Aviation plug positioning clamp

Through the aviation plug positioning fixture with self-locking structure of guide rails and worm gear, the problem of insufficient dimensional adaptability in the prior art is solved, and stable clamping of plugs of different sizes is achieved, thereby improving clamping strength and stability.

CN223205514UActive Publication Date: 2025-08-08SUZHOU GREENTECH NEW ENERGY CO LTD
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Patent Information

Application Number
CN202422032413.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-08-21
Publication Date
2025-08-08
Estimated Expiration
2034-08-21

AI Technical Summary

Technical Problem

Existing aviation plug positioning fixtures are difficult to adapt to aviation plugs of different sizes, resulting in unstable clamping and reduced practicality.

Method used

An aviation plug positioning fixture including a guide rail, a positioning assembly and a drive assembly is designed. The clamping plate is driven to move through the sliding grooves and a drive assembly on the guide rail, and combined with the worm gear and worm self-locking structure, stable clamping of plugs of different sizes is achieved.

Benefits of technology

It realizes stable clamping of aviation plugs of different sizes, improves clamping strength and stability, and has a wider adaptability.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of aviation plug clamp tools, in particular to an aviation plug positioning clamp. The aviation plug positioning clamp comprises a guide rail, and a sliding groove is formed in the top of the guide rail. According to the clamping device, the two first clamping plates and the two second clamping plates can be driven to synchronously move inwards by rotating the hand wheel to perform double centering clamping and positioning on the outer side of the aviation plug, so that the clamping strength is ensured, and the moving distance of the two first clamping plates and the two second clamping plates can be changed by changing the number of turns of rotation of the hand wheel; therefore, aviation plugs with different sizes can be positioned and clamped; the second clamping plate can extrude the spring during clamping, the spring reversely pushes the second clamping plate through the resilience force of the spring, the clamping stability of the second clamping plate to the aviation plug is further improved, and the clamping and positioning stability of the device to the aviation plug can be effectively guaranteed through the self-locking performance of the worm gear and the worm.
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Description

Technical Field

[0001] The utility model relates to the technical field of aviation plug fixture tooling, in particular to an aviation plug positioning fixture. Background Art

[0002] During the production of aviation plugs with cables, the pins must be tested to verify their secure installation. Due to their small size and high contact density, aviation plugs can exhibit structural deformation, bending, poor contact, and other issues during testing, especially in challenging operating environments.

[0003] Chinese patent publication number CN219302525U discloses an aviation plug positioning fixture, comprising a base, a support member disposed above the base, and a plug pressure plate located directly above the support member. The support member is provided with a cavity for accommodating the aviation plug, and a boss extending toward the axis at its top. A positioning member for limiting the position of the aviation plug is mortised on the upper surface of the boss, and a circular hole is provided on the plug pressure plate to expose the aviation plug pins. A clamping mechanism is connected between the support member and the plug pressure plate to press the aviation plug onto the positioning member. In this design, the positioning member is disposed on the top boss of the support member to determine the relative position of the aviation plug during assembly, and the three protrusions on the positioning member match the corresponding circular hollow holes on the aviation plug. This vertical fixing method ensures the positioning accuracy of the fixture.

[0004] The above-mentioned existing technical solutions have the following defects: the sizes of the support member and the positioning member are fixed, and the size of the plug pressure plate used to fix the top of the aviation plug is also fixed, which makes it difficult for the device to position and clamp aviation plugs of different sizes, thereby reducing the practicality of the device. In response to the above situation, technical innovation is carried out based on the existing aviation plug positioning fixture. Utility Model Content

[0005] The purpose of the utility model is to provide an aviation plug positioning fixture to solve the problems raised in the above background technology.

[0006] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an aviation plug positioning fixture, comprising:

[0007] The guide rail has a slide groove on the top, a driving assembly is placed in the slide groove, a positioning assembly is placed above the guide rail, two groups of fixing sleeves are evenly arranged on the front and rear sides of the guide rail, and two groups of rotating shaft seats are evenly arranged on the right side of the guide rail.

[0008] Preferably, the positioning assembly includes a storage box, and a group of storage grooves are provided on opposite sides of the two groups of storage boxes, a second clamping plate is provided in the storage groove, a groove is provided on the top of the second clamping plate, and rollers are evenly provided in the groove through a rotating shaft, and a group of first clamping plates are provided on opposite sides of the two groups of storage boxes, and the first clamping plates are located above the rollers, and a group of springs are provided on opposite sides of the two groups of second clamping plates, and the springs are provided in the storage groove.

