CN210806188U - Aviation plug - Google Patents

Aviation plug Download PDF

Info

Publication number
CN210806188U
CN210806188U CN201921984030.5U CN201921984030U CN210806188U CN 210806188 U CN210806188 U CN 210806188U CN 201921984030 U CN201921984030 U CN 201921984030U CN 210806188 U CN210806188 U CN 210806188U
Authority
CN
China
Prior art keywords
sub
joint
lantern ring
groove
connector
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
Application number
CN201921984030.5U
Other languages
Chinese (zh)
Inventor
董亚勇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201921984030.5U priority Critical patent/CN210806188U/en
Application granted granted Critical
Publication of CN210806188U publication Critical patent/CN210806188U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Details Of Connecting Devices For Male And Female Coupling (AREA)

Abstract

The utility model relates to an electricity connects technical field, concretely relates to aviation plug. Including son joint and female joint, the spout has been seted up to son joint outer fringe bilateral symmetry, female joint outer fringe bilateral symmetry is fixed with the fixed strip, the fixed strip corresponds with the spout, the fixed strip is located the spout, perpendicular groove has been seted up to the terminal surface upper end that the fixed strip connects to the son dorsad, the arc wall has been seted up on the fixed strip of perpendicular groove one side, arc wall and perpendicular groove lower extreme intercommunication, the cover is equipped with rather than sliding fit's last lantern ring on the son joint, it is fixed with the fixed column to go up lantern ring inner edge bilateral symmetry, the fixed column is located the spout, threaded connection has the lower lantern ring on the son joint of going up lantern ring below, the circumrotate the rotation direction of going upward the lower lantern ring is the same with the. The utility model discloses, simple structure, the son connects and female joint is connected conveniently, and the connection back stability can be good, has improved the stability of plug bush, contact pin, can prevent effectively that son connects and female joint from droing.

