Unmanned aerial vehicle assembling device
By using hydraulic rods and push blocks in the drone assembly device to achieve rapid loading and unloading of parts, combined with the efficient assembly of stepper motors and clamping blocks, the problems of low assembly convenience and efficiency in the existing technology are solved, and efficient assembly of drone parts is achieved.
Patent Information
- Application Number
- CN202520188881.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-02-07
- Publication Date
- 2026-01-02
- Estimated Expiration
- 2035-02-07
AI Technical Summary
Existing assembly equipment cannot quickly load and unload drone parts, resulting in poor assembly convenience and low assembly efficiency.
The drone assembly device, which includes a base, a conveying assembly, and a hydraulic cylinder, enables rapid loading and unloading of parts through hydraulic rods and push blocks, and efficient assembly through stepper motors and clamping blocks.
It enables rapid loading and unloading of drone parts, improving the convenience and efficiency of assembly.
Smart Images

Figure CN223748997U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to unmanned plane assembly technical field, concretely is a kind of unmanned plane assembly device. BACKGROUND
[0002] Intelligent unmanned aircraft is a kind of aircraft that can perform flight tasks without human control, it is usually equipped with autonomous navigation system, sensor, camera and other equipment, assembly device needs to be used in the process of assembling unmanned plane.
[0003] One Chinese patent with application publication number CN 118637073 A discloses a fixed-wing unmanned aerial vehicle tail wing assembly device, relating to unmanned aerial vehicle technical field, the device includes bottom plate and moving plate, characterized in that, still include fixed assembly and rotating assembly, the bottom plate upper surface is provided with two moving plates, the moving plate upper surface is fixedly connected with fixed frame, the fixed assembly includes hydraulic cylinder, lifting box, rotating shaft, clamping block, the fixed frame is connected with two symmetrical rotating shafts through bearing, one end of the rotating shaft is fixedly connected with gear, the rotating shaft is fixedly connected with clamping block and penetrates, the moving plate upper surface is fixedly connected with hydraulic cylinder.The present application completes the automatic fixing of unmanned aerial vehicle fuselage by fixed assembly, without manual fixing of unmanned aerial vehicle, and the fixing operation is quick and convenient;Unmanned aerial vehicle is rotated by rotating assembly 360 degrees, and it is convenient for staff to check unmanned aerial vehicle after assembly.
[0004] The existing assembly device cannot quickly feed and discharge the parts of unmanned aerial vehicle during the assembly process of unmanned aerial vehicle, so that the convenience of assembly is poor;Therefore, in view of the above problems, an unmanned aerial vehicle assembly device is proposed. UTILITY MODEL CONTENT
[0005] In order to make up for the deficiencies of prior art and solve the problems existing in prior art, the utility model provides an unmanned aerial vehicle assembly device.
[0006] The utility model discloses a technical scheme that solves its technical problem adopts a kind of unmanned vehicle assembling device, including base, first conveying assembly is installed on the base by foot support, first conveying assembly includes guide table, is set in the conveying groove in the guide table, four groups of fixing frame are installed on the guide table, first hydraulic cylinder, second hydraulic cylinder, third hydraulic cylinder and fourth hydraulic cylinder are respectively installed on four groups of fixing frame, first hydraulic cylinder, second hydraulic cylinder, third hydraulic cylinder and fourth hydraulic cylinder are respectively installed with first hydraulic rod, second hydraulic rod, third hydraulic rod and fourth hydraulic rod, push block is installed on first hydraulic rod, second hydraulic rod, third hydraulic rod and fourth hydraulic rod, first conveying assembly is placed with multiple groups of first fixture in the conveying groove, organism is placed in the first fixture, second conveying assembly is installed on the base by foot support, multiple groups of second fixture are placed in the conveying groove of second conveying assembly, four groups of paddle are placed in the second fixture, push block is moved horizontally backward and retracts by first hydraulic rod, first fixture removes the organism that assembly is completed from assembly position, realizes to organism blanking, push block promotes all first fixture at the front end of conveying groove and moves one position to right, first fixture drives the organism to be assembled and moves to assembly position, realizes to the organism feeding, this structure can be the part of unmanned vehicle and carry out fast feeding and blanking, be favorable to the convenience of improving assembly.
