) is in corresponding connecting groove (33), and the bottom face of union joint (21) is pressed against on the bottom surface of connecting groove (33).
- 4. the fixed Aviation Connector device of one according to claim 3, it is characterised in that: the bottom surface of described connecting groove (33) has electric wire through-hole (34), and electric wire (2) sleeve is in electric wire through-hole (34).
- 5. the fixed Aviation Connector device of one according to claim 4, it is characterized in that: the bottom inside wall of the electric wire through-hole (34) of described bottom resilient holding block (3) has the main groove of connection (35), annular sleeve (36) holding is in connecting main groove (35), and electric wire (2) sleeve is in annular sleeve (36).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521111826.1U CN205376953U (en) | 2015-12-29 | 2015-12-29 | Fixed aviation connector device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521111826.1U CN205376953U (en) | 2015-12-29 | 2015-12-29 | Fixed aviation connector device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205376953U true CN205376953U (en) | 2016-07-06 |
Family
ID=56257637
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521111826.1U Expired - Fee Related CN205376953U (en) | 2015-12-29 | 2015-12-29 | Fixed aviation connector device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205376953U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105490111A (en) * | 2015-12-29 | 2016-04-13 | 苏州卓德电子有限公司 | Fixed aviation connector device |
-
2015
- 2015-12-29 CN CN201521111826.1U patent/CN205376953U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105490111A (en) * | 2015-12-29 | 2016-04-13 | 苏州卓德电子有限公司 | Fixed aviation connector device |
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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: 20160706 Termination date: 20161229 |