Detachable flight control module mounting seat for multi-rotor unmanned aerial vehicle

Abstract

The utility model discloses a detachable flight control module mounting seat for a multi-rotor unmanned aerial vehicle. The detachable flight control module mounting seat comprises a mounting seat main body and a flight control module, a connecting plate is arranged at the bottom of the mounting seat main body, and the mounting seat main body is fixed at the bottom of the multi-rotor unmanned aerial vehicle through the connecting plate; a mounting cavity is formed in the mounting seat main body in a controlled manner, and a cover plate is arranged above the mounting seat main body; a fixing assembly is arranged between the lower part of the cover plate and the mounting cavity, and the flight control module is fixed in the mounting cavity through the fixing assembly. According to the utility model, the mounting and dismounting of the flight control module become simple and efficient through the connecting sheets and the fixing screws; an operator only needs to loosen the fixing screws, the flight control module can be quickly disassembled, and maintenance and replacement are convenient.

Description

Technical Field

[0001] This utility model relates to a drone, specifically to a detachable flight control module mounting base for a multi-rotor drone. Background Technology

[0002] In modern multi-rotor drone applications, the flight control module is a key component ensuring safe flight and accurate navigation. Many traditional installation methods are susceptible to vibration and impact during multi-rotor drone flight, leading to instability of the flight control module, or even causing the module to loosen or detach, thus affecting flight safety.

[0003] Some flight control modules have complex installation methods and cumbersome disassembly and replacement processes, often requiring professional tools and technical support, which causes inconvenience to users and affects the efficiency of drone use and maintenance. Utility Model Content

[0004] The technical problem to be solved by this utility model is to provide a detachable flight control module mounting base for multi-rotor UAVs, so as to solve the problems existing in the background art.

[0005] The detachable flight control module mounting base for multi-rotor UAVs is achieved through the following technical solution, including a mounting base body and a flight control module;

[0006] The bottom of the mounting base body is provided with a connecting plate, and the mounting base body is fixed to the bottom of the multi-rotor UAV through the connecting plate; the internal control of the mounting base body forms a mounting cavity, and a cover plate is provided on the top of the mounting base body; a fixing component is provided below the cover plate between the mounting cavity, and the flight control module is fixed in the mounting cavity through the fixing component.

[0007] As a preferred technical solution, guide blocks are provided on both sides of the mounting base body, and the mounting base body is guided and positioned on the bottom of the multi-rotor UAV by the guide blocks and positioned by the positioning structure.

[0008] As a preferred technical solution, the fixing component includes a fixing upper seat and a fixing lower seat;

[0009] The upper fixing seat is located around the lower part of the cover plate, and the lower fixing seat is located around the upper part of the mounting cavity.

[0010] The upper fixed base is provided with a plug rod, and the lower fixed base is provided with a plug hole. When the cover plate is spliced ​​with the main body of the mounting base, the plug rod passes through the through hole of the flight control module and is placed in the plug hole, thereby realizing the fixation of the flight control module.

[0011] As a preferred technical solution, an upper support seat is provided under the cover plate and a lower support seat is provided on the mounting cavity;

[0012] Both the upper and lower support bases are provided with extrusion silicone, and the extrusion silicone is in contact with the flight control module, thus providing a buffering effect.

[0013] As a preferred technical solution, a fixing groove is provided at the bottom of the mounting base body, and the fixing groove is connected to the mounting cavity; a semiconductor cooling chip is fixed above the fixing groove, and the cooling end of the semiconductor cooling chip is in contact with the flight control module; a heat dissipation fin is provided below the fixing groove, and the heat dissipation fin is in contact with the heating end of the semiconductor cooling chip, thereby dissipating the heat of the semiconductor cooling chip.

[0014] As a preferred technical solution, the positioning structure includes a spring groove and a positioning ball disposed on the guide block;

[0015] The positioning ball is positioned at the end of the spring groove, and a compression spring is provided between the positioning ball and the spring groove. The compression spring compresses the positioning ball to be placed in the positioning hole of the multi-rotor UAV, thereby fixing the main body of the mounting base.

[0016] As a preferred technical solution, a locking screw is provided on the side of the mounting base body, and the locking end of the locking screw passes through the mounting base body and connects with the upper support of the cover plate, thereby fixing the upper cover.

[0017] As a preferred technical solution, the flight control module is provided with a connection connector, and the connection connector passes through the cover plate; the connection connector corresponds to the connection interface of the multi-rotor UAV.

[0018] As a preferred technical solution, the mounting base body has fixing screws around the connecting plate, and the locking end of the fixing screws is connected to the bottom of the multi-rotor drone. The multi-rotor drone can be disassembled by loosening the fixing screws.