Description

Aviation plug
Technical Field
The utility model relates to an electricity connects technical field, concretely relates to aviation plug.
Background
The aviation plug is one of connectors, originates from the military industry, is named as aviation plug for short, and is commonly called large DIN in the industry. The aviation plug has the main function of connecting a power supply or a signal, particularly connecting a wiring harness with a large number of cores by using the aviation plug socket, and has the advantages of safety, reliability, convenience in operation and more attractiveness.
The mode of the sub-joint of general stable behind current aviation plug installation and female joint is for through lantern ring threaded connection, and the lantern ring pin joint is on the sub-joint promptly, then makes lantern ring and female joint threaded connection, above-mentioned connection process, appears sub-joint and female joint slope easily, the problem that the lantern ring can not be connected with the female joint, and the phenomenon of wrong silk appears easily in the lantern ring and the female joint simultaneously.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that a simple structure, simple to operate connects stable aviation plug.
In order to realize the purpose, the utility model provides a technical scheme is:
the utility model provides an aviation plug, including sub-joint and the female joint of mutually supporting, the spout has been seted up to sub-joint outer fringe bilateral symmetry, female joint outer fringe bilateral symmetry is fixed with the fixed strip, the fixed strip corresponds with the spout, the fixed strip is located the spout, the vertical groove has been seted up to the terminal surface upper end of fixed strip dorsad sub-joint, the arc wall has been seted up on the fixed strip of vertical groove one side, arc wall and vertical groove lower extreme intercommunication, vertical groove and arc wall on two fixed strips are according to the axle center central symmetry of sub-joint, the cover is equipped with rather than sliding fit's last lantern ring on the sub-joint, it is fixed with the fixed column to go up lantern ring inner edge bilateral symmetry, the fixed column is located the spout, threaded connection has the lower lantern ring on the sub-joint of last lantern ring below, the rotation direction of lower lantern ring.
Specifically, the lower end of the sub-joint is provided with a convex column concentric with the sub-joint, a first groove is formed in the convex column, a plurality of plug bushes electrically connected with the electric wires on the sub-joint are fixed in the first groove, a second groove is formed in the upper end of the female joint, the convex column is located in the second groove, a plurality of contact pins electrically connected with the electric wires on the female joint are fixed in the second groove, the contact pins correspond to the plug bushes, and the contact pins are inserted in the plug bushes.
Specifically, the fixing strip is in sliding contact with a groove wall of the sliding groove where the fixing strip is located.
Specifically, the arc-shaped groove is concentric with the sub-joint.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model discloses, simple structure, the son connects and female joint is connected conveniently, and the connection back stability can be good, has improved the stability of plug bush, contact pin, can prevent effectively that son connects and female joint from droing.
Drawings
Fig. 1 is a schematic structural diagram of the present invention.
Fig. 2 is a side view of the mating of a male sub with a female sub.
FIG. 3 is a schematic view of the structure of the female and male connectors after connection.
Detailed Description
As shown in fig. 1-3, an aviation plug comprises a sub connector 1 and a female connector 2 which are matched with each other, wherein a convex column 3 concentric with the sub connector 1 is arranged at the lower end of the sub connector 1, a first groove 4 is formed in the convex column 3, a plurality of plug bushes 6 electrically connected with wires on the sub connector 1 are fixed in the first groove 4, a second groove 7 is formed in the upper end of the female connector 2, the convex column 3 is located in the second groove 7, a plurality of contact pins 5 electrically connected with the wires on the female connector 2 are fixed in the second groove 7, the contact pins 5 correspond to the plug bushes 6, and the contact pins 5 are inserted in the plug bushes 6.
The two sides of the outer edge of the sub-joint 1 are symmetrically provided with sliding chutes 9, the two sides of the outer edge of the female joint 2 are symmetrically fixed with fixing strips 8, the fixing strips 8 correspond to the sliding chutes 9, the fixing strips 8 are positioned in the sliding chutes 9, the fixed strip 8 is in sliding contact with the groove wall of the sliding groove 9 where the fixed strip is positioned, the upper end of the end surface of the fixed strip 8, which is back to the sub-joint 1, is provided with a vertical groove 13, the fixed strip 8 at one side of the vertical groove 13 is provided with an arc-shaped groove 14, the arc-shaped groove 14 is concentric with the sub-joint 1, the arc-shaped groove 14 is communicated with the lower end of the vertical groove 13, the vertical groove 13 and the arc-shaped groove 14 on the two fixing strips 8 are symmetrical according to the center of the axis of the sub-joint 1, the sub-joint 1 is sleeved with an upper lantern ring 11 in sliding fit with the sub-joint 1, fixing columns 12 are symmetrically fixed on two sides of the inner edge of the upper lantern ring 11, the fixing columns 12 are located in the sliding grooves 9, a lower lantern ring 10 is connected to the sub-joint 1 below the upper lantern ring 11 in a threaded mode, and the rotating direction of the lower lantern ring 10 in the rotating upward direction is the same.
When the utility model is used, the fixing strip 8 corresponds to the sliding groove 9, then the convex column 3 of the sub-joint 1 is inserted into the second groove 7 of the main joint 2, at the moment, the inserting needle 5 is inserted into the inserting sleeve 6, under the matching action of the fixing strip 8 and the sliding groove 9, the main joint 2 and the sub-joint 1 can be positioned when being inserted, further, the inserting needle 5 can be correctly inserted into the inserting sleeve 6, then, the fixing column 12 at the inner edge of the upper sleeve ring 11 corresponds to the vertical groove 13 on the fixing strip 8, the upper sleeve ring 11 descends, the fixing column 12 enters the bottom of the vertical groove 13 and then rotates the upper sleeve ring 10, the fixing column 12 is positioned in the arc-shaped groove 14, the lower sleeve ring 10 is screwed to spirally ascend, when the lower sleeve ring 10 tightly abuts against the upper sleeve ring 11, the fixing strip 8 on the main joint 2 is stabilized in the sliding groove 9 of the sub-joint 1, further, the main joint 2 and the sub-joint 1 are stabilized, because the rotating direction of the lower sleeve ring 10 is the same as the extending direction of, therefore, when the lower sleeve ring 10 is screwed up and tightly pressed against the upper sleeve ring 11, the fixing posts 12 on the inner edge of the upper sleeve ring 11 are not withdrawn from the arc-shaped grooves 14.
The above description is only exemplary of the present invention and should not be taken as limiting the scope of the present invention, as any modifications, equivalents, improvements and the like made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims (4)