[0007] Preferably, the base is provided with a support frame, a control panel is installed on the side wall of the support frame, an installation plate is installed on the support frame, a moving groove is formed in the installation plate, a first stepper motor is installed on the side wall of the installation plate through a machine base, a first screw rod is installed on the output shaft of the first stepper motor, the first screw rod is rotatably installed in the moving groove, a moving block is assembled in the moving groove, an installation frame is installed on the moving block, a fifth hydraulic cylinder is installed on the installation frame, a fifth hydraulic rod is installed on the fifth hydraulic cylinder, a lifting plate is installed at the bottom side of the fifth hydraulic rod, four guide plates are installed at the bottom side of the lifting plate, a sliding groove is formed in the guide plate, two groups of sliding blocks are symmetrically assembled in the sliding groove, a clamping block is installed at the bottom side of the sliding block, a second stepper motor is installed on the side wall of the guide plate through a machine base, a second screw rod is installed on the output shaft of the second stepper motor, the second screw rod is rotatably installed in the sliding groove, the thread direction of the second screw rod is symmetrically opposite, four clamping blocks clamp four paddles by simultaneous operation of the four second stepper motors; then the lifting plate moves directly above the first fixture, four clamping blocks drive four paddles to move vertically downward, so that four paddles are simultaneously inserted into four shafts of the organism, achieving efficient assembly of four paddles and the organism, and improving assembly efficiency.
[0008] The utility model has the advantages that:
[0009] 1. The utility model discloses a first hydraulic rod drives push block horizontal backward movement and retracts, and the first fixture drives the assembled body to remove the assembly position, realizes the body blanking, and push block promotes all first fixtures of the front end of conveying groove to move right one position, and the first fixture drives the body to be assembled to move to the assembly position, realizes the body feeding, and this structure can be the part of unmanned plane and carries out quick feeding and unloading, is favorable to improve the convenience of assembly.
[0010] 2. The utility model discloses through four groups of second stepper motor simultaneous operation, four groups of clamping block are clamped to four oars, after lifting plate moves to the just above first fixture, four groups of clamping block drive four oars vertical downward movement, make four oars be inserted on four pivot of body simultaneously, realize four oars and the efficient assembly of body, be favorable to improve the assembly efficiency. DRAWINGS
[0011] In order to more clearly illustrate the technical scheme in the embodiment of the utility model or prior art, below will to the drawing needed to be used in the embodiment or prior art description simple introduction, obviously, the drawing in the following description only some embodiments of the utility model, for those skilled in the art, under the premise of not paying the creative labor, can also obtain other drawings according to these drawings.
[0012] Figure 1 It is first perspective three-dimensional structure schematic view;
[0013] Figure 2 It is first conveying assembly three-dimensional three-dimensional structure schematic view;
[0014] Figure 3 It is first fixture three-dimensional structure schematic view;
[0015] Figure 4 It is second fixture three-dimensional structure schematic view;
[0016] Figure 5 It is clamping block place three-dimensional structure schematic view.
[0017] In the drawing: 1, base;2, guide table;3, conveying groove;4, fixed frame;5, first hydraulic cylinder;6, second hydraulic cylinder;7, third hydraulic cylinder;8, fourth hydraulic cylinder;9, push block;10, first fixture;11, body;12, second conveying assembly;13, second fixture;14, oar;15, support frame;16, control panel;17, mounting plate;18, moving groove;19, first stepper motor;20, first screw;21, moving block;22, mounting frame;23, fifth hydraulic cylinder;24, lifting plate;25, guide plate;26, sliding slot;27, second stepper motor;28, clamping block. DETAILED DESCRIPTION
[0018] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments of the utility model, all other embodiments obtained by those skilled in the art without creative labor belong to the protection scope of the utility model.
