CN214335023U

CN214335023U - Aviation connector contact pin electric conductivity detection device

Info

Publication number: CN214335023U
Application number: CN202120315288.7U
Authority: CN
Inventors: 陈春香
Original assignee: Shenzhen Wanmingxin Electronic Technology Co ltd
Current assignee: Shenzhen Wanmingxin Electronic Technology Co ltd
Priority date: 2021-02-03
Filing date: 2021-02-03
Publication date: 2021-10-01
Anticipated expiration: 2031-02-03

Abstract

The utility model relates to the technical field of electronic components, in particular to an aviation connector contact pin conductivity detection device, which comprises a base, wherein a slide rail is fixedly arranged on the base, a slide seat is arranged on the slide rail in a sliding manner, a clamp is fixedly arranged on the slide seat, a movable arm is fixedly arranged on the slide seat, a driving rod is fixedly arranged on the movable arm, a rack is arranged on the driving rod, a supporting wheel is rotatably arranged in the base, a through groove is arranged on the base, a speed reducing spring is fixedly arranged on the base, and a driving gear is rotatably arranged in the base; through the base for major structure, through drive gear's rotation during the use, with the rack toothing on the actuating lever, can drive two digging arm reverse motion to through digging arm control anchor clamps, carry out the centre gripping through anchor clamps or release, with automatic effectual fixed of carrying out aviation connector, liberation detector's both hands are convenient for carry out the detection of stable accurate contact pin electric conductive property.

Description

Aviation connector contact pin electric conductivity detection device

Technical Field

The utility model relates to an electronic component technical field specifically is aviation connector contact pin electric conductive property detection device.

Background

Aviation connectors are one type of connector, originating from the military industry. Aeronautical connectors are electromechanical elements that connect electrical lines, and therefore their own electrical parameters are the first consideration in selecting an aeronautical connector, the correct selection and use of which is an important aspect in ensuring the reliability of the circuit.

When the aviation connector is used and the aviation connector is subjected to factory inspection, the conductivity of a contact pin of the aviation connector needs to be detected so as to ensure the normal use of the aviation connector. However, there is no means for fixing the connector effectively, and it is difficult for one person to keep the connector stable and perform the test by hand, and the shaking of the connector may cause the test result to lose accuracy. In view of this, we propose an aviation connector pin conductivity detection device.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an aviation connector contact pin electric conductive property detection device to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: aviation connector contact pin electric conductive property detection device, the on-line screen storage device comprises a base, fixed mounting has the slide rail on the base, and slidable mounting has the slide on the slide rail, fixed mounting has anchor clamps on the slide, and fixed mounting has the digging arm on the slide, fixed mounting has the actuating lever on the digging arm, and is provided with the rack on the actuating lever, the supporting wheel is installed in the rotation in the base, and is provided with logical groove on the base, fixed mounting has speed reduction spring on the base, and rotates in the base and install drive gear.

Preferably, slide rail fixed mounting is at the upper surface of base, and the slide connects in the slide rail cooperation, the slide symmetry is provided with two, and anchor clamps are installed in the inboard of slide, anchor clamps are provided with the arcwall face, and are provided with the bed course on the arcwall face.

Preferably, be provided with the cavity in the base, and lead to groove in the cavity intercommunication, the digging arm is connected in leading to the groove, and the digging arm is door type structure, the tip at the digging arm is installed to the actuating lever, and the rack is installed in the recess of actuating lever.

Preferably, the supporting wheel is installed in the cavity of the base and is in contact connection with the movable arm, the speed reduction spring is located on the side face of the through groove, and the driving gear is meshed between the racks of the two driving rods.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the base is of a main structure, the slide rail forms a guide channel on the base, and when the device is used, the slide rail is meshed with the rack on the driving rod through the rotation of the driving gear and can drive the two movable arms to move in opposite directions, so that the clamp is controlled through the movable arms, and is clamped or released through the clamp, the aviation connector is automatically and effectively fixed, the hands of a detector are released, and the stable and accurate detection of the conductivity of the contact pin is facilitated;

2. the utility model provides a speed reduction spring cup joints on the digging arm, and when the digging arm began to remove, its vertical pole did not contact with speed reduction spring, drove anchor clamps quick travel, when anchor clamps were close to the connector afterwards, the digging arm received speed reduction spring's elastic action, carried out the deceleration and removed, prevented that too fast speed from causing the injury to the aviation connector.

Drawings

Fig. 1 is a front view of the overall structure of the present invention;

fig. 2 is a schematic view of the clamping structure of the present invention.

In the figure: the device comprises a base 1, a sliding rail 2, a sliding seat 3, a clamp 4, a movable arm 5, a driving rod 6, a rack 7, a supporting wheel 8, a through groove 9, a speed reduction spring 10 and a driving gear 11.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1 to 2, the present invention provides a technical solution: aviation connector contact pin electric conductive property detection device, including base 1, fixed mounting has slide rail 2 on the base 1, and slidable mounting has slide 3 on the slide rail 2, fixed mounting has anchor clamps 4 on the slide 3, and fixed mounting has digging arm 5 on the slide 3, fixed mounting has actuating lever 6 on the digging arm 5, and be provided with rack 7 on the actuating lever 6, the supporting wheel 8 is installed in the rotation in the base 1, and be provided with logical groove 9 on the base 1, fixed mounting has speed reduction spring 10 on the base 1, and rotate in the base 1 and install drive gear 11.

