Turnover device for aircraft part machining and production

Abstract

The utility model provides a turnover device for processing and producing airplane parts. The turnover device comprises two supports which are oppositely arranged; the U-shaped plate is arranged between the two supporting seats, and the U-shaped plate is rotationally connected with the U-shaped plate; the number of the pressing plates is two, and the two pressing plates are oppositely arranged at the two ends of the U-shaped plate; the number of the supporting blocks is two, and the supporting blocks are arranged at the two ends of the U-shaped plate in a relatively sliding mode. When facing different parts, the height of the pressing plate can be adjusted to clamp the different parts, the expansion plate is moved outwards, the expansion plate is moved out of the storage groove, and then the width of the pressing plate is increased so that the parts of different sizes can be clamped; and the second sliding block can be driven to move up and down through the arranged first electric telescopic rod, and then the pressing plate is driven to move up and down.

Description

Technical Field

[0001] This utility model relates to the field of aircraft processing and production, and in particular to a flipping device for processing and producing aircraft parts. Background Technology

[0002] In the process of aircraft manufacturing, some machining worktables are needed to process parts. Traditional worktables are mostly fixed and horizontal, which means that parts can only be processed by placing them flat on the worktable.

[0003] The prior art can be referenced in Chinese authorized utility model patent CN221186460U, which specifically describes a flipping device for aircraft parts processing and production. This device includes a flipping mechanism, a clamping mechanism, a supporting vertical plate, and a controller. The flipping mechanism is located inside the supporting vertical plate, the clamping mechanism is located in the middle of the flipping mechanism, the controller is fixedly connected to the upper right side of the supporting vertical plate, a motor is located on one side of the flipping mechanism, a drive wheel is connected to the output end of the motor, a belt is movably connected to the outer surface of the drive wheel, a driven wheel is movably connected to the higher end of the belt, a first rotating shaft is fixedly connected to the inside of the driven wheel, and a fixed base is rotatably connected to the middle outer surface of the first rotating shaft. This prior art, mainly by setting up a motor, a first rotating shaft, and a second rotating shaft, enables the device to flip at any angle.

[0004] The aforementioned prior art has the following shortcomings in actual implementation: the height and width of the pressure plate cannot be adjusted, making it inconvenient to clamp and flip parts of different sizes. Utility Model Content

[0005] To address the aforementioned problems, this utility model proposes a flipping device for aircraft parts processing and production, thereby resolving the issues present in the prior art.

[0006] To achieve the above objectives, the present invention provides a flipping device for aircraft parts processing and production, comprising: a support, wherein two supports are provided and arranged opposite to each other;

[0007] A U-shaped plate is arranged between the two supports and is rotatably connected to them;

[0008] Two pressure plates are provided, which are arranged opposite each other at both ends of the U-shaped plate;

[0009] Support blocks, wherein two support blocks are provided and are slidably arranged at both ends of the U-shaped plate;

[0010] The support block is connected to the pressure plate, and the pressure plate can slide along the height of the support block. Multiple slots are provided on both sides of the pressure plate, and an extension plate is slidably arranged inside the slots.

[0011] Furthermore, a second sliding groove is provided on one side of the support block, and a second slider is slidably disposed inside the second sliding groove. The second slider is fixedly connected to the pressure plate.

[0012] Furthermore, a first electric telescopic rod is fixedly installed on the top of the support block, and the output end of the first electric telescopic rod extends into the interior of the second slide groove and is fixedly connected to the second slider.

[0013] Furthermore, a folding plate is provided at one end of the expansion plate, and a second electric telescopic rod is provided at both ends of the support block, with the output end of the second electric telescopic rod being fixedly connected to the folding plate.

[0014] Furthermore, a linkage plate is provided between two adjacent folding plates, and both ends of the linkage plate are connected to the folding plates.

[0015] Furthermore, the top of the U-shaped plate is provided with a first groove, and the two ends of the first groove are slidably provided with first sliders, the top of the first sliders being fixedly connected to the support block.

[0016] Furthermore, a fixed box is provided at the bottom of the support, the fixed box is connected to the first slide groove, a bidirectional lead screw is rotatably provided inside the fixed box, the first slider is connected to both ends of the bidirectional lead screw, a second motor is provided at one end of the fixed box, and the output end of the second motor is connected to one end of the bidirectional lead screw.