[0009] Preferably, a group of guide grooves are provided on both the front and rear sides of the inner side wall of the receiving groove, and a group of guide blocks are provided on both the front and rear sides of the second clamping plate, and the guide blocks are arranged in the guide grooves.

[0010] Preferably, the drive assembly includes a bidirectional screw, which is arranged in the slide groove of the guide rail. The right side of the bidirectional screw passes through the right side of the guide rail and is connected to a worm wheel. The top of the worm wheel is engaged with a worm, and a handwheel is provided on the front side of the worm. The outer wall of the bidirectional screw is evenly screwed with two groups of internal threaded slides.

[0011] Preferably, the storage box is arranged on the top of the internal thread slide, and the two groups of the rotating shaft seats are evenly sleeved on the outer side wall of the worm.

[0012] Preferably, an aviation plug is placed above the guide rail, and the aviation plug is located between the two groups of second clamping plates and the two groups of first clamping plates.

[0013] Compared with the prior art, the beneficial effects of the present invention are as follows:

[0014] The utility model can drive the two sets of first clamping plates and the two sets of second clamping plates to move inward synchronously by turning the hand wheel to double-center the outer side of the aviation plug to ensure the clamping strength. By changing the number of turns of the hand wheel, the moving distance of the two sets of first clamping plates and the two sets of second clamping plates can be changed, thereby making it possible to position and clamp aviation plugs of different sizes.

[0015] The second clamping plate will squeeze the spring when clamping, and the spring will push the second clamping plate in the opposite direction through its own rebound force, thereby improving the clamping stability of the second clamping plate on the aviation plug. In addition, the self-locking property of the worm gear and worm can effectively ensure the clamping and positioning stability of the device on the aviation plug. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 This is a structural diagram of an aviation plug positioning fixture of the utility model;

[0017] Figure 2 This is a front cross-sectional view of an aviation plug positioning fixture of the utility model;

[0018] Figure 3 For this utility model Figure 2 Magnified view of part A.

[0019] In the figure: 1. Guide rail; 11. Fixed sleeve; 12. Worm gear; 13. Worm; 14. Rotating shaft seat; 15. Handwheel; 16. Bidirectional screw rod; 17. Internal thread slide; 2. Storage box; 21. First clamping plate; 22. Second clamping plate; 23. Guide block; 24. Roller; 25. Spring; 3. Aviation plug. DETAILED DESCRIPTION

[0020] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0021] See also Figure 1-Figure 3 The top of the guide rail 1 is provided with a slide groove, and a driving assembly is placed in the slide groove. A positioning assembly is placed above the guide rail 1, and two sets of fixing sleeves 11 are evenly fixed on the front and rear sides of the guide rail 1. The bolts pass through the fixing sleeves 11 and are screwed with the threaded holes on the external platform, so that the guide rail 1 can be fixed. Two sets of rotating shaft seats 14 are evenly fixed on the right side of the guide rail 1. The positioning assembly includes a storage box 2, and the opposite sides of the two groups of storage boxes 2 are provided with a group of storage grooves. A second clamping plate 22 is slidably provided in the storage groove, and a groove is provided on the top of the second clamping plate 22. A roller 24 is evenly rotated in the groove by a rotating shaft. A group of first clamping plates 21 are fixed on the opposite sides of the two groups of storage boxes 2. The first clamping plate 21 is located above the roller 24, and a group of springs 25 are fixed on the opposite sides of the two groups of second clamping plates 22. The springs 25 are fixed in the storage groove. The front and rear sides of the inner wall of the storage groove are provided with a group of guide grooves, and the front and rear sides of the second clamping plate 22 are fixedly provided with a group of guide blocks 23, which are slidably arranged in the guide grooves, and the second clamping plate 22 is assisted to move stably left and right by the guide blocks 23. The driving assembly includes a two-way screw rod 16, and the two-way screw rod 16 is rotatably arranged in the slide groove of the guide rail 1. The right side of the two-way screw rod 16 passes through the right side of the guide rail 1 and is connected to the worm gear 12. The top of the worm gear 12 is meshed with the worm 13, and the front side of the worm 13 is fixedly provided with a handwheel 15. The outer side wall of the two-way screw rod 16 is evenly screwed with two groups of internal threaded slides 17. The storage box 2 is fixedly provided on the top of the internal threaded slide 17. The two groups of rotating shaft seats 14 are evenly sleeved on the outer side wall of the worm 13, and the worm 13 is supported to rotate by the rotating shaft seat 14. An aviation plug 3 is placed above the guide rail 1, and the aviation plug 3 is located between the two groups of second clamping plates 22 and the two groups of first clamping plates 21.

