Unmanned aerial vehicle wing stamping device

Abstract

The utility model discloses an unmanned aerial vehicle wing stamping device and relates to the technical field of stamping devices, the unmanned aerial vehicle wing stamping device comprises a main body structure, a base, a stand column, an upper die and a lower die, the stand column is fixedly connected to the top of the base, the upper die is arranged at the top of one side of the stand column, and the lower die is located at the bottom of the upper die; and a cutting assembly; by arranging the cutting assembly, manual cutting of leftover materials obtained after wing stamping is avoided, manpower input is reduced, the working efficiency is improved, time and labor are saved, die replacement operation is easy and convenient through the design of the disassembling and assembling assembly, die disassembling and assembling can be rapidly completed, and the requirement for rapid die replacement is met; and the flexibility and continuity of production are greatly improved, the production stagnation time caused by die damage or replacement is shortened, and the overall production efficiency and economic benefits are further improved.

Description

Technical Field

[0001] This utility model relates to the field of stamping device technology, and in particular to a stamping device for unmanned aerial vehicle (UAV) wings. Background Technology

[0002] In the field of drone manufacturing, the wing is a key component, and its processing quality directly affects the performance of the drone. The drone wing stamping device is an important piece of equipment for achieving efficient and precise processing of the wing.

[0003] Existing technology requires manual cutting of scrap materials after wing stamping, which increases manpower input and is time-consuming and labor-intensive. At the same time, if the mold is damaged and needs to be replaced, it takes a lot of time to cut and reinstall a new mold, which is cumbersome and cannot meet the need for rapid mold replacement. Utility Model Content

[0004] The purpose of this section is to outline some aspects of embodiments of the present invention and to briefly describe some preferred embodiments. Simplifications or omissions may be made in this section, as well as in the abstract and title of this application, to avoid obscuring the purpose of these documents; however, such simplifications or omissions should not be construed as limiting the scope of the present invention.

[0005] In view of the problems existing in the above and / or existing UAV wing stamping devices, this utility model is proposed.

[0006] Therefore, the problem that this utility model aims to solve is how to address the need for manual cutting of scrap materials, which increases manpower input, and the inability to quickly replace molds once they are damaged.

[0007] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a wing stamping device for unmanned aerial vehicles, comprising,

[0008] The main structure includes a base, a column, an upper mold, and a lower mold. The column is fixedly connected to the top of the base, the upper mold is located on the top of one side of the column, and the lower mold is located at the bottom of the upper mold; and...

[0009] A cutting assembly, disposed on the top of a base, includes a tipping bucket, a hinge, a cutter, a drive component, and a pusher. The tipping bucket is hinged to the top of the base via the hinge, and the bottom of the tipping bucket contacts a column. The cutter is disposed on the top of the lower mold, the drive component is disposed on one side of the cutter, and the pusher is disposed on one side of the drive component; and...

[0010] The assembly and disassembly components are located at the bottom of the lower mold and include an installation groove, an installation block, and a fixing component. The installation groove is located at the top of the tipping bucket, the installation block is fixedly connected to the bottom of the lower mold and cooperates with the installation groove, and the fixing component is located on one side of the installation block.

[0011] In a preferred embodiment of the UAV wing stamping device of this utility model, the driving component includes a motor fixedly connected to one side of the column, a lead screw fixedly connected to the output shaft of the motor, a first movable block threadedly connected to one side of the lead screw, and a cutter fixedly connected to one side of the first movable block.

[0012] As a preferred embodiment of the UAV wing stamping device of this utility model, the driving component further includes a first support block fixedly connected to one side of the cutter, and a first support groove is provided on one side of the base and cooperates with the first support block.

[0013] As a preferred embodiment of the UAV wing stamping device of this utility model, the pushing component includes a second movable block threadedly connected to the other side of the lead screw surface, a pushing roller fixedly connected to one side of the second movable block, and a triangular block fixedly connected to one side of the tipping bucket, which cooperates with the pushing roller.

[0014] As a preferred embodiment of the UAV wing stamping device of this utility model, the pushing member further includes a second support block fixedly connected to one side of the pushing roller, and the top of the base is provided with a second support groove that cooperates with the second support block.

[0015] In a preferred embodiment of the UAV wing stamping device of this utility model, the end of the lead screw is rotatably connected to a limiting block via a bearing, and the limiting block is fixedly connected to the top of the base.

