Unmanned aerial vehicle tail cover assembling equipment

Abstract

The utility model relates to the technical field of unmanned aerial vehicle tail cover assembling equipment, in particular to unmanned aerial vehicle tail cover assembling equipment which comprises a bottom frame, multiple sets of vertical pipes are assembled on the surface of the top end of the bottom frame, vertical cylinders are installed on the inner sides of the vertical pipes in a sliding mode, and frames located on the tops of the vertical pipes are assembled among the multiple sets of vertical cylinders. An electric push rod A used for pushing the vertical cylinder to ascend and descend is assembled in the vertical pipe. When the equipment for assembling the tail cover of the unmanned aerial vehicle is used, an electric push rod A in a vertical pipe at the top of a bottom frame can operate according to use requirements, the electric push rod A operates to conveniently push a vertical cylinder in the vertical pipe, so that the vertical cylinder ascends and descends under thrust and drives a frame to move, and the height of the frame is conveniently adjusted; and the height of the fixture at the top of the frame is changed accordingly, workers can conveniently use the fixture, and the unmanned aerial vehicle tail cover can be conveniently assembled.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle (UAV) tail cover assembly equipment, in particular to a UAV tail cover assembly equipment. Background Art

[0002] The aircraft tail cowl is a critical component of the aircraft structure, generally used to protect the aircraft's engine while meeting the overall aerodynamic shape requirements of the fuselage. Patent No. CN202122787512.5 discloses a UAV tail cowl assembly jig. Structural assembly is based on the positioning of skeleton components. This assembly method uses the skeleton's internal shape as a positioning reference to ensure the aircraft's shape, efficient assembly, and low-cost manufacturing. However, due to the fixed height of the assembly jig, workers often encounter certain inconveniences when using it to assemble the UAV tail cowl. To address this issue, we propose a UAV tail cowl assembly device. Utility Model Content

[0003] In view of the problems in the prior art, the utility model provides a UAV tail cover assembly device.

[0004] The technical solution adopted by the present invention to solve the technical problem is a UAV tail cover assembly device, comprising a base frame, a vertical tube mounted on the top surface of the base frame, and multiple sets of vertical tubes, vertical cylinders slidably mounted on the inner sides of the vertical tubes, and a frame located at the top of the vertical tubes is mounted between the multiple sets of vertical tubes, and an electric push rod A is mounted inside the vertical tubes for pushing the vertical tubes to move up and down;

[0005] An arc-shaped groove is provided on the bottom surface of the chassis, and there are multiple groups of arc-shaped grooves. A swing arm is hinged on the inner side of the arc-shaped groove, and a wheel is rotatably installed on the end of the swing arm away from the arc-shaped groove. Ear seats are installed between the outer wall of the swing arm and the inner wall of the arc-shaped groove, and an electric push rod B is hinged between the two groups of ear seats.

[0006] By adopting the above technical solution, when the equipment for assembling the tail cover of the drone is used, the electric push rod A in the vertical tube at the top of the chassis can be operated according to the needs during use. The operation of the electric push rod A facilitates the pushing of the vertical cylinder in the vertical tube, so that the vertical cylinder moves up and down under the thrust and drives the frame to move, which is convenient for adjusting the height of the frame and causing the jig on the top of the frame to change its height accordingly, making it convenient for the staff to use the jig and facilitate the assembly of the tail cover of the drone;

[0007] When the position of the assembly equipment for the tail cover of the drone needs to be adjusted, the electric push rod B in the arc-shaped groove at the bottom of the chassis can be operated. The electric push rod B can conveniently push the swing arm hinged in the arc-shaped groove through the ear seat, so that the swing arm swings out of the arc-shaped groove under the action of thrust, and conveniently drives the wheels to support the chassis, and the assembly equipment is supported accordingly, thereby facilitating the movement of the chassis and the adjustment of the position of the assembly equipment. After the adjustment is completed, the wheels can be conveniently retracted into the arc-shaped groove for easy storage.

