Aviation plug welding fixing seat

Abstract

The utility model relates to the field of plug welding, and discloses an aviation plug welding fixing seat which comprises a bottom plate, a vertical plate is fixedly connected to the outer wall of the upper end of the bottom plate, a fixing block is fixedly connected to the outer wall of the left end of the vertical plate, and a toothed plate is slidably connected to the inner wall of the front end of the fixing block. The outer wall of the left end of the fixing block is elastically connected with a limiting assembly through a first spring, a rotating shaft penetrates through the inner wall of the left end of the vertical plate and is rotationally connected with the inner wall of the left end of the vertical plate, a rotating plate is fixedly connected to the outer wall of the rotating shaft, a gear is fixedly connected to the outer wall of the rotating shaft, and a toothed cylinder is fixedly connected to the outer wall of the rotating shaft. An adjusting assembly is slidably connected to the inner wall of the rear side of the upper end of the rotating plate. The clamping block is moved leftwards to leave the outer wall of the toothed cylinder, the toothed plate is moved to drive the gear and the rotating shaft to rotate so that the rotating plate can rotate to adjust the angle, after adjustment, the clamping block is released to be clamped to the outer wall of the toothed cylinder to fix the angle of the rotating plate, and adjustment is convenient.

Description

Technical Field

[0001] The utility model relates to the field of plug welding, in particular to a welding fixing seat for an aviation plug. Background Art

[0002] An aviation plug refers to a plug used to connect electrical equipment or systems on an aircraft, or a standardized plug interface in the aviation industry. These plugs are usually designed to withstand extreme environments such as high temperature, high pressure, and high-frequency vibration, and comply with the standards of aviation safety and aviation electrical systems.

[0003] After retrieval, Chinese Patent Publication No.: CN219881525U discloses a welding fixing seat for an aviation plug, which includes two vertical plates and a rotating plate arranged between the two vertical plates. The rotating plate is rotatably connected to the vertical plates, and a first fixing hole for placing the aviation plug is arranged on the plate surface of the rotating plate; it also includes a positioning rod, which is arranged radially along the first fixing hole and extends into the first fixing hole, and the positioning rod is used to insert into a sliding groove on the side of the aviation plug. By rotating the rotating plate, the aviation plug is rotated to the lower left of the operator, and the neck can maintain a more natural angle under visual observation, and the welding plug is also far away from the operator, avoiding directly inhaling the fumes generated by soldering. The angle of the rotating plate and the distance from the operator can be adjusted, so production operations can be carried out in a more comfortable posture.

[0004] In the above technology, although the wing nut is loosened, the rotating plate can be rotated arbitrarily and adjusted to the required angle, and the support and fastening of the rotating plate are achieved by tightening the wing nut. However, the adjustment of the rotating plate is achieved by tightening and loosening the wing nut, and the adjustment is relatively troublesome. Therefore, a welding fixing seat for an aviation plug is proposed to solve the above problems. Content of the Utility Model

[0005] In order to make up for the above deficiencies, the utility model provides a welding fixing seat for an aviation plug, aiming to improve the problem that it is relatively troublesome to adjust the rotating plate by wing nuts in the prior art.

[0006] To achieve the above purpose, the utility model adopts the following technical scheme: A welding fixing seat for an aviation plug includes a bottom plate, a vertical plate is fixedly connected to the outer wall of the upper end of the bottom plate, a fixing block is fixedly connected to the outer wall of the left end of the vertical plate, a toothed plate is slidably connected to the inner wall of the front end of the fixing block, a limiting component is elastically connected to the outer wall of the left end of the fixing block through a first spring, a rotating shaft penetrates and is rotatably connected to the inner wall of the left end of the vertical plate, a rotating plate is fixedly connected to the outer wall of the rotating shaft, a gear is fixedly connected to the outer wall of the rotating shaft, a toothed cylinder is fixedly connected to the outer wall of the rotating shaft, and an adjusting component is slidably connected to the inner wall of the upper rear side of the rotating plate.