[0019] Please refer to Figures 1-4 As shown in FIG. 1, a kind of unmanned aerial vehicle assembly device, including base 1, first conveying assembly is installed on base 1 by support, first conveying assembly includes guide table 2, conveying groove 3 is opened in guide table 2, four sets of fixing frame 4 are installed on guide table 2, first hydraulic cylinder 5, second hydraulic cylinder 6, third hydraulic cylinder 7 and fourth hydraulic cylinder 8 are respectively installed on four sets of fixing frame 4, first hydraulic rod, second hydraulic rod, third hydraulic rod and fourth hydraulic rod are respectively installed on first hydraulic cylinder 5, second hydraulic cylinder 6, third hydraulic cylinder 7 and fourth hydraulic cylinder 8, push block 9 is installed on first hydraulic rod, second hydraulic rod, third hydraulic rod and fourth hydraulic rod, multiple groups of first fixture 10 are placed in the conveying groove 3 of first conveying assembly, organism 11 is placed in first fixture 10, second conveying assembly 12 is installed on base 1 by support, multiple groups of second fixture 13 are placed in the conveying groove 3 of second conveying assembly 12, four groups of paddle 14 are placed in second fixture 13;When working, existing assembly device cannot quickly feed and discharge the parts of unmanned aerial vehicle in the process of assembling unmanned aerial vehicle, so that the convenience of assembly is poor, by placing multiple unmanned aerial vehicle organisms 11 in multiple first fixtures 10, multiple paddles 14 are placed in multiple second fixtures 13, the guide table 2 below mounting plate 17 in first conveying assembly is assembly site, when organism 11 and paddle 14 on assembly site are assembled, first hydraulic cylinder 5 operates, first hydraulic rod drives push block 9 to move horizontally backward and retract, push block 9 drives all first fixtures 10 at the right end of conveying groove 3 to move one position backward, first fixture 10 drives assembled organism 11 to move out of assembly site, achieving organism 11 discharge;
[0020] Then second hydraulic cylinder 6 operates, second hydraulic rod drives push block 9 to move horizontally right and retract, push block 9 drives all first fixtures 10 at the front end of conveying groove 3 to move one position right, first fixture 10 drives organism 11 to be assembled to move to assembly site, achieving organism 11 feeding;
[0021] Then third hydraulic cylinder 7 and fourth hydraulic cylinder 8 operate in turn, achieving the circulation of first fixture 10, similarly, second conveying assembly 12 operates, drives second fixture 13 on it to circulate, achieving paddle 14 feeding and discharging;This structure can quickly feed and discharge the parts of unmanned aerial vehicle, which is conducive to improving the convenience of assembly.
[0022] Please refer to Figure 5 As shown, the base 1 is installed with a support frame 15, the side wall of the support frame 15 is installed with a control panel 16, the support frame 15 is installed with a mounting plate 17, the mounting plate 17 is provided with a moving groove 18, the side wall of the mounting plate 17 is installed with a first stepper motor 19 through the machine base, the output shaft of the first stepper motor 19 is installed with a first lead screw 20, the first lead screw 20 is rotatably installed in the moving groove 18, the moving groove 18 is assembled with a moving block 21, the moving block 21 is installed with a mounting frame 22, the mounting frame 22 is installed with a fifth hydraulic cylinder 23, the fifth hydraulic cylinder 23 is installed with a fifth hydraulic rod, the fifth hydraulic rod is installed with a lifting plate 24 at the bottom side, the lifting plate 24 is installed with four groups of guide plates 25 at the bottom side, the guide plates 25 are provided with a sliding groove 26, the sliding groove 26 is symmetrically assembled with two groups of sliding blocks, the sliding blocks are installed with clamping blocks 28 at the bottom side, the side wall of the guide plates 25 is installed with a second stepper motor 27 through the machine base, the output shaft of the second stepper motor 27 is installed with a second lead screw, the second lead screw is rotatably installed in the sliding groove 26, and the thread directions of the second lead screws are symmetrically opposite; During work, the existing assembly device can only assemble one part at a time during the assembly of the unmanned aerial vehicle, resulting in low assembly efficiency. The lifting plate 24 is located directly above the second jig 13, the fifth hydraulic cylinder 23 operates, the fifth hydraulic rod drives the lifting plate 24 to move vertically downward, the lifting plate 24 drives the