Assembly tool for additional module on unmanned aerial vehicle clamping seat

Abstract

The utility model discloses an assembly tool for an additional module on a clamping seat of an unmanned aerial vehicle. The assembly tool comprises the clamping seat located on the unmanned aerial vehicle and the additional module locked or unlocked with the clamping seat through a quick connecting mechanism. A retaining cavity is partially formed in the clamping seat, a clamping mechanism is arranged at the position, close to the retaining cavity, of the additional module, and the inner wall of the retaining cavity and the outer wall of the additional module are limited and clamped through the clamping mechanism. Fixing screw holes do not need to be additionally arranged, flexible assembly of the additional module on the clamping seat is achieved, the clamping seat is suitable for additional arrangement of various modules, and a foundation is provided for development of more functions of the unmanned aerial vehicle.

Description

TECHNICAL FIELD

[0001] The utility model relates to the increase technical field of micro module on unmanned plane, especially the assembly tool of additional module on unmanned plane card seat. BACKGROUND

[0002] In prior art, additional autonomous flight module is assembled on the body of unmanned plane, and additional autonomous function can be realized, when realizing quick disassembly and firm installation of different modules, most of the modules are fixed through screws, however, in prior art, unmanned plane screw fixing hole position is extremely not unified, module needs to be transformed every time when installing external module, which is not firm, increases cost, and also causes great safety hazard in flight. UTILITY MODEL CONTENTS

[0003] The utility model discloses a kind of assembly tool of additional module on unmanned plane card seat, not only reduce the setting of screw hole, and the limitation that fixed screw hole must be assembled in set position, and realize the effect of quick assembly and disassembly.

[0004] To achieve the above object, the utility model is realized by the following technical scheme.

[0005] The assembly tool of additional module on unmanned plane card seat includes the card seat on unmanned plane, and additional module is locked or unlocked assembly with the card seat through quick connection mechanism;

[0006] The card seat forms partial enclosure, additional module is equipped with clamping mechanism near enclosure, and the inner wall of enclosure and the outer wall of additional module are clamped by clamping mechanism.

[0007] Further, the quick connection mechanism and the clamping mechanism form two side connection clamps at both ends of the card seat respectively.

[0008] Further, the quick connection mechanism completes assembly or disassembly along horizontal direction linear motion, and the clamping mechanism completes clamping or loosening along vertical direction rotary motion.

[0009] Further, the quick connection mechanism includes connecting rod connecting the card seat and additional module along horizontal direction.

[0010] Further, the card seat is partially raised to form assembly part, and the first perforation for the connecting rod to pass through is arranged on the assembly part.

[0011] Further, additional module is partially extended downward to form mounting part, and the second perforation is arranged on the corresponding position of the mounting part and the assembly part.

[0012] Further, the first perforation has a length greater than that of the second perforation, and the mounting portion is provided with a baffle parallel to the mounting portion on both sides thereof.

[0013] Further, the additional module forms a mounting shell, and a partition plate in the mounting shell divides the mounting shell into an upper shell and a lower shell, the upper shell is provided with electronic components, and the lower shell is supported on the card seat.

[0014] Further, the lower shell is partially recessed to form a clamping portion, the surrounding baffle cavity is partially extended inward to form a blocking cavity, and the clamping portion enters or leaves the blocking cavity in the rotation of the additional module.

[0015] Further, the blocking cavity is located in the lower part of the surrounding baffle cavity, and the upper and lower sides of the partially extended surrounding baffle cavity are both formed with guide inclined surfaces, and the upper surface of the clamping portion is provided with a transition inclined surface matched with the guide inclined surfaces.

[0016] The beneficial effects of the utility model are as follows:

[0017] In the utility model, when assembling the tool, the main part is the card seat adapted to the unmanned aerial vehicle and the additional module (such as a micro module). The card seat can be changed in structure to adapt to large, medium and small models as necessary, the micro module and the card seat are fixed by a unified clamping quick release mechanism, and the micro module can be any functional module that needs to be expanded.

[0018] In the utility model, the card seat does not need to be provided with fixed screw holes, and only needs to be provided with a quick connection mechanism adapted to the module at the position needing assembly, such as a unified size, so that the additional modules with different functions also have the quick release interface, and direct assembly is facilitated. DRAWINGS

[0019] Figure 1 One of the structure schematic views of the assembly tool of the additional module on the card seat of the unmanned aerial vehicle is provided in the utility model;

[0020] Figure 2 The second structure schematic view of the assembly tool of the additional module on the card seat of the unmanned aerial vehicle is provided in the utility model;

[0021] Figure 3 The partial assembly view of the assembly tool of the additional module on the card seat of the unmanned aerial vehicle is provided in the utility model;

[0022] Figure 4 The exploded view of the assembly tool of the additional module on the card seat of the unmanned aerial vehicle is provided in the utility model;

[0023] Figure 5 The structure schematic view of the additional module is provided in the utility model;

[0024] Fig.:

[0025] 100, card seat; 110, enclosure cavity; 120, assembly part; 121, first through hole; 200, quick connection mechanism; 210, mounting part; 211, second through hole; 220, baffle; 300, additional module; 310, mounting shell; 311, isolation plate; 312, upper shell; 313, lower shell; 400, clamping mechanism; 410, clamping part; 411, transition slope; 420, clamping cavity; 421, guide slope; 500, communication interface. DETAILED DESCRIPTION

[0026] The embodiments shown in the drawings will be described in detail below, but it should be noted that these embodiments are not a limitation on the utility model, and equivalent changes or substitutions in function, method, or structure made by those skilled in the art based on these embodiments are within the scope of protection of the utility model.