[0017] Furthermore, a first motor is fixedly installed on one side of one of the supports, and the output end of the first motor is connected to one end of the U-shaped plate.

[0018] Compared with the prior art, the beneficial effects of this utility model are as follows: when facing different parts, the height of the pressure plate can be adjusted to clamp different parts, and the expansion plate can be moved outward to move the expansion plate out of the inside of the receiving and releasing slot, thereby increasing the width of the pressure plate so as to clamp parts of different sizes. The first electric telescopic rod can drive the second slider to move up and down, thereby driving the pressure plate to move up and down.

[0019] To better understand and implement this invention, the following detailed description is provided in conjunction with the accompanying drawings. Attached Figure Description

[0020] Figure 1 This is a first three-dimensional structural schematic diagram of this utility model;

[0021] Figure 2 This is a schematic diagram of the second three-dimensional structure of this utility model;

[0022] Figure 3 This is a schematic diagram of the internal structure of the fixed box in this utility model;

[0023] Figure 4 This is a side view of the pressure plate in this utility model;

[0024] Figure 5 This is a schematic diagram of the internal structure of the support block in this utility model.

[0025] In the diagram: 1. Support; 2. U-shaped plate; 3. First motor; 4. Support block; 5. Pressure plate; 6. First electric telescopic rod; 7. Extension plate; 8. Linkage plate; 9. Fixing box; 10. Second electric telescopic rod; 11. First slide groove; 12. Two-way lead screw; 13. Folding plate; 14. First slider; 15. Retraction groove; 16. Second slide groove; 17. Second slider; 18. Second motor. Detailed Implementation

[0026] To provide a clearer understanding of the technical features, objectives, and effects of this utility model, specific embodiments of this utility model are now described with reference to the accompanying drawings. However, the scope of protection of this utility model is not limited to the following description.

[0027] Reference Figure 1-5 As shown, a flipping device for processing and producing aircraft parts includes: a support 1, two supports 1 are provided and arranged opposite to each other; a U-shaped plate 2 is arranged between the two supports 1 and rotatably connected to the U-shaped plate 2; a pressure plate 5, two pressure plates 5 are provided and arranged opposite to each other at both ends of the U-shaped plate 2; and two support blocks 4 are provided and slidably arranged opposite to each other at both ends of the U-shaped plate 2. A first motor 3 is fixedly provided on one side of one of the supports 1, and the output end of the first motor 3 is connected to one end of the U-shaped plate 2.

[0028] The support block 4 is connected to the pressure plate 5. The pressure plate 5 can slide along the height of the support block 4. Multiple receiving and releasing slots 15 are provided on both sides of the pressure plate 5. An extension plate 7 is slidably arranged inside the receiving and releasing slot 15. A second sliding groove 16 is provided on one side of the support block 4. A second slider 17 is slidably arranged inside the second sliding groove 16. The second slider 17 is fixedly connected to the pressure plate 5. A first electric telescopic rod 6 is fixedly arranged on the top of the support block 4. The output end of the first electric telescopic rod 6 extends into the interior of the second sliding groove 16 and is fixedly connected to the second slider 17.

[0029] The present invention provides a technical solution in which, during use, the component is placed on the U-shaped plate 2, positioned between two pressure plates 5. The two pressure plates 5 are then moved closer together to clamp the component. The first motor 3 is then activated, driving the U-shaped plate 2 to rotate, thereby flipping the component. When dealing with different components, the height of the pressure plates 5 can be adjusted to clamp different components. Furthermore, the extension plate 7 can be moved outwards, extending it beyond the receiving / discharging slot 15, thus increasing the width of the pressure plates 5 to clamp components of different sizes. The first electric telescopic rod 6 drives the second slider 17 to move up and down, thereby moving the pressure plates 5 up and down.

[0030] Preferably, one end of the expansion plate 7 is provided with a folding plate 13, and both ends of the support block 4 are provided with a second electric telescopic rod 10. The output end of the second electric telescopic rod 10 is fixedly connected to the folding plate 13. A linkage plate 8 is provided between two adjacent folding plates 13, and both ends of the linkage plate 8 are connected to the folding plate 13.