[0019] The beneficial effects of this utility model are:

[0020] This invention simplifies and simplifies the installation and removal of the flight control module by using connecting pieces and fixing screws. Operators can quickly disassemble the flight control module simply by loosening the fixing screws, facilitating maintenance and replacement.

[0021] This invention, through the setting of a fixed upper seat, a fixed lower seat, and a plug-in rod and plug-in hole, allows the flight control module to be fixed in the mounting cavity. The extrusion silicone on the upper and lower support seats provides a good buffering effect, effectively absorbing vibrations during flight, protecting the flight control module from damage, and providing support to enhance the stability of the overall structure. Attached Figure Description

[0022] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art 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.

[0023] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0024] Figure 2 This is a schematic diagram of the exploded structure of this utility model;

[0025] Figure 3 This is a schematic diagram of the positioning structure of this utility model.

[0026] 1. Mounting base body; 2. Flight control module; 3. Connecting plate; 4. Mounting cavity; 5. Cover plate; 6. Guide block; 7. Upper fixed base; 8. Lower fixed base; 9. Connecting rod; 10. Connecting hole; 11. Upper support base; 12. Lower support base; 13. Extruded silicone; 14. Fixing groove; 15. Semiconductor cooling chip; 16. Heat sink fins; 17. Spring groove; 18. Positioning ball; 19. Locking screw; 20. Connecting connector; 21. Fixing screw. Detailed Implementation

[0027] All features disclosed in this specification, or steps in all methods or processes disclosed herein, may be combined in any way, except for mutually exclusive features and / or steps.

[0028] like Figures 1-3 As shown, the present invention provides a detachable flight control module mounting base for a multi-rotor unmanned aerial vehicle, comprising a mounting base body 1 and a flight control module 2.

[0029] The bottom of the mounting base body 1 is provided with a connecting plate 3, and the mounting base body 1 is fixed to the bottom of the multi-rotor UAV through the connecting plate 3; the interior of the mounting base body 1 forms a mounting cavity 4, and a cover plate 5 is provided on the top of the mounting base body 1; a fixing component is provided below the cover plate 5 and between the mounting cavity 4, and the flight control module 2 is fixed in the mounting cavity 4 through the fixing component.

[0030] The mounting base body 1 has guide blocks 6 on both sides, and the mounting base body 1 is guided and positioned at the bottom of the multi-rotor UAV by the guide blocks 6 and positioned by the positioning structure.

[0031] To facilitate the fixing of the flight control module, in this embodiment, the fixing components include a fixing upper seat 7 and a fixing lower seat 8;

[0032] The upper fixing seat 7 is located around the lower part of the cover plate 5, and the lower fixing seat 8 is located around the upper part of the mounting cavity 4.

[0033] The upper fixed seat 7 is provided with a plug rod 9, and the lower fixed seat 8 is provided with a plug hole 10. When the cover plate 5 is spliced ​​with the mounting body 1, the plug rod 9 passes through the through hole of the flight control module 2 and is placed in the plug hole 10, thereby fixing the flight control module 2.

[0034] In order to provide support, in this embodiment, an upper support seat 11 is provided below the cover plate 5 and a lower support seat 12 is provided on the mounting cavity 4.

[0035] Both the upper support base 11 and the lower support base 12 are provided with extrusion silicone 13, and the extrusion silicone 13 is in contact with the flight control module 2, and the extrusion silicone 13 plays a buffering role.

[0036] To achieve a cooling effect, a fixing groove 14 is provided at the bottom of the mounting base body 1, and the fixing groove 14 is connected to the mounting cavity 4; a semiconductor cooling chip 15 is fixed above the fixing groove 14, and the cooling end of the semiconductor cooling chip 15 is in contact with the flight control module 2; a heat dissipation fin 16 is provided below the fixing groove 14, and the heat dissipation fin 16 is in contact with the heating end of the semiconductor cooling chip 15, thereby dissipating the heat of the semiconductor cooling chip 15.

[0037] The positioning structure includes a spring groove 17 and a positioning ball 18 disposed on the guide block 6;

[0038] The positioning ball 18 is positioned at the end of the spring groove 17, and a compression spring is provided between the positioning ball 18 and the spring groove 17. The compression spring compresses the positioning ball 18 into the positioning hole of the multi-rotor UAV, thereby fixing the mounting body 1.

[0039] In order to fix the cover plate, in this embodiment, a locking screw 19 is provided on the side of the mounting base body 1, and the locking end of the locking screw 19 passes through the mounting base body 1 and is connected to the upper support seat 11 of the cover plate 5, thereby fixing the upper cover.

[0040] To facilitate signal connection, in this embodiment, the flight control module 2 is provided with a connection connector 20, and the connection connector 20 passes through the cover plate 5; the connection connector 20 corresponds to the connection interface of the multi-rotor UAV.

