一种航空钣金件焊接夹具

By designing a welding fixture for aerospace sheet metal parts with a base plate and a rotating carrier plate, the problem of existing welding fixtures being unable to readjust their position was solved, achieving precise positioning and efficient clamping of the workpiece, and improving the stability and efficiency of the welding operation.

CN224508883UActive Publication Date: 2026-07-17

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Filing Date
2025-08-21
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing welding fixtures cannot readjust the position when positioning and clamping workpieces, resulting in low operating efficiency.

Method used

A welding fixture for aerospace sheet metal parts, comprising a base plate, a rotating carrier plate, and an adjusting frame, is designed. By extending and retracting the adjusting frame and deflecting the rotating carrier plate, the workpiece can be accurately positioned and reliably clamped, allowing for angle adjustment after fixing.

Benefits of technology

This achieves stability in workpiece welding and simplifies operation, thereby improving welding efficiency.

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Abstract

本实用新型涉及焊接夹具技术领域,尤其涉及一种航空钣金件焊接夹具。其技术方案:包括基板,所述基板其中一侧为方形结构,另一侧为半圆弧结构,所述基板上固定有固定框,所述基板上转动连接有转动载板,所述转动载板上滑动连接有调节框,所述调节框内设置有固定槽,所述固定槽内设置双向夹持组件,所述转动载板端部固定有连接板,所述连接板转动连接在基板上。本实用新型将焊接件分别固定在固定框和调节框内,通过调节框的伸缩,使工件焊接端相抵,进行焊接,并且利用转动载板的转动,可以带动调节框进行偏转,进而实现不同角度的焊接,操作更加简单,可以保证焊接工作的稳定。
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Claims

1. An aircraft sheet metal part welding fixture comprising a base plate (1), characterized in that: The substrate (1) has a square structure on one side and a semi-circular arc structure on the other side. A fixing frame (2) is fixed on the substrate (1). A rotating carrier plate (5) is rotatably connected to the substrate (1). An adjusting frame (3) is slidably connected to the rotating carrier plate (5). A fixing groove (4) is provided in the adjusting frame (3). A bidirectional clamping assembly is provided in the fixing groove (4). A connecting plate (54) is fixed at the end of the rotating carrier plate (5). The connecting plate (54) is rotatably connected to the substrate (1).

2. The welding fixture for an aircraft sheet metal part according to claim 1, characterized in that: An arc-shaped track (6) is fixed on the outer periphery of one arc side of the substrate (1). A track block (61) is slidably connected on the arc-shaped track (6). A locking bolt (7) is installed on the track block (61). The upper end of the track block (61) is fixedly connected to the bottom of the rotating carrier plate (5).

3. The welding fixture for an aircraft sheet metal part according to claim 1, characterized in that: The center of the arc around the substrate (1) coincides with the pivot of the connecting plate (54), and the surface of the arc end of the substrate (1) is provided with deflection angle scale lines (11).

4. The aircraft sheet metal part welding fixture of claim 1, wherein: The rotating carrier plate (5) is L-shaped in general, and the upper end is provided with an adapter groove (51) that is compatible with the fixed groove (4). A telescopic cylinder (52) is fixed in the middle of the right-angle side wall of the rotating carrier plate (5), and the output end of the telescopic cylinder (52) is fixed on the adjustment frame (3).

5. The aircraft sheet metal part welding fixture of claim 4, wherein: A pair of guide blocks (53) are fixed to the right-angle sidewall of the rotating carrier plate (5), and a guide groove is provided at the bottom of the adjusting frame (3) and at the position corresponding to the guide blocks (53).

6. The aircraft sheet metal part welding fixture of claim 1, wherein: The bidirectional clamping assembly includes a clamping plate (41) and a drive groove (42). The clamping plate (41) is installed on both sides of the fixed groove (4). The drive groove (42) is opened at the bottom of the fixed groove (4). A sliding block (44) is slidably connected in the drive groove (42). The upper end of the sliding block (44) is fixedly connected to the clamping plate (41). A bidirectional lead screw (43) is rotatably connected in the drive groove (42). The bidirectional lead screw (43) passes through the sliding block (44) and is threadedly connected to the sliding block (44). One end of the bidirectional lead screw (43) extends out of the drive groove (42) and is fixedly connected to a knob (45).