[0016] As a preferred embodiment of the UAV wing stamping device of this utility model, the fixing member includes a fixing rod disposed on one side of the tipping bucket, one side of the fixing rod penetrating the tipping bucket and extending into the mounting groove, one side of the mounting block having a fixing groove and cooperating with the fixing rod, and one side of the fixing rod being disposed in the clamping part.

[0017] In a preferred embodiment of the UAV wing stamping device of this utility model, the clamping part includes a clamping plate fixedly connected to the surface of the fixing rod, a spring fixedly connected to one side of the clamping plate, and a tipping bucket fixedly connected to one side of the spring.

[0018] In a preferred embodiment of the UAV wing stamping device of this utility model, the springs are in multiple sets and are evenly distributed on one side of the clamping plate.

[0019] As a preferred embodiment of the UAV wing stamping device of this utility model, the fixing component further includes a first threaded hole opened on one side of the tipping bucket, and a second threaded hole opened on one side of the mounting block. The inner cavities of the first threaded hole and the second threaded hole are both threaded with bolts.

[0020] The beneficial effects of this utility model are as follows: by setting up a cutting component, manual cutting of the scrap material after wing stamping is avoided, reducing manpower input, improving work efficiency, and saving time and effort. The design of the disassembly and assembly component makes mold replacement operation simple, and the mold can be quickly disassembled and installed, meeting the need for rapid mold replacement. This greatly improves the flexibility and continuity of production, reduces the production downtime caused by mold damage or replacement, and thus improves overall production efficiency and economic benefits. Attached Figure Description

[0021] To more clearly illustrate the technical solutions of the embodiments of this utility model, the drawings used in the description of the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort. Among them:

[0022] Figure 1 This is a structural diagram of the wing stamping device for a drone.

[0023] Figure 2 This is a side view of the wing stamping device for a drone.

[0024] Figure 3 This is a side view of the styrofoam stamping device for a drone wing from another perspective.

[0025] Figure 4 This is a partial structural diagram of the drive and propulsion components of the wing stamping device for a drone.

[0026] Figure 5 This is an exploded view of the disassembled assembly structure of the wing stamping device for a drone.

[0027] Figure 6 Stamping device for drone wings Figure 5 Enlarged view of region A in the image.

[0028] In the diagram: 100, Main structure; 101, Base; 102, Column; 103, Upper mold; 104, Lower mold; 200, Cutting assembly; 201, Tilting bucket; 202, Hinge seat; 203, Cutting blade; 204, Driving component; 205, Pushing component; 300, Assembly / disassembly assembly; 301, Mounting slot; 302, Mounting block; 303, Fixing component; 204a, Motor; 204b, Lead screw; 204c, First movable block; 204d, First... Support block; 204e, first support groove; 205a, second movable block; 205b, push roller; 205c, triangular block; 205d, second support block; 205e, second support groove; 204b-1, limit block; 303a, fixing rod; 303b, fixing groove; 303c, clamping part; 303d, first threaded hole; 303e, second threaded hole; 303f, bolt; 303c-1, clamping plate; 303c-2, spring. Detailed Implementation

[0029] To make the above-mentioned objectives, features and advantages of this utility model more apparent and understandable, the specific embodiments of this utility model will be described in detail below with reference to the accompanying drawings.

[0030] Many specific details are set forth in the following description in order to provide a full understanding of the present invention. However, the present invention may also be implemented in other ways different from those described herein. Those skilled in the art can make similar extensions without departing from the spirit of the present invention. Therefore, the present invention is not limited to the specific embodiments disclosed below.

[0031] Secondly, the term "an embodiment" or "embodiment" as used herein refers to a specific feature, structure, or characteristic that may be included in at least one implementation of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a single or selective embodiment that excludes other embodiments.

[0032] Example 1

[0033] Reference Figures 1-6 This is the first embodiment of the present invention. This embodiment provides a drone wing stamping device. The drone wing stamping device includes a cutting component 200 and a disassembly and assembly component 300. The cutting component 200 avoids the need for manual cutting of the scrap material after wing stamping, reducing manpower input and improving work efficiency. The disassembly and assembly component 300 makes mold replacement operation simple and can quickly complete mold disassembly and installation.