[0027] Referring to the drawings Figures 1-5 As shown, the assembly tool of the additional module on the unmanned aerial vehicle card seat in the embodiment does not need to be fixed, and the hole position is not punched, and the bone modification of the additional module is not needed, thereby avoiding the problems of firm assembly and cost increase, and reducing the safety hazards in the flight of the unmanned aerial vehicle.

[0028] Specifically, the embodiment includes a card seat 100 on an unmanned aerial vehicle, and an additional module 300 assembled by locking or unlocking with a quick connection mechanism 200; compared with the setting of punching and assembling nuts, this direct locking method has high adaptability and is easy to disassemble.

[0029] In order to further limit, in the embodiment, a clamping position is also added, specifically, the card seat 100 forms a partial enclosure cavity 110, for example, the card seat 100 of the plate material extends upward in part, forming a partial enclosure, and then the clamping mechanism 400 is arranged on the additional module 300 close to the enclosure cavity 110, and the inner wall of the enclosure cavity 110 and the outer wall of the additional module 300 are clamped by the clamping mechanism 400, avoiding the problems of loosening or disengagement in flight.

[0030] In the embodiment, the quick connection and clamping are arranged at the same time, so that the card seat and the additional module are connected and assembled at multiple positions, the firmness of assembly is improved, and punching is not needed, and locking and limiting can be directly achieved, which is convenient to operate.

[0031] In order to realize assembly at multiple positions and stability at a large distance, the quick connection mechanism 200 and the clamping mechanism 400 are respectively arranged at both ends of the card seat 100 to form two clamping positions. For example, two ends of the card seat 100 are arranged at the front and rear or left and right ends, respectively, to improve the firmness.

[0032] In this embodiment, in order to realize the assembly of multiple directions, avoid the problem of poor stability in single direction, and further set the quick connection mechanism 200 and the clamping mechanism 400 in the horizontal direction and the vertical direction respectively, and further use, the quick connection mechanism 200 moves linearly along the horizontal direction to complete the assembly or disassembly, such as directly moving linearly along the left-right direction to complete the assembly, and the clamping mechanism 400 completes the clamping or loosening in the vertical direction, at this time the rotation range is less than 90°, that is, the assembly or disassembly is completed in less than 90° rotation.

[0033] In this embodiment, the quick connection mechanism 200 specifically includes a connecting rod connecting the card seat 100 and the external module 200 in the horizontal direction. At this time, such as selecting a pin as the connecting rod to quickly complete the assembly, and then the pin can be located in the lower part of the external module, providing space for the subsequent assembly of the upper part.

[0034] In this embodiment, since the external module needs to be provided with circuits and chips, etc., and the assembly of electronic devices can be bypassed, at this time the card seat 100 and the external module 300 can be completed by partial assembly in the air, such as pin assembly in the air, specifically, the card seat 100 forms an assembly part 120 through partial protrusion, the assembly part 120 is provided with a first through hole 121 for the connecting rod to pass through, and the external module 200 is partially extended downward to form a mounting part 210, the mounting part 210 is provided with a second through hole 211 at a position corresponding to the assembly part 120, and the pin is assembled by passing through the first through hole 121 and the second through hole 211 respectively to complete the entire assembly.

[0035] In this embodiment, a screw rod can also be used for assembly of the two through holes, at this time it is also completed by rotation, but compared with the pin, the operation is too cumbersome.

[0036] In order to realize shielding protection, the length of the first through hole 121 is greater than the length of the second through hole 211, so that the contact assembly with the card seat 100 is increased, providing more assembly space for the external module, at this time the mounting part 210 is provided with a baffle 220 on both sides, which is parallel to the assembly part 120. The baffle 220 forms a blocking cavity, so that the entire quick connection assembly is isolated from the outside world, achieving protection.

[0037] In this embodiment, the external module 300 needs to be assembled with chips, etc., and the external module 300 forms a mounting shell 310, an isolation plate 311 in the mounting shell 310 divides the mounting shell 310 into an upper shell 312 and a lower shell 313, the upper shell 312 is provided with electronic elements such as a circuit board, a chip, and various circuits, etc., and a communication interface 500 connected with the circuit board is arranged on the mounting shell for subsequent data reading and software programming, etc., and the lower shell 312 is supported on the card seat 100.

[0038] For the specific clamping mechanism, it is specifically that the lower shell 313 is partially recessed to form a clamping part 410, the surrounding blocking cavity 110 is partially extended inward to form a blocking cavity 420, and the additional module 300 drives the clamping part 410 to enter or leave the blocking cavity 420 in rotation, thereby completing the conversion of limiting or leaving.