[0007] As a further description of the above technical solution:

[0008] The adjusting component includes a slider. The inner wall of the rear end of the slider penetrates and is threadedly connected with a threaded rod. The front end outer wall of the threaded rod is rotatably connected with a top block. The upper rear side outer wall of the rotating plate is elastically connected with an insertion block through a second spring.

[0009] As a further description of the above technical solution:

[0010] The limiting component includes a clamping block. The right outer wall of the clamping block is elastically connected to the left end outer wall of the fixed block through a first spring.

[0011] As a further description of the above technical solution:

[0012] One end of the first spring is fixedly connected to the right outer wall of the clamping block, and the other end of the first spring is fixedly connected to the left end outer wall of the fixed block.

[0013] As a further description of the above technical solution:

[0014] One end of the second spring is fixedly connected to the upper rear side outer wall of the rotating plate, and the other end of the second spring is fixedly connected to the lower side outer wall of the insertion block.

[0015] As a further description of the above technical solution:

[0016] The lower side outer wall of the insertion block is slidably connected to the upper rear side inner wall of the rotating plate, and the lower side outer wall of the insertion block is slidably connected to the upper end inner wall of the slider.

[0017] As a further description of the above technical solution:

[0018] The outer wall of the clamping block penetrates and is slidably connected to the left end inner wall of the fixed block. A long strip protrusion is provided on the middle section outer wall of the clamping block. A limiting groove is opened on the right end inner wall of the clamping block. The shape of the limiting groove of the clamping block fits the outer wall of the toothed cylinder.

[0019] As a further description of the above technical solution:

[0020] The front side outer wall of the threaded rod is slidably connected to the rear end inner wall of the rotating plate.

[0021] The utility model has the following beneficial effects:

[0022] 1. In the utility model, by moving the clamping block to the left away from the outer wall of the toothed cylinder, the rotating plate is rotated to adjust the angle by moving the toothed plate to drive the rotation of the gear and the rotating shaft. After adjustment, the clamping block is released to be clamped on the outer wall of the toothed cylinder to fix the angle of the rotating plate, and the adjustment is convenient.

[0023] 2. In the present utility model, by moving the insert block upward to release the limit on the slider, the slider can be moved backward to drive the threaded rod and the top block to move backward away from the outer wall of the aviation plug, thus realizing the rapid disassembly of the aviation plug. At the same time, by limiting the movement of the slider through the insert block, the rapid fixation of plugs of the same specification can be achieved. BRIEF DESCRIPTION OF THE DRAWINGS

[0024] Figure 1 FIG. 1 is a perspective view of a welding fixing seat for an aviation plug proposed by the present utility model;

[0025] Figure 2 FIG. 2 is a schematic diagram of a toothed cylinder of a welding fixing seat for an aviation plug proposed by the present utility model;

[0026] Figure 3 FIG. 3 is a schematic diagram of a welding fixing seat for an aviation plug proposed by the present utility model Figure 2 with an enlarged view at position A.

[0027] LEGEND DESCRIPTION:

[0028] 1. Base plate; 2. Vertical plate; 3. Toothed plate; 4. Block; 5. Spring 1; 6. Fixed block; 7. Top block; 8. Rotating shaft; 9. Toothed cylinder; 10. Gear; 11. Slider; 12. Threaded rod; 13. Spring 2; 14. Insert block; 15. Rotating plate. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0029] The technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Apparently, the described embodiments are only a part of the embodiments of the present utility model, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0030] Refer to Figures 1 - 3, The utility model provides an embodiment: an aviation plug welding fixed seat, including a bottom plate 1, the outer wall of the bottom plate 1 is smooth and easy to clean, the bottom plate 1 provides support for the aviation plug welding fixed seat, the upper end outer wall of the bottom plate 1 is fixedly connected with a vertical plate 2, the vertical plates 2 are symmetrically arranged, the vertical plates 2 provide support for the rotation of the rotating shaft 8, the left end outer wall of the vertical plate 2 is fixedly connected with a fixed block 6, the setting of the fixed block 6 provides support for the sliding of the tooth plate 3, the front end inner wall of the fixed block 6 is slidably connected with a tooth plate 3, the movement of the tooth plate 3 can drive the rotation of the gear 10, the left end outer wall of the fixed block 6 is elastically connected to the limited position component through a spring 5, the vertical plate 2 is fixedly connected with a fixed block 6, the fixed block 6 is fixedly connected with a fixed block 6, the fixed block 6 is fixedly connected with a fixed block 6, the front end inner wall of the fixed block 6 is fixedly connected with a tooth plate 3, the movement of the tooth plate 3 can drive the rotation of the gear 10, the left end outer wall of the fixed block 6 is elastically connected to the limited position component through a spring 5, A rotating shaft 8 passes through and is rotatably connected to the inner wall of the left end of the plate 2. The rotating shaft 8 drives the rotating plate 15 to rotate through the rotation of the gear 10. The outer wall of the rotating shaft 8 is fixedly connected to the rotating plate 15. The rotating plate 15 rotates to adjust the angle of the rotating plate 15, so that the angle of the aviation plug on the rotating plate 15 is adjusted to an angle that makes the workers comfortable welding. A gear 10 is fixedly connected to the outer wall of the rotating shaft 8, which drives the rotation of the rotating shaft 8. A toothed cylinder 9 is fixedly connected to the outer wall of the rotating shaft 8. When the inner wall of the right end of the block 4 is clamped on the outer wall of the toothed cylinder 9, the rotation of the rotating shaft 8 and the rotating plate 15 is restricted. An adjustment component is slidably connected to the inner wall of the upper rear side of the rotating plate 15.

[0031] Reference Figure 2 and Figure 3 The adjustment component includes a slider 11. The movement of the slider 11 can drive the movement of the threaded rod 12. The rear end inner wall of the slider 11 passes through and is threadedly connected with the threaded rod 12. The threaded rod 12 rotates to drive the top block 7 to move, which is used to fix the aviation plug. The front end outer wall of the threaded rod 12 is rotatably connected to the rear end inner wall of the top block 7. The front side outer wall of the threaded rod 12 is slidably connected to the rear end inner wall of the rotating plate 15. The front end outer wall of the threaded rod 12 is rotatably connected to the top block 7. The top block 7 is used to hold the outer wall of the aviation plug to fix the aviation plug. The outer wall of the top block 7 slides It is connected to the rear end inner wall of the rotating plate 15, and the upper rear outer wall of the rotating plate 15 is elastically connected with an insert 14 through a second spring 13. The lower outer wall of the insert 14 is slidably connected to the upper rear inner wall of the rotating plate 15, and the lower outer wall of the insert 14 is slidably connected to the upper inner wall of the slider 11. By moving the insert 14 upward to leave the upper inner wall of the slider 11, the slider 11 can be released. One end of the second spring 13 is fixedly connected to the upper rear outer wall of the rotating plate 15, and the other end of the second spring 13 is fixedly connected to the lower outer wall of the insert 14.

[0032] Reference Figure 2, the limiting component includes a clamping block 4. The clamping block 4 slides on the outer wall of the toothed cylinder 9, and thus the rotating plate 15 can be fixed by fixing the toothed cylinder 9. The outer wall of the clamping block 4 penetrates and is slidably connected to the inner wall of the left end of the fixed block 6. A long protrusion is provided on the outer wall of the middle section of the clamping block 4. A limiting groove is formed in the inner wall of the right end of the clamping block 4. The shape of the limiting groove of the clamping block 4 matches the outer wall of the toothed cylinder 9. By moving the clamping block 4 to the left away from the outer wall of the toothed cylinder 9, the limitation on the rotating shaft 8 is released. The outer wall of the right side of the clamping block 4 is elastically connected to the outer wall of the left end of the fixed block 6 through a first spring 5. One end of the first spring 5 is fixedly connected to the outer wall of the right side of the clamping block 4, and the other end of the first spring 5 is fixedly connected to the outer wall of the left end of the fixed block 6.