1. An aviation plug comprises a sub-connector (1) and a female connector (2) which are matched with each other, and is characterized in that sliding grooves (9) are symmetrically formed in two sides of the outer edge of the sub-connector (1), fixing strips (8) are symmetrically fixed on two sides of the outer edge of the female connector (2), the fixing strips (8) correspond to the sliding grooves (9), the fixing strips (8) are located in the sliding grooves (9), vertical grooves (13) are formed in the upper ends, back to the sub-connector (1), of the fixing strips (8), arc-shaped grooves (14) are formed in the fixing strips (8) on one sides of the vertical grooves (13), the arc-shaped grooves (14) are communicated with the lower ends of the vertical grooves (13), the vertical grooves (13) and the arc-shaped grooves (14) in the two fixing strips (8) are symmetrical according to the center of the axis of the sub-connector (1), an upper lantern ring (11) in sliding fit with the sub-connector (1) is sleeved on the sub, the fixed column (12) is positioned in the sliding groove (9), the sub-joint (1) below the upper lantern ring (11) is connected with a lower lantern ring (10) in a threaded mode, and the rotating direction of the lower lantern ring (10) in the rotating upward direction is the same as the extending direction of one end, away from the vertical groove (13), of the arc-shaped groove (14).
2. The aviation plug as claimed in claim 1, wherein the lower end of the sub-connector (1) is provided with a convex pillar (3) concentric with the sub-connector, a first groove (4) is formed in the convex pillar (3), a plurality of plug bushes (6) electrically connected with the wires on the sub-connector (1) are fixed in the first groove (4), a second groove (7) is formed in the upper end of the female connector (2), the convex pillar (3) is located in the second groove (7), a plurality of contact pins (5) electrically connected with the wires on the female connector (2) are fixed in the second groove (7), the contact pins (5) correspond to the plug bushes (6), and the contact pins (5) are inserted in the plug bushes (6).
3. An aircraft plug according to claim 1, characterised in that the fixing strip (8) is in sliding contact with the wall of the slot (9) in which it is located.
4. An aircraft plug according to claim 1, characterised in that the arcuate slot (14) is concentric with the sub-connector (1).
CN201921984030.5U 2019-11-18 2019-11-18 Aviation plug Expired - Fee Related CN210806188U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921984030.5U CN210806188U (en) 2019-11-18 2019-11-18 Aviation plug

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921984030.5U CN210806188U (en) 2019-11-18 2019-11-18 Aviation plug

Publications (1)

Publication Number Publication Date
CN210806188U true CN210806188U (en) 2020-06-19

Family

ID=71226365

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921984030.5U Expired - Fee Related CN210806188U (en) 2019-11-18 2019-11-18 Aviation plug

Country Status (1)

Country Link
CN (1) CN210806188U (en)

Similar Documents

Publication Publication Date Title
US6227883B1 (en) Electric combination socket
CN205790687U (en) A kind of adapter
CN202662907U (en) Plug and socket for central screw-located micro rectangular electric connectors
CN210806188U (en) Aviation plug
CN205029067U (en) Binding post connector
CN201126892Y (en) Explosion-proof inserted apparatus
CN201927758U (en) Adaptor
CN205376907U (en) Electric connector
CN209561771U (en) A kind of anti-error electric connector of rectangle high frequency integrated form
CN208489409U (en) A kind of plug for electric energy meter RS485 communication
CN210779103U (en) Push-pull circular electric connector
CN209561772U (en) A kind of high frequency integrated form Anti-misplugging electric connector
CN209592389U (en) A kind of ready-package waterproof connector
CN208753659U (en) A kind of novel electric connector
CN108336531B (en) Socket, plug, wiring board and electric device
CN206163830U (en) Connector joint structure
CN206340719U (en) A kind of Mini USB connectors
CN206134997U (en) Exempt from spiral shell formula grafting external member
CN205863577U (en) A kind of modularity is to socket, connector
CN205693072U (en) A kind of electric wiring fast connecting terminal
CN216251318U (en) Waterproof halogen-free DC threaded female socket
CN211743602U (en) Multi-head connector for lamp tube
CN202564730U (en) Electric connector
CN215008814U (en) Automobile ignition clamp male and female seats
CN217983893U (en) Novel plug connector

Legal Events

Date Code Title Description
GR01 Patent grant
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: 20200619

Termination date: 20201118