[0041] To achieve the detachable effect, in this embodiment, fixing screws 21 are provided around the connecting piece of the mounting base body 1, and the locking end of the fixing screws 21 is connected to the bottom of the multi-rotor drone. The multi-rotor drone can be disassembled by loosening the fixing screws 21.

[0042] This invention simplifies and simplifies the installation and disassembly of the flight control module through connecting plates and fixing screws. Operators can quickly disassemble the flight control module by simply loosening the fixing screws, facilitating maintenance and replacement. The upper and lower fixing seats, as well as the plug-in rods and plug-in holes, allow the flight control module to be fixed within the mounting cavity. The extrusion silicone on the upper and lower support seats provides excellent cushioning, effectively absorbing vibrations during flight, protecting the flight control module from damage, and providing support to enhance the overall structural stability.

[0043] The above description is merely a specific embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any changes or substitutions conceived without inventive effort should be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the scope defined in the claims.

Claims

1. A detachable flight control module mount for a multi-copter drone, characterized in that, It includes the mounting base body (1) and the flight control module (2); The mounting base body (1) has a connecting plate (3) at its bottom, and the mounting base body (1) is fixed to the bottom of the multi-rotor UAV by the connecting plate (3); the internal control of the mounting base body (1) forms a mounting cavity (4), and a cover plate (5) is provided on the top of the mounting base body (1); a fixing component is provided below the cover plate (5) between the mounting cavity (4), and the flight control module (2) is fixed in the mounting cavity (4) by the fixing component.

2. The detachable flight control module mount for multi-copters according to claim 1, wherein: Guide blocks (6) are provided on both sides of the mounting base body (1), and the mounting base body (1) is guided and positioned at the bottom of the multi-rotor UAV by the guide blocks (6) and positioned by the positioning structure.

3. The detachable flight control module mount for multi-copters according to claim 1, wherein: The fixing assembly includes a fixing upper seat (7) and a fixing lower seat (8); The upper fixing seat (7) is located around the lower part of the cover plate (5), and the lower fixing seat (8) is located around the upper part of the mounting cavity (4). The upper fixed seat (7) is provided with a plug rod (9), and the lower fixed seat (8) is provided with a plug hole (10). When the cover plate (5) is spliced ​​with the mounting body (1), the plug rod (9) passes through the through hole of the flight control module (2) and is placed in the plug hole (10), thereby fixing the flight control module (2).

4. The detachable flight control module mount for multi-copters according to claim 1, wherein: Each of the cover plates (5) is provided with an upper support seat (11) below it, and a lower support seat (12) is provided on the mounting cavity (4); Both the upper support base (11) and the lower support base (12) are provided with extruded silicone (13), and the extruded silicone (13) is in contact with the flight control module (2), and the extruded silicone (13) plays a buffering role.

5. The detachable flight control module mount for multi-copters according to claim 1, wherein: The mounting base body (1) has a fixing groove (14) at its bottom, and the fixing groove (14) is connected to the mounting cavity (4); a semiconductor cooling chip (15) is fixed above the fixing groove (14), and the cooling end of the semiconductor cooling chip (15) is in contact with the flight control module (2); a heat dissipation fin (16) is provided below the fixing groove (14), and the heat dissipation fin (16) is in contact with the heating end of the semiconductor cooling chip (15), thereby dissipating the heat of the semiconductor cooling chip (15).

6. The detachable flight control module mount for a multi-copter drone of claim 2, wherein: The positioning structure includes a spring groove (17) and a positioning ball (18) disposed on the guide block (6); The positioning ball (18) is positioned at the end of the spring groove (17), and a compression spring is provided between the positioning ball (18) and the spring groove (17). The positioning ball (18) is placed in the positioning hole of the multi-rotor UAV by the compression spring, thereby fixing the mounting body (1).

7. The detachable flight control module mount for multi-copters according to claim 1, wherein: The mounting base body (1) is provided with a locking screw (19) on its side, and the locking end of the locking screw (19) passes through the mounting base body (1) and is connected to the upper support seat (11) of the cover plate (5), thereby fixing the upper cover.

8. The detachable flight control module mounting base for a multi-rotor UAV according to claim 1, characterized in that: The flight control module (2) is provided with a connection connector (20), and the connection connector (20) passes through the cover plate (5); the connection connector (20) corresponds to the connection interface position of the multi-rotor UAV.

9. The detachable flight control module mount for multi-copters according to claim 1, wherein: The mounting base body (1) is provided with fixing screws (21) around the connecting piece, and the locking end of the fixing screws (21) is connected to the bottom of the multi-rotor drone. The multi-rotor drone can be disassembled by loosening the fixing screws (21).

Images