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.
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
Existing welding fixtures cannot readjust the position when positioning and clamping workpieces, resulting in low operating efficiency.
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.
This achieves stability in workpiece welding and simplifies operation, thereby improving welding efficiency.
Smart Images

Figure CN224508883U_ABST
Abstract
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).