[0034] Specifically, the main structure 100 includes a base 101, a column 102, an upper mold 103, and a lower mold 104. The column 102 is fixedly connected to the top of the base 101, the upper mold 103 is located on the top of one side of the column 102, and the lower mold 104 is located at the bottom of the upper mold 103; and,

[0035] A cutting assembly 200, disposed on the top of the base 101, includes a tipping bucket 201, a hinge 202, a cutter 203, a drive member 204, and a pusher 205. The tipping bucket 201 is hinged to the top of the base 101 via the hinge 202, and the bottom of the tipping bucket 201 contacts the column 102. The cutter 203 is disposed on the top of the lower mold 104, the drive member 204 is disposed on one side of the cutter 203, and the pusher 205 is disposed on one side of the drive member 204; and...

[0036] The assembly 300 is located at the bottom of the lower mold 104 and includes an installation groove 301, an installation block 302, and a fixing member 303. The installation groove 301 is located at the top of the tipping bucket 201. The installation block 302 is fixedly connected to the bottom of the lower mold 104 and cooperates with the installation groove 301. The fixing member 303 is located on one side of the installation block 302.

[0037] The base 101 serves as the supporting foundation for the entire device, maintaining its stability. The column 102 is fixed to the top of the base 101, providing a position for the installation and support of the upper mold 103. During the stamping operation, the upper mold 103 is driven downward by an external stamping power system (not described in detail in the text, usually a hydraulic or pneumatic drive device, which is existing technology and will not be described in detail here). It cooperates with the lower mold 104 located below it to apply pressure to the drone wing material to be stamped, causing it to undergo plastic deformation, thereby completing the stamping of the wing.

[0038] The tipping bucket 201 is hinged to the top of the base 101 via the hinge seat 202. When subjected to external force, the tipping bucket 201 can rotate around the hinge seat 202. Its bottom contacts the column 102, providing a certain support and limiting function. The cutter 203 is set on the top of the lower mold 104. After stamping, under the action of the drive component 204, the cutter 203 will move along a certain trajectory to cut the scrap material of the stamped wing. The drive component 204 provides power for the movement of the cutter 203 to achieve the cutting of the scrap material. The pusher 205 can realize the dumping of the collected scrap material for subsequent processing.

[0039] The mounting slot 301 and mounting block 302 provide a positioning and connection base for the installation of the lower mold 104, enabling the lower mold 104 to be accurately installed on the tipping bucket 201. The fixing part 303 achieves a firm connection between the lower mold 104 and the tipping bucket 201, while facilitating quick disassembly and installation to meet the needs of quick mold replacement.

[0040] Specifically, the drive unit 204 includes a motor 204a fixedly connected to one side of the column 102, a lead screw 204b fixedly connected to the output shaft of the motor 204a, a first movable block 204c threadedly connected to one side of the surface of the lead screw 204b, and a cutter 203 fixedly connected to one side of the first movable block 204c.

[0041] By fixing the motor 204a in the drive unit 204 to one side of the column 102, after the motor 204a is started, its output shaft drives the lead screw 204b fixedly connected to it to rotate. Since one side of the surface of the lead screw 204b is threadedly connected to the first movable block 204c, the rotation of the lead screw 204b will cause the first movable block 204c to move along the axial direction of the lead screw 204b. Since the first movable block 204c is fixedly connected to the cutter 203, the movement of the first movable block 204c will drive the cutter 203 to move, thereby realizing the cutting action of the cutter 203 on the scrap material of the stamped wing. In this way, the rotational motion of the motor 204a can be converted into the linear motion of the cutter 203 through the lead screw 204b and the first movable block 204c, providing power for the movement of the cutter 203, realizing the automatic cutting of scrap material, improving work efficiency and reducing manpower input.

[0042] Specifically, the drive component 204 also includes a first support block 204d fixedly connected to one side of the cutter 203, and a first support groove 204e is provided on one side of the base 101, which cooperates with the first support block 204d.

[0043] By fixing the first support block 204d to one side of the cutter 203 and cooperating with the first support groove 204e opened on one side of the base 101, the first support block 204d slides in the first support groove 204e as the cutter 203 moves axially along the lead screw 204b with the first movable block 204c. This provides support and guidance for the cutter 203, ensuring the stability and accuracy of the cutter 203's movement. This enhances the stability of the cutter 203 during movement and prevents it from shifting or shaking, thus ensuring the precision and quality of scrap cutting.

[0044] Specifically, the fixing member 303 includes a fixing rod 303a disposed on one side of the tipping bucket 201. One side of the fixing rod 303a passes through the tipping bucket 201 and extends into the mounting groove 301. A fixing groove 303b is provided on one side of the mounting block 302 and cooperates with the fixing rod 303a. One side of the fixing rod 303a is disposed in the clamping part 303c.