[0039] In order to facilitate rotation into or out of, the blocking cavity 420 is located in the lower part of the surrounding blocking cavity 110, at this time the quick connection mechanism and the clamping mechanism are controlled at low and high positions respectively, and then the upper and lower sides of the partially extended part of the surrounding blocking cavity 110 are formed with guide inclined surfaces 421, such as the upper extension of the surrounding blocking cavity 110, the upper and lower sides of the extension are formed with reverse inclined inclined guide surfaces, such as the upper guide inclined surface is formed in the inward direction to form a downward extending inclined surface, and the lower guide inclined surface is from the outer side to the inner side of the surrounding blocking cavity, forming an upward inclined surface, at this time the whole mass is lighter, and the upper inclined surface provides space for rotation,

[0040] The upper surface of the clamping part 410 is provided with a transition inclined surface 411 matched with the guide inclined surface 421, and the inclined surface makes the rotation easier.

[0041] In the embodiment, the clamping part 410 and the lower shell 313 are provided with a space in the horizontal direction, which is to facilitate rotation.

[0042] In the utility model, the additional module forms a module with the function of containing electronic products, and the bottom of the additional module and the card seat are connected with the quick disassembly structure, so that the quick fixing is realized, and the single-handed pick pin can be easily disassembled.

[0043] In the embodiment, the communication interface is arranged on the additional module, and the powerful unmanned aerial vehicle also has an expansion interface, which is matched with the additional module in the future, mainly for the secondary development needs of special functions, and has a communication power supply interface and a fixed installation interface, and various unmanned aerial vehicle fixing interfaces can be added.

[0044] The series of detailed descriptions listed above are only specific descriptions of the feasible implementation mode of the utility model, and they are not used to limit the protection scope of the utility model, and equivalent implementation modes or changes made without departing from the spirit of the utility model art should be included in the protection scope of the utility model.

[0045] It is apparent for a person skilled in the art that the present application is not limited to the details of the above-described exemplary embodiments, but that it can be implemented in other concrete forms without departing from the spirit or the essential characteristics of the present application. Therefore, the embodiments should be considered as exemplary and non-limiting, the scope of the present application being defined by the claims appended hereto rather than by the above description, and all the changes which fall within the meaning and the scope of the equivalent elements of the claims are intended to be embraced therein. Any reference signs in the claims should not be construed as limiting the claims to the figures in which the reference signs are used.

[0046] Furthermore, it should be understood that although the present specification describes exemplary embodiments, not every embodiment contains only one independent technical solution, and the present specification is described in this way only for the sake of clarity, and a person skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that a person skilled in the art can understand.

Claims

1. An assembly tool for assembling an external module on a drone socket, characterized in that, The application relates to a quick-assembly module for unmanned aerial vehicles, comprising a card seat on the unmanned aerial vehicle and an additional module assembled with the card seat through a quick-assembly mechanism. The card seat partially forms an enclosure cavity, the additional module is provided with a clamping mechanism near the enclosure cavity, and the inner wall of the enclosure cavity and the outer wall of the additional module are clamped through the clamping mechanism.

2. The assembly fixture of the external module on the drone socket according to claim 1, wherein, The quick-assembly mechanism and the clamping mechanism are respectively formed on both sides of the two ends of the card seat.

3. The assembly tool of the external module on the drone socket according to claim 1 or 2, characterized in that, The quick-assembly mechanism is linearly moved along the horizontal direction to complete assembly or disassembly, and the clamping mechanism is rotationally moved along the vertical direction to complete clamping or loosening.

4. The assembly fixture of claim 1, wherein, The quick-assembly mechanism comprises a connecting rod connecting the card seat and the additional module along the horizontal direction.

5. The assembly fixture of the external module on the drone socket according to claim 4, wherein, The card seat is partially protruded to form an assembly part, and the assembly part is provided with a first through hole for the connecting rod.

6. The assembly fixture of the external module on the drone socket according to claim 5, wherein, The additional module is partially extended downward to form a mounting part, and the mounting part is provided with a second through hole corresponding to the assembly part.

7. The assembly fixture of the external module on the drone socket according to claim 6, wherein, The length of the first through hole is greater than that of the second through hole, and the mounting part is respectively provided with a baffle parallel to the assembly part on both sides.

8. The assembly fixture of the external module on the drone socket according to claim 1, wherein, The additional module forms a mounting shell, an isolation plate in the mounting shell divides the mounting shell into an upper shell and a lower shell, the upper shell is provided with electronic elements, and the lower shell is supported on the card seat.

9. The assembly fixture of the external module on the drone socket according to claim 8, wherein, The lower shell is partially recessed to form a clamping part, the enclosure cavity is partially extended inward to form a blocking cavity, and the clamping part enters or leaves the blocking cavity during rotation of the additional module.

10. The assembly fixture of the external module on the drone socket according to claim 9, wherein, The blocking cavity is located in the lower part of the enclosure cavity, the upper and lower sides of the partially extended enclosure cavity are respectively formed with guide inclined surfaces, and the upper surface of the clamping part is provided with a transition inclined surface matched with the guide inclined surfaces.

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