[0033] Working principle: By rotating the threaded rod 12 to drive the top block 7 to move forward to fix the position of the aviation plug. Move the clamping block 4 to the left away from the outer wall of the toothed cylinder 9. By moving the toothed plate 3 to drive the rotation of the gear 10 and the rotating shaft 8, the rotating plate 15 is adjusted to an appropriate angle. After adjustment, release the clamping block 4 to be clamped on the outer wall of the toothed cylinder 9 to fix the angle of the rotating plate 15, and complete the adjustment of the rotating plate 15. After welding is completed, release the limitation on the slider 11 by moving the insert block 14 upward. By moving the slider 11 backward to drive the threaded rod 12 and the top block 7 to move backward away from the outer wall of the aviation plug, the rapid disassembly of the aviation plug can be realized. At the same time, by moving the slider 11 and limiting it through the insert block 14, the rapid fixation of plugs of the same specification can be realized.

[0034] Finally, it should be noted that the above are only the preferred embodiments of the present invention and are not used to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements on some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included in the protection scope of the present invention.

Claims

1. An aviation plug welding and fixing seat, comprising a bottom plate (1), characterized in that: On the outer wall of the upper end of the bottom plate (1), a vertical plate (2) is fixedly connected. On the outer wall of the left end of the vertical plate (2), a fixed block (6) is fixedly connected. On the inner wall of the front end of the fixed block (6), a toothed plate (3) is slidably connected. On the outer wall of the left end of the fixed block (6), a limiting component is elastically connected through a first spring (5). On the inner wall of the left end of the vertical plate (2), a rotating shaft (8) is penetrated and rotatably connected. On the outer wall of the rotating shaft (8), a rotating plate (15) is fixedly connected. On the outer wall of the rotating shaft (8), a gear (10) is fixedly connected. On the outer wall of the rotating shaft (8), a toothed cylinder (9) is fixedly connected. On the inner wall of the upper rear side of the rotating plate (15), an adjusting component is slidably connected.

2. The welding and fixing seat for an aviation plug according to claim 1, wherein: The adjusting component includes a slider (11). The inner wall of the rear end of the slider (11) is penetrated and threadedly connected with a threaded rod (12). On the outer wall of the front end of the threaded rod (12), a top block (7) is rotatably connected. On the outer wall of the upper rear side of the rotating plate (15), an insert block (14) is elastically connected through a second spring (13).

3. The welding and fixing seat of an aviation plug according to claim 1, characterized in that: The limiting component includes a clamping block (4). On the outer wall of the right side of the clamping block (4), it is elastically connected to the outer wall of the left end of the fixed block (6) through a first spring (5).

4. The welding and fixing base for an aviation plug according to claim 3, characterized in that: One end of the first spring (5) is fixedly connected to the outer wall of the right side of the clamping block (4), and the other end of the first spring (5) is fixedly connected to the outer wall of the left end of the fixed block (6).

5. The welding and fixing seat of an aviation plug according to claim 2, characterized in that: One end of the second spring (13) is fixedly connected to the outer wall of the upper rear side of the rotating plate (15), and the other end of the second spring (13) is fixedly connected to the lower outer wall of the insert block (14).

6. The welding and fixing base of an aviation plug according to claim 2, wherein: The lower outer wall of the insert block (14) is slidably connected to the inner wall of the upper rear side of the rotating plate (15), and the lower outer wall of the insert block (14) is slidably connected to the inner wall of the upper end of the slider (11).

7. The welding and fixing seat for an aviation plug according to claim 3, characterized in that: The outer wall of the clamping block (4) is penetrated and slidably connected to the inner wall of the left end of the fixed block (6). On the outer wall of the middle section of the clamping block (4), there is a long protrusion. On the inner wall of the right end of the clamping block (4), a limiting groove is provided. The shape of the limiting groove of the clamping block (4) fits the outer wall of the toothed cylinder (9).

8. The welding and fixing base of an aviation plug according to claim 2, characterized in that: The outer wall of the front side of the threaded rod (12) is slidably connected to the inner wall of the rear end of the rotating plate (15).

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