[0045] By setting the fixing rod 303a in the fixing member 303 on one side of the tipping bucket 201, with one side penetrating the tipping bucket 201 and extending into the mounting groove 301, after the mounting block 302 is inserted into the mounting groove 301, the fixing rod 303a is inserted into the fixing groove 303b opened on one side of the mounting block 302, thus achieving the initial fixation of the mounting block 302 and the tipping bucket 201. The clamping part 303c is set on one side of the fixing rod 303a to further fix the fixing rod 303a and prevent it from loosening. Thus, through the cooperation of the fixing rod 303a and the fixing groove 303b, the mounting block 302 at the bottom of the lower mold 104 can be firmly fixed in the mounting groove 301 at the top of the tipping bucket 201, ensuring the stability of the lower mold 104 during the stamping process, and providing a foundation for the further fixation of the clamping part 303c.

[0046] Specifically, the clamping part 303c includes a clamping plate 303c-1 fixedly connected to the surface of the fixing rod 303a, a spring 303c-2 fixedly connected to one side of the clamping plate 303c-1, and one side of the spring 303c-2 fixedly connected to the tipping bucket 201.

[0047] By fixing the clamping plate 303c-1 in the clamping part 303c to the surface of the fixing rod 303a, one side of the spring 303c-2 is fixedly connected to the clamping plate 303c-1, and the other side is fixedly connected to the tipping bucket 201. When the fixing rod 303a is inserted into the fixing groove 303b, the spring 303c-2 is in a compressed state. The elastic force generated causes the clamping plate 303c-1 to apply a force to the fixing rod 303a in the direction of the mounting groove 301, thereby ensuring that the fixing rod 303a and the fixing groove 303b are tightly fitted and preventing the fixing rod 303a from loosening. This enhances the tightness and stability of the fit between the fixing rod 303a and the fixing groove 303b, ensuring that the fixing rod 303a will not loosen due to vibration or other reasons during the stamping process of the lower die 104, and further improving the reliability of the installation of the lower die 104.

[0048] Specifically, there are multiple sets of springs 303c-2, which are evenly distributed on one side of the clamping plate 303c-1.

[0049] By evenly distributing multiple sets of springs 303c-2 on one side of the clamping plate 303c-1, these springs 303c-2 work together to generate a uniform elastic force distribution on the clamping plate 303c-1, so that the clamping plate 303c-1 applies a more uniform clamping force to the fixing rod 303a. This makes the clamping force on the fixing rod 303a more uniform in all directions, avoiding the situation where the fixing rod 303a tilts or loosens due to uneven local force, and further improving the fixing effect and stability of the fixing component 303 on the lower mold 104.

[0050] Specifically, the fastener 303 also includes a first threaded hole 303d on one side of the tipping bucket 201, and a second threaded hole 303e on one side of the mounting block 302. The inner cavities of the first threaded hole 303d and the second threaded hole 303e are both threadedly connected to bolts 303f.

[0051] By opening the first threaded hole 303d on one side of the tipping bucket 201 and the second threaded hole 303e on one side of the mounting block 302, after the mounting block 302 is inserted into the mounting groove 301 and the fixing rod 303a is inserted into the fixing groove 303b, the bolt 303f is screwed into the inner cavity of the first threaded hole 303d and the second threaded hole 303e. Through the threaded engagement of the bolt 303f and the threaded hole, the fixing of the mounting block 302 and the tipping bucket 201 is further strengthened. When disassembling, the bolt 303f is unscrewed first, and then other disassembly operations are performed. In this way, on the basis of fixing the fixing rod 303a and the clamping part 303c, the connection between the lower mold 104 and the tipping bucket 201 is further strengthened, and the installation firmness of the lower mold 104 is improved. At the same time, the bolt connection makes it easy to disassemble when the mold needs to be replaced, meeting the need for quick mold replacement.

[0052] Example 2

[0053] Reference Figure 2 and Figure 4 This is the second embodiment of the present invention, which is based on the previous embodiment.

[0054] Specifically, the pusher 205 includes a second movable block 205a threadedly connected to the other side of the surface of the lead screw 204b. A pusher roller 205b is fixedly connected to one side of the second movable block 205a, and a triangular block 205c is fixedly connected to one side of the tipping bucket 201 and cooperates with the pusher roller 205b.