[0031] Specifically, the second electric telescopic rod 10 can drive the extension plate 7 to move, thereby facilitating the adjustment of the width of the pressure plate 5. The folding plate 13 facilitates the movement of the extension plate 7 by the second electric telescopic rod 10, and the linkage plate 8 facilitates the synchronous movement of multiple extension plates 7.

[0032] Preferably, the top of the U-shaped plate 2 is provided with a first sliding groove 11, and the two ends of the first sliding groove 11 are slidably provided with a first slider 14. The top of the first slider 14 is fixedly connected to the support block 4. The bottom of the support 1 is provided with a fixed box 9, which is connected to the first sliding groove 11. The fixed box 9 is rotatably provided with a bidirectional lead screw 12. The first slider 14 is connected to the two ends of the bidirectional lead screw 12. One end of the fixed box 9 is provided with a second motor 18, and the output end of the second motor 18 is connected to one end of the bidirectional lead screw 12.

[0033] Specifically, the second motor 18 can drive the bidirectional lead screw 12 to rotate, and the rotation of the bidirectional lead screw 12 can drive the first slider 14 to move, thereby facilitating the movement of the pressure plate 5.

[0034] The above-disclosed embodiments are merely preferred embodiments of the present utility model and should not be construed as limiting the scope of the present utility model. Therefore, any equivalent variations made in accordance with the claims of the present utility model shall still fall within the scope of the present utility model.

Claims

1. An overturning device for processing and producing aircraft parts, characterized in that, include: Support (1), two supports (1) are provided and arranged opposite to each other; U-shaped plate (2), the U-shaped plate (2) is arranged between the two supports (1) and is rotatably connected to the U-shaped plate (2); Two pressure plates (5) are provided, which are arranged opposite to each other at both ends of the U-shaped plate (2); Support blocks (4), two of which are provided and are slidably arranged at both ends of the U-shaped plate (2); The support block (4) is connected to the pressure plate (5). The pressure plate (5) can slide along the height of the support block (4). Multiple receiving and releasing slots (15) are provided on both sides of the pressure plate (5). An extension plate (7) is slidably arranged inside the receiving and releasing slot (15).

2. The turnover device for processing and producing aircraft parts according to claim 1, characterized in that: A second slide groove (16) is provided on one side of the support block (4), and a second slider (17) is slidably arranged inside the second slide groove (16). The second slider (17) is fixedly connected to the pressure plate (5).

3. The turnover device for processing and producing aircraft parts according to claim 2, characterized in that: The top of the support block (4) is fixedly provided with a first electric telescopic rod (6), and the output end of the first electric telescopic rod (6) extends into the interior of the second slide groove (16) and is fixedly connected to the second slider (17).

4. The turnover device for processing and producing aircraft parts according to claim 1, characterized in that: One end of the expansion plate (7) is provided with a folding plate (13), and both ends of the support block (4) are provided with a second electric telescopic rod (10), the output end of the second electric telescopic rod (10) is fixedly connected to the folding plate (13).

5. A flipping device for aircraft parts processing and production according to claim 4, characterized in that: A linkage plate (8) is provided between two adjacent folding plates (13), and both ends of the linkage plate (8) are connected to the folding plate (13).

6. The turnover device for processing and producing aircraft parts according to claim 1, characterized in that: The top of the U-shaped plate (2) is provided with a first groove (11), and the two ends of the first groove (11) are slidably provided with a first slider (14), and the top of the first slider (14) is fixedly connected to the support block (4).

7. The turnover device for processing and producing aircraft parts according to claim 6, characterized in that: The bottom of the support (1) is provided with a fixed box (9), which is connected to the first slide groove (11). A bidirectional lead screw (12) is rotatably provided inside the fixed box (9). The first slider (14) is connected to both ends of the bidirectional lead screw (12). A second motor (18) is provided at one end of the fixed box (9), and the output end of the second motor (18) is connected to one end of the bidirectional lead screw (12).

8. The turnover device for processing and producing aircraft parts according to claim 1, characterized in that: A first motor (3) is fixedly installed on one side of the support (1), and the output end of the first motor (3) is connected to one end of the U-shaped plate (2).

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