[0008] Specifically, a square groove is opened on the outer wall surface of the vertical tube, and a vertical plate that fits the square groove is assembled on the bottom surface of the frame. The outer wall surface of the vertical plate and the outer wall of the vertical tube are both coated with scale lines.

[0009] By adopting the above technical solution, the vertical plate can be easily slid and displaced in the square groove, and when the frame is raised or lowered, it can be easily driven to move the vertical plate in the square groove. The scale lines on the outer periphery of the vertical plate and the scale lines on the outer periphery of the vertical tube can cooperate with each other, so that personnel can more clearly understand the distance between the frame and the base frame after movement, which is convenient for personnel to adjust.

[0010] Specifically, transverse plates are installed between the multiple groups of vertical pipes, and there are multiple groups of transverse plates.

[0011] By adopting the above technical solution, the horizontal plate facilitates supporting multiple groups of vertical pipes, so that the vertical pipes can be used more stably.

[0012] Specifically, the inner wall of the vertical tube and the outer wall of the vertical cylinder are both provided with grooves, and there are multiple groups of grooves. The inner wall of the vertical tube and the outer wall of the vertical cylinder are both integrally constructed with convex strips that fit with the grooves.

[0013] By adopting the above technical solution, the convex strips and the grooves fit together, which facilitates improving the stability of the vertical cylinder when it slides and displaces inside the vertical pipe.

[0014] Specifically, the inner wall of the base frame is equipped with a battery pack, and the outer wall of the vertical pipe is equipped with a controller electrically connected to the battery pack.

[0015] By adopting the above technical solution, the battery pack can conveniently provide power support for the operation of the electric push rod A and the electric push rod B, and the controller can conveniently control the operation of the two. At the same time, the operation of the electric push rod A and the electric push rod B can also be controlled without the need for an external power supply.

[0016] Compared with the prior art, the present invention has the following beneficial effects:

[0017] 1. The technical solution of the present application, through the design of the vertical tube, vertical cylinder, frame and electric push rod A, can operate the electric push rod A in the vertical tube at the top of the base frame according to the needs during use when the equipment for assembling the tail cover of the drone is used. The operation of the electric push rod A facilitates pushing the vertical cylinder in the vertical tube, so that the vertical cylinder is lifted and lowered under the thrust and drives the frame to move, which is convenient for adjusting the height of the frame and causing the jig on the top of the frame to change its height accordingly, making it convenient for the staff to use the jig and facilitate the assembly of the tail cover of the drone.

[0018] 2. The technical solution of the present application, through the design of the arc groove, swing arm, wheel, ear seat and electric push rod B, can enable the electric push rod B in the arc groove at the bottom of the chassis to operate when it is necessary to adjust the position of the assembly equipment for the tail cover of the drone. The operation of the electric push rod B is convenient for pushing the swing arm hinged in the arc groove through the ear seat, so that the swing arm swings out of the arc groove under the action of the thrust, and conveniently drives the wheel to support the chassis, and the assembly equipment is supported accordingly, thereby facilitating the movement of the chassis and the adjustment of the position of the assembly equipment. After the adjustment is completed, the wheel can be conveniently retracted into the arc groove for easy storage. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0020] Figure 1 This is an axonometric drawing of the present utility model;

[0021] Figure 2 This is an exploded view of the connection structure between the vertical cylinder and the vertical pipe of the present utility model;

[0022] Figure 3 This is a schematic plan view of the inner structure of the arc-shaped groove of the present invention;

[0023] In the figure: 1. Base frame; 2. Vertical tube; 3. Vertical cylinder; 4. Frame; 5. Electric push rod A; 6. Arc groove; 7. Swing arm; 8. Wheel; 9. Ear seat; 10. Electric push rod B; 11. Groove; 12. Raised strip; 13. Square groove; 14. Vertical plate; 15. Scale line; 16. Horizontal plate; 17. Battery pack; 18. Controller. DETAILED DESCRIPTION

[0024] In order to make the technical means, creative features, objectives and effects achieved by the present invention easier to understand, the present invention is further described below in conjunction with specific implementation methods.