[0055] By threading the second movable block 205a in the pusher 205 to the other side of the surface of the lead screw 204b, when the motor 204a drives the lead screw 204b to rotate, the second movable block 205a will move along the axial direction of the lead screw 204b. The movement of the second movable block 205a drives the push roller 205b fixedly connected to it to move. A triangular block 205c is fixed on one side of the tipping bucket 201. When the push roller 205b moves to contact the triangular block 205c, the push roller 205b will roll upward along the inclined surface of the triangular block 205c, thereby pushing the triangular block 205c to make the tipping bucket 201 rotate around the hinge seat 202, realizing the tipping bucket 201 flipping. Thus, the rotation of the lead screw 204b can be used to push the tipping bucket 201 to flip through the second movable block 205a and the push roller 205b, realizing the dumping of the scraps collected in the tipping bucket 201, which is convenient for the centralized processing of scraps and improves the continuity and efficiency of the work.

[0056] Specifically, the pusher 205 also includes a second support block 205d fixedly connected to one side of the pusher roller 205b, and a second support groove 205e is provided on the top of the base 101 and cooperates with the second support block 205d.

[0057] By fixing the second support block 205d to one side of the push roller 205b and cooperating with the second support groove 205e opened on the top of the base 101, the second support block 205d slides in the second support groove 205e during the process of the push roller 205b moving axially along the screw 204b with the second movable block 205a. This provides support and guidance for the push roller 205b, ensuring the stability of the push roller 205b's movement. This enhances the stability of the push roller 205b during its movement, ensuring that the push roller 205b can accurately cooperate with the triangular block 205c to smoothly push the tipping bucket 201 to flip, thus improving the reliability of the tipping bucket 201's flipping action.

[0058] Specifically, the end of the lead screw 204b is rotatably connected to a limit block 204b-1 via a bearing, and the limit block 204b-1 is fixedly connected to the top of the base 101.

[0059] By rotatably connecting the end of the lead screw 204b to a limiting block 204b-1 via a bearing, and fixing the limiting block 204b-1 to the top of the base 101, the limiting block 204b-1 restricts the axial movement of the lead screw 204b during the rotation of the lead screw 204b driven by the motor 204a, allowing the lead screw 204b to rotate only around its axis. This ensures the stability of the rotation of the lead screw 204b and prevents axial movement of the lead screw 204b during rotation, thereby ensuring that the first movable block 204c and the second movable block 205a can move accurately along the predetermined trajectory, thus improving the stability and reliability of the entire transmission system.

[0060] In use, the cutting assembly 200 and the disassembly assembly 300 work together. Regarding the cutting assembly 200, the tipping bucket 201 is hinged to the top of the base 101 via a hinge seat 202. Under normal conditions, the bottom contacts the column 102 and remains stable. After stamping is completed, the drive unit 204 starts working, and the motor 204a starts, driving the lead screw 204b to rotate. The first movable block 204c, threaded onto the lead screw 204b, moves axially along the lead screw. Since the first movable block 204c is fixedly connected to the cutter 203, the cutter 203 is positioned in the lower die. The top of the 104 unit moves to cut the wing scraps, thus avoiding manual operation and saving a lot of manpower and time. At the same time, the rotation of the lead screw 204b causes the second movable block 205a on the other side to move, which in turn drives the push roller 205b to move. When the push roller 205b contacts the triangular block 205c on one side of the tipping bucket 201, the push roller 205b rolls along the inclined surface of the triangular block 205c, pushing the tipping bucket 201 to flip around the hinge seat 202. This allows for the centralized collection and processing of the cut scraps, keeping the working environment clean and orderly.

[0061] When disassembling and assembling component 300, during the installation of the lower mold 104, the mounting block 302 at its bottom is aligned with the mounting groove 301 at the top of the tipping bucket 201 and inserted for initial positioning. Next, the fixing rod 303a is inserted through the tipping bucket 201 into the fixing groove 303b of the mounting block 302 for initial fixation. The clamping part 303c then functions, with the clamping plate 303c-1 fixed to the surface of the fixing rod 303a. Multiple evenly distributed springs 303c-2 are compressed, generating elastic force that causes the clamping plate 303c-1 to clamp the fixing rod 303a. 03a applies a force toward the mounting groove 301 to prevent the fixing rod 303a from loosening. Finally, the bolt 303f is screwed into the first threaded hole 303d on one side of the tipping bucket 201 and the second threaded hole 303e on the side of the mounting block 302 for further reinforcement. When disassembling, first unscrew the bolt 303f, and then pull out the fixing rod 303a against the elastic force of the spring 303c-2, so that the lower mold 104 can be removed. This can meet the need for quick mold change in production, reduce production downtime, and improve overall production efficiency.