The slide rail 2 is fixedly arranged on the upper surface of the base 1, the slide seats 3 are connected with the slide rail 2 in a matching manner, the slide seats 3 are symmetrically arranged in two, the clamps 4 are arranged on the inner sides of the slide seats 3, the clamps 4 are provided with arc surfaces, cushion layers are arranged on the arc surfaces, the base 1 is of a main body structure, and a guide channel is formed on the base 1 through the slide rail 2, so that the two slide seats 3 can slide on the base 1, the clamps 4 are controlled to move, and the aviation connector is clamped and released;

the base 1 is provided with a cavity, the through groove 9 is communicated with the cavity, the movable arm 5 is connected in the through groove 9, the movable arm 5 is of a door-shaped structure, the driving rod 6 is installed at the end part of the movable arm 5, the rack 7 is installed in a groove of the driving rod 6, the movable arm 5 is driven by the driving rod 6, so that the clamp 4 is controlled by the movable arm 5, and is meshed with the rack 7 on the driving rod 6 through the rotation of the driving gear 11, the two movable arms 5 can be driven to move reversely and can move inwards or outwards simultaneously, and clamping or releasing is performed;

the supporting wheel 8 is arranged in a cavity of the base 1, the supporting wheel 8 is in contact connection with the movable arm 5, the speed reduction spring 10 is located on the side face of the through groove 9, the driving gear 11 is meshed between the racks 7 of the two driving rods 6, the supporting wheel 8 and the through groove 9 are both of guide structures of the movable arm 5, the driving gear 11 is of a driving structure, the clamp 4 is controlled by meshing the driving gear 11 and the racks 7, the speed reduction spring 10 is sleeved on the movable arm 5, when the movable arm 5 starts to move, a vertical rod of the movable arm 5 is not in contact with the speed reduction spring 10, the clamp 4 is driven to move rapidly, and then the movable arm 5 is subjected to the elastic force action of the speed reduction spring 10 to perform speed reduction movement, so that the aviation connector is prevented from being damaged by too fast speed;

the working principle is as follows: firstly, the base 1 is a main structure, a guide channel is formed on the base 1 through the slide rail 2, so that two slide seats 3 can slide on the base 1, thereby driving the clamps 4 to move, when in use, the aviation connector is placed between the two clamps 4, and is meshed with the rack 7 on the driving rod 6 through the rotation of the driving gear 11, so that the two movable arms 5 can be driven to move in opposite directions, thereby controlling the clamps 4 through the movable arms 5, and because the two movable arms 5 move in opposite directions synchronously, the aviation connector can move inwards or outwards simultaneously, thereby being clamped or released through the clamps 4, the aviation connector is effectively and fixedly supported, so as to accurately detect the electrical conductivity of the contact pin, the supporting wheel 8 and the through groove 9 are guide structures of the movable arms 5, the stability of the clamps 4 is ensured by matching with the slide rail 2, the speed reducing spring 10 is sleeved on the movable arms 5, when the movable arms 5 start to move, its vertical pole does not contact with speed reducing spring 10, drives anchor clamps 4 rapid draing, and the digging arm 5 receives speed reducing spring 10's elasticity effect afterwards, has carried out the speed reducing and has removed, prevents that too fast speed from causing the injury to aviation connector.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. Aviation connector contact pin electric conductive property detection device, including base (1), its characterized in that: fixed mounting has slide rail (2) on base (1), and slidable mounting has slide (3) on slide rail (2), fixed mounting has anchor clamps (4) on slide (3), and fixed mounting has digging arm (5) on slide (3), fixed mounting has actuating lever (6) on digging arm (5), and is provided with rack (7) on actuating lever (6), it has supporting wheel (8) to rotate in base (1), and is provided with logical groove (9) on base (1), fixed mounting has speed reduction spring (10) on base (1), and rotates in base (1) and install drive gear (11).

2. The aviation connector pin conductivity detection device as claimed in claim 1, wherein: slide rail (2) fixed mounting is at the upper surface of base (1), and slide (3) are connected in slide rail (2) cooperation, slide (3) symmetry is provided with two, and installs the inboard at slide (3) anchor clamps (4), anchor clamps (4) are provided with the arcwall face, and are provided with the bed course on the arcwall face.

3. The aviation connector pin conductivity detection device as claimed in claim 1, wherein: be provided with the cavity in base (1), and lead to groove (9) in the cavity intercommunication, digging arm (5) are connected in leading to groove (9), and digging arm (5) are door type structure, the tip at digging arm (5) is installed in actuating lever (6), and rack (7) are installed in the recess of actuating lever (6).

4. The aviation connector pin conductivity detection device as claimed in claim 1, wherein: the supporting wheel (8) is installed in a cavity of the base (1), the supporting wheel (8) is in contact connection with the movable arm (5), the speed reduction spring (10) is located on the side face of the through groove (9), and the driving gear (11) is meshed between the racks (7) of the two driving rods (6).