[0025] See also Figure 1-3The embodiment of the utility model provides a technical solution: an assembly device for a tail cover of an unmanned aerial vehicle, comprising a base frame 1, a vertical tube 2 being assembled on the top surface of the base frame 1, and the vertical tube 2 having multiple groups, a vertical cylinder 3 being slidably mounted on the inside of the vertical tube 2, and a frame 4 being assembled between the multiple groups of vertical cylinders 3 and located at the top of the vertical tube 2, an electric push rod A5 being assembled inside the vertical tube 2 for pushing the vertical cylinder 3 up and down; an arc-shaped groove 6 being opened on the bottom surface of the base frame 1, and the arc-shaped groove 6 having multiple groups, a swing arm 7 being hinged on the inside of the arc-shaped groove 6, and a wheel 8 being rotatably mounted on the end of the swing arm 7 away from the arc-shaped groove 6, an ear seat 9 being assembled between the outer wall of the swing arm 7 and the inner wall of the arc-shaped groove 6, and an electric push rod B10 being hinged between the two groups of ear seats 9.

[0026] During use, when the equipment for assembling the tail cover of the drone is used, the electric push rod A5 in the vertical tube 2 at the top of the base frame 1 can be operated according to the needs of use. The operation of the electric push rod A5 facilitates the pushing of the vertical cylinder 3 in the vertical tube 2, so that the vertical cylinder 3 is moved up and down under the thrust and drives the frame 4 to move, which is convenient for adjusting the height of the frame 4 and causing the jig on the top of the frame 4 to change its height accordingly, making it convenient for the staff to use the jig and facilitate the assembly of the tail cover of the drone;

[0027] When it is necessary to adjust the position of the assembly equipment for the tail cover of the drone, the electric push rod B10 in the arc groove 6 at the bottom of the chassis 1 can be operated. The electric push rod B10 can conveniently push the swing arm 7 hinged in the arc groove 6 through the ear seat 9, so that the swing arm 7 swings out of the arc groove 6 under the action of the thrust, and conveniently drives the wheel 8 to support the chassis 1, and the assembly equipment is supported accordingly, thereby facilitating the movement of the chassis 1 and the adjustment of the position of the assembly equipment. After the adjustment is completed, the wheel 8 can be conveniently retracted into the arc groove 6 for easy storage.

[0028] like Figure 1 As shown, a square groove 13 is opened on the outer wall surface of the vertical tube 2, and a vertical plate 14 is assembled on the bottom surface of the frame 4 to fit with the square groove 13. The outer wall surface of the vertical plate 14 and the outer wall of the vertical tube 2 are both coated with scale lines 15.

[0029] When in use, the vertical plate 14 can slide and move in the square groove 13 conveniently. When the frame 4 is lifted or lowered, the vertical plate 14 can be driven to move in the square groove 13 conveniently. The scale lines 15 on the outer periphery of the vertical plate 14 and the scale lines 15 on the outer periphery of the vertical tube 2 can cooperate with each other, so that personnel can more clearly understand the distance between the frame 4 and the base frame 1 after movement, which is convenient for personnel to adjust.

[0030] like Figure 1 As shown, transverse plates 16 are installed between the multiple groups of vertical pipes 2, and there are multiple groups of transverse plates 16.

[0031] When in use, the horizontal plate 16 facilitates support between multiple groups of vertical pipes 2, so that the vertical pipes 2 can be used more stably.

[0032] like Figure 2 As shown, grooves 11 are formed on the inner wall of the vertical tube 2 and the outer wall of the vertical cylinder 3 , and there are multiple groups of grooves 11 . The inner wall of the vertical tube 2 and the outer wall of the vertical cylinder 3 are integrally constructed with ridges 12 that fit with the grooves 11 .

[0033] When in use, the ridges 12 and the grooves 11 fit together, thereby improving the stability of the vertical cylinder 3 when it slides inside the vertical pipe 2 .

[0034] like Figure 1 As shown, a battery pack 17 is mounted on the inner wall of the base frame 1 , and a controller 18 electrically connected to the battery pack 17 is mounted on the outer wall of the vertical tube 2 .