[0062] It should be noted that the above embodiments are only used to illustrate the technical solution of this utility model and are not intended to limit it. Although this utility model has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solution of this utility model without departing from the spirit and scope of the technical solution of this utility model, and all such modifications or substitutions should be covered within the scope of the claims of this utility model.

Claims

1. A wing stamping device for unmanned aerial vehicles (UAVs), characterized in that: include, The main structure (100) includes a base (101), a column (102), an upper mold (103), and a lower mold (104). The column (102) is fixedly connected to the top of the base (101), the upper mold (103) is disposed on the top of one side of the column (102), and the lower mold (104) is located at the bottom of the upper mold (103). A cutting assembly (200), disposed on the top of a base (101), includes a tipping bucket (201), a hinge (202), a cutter (203), a drive member (204), and a pusher (205). The tipping bucket (201) is hinged to the top of the base (101) via the hinge (202), and the bottom of the tipping bucket (201) contacts the column (102). The cutter (203) is disposed on the top of the lower mold (104), the drive member (204) is disposed on one side of the cutter (203), and the pusher (205) is disposed on one side of the drive member (204). The assembly / disassembly component (300) is located at the bottom of the lower mold (104) and includes an installation groove (301), an installation block (302), and a fixing member (303). The installation groove (301) is located at the top of the tipping bucket (201). The installation block (302) is fixedly connected to the bottom of the lower mold (104) and cooperates with the installation groove (301). The fixing member (303) is located on one side of the installation block (302).

2. The UAV wing stamping device as described in claim 1, characterized in that: The drive unit (204) includes a motor (204a) fixedly connected to one side of the column (102), the output shaft of the motor (204a) is fixedly connected to a lead screw (204b), one side of the surface of the lead screw (204b) is threadedly connected to a first movable block (204c), and one side of the first movable block (204c) is fixedly connected to a cutter (203).

3. The UAV wing stamping device as described in claim 2, characterized in that: The drive unit (204) also includes a first support block (204d) fixedly connected to one side of the cutter (203), and a first support groove (204e) is provided on one side of the base (101) and cooperates with the first support block (204d).

4. The UAV wing stamping device as described in claim 3, characterized in that: The pusher (205) includes a second movable block (205a) threaded to the other side of the surface of the lead screw (204b). A push roller (205b) is fixedly connected to one side of the second movable block (205a). A triangular block (205c) is fixedly connected to one side of the tipping bucket (201) and cooperates with the push roller (205b).

5. The UAV wing stamping device as described in claim 4, characterized in that: The pusher (205) also includes a second support block (205d) fixedly connected to one side of the push roller (205b). The top of the base (101) is provided with a second support groove (205e) that cooperates with the second support block (205d).

6. The UAV wing stamping device as described in claim 5, characterized in that: The end of the lead screw (204b) is rotatably connected to a limiting block (204b-1) via a bearing, and the limiting block (204b-1) is fixedly connected to the top of the base (101).

7. The UAV wing stamping device as described in claim 6, characterized in that: The fixing member (303) includes a fixing rod (303a) disposed on one side of the tipping bucket (201). One side of the fixing rod (303a) passes through the tipping bucket (201) and extends into the mounting groove (301). One side of the mounting block (302) is provided with a fixing groove (303b) and cooperates with the fixing rod (303a). One side of the fixing rod (303a) is disposed in the clamping part (303c).

8. The UAV wing stamping device as described in claim 7, characterized in that: The clamping part (303c) includes a clamping plate (303c-1) fixedly connected to the surface of the fixing rod (303a). A spring (303c-2) is fixedly connected to one side of the clamping plate (303c-1), and one side of the spring (303c-2) is fixedly connected to the tipping bucket (201).

9. The UAV wing stamping device as described in claim 8, characterized in that: There are multiple sets of springs (303c-2), which are evenly distributed on one side of the clamping plate (303c-1).

10. The UAV wing stamping device as described in claim 9, characterized in that: The fastener (303) also includes a first threaded hole (303d) on one side of the tipping bucket (201), and a second threaded hole (303e) on one side of the mounting block (302). The inner cavities of the first threaded hole (303d) and the second threaded hole (303e) are both threaded with bolts (303f).

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