four groups of guide plates 25 to move vertically downward, then the four groups of second stepper motors 27 operate simultaneously, driving the second lead screws to rotate, the second lead screws drive the two sliding blocks thereon to move synchronously and oppositely, the two sliding blocks drive the two clamping blocks 28 to move synchronously and oppositely, and the two clamping blocks 28 clamp and fix the paddle 14, that is, the four clamping blocks 28 clamp and fix the four paddles 14. Then the fifth hydraulic rod drives the lifting plate 24 to move vertically upward, the first stepper motor 19 operates, driving the first lead screw 20 to rotate, the first lead screw 20 drives the moving block 21 thereon to move horizontally to the left, so that the moving block 21 drives the lifting plate 24 to move to the upper side of the first jig 10, then the fifth hydraulic rod drives the lifting plate 24 to move vertically downward, the lifting plate 24 drives the four groups of clamping blocks 28 to move vertically downward, and the four groups of clamping blocks 28 drive the four paddles 14 to move vertically downward, so that the four paddles 14 are simultaneously inserted on the four rotating shafts of the machine body 11, realizing efficient assembly of the four paddles 14 and the machine body 11, and facilitating improvement of assembly efficiency.
[0023] The working principle is that in the process of assembling the unmanned aerial vehicle, the existing assembly device can usually only assemble one part at a time, resulting in low assembly efficiency. The lifting plate 24 is located directly above the second jig 13. The fifth hydraulic cylinder 23 operates, the fifth hydraulic rod drives the lifting plate 24 to move vertically downward, the lifting plate 24 drives the four sets of guide plates 25 to move vertically downward, and then the four sets of second stepping motors 27 operate simultaneously, driving the second lead screws to rotate, the second lead screws drive the two sliders on them to move synchronously, the two sliders drive the two clamping blocks 28 to move synchronously, the two clamping blocks 28 clamp and fix the blades 14, that is, the four clamping blocks 28 clamp the four blades 14. Then the fifth hydraulic rod drives the lifting plate 24 to move vertically upward, the first stepping motor 19 operates, driving the first lead screw 20 to rotate, the first lead screw 20 drives the moving block 21 on it to move horizontally to the left, so that the moving block 21 drives the lifting plate 24 to move to the upper side of the first jig 10, and then the fifth hydraulic rod drives the lifting plate 24 to move vertically downward, the lifting plate 24 drives the four sets of clamping blocks 28 to move vertically downward, and the four sets of clamping blocks 28 drive the four blades 14 to move vertically downward, so that the four blades 14 are simultaneously inserted on the four shafts of the body 11, realizing efficient assembly of the four blades 14 and the body 11, and facilitating improvement of assembly efficiency. In the process of assembling the unmanned aerial vehicle, the existing assembly device cannot quickly feed and discharge the parts of the unmanned aerial vehicle, resulting in poor assembly convenience. The bodies 11 of multiple unmanned aerial vehicles are placed in multiple first jigs 10, and the blades 14 are placed in multiple second jigs 13. The guide table 2 below the mounting plate 17 in the first conveying assembly is the assembly position. When the bodies 11 and blades 14 on the assembly position are assembled, the first hydraulic cylinder 5 operates, the first hydraulic rod drives the push block 9 to move horizontally backward and retract, the push block 9 pushes all the first jigs 10 at the right end of the conveying groove 3 to move one position backward, the first jig 10 drives the assembled body 11 to move out of the assembly position, realizing discharging of the body 11. Then the second hydraulic cylinder 6 operates, the second hydraulic rod drives the push block 9 to move horizontally to the right and retract, the push block 9 pushes all the first jigs 10 at the front end of the conveying groove 3 to move one position to the right, the first jig 10 drives the body 11 to be assembled to move to the assembly position, realizing feeding of the body 11. Then the third hydraulic cylinder 7 and the fourth hydraulic cylinder 8 operate in turn, realizing circulation of the first jig 10. Similarly, the second conveying assembly 12 operates, driving the second jigs 13 on it to circulate, realizing feeding and discharging of the blades 14. This structure can quickly feed and discharge the parts of the unmanned aerial vehicle, facilitating improvement of assembly convenience.