[0022] Working principle: The bolts are passed through the fixing sleeve 11 and screwed into the threaded holes on the external platform to fix the aviation plug 3. The aviation plug 3 is placed between the two sets of second clamping plates 22 and the two sets of first clamping plates 21, and the hand wheel 15 is turned to drive the worm gear 12 to rotate through the worm 13. The worm gear 12 drives the internal thread slide 17 to move inward synchronously through the two sets of bidirectional screw rods 16, thereby driving the positioning assembly to move synchronously. When the two sets of second clamping plates 22 move to the bottom of the fixing ring of the aviation plug 3, the aviation plug 3 can be placed on the top of the two sets of second clamping plates 22. At this time, continue to turn the hand wheel 15 to make the two sets of second clamping plates 22 continue to move inward to fix the outer surface of the aviation plug 3. The side wall is centered and clamped, and the roller 24 can assist the second clamping plate 22 to slide smoothly on the bottom of the fixed ring of the aviation plug 3. As the handwheel 15 rotates, the two groups of first clamping plates 21 will gradually move inward and perform a second centered clamping and positioning on the outer side of the aviation plug 3. At the same time, the second clamping plate 22 will gradually slide into the storage groove of the storage box 2 due to the obstruction of the aviation plug 3 and squeeze the spring 25. The spring 25 pushes the second clamping plate 22 in the opposite direction through its own rebound force, thereby improving the clamping stability of the second clamping plate 22 on the aviation plug 3, and the self-locking property of the worm gear 12 and the worm 13 can effectively ensure the clamping and positioning stability of the device on the aviation plug 3.

Claims

1. An aviation plug positioning fixture, characterized in that: include: A guide rail (1) is provided with a slide groove at the top of the guide rail (1), a driving assembly is placed in the slide groove, a positioning assembly is placed above the guide rail (1), two groups of fixing sleeves (11) are evenly arranged on the front and rear sides of the guide rail (1), and two groups of rotating shaft seats (14) are evenly arranged on the right side of the guide rail (1).

2. The aviation plug positioning fixture according to claim 1, characterized in that: The positioning assembly includes a storage box (2), and a group of storage grooves are provided on opposite sides of the two groups of storage boxes (2), a second clamping plate (22) is provided in the storage groove, a groove is provided on the top of the second clamping plate (22), and rollers (24) are evenly provided in the groove through a rotating shaft, and a group of first clamping plates (21) are provided on opposite sides of the two groups of storage boxes (2), and the first clamping plates (21) are located above the rollers (24), and a group of springs (25) are provided on opposite sides of the two groups of second clamping plates (22), and the springs (25) are provided in the storage groove.

3. The aviation plug positioning fixture according to claim 2, characterized in that: A group of guide grooves are provided on both the front and rear sides of the inner side wall of the receiving groove, and a group of guide blocks (23) are provided on both the front and rear sides of the second clamping plate (22), and the guide blocks (23) are arranged in the guide grooves.

4. The aviation plug positioning fixture according to claim 2, characterized in that: The driving assembly includes a bidirectional screw rod (16), which is arranged in a slide groove of the guide rail (1). The right side of the bidirectional screw rod (16) passes through the right side of the guide rail (1) and is connected to a worm wheel (12). The top of the worm wheel (12) is engaged with a worm (13). The front side of the worm (13) is provided with a hand wheel (15). The outer side wall of the bidirectional screw rod (16) is evenly screwed with two groups of internal thread slide plates (17).

5. The aviation plug positioning fixture according to claim 4, characterized in that: The storage box (2) is arranged on the top of the internal thread slide (17), and the two groups of rotating shaft seats (14) are evenly sleeved on the outer side wall of the worm (13).

6. The aviation plug positioning fixture according to claim 2, characterized in that: An aviation plug (3) is placed above the guide rail (1), and the aviation plug (3) is located between two groups of second clamping plates (22) and two groups of first clamping plates (21).

Citation Information

Patent Citations

  • Aviation plug positioning clamp

    CN219302525U