[0035] When in use, the battery pack 17 provides power support for the operation of the electric push rod A5 and the electric push rod B10, and the controller 18 facilitates the control of the operation of the two. At the same time, the operation of the electric push rod A5 and the electric push rod B10 can be controlled without an external power supply.

[0036] The working principle and use process of the utility model are as follows: when in use, first install the corresponding structural components in the appropriate position. When using the equipment for assembling the tail cover of the drone, the electric push rod A5 in the vertical tube 2 at the top of the base frame 1 can be operated according to the needs of use. The operation of the electric push rod A5 facilitates the pushing of the vertical cylinder 3 in the vertical tube 2, so that the vertical cylinder 3 is lifted and displaced under the thrust and drives the frame 4 to move, which is convenient for adjusting the height of the frame 4 and making the height of the frame at the top of the frame 4 change accordingly, making it convenient for the staff to use the frame and facilitate the assembly of the drone tail cover. Assembly, at the same time, when it is necessary to adjust the position of the assembly equipment for the tail cover of the drone, the electric push rod B10 in the arc groove 6 at the bottom of the chassis 1 can be operated. The electric push rod B10 can conveniently push the swing arm 7 hinged in the arc groove 6 through the ear seat 9, so that the swing arm 7 swings out from the arc groove 6 under the action of thrust, and conveniently drives the wheel 8 to support the chassis 1, and the assembly equipment is supported accordingly, so as to facilitate the movement of the chassis 1 and the adjustment of the position of the assembly equipment, and after the adjustment is completed, it is convenient to retract the wheel 8 into the arc groove 6 for storage.

[0037] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely illustrative of the principles of the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention. Such changes and improvements are intended to fall within the scope of the present invention. The scope of protection claimed in the present invention is defined by the appended claims and their equivalents.

Claims

1. A UAV tail cover assembly device, characterized in that: The utility model comprises a base frame (1), wherein a vertical tube (2) is mounted on the top surface of the base frame (1), and the vertical tubes (2) are provided in a plurality of groups, a vertical cylinder (3) is slidably mounted on the inner side of the vertical tube (2), and a frame (4) located at the top of the vertical tube (2) is mounted between the plurality of groups of vertical cylinders (3), and an electric push rod A (5) is mounted inside the vertical tube (2) for pushing the vertical cylinder (3) to move up and down; The bottom surface of the chassis (1) is provided with an arc-shaped groove (6), and there are multiple groups of arc-shaped grooves (6). A swing arm (7) is hingedly connected to the inner side of the arc-shaped groove (6), and a wheel (8) is rotatably mounted on the end of the swing arm (7) away from the arc-shaped groove (6). Ear seats (9) are installed between the outer wall of the swing arm (7) and the inner wall of the arc-shaped groove (6), and an electric push rod B (10) is hingedly connected between the two groups of ear seats (9).

2. The UAV tail cover assembly equipment according to claim 1, characterized in that: The outer wall surface of the vertical tube (2) is provided with a square groove (13), and the bottom surface of the frame (4) is equipped with a vertical plate (14) that fits with the square groove (13), and the outer wall surface of the vertical plate (14) and the outer wall of the vertical tube (2) are both coated with scale lines (15).

3. The UAV tail cover assembly equipment according to claim 1, characterized in that: A transverse plate (16) is installed between the plurality of groups of vertical pipes (2), and there are a plurality of groups of transverse plates (16).

4. The UAV tail cover assembly equipment according to claim 1, characterized in that: The inner wall of the vertical tube (2) and the outer wall of the vertical cylinder (3) are both provided with grooves (11), and there are multiple groups of grooves (11). The inner wall of the vertical tube (2) and the outer wall of the vertical cylinder (3) are both integrally constructed with convex strips (12) that fit with the grooves (11).

5. The UAV tail cover assembly equipment according to claim 1, characterized in that: The inner wall of the base frame (1) is equipped with a battery pack (17), and the outer wall of the vertical pipe (2) is equipped with a controller (18) electrically connected to the battery pack (17).

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