[0024] The basic principle, main features and advantages of the present application are shown and described above. Those skilled in the art should understand that the present application is not limited by the above examples, and the above examples and descriptions in the specification are only to illustrate the principles of the present application. Without departing from the spirit and scope of the present application, various changes and improvements can be made to the present application, and these changes and improvements all fall within the scope of the claimed present application.
Claims
1. An unmanned aerial vehicle assembly apparatus, characterized by: The utility model provides a kind of first transmission assembly and second transmission assembly, including base (1), first transmission assembly is installed on the base (1) by trestle, first transmission assembly includes guide platform (2), transmission slot (3) is opened in the guide platform (2), four groups of fixed frame (4) are installed on the guide platform (2), first hydraulic cylinder (5), second hydraulic cylinder (6), third hydraulic cylinder (7) and fourth hydraulic cylinder (8) are respectively installed on four groups of fixed frame (4), first hydraulic rod, second hydraulic rod, third hydraulic rod and fourth hydraulic rod are respectively installed on the first hydraulic cylinder (5), second hydraulic cylinder (6), third hydraulic cylinder (7) and fourth hydraulic cylinder (8), push block (9) is installed on first hydraulic rod, second hydraulic rod, third hydraulic rod and fourth hydraulic rod, multiple groups of first fixture (10) are placed in the transmission slot (3) of first transmission assembly, organism (11) is placed in the first fixture (10), second transmission assembly (12) is installed on the base (1) by trestle, multiple groups of second fixture (13) are placed in the transmission slot (3) of second transmission assembly (12), four groups of paddle (14) are placed in the second fixture (13).
2. The unmanned aerial vehicle assembly device of claim 1, wherein: Support frame (15) is installed on the base (1), control panel (16) is installed on the side wall of support frame (15), mounting plate (17) is installed on the support frame (15).
3. The unmanned aerial vehicle assembly apparatus of claim 2, wherein: Moving slot (18) is opened in the mounting plate (17), first stepper motor (19) is installed on the side wall of mounting plate (17) by machine base, first lead screw (20) is installed on the output shaft of first stepper motor (19), first lead screw (20) is rotatably installed in moving slot (18).
4. The unmanned aerial vehicle assembly device of claim 3, wherein: Moving block (21) is assembled in the moving slot (18), mounting frame (22) is installed on the moving block (21), fifth hydraulic cylinder (23) is installed on the mounting frame (22), fifth hydraulic rod is installed on the fifth hydraulic cylinder (23), lifting plate (24) is installed on the bottom side of fifth hydraulic rod.
5. The unmanned aerial vehicle assembly apparatus of claim 4, wherein: Four groups of guide plates (25) are installed on the bottom side of lifting plate (24), sliding groove (26) is opened in the guide plate (25), two groups of sliding blocks are symmetrically assembled in the sliding groove (26), clamping block (28) is installed on the bottom side of sliding block.
6. The unmanned aerial vehicle assembly apparatus of claim 5, wherein: Second stepper motor (27) is installed on the side wall of guide plate (25) by machine base, second lead screw is installed on the output shaft of second stepper motor (27), second lead screw is rotatably installed in sliding groove (26), the thread direction on second lead screw is symmetrically opposite.
Citation Information
Patent Citations
Assembling device for empennage of fixed-wing unmanned aerial vehicle
CN118637073A