Connecting assembly for arms and fuselage of multi-rotor unmanned aerial vehicle

Abstract

The utility model discloses a multi-rotor unmanned aerial vehicle arm and fuselage connecting assembly, which relates to the technical field of unmanned aerial vehicles, and comprises two connecting plates symmetrically arranged on a fuselage and fixedly connected with the fuselage; the clamping mechanism is arranged on the supporting column and used for clamping the supporting column; the clamping groove is formed in the supporting column; the number of the clamping rings is two, and the two clamping rings are symmetrically arranged in the clamping groove and are in sliding connection with the clamping groove; the clamping column is arranged on the clamping ring and is fixedly connected with the clamping ring; the driving part is arranged on the supporting block; the fixing mechanism is arranged on the supporting plate and used for fixing the supporting shaft; the clamping mechanism and the driving part are arranged, so that the supporting column is clamped, and the supporting column is convenient to replace; and by arranging the fixing mechanism, the supporting shaft is clamped and fixed, and it is avoided that when the supporting blades are damaged, disassembly is difficult.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a multi-rotor UAV arm-body connection component. Background Technology

[0002] The UAV arm-body connection assembly mainly includes a fixed arm and a movable arm, as well as threaded sleeves and locking components that connect these components. Specifically, this assembly is designed to fix the fixed arm and the movable arm in the deployed state, and through the engagement of the locking component with the locking mating part, restricts the rotation of the threaded sleeve relative to the fixed arm and the movable arm, thereby improving the reliability of the deployed arm fixation.

[0003] Most existing drone arm connection components are installed using threaded sleeves. However, drones are prone to damaging these components during use, and disassembly is difficult, leading to installation errors and affecting drone operation. Therefore, improvements are needed. Utility Model Content

[0004] In view of the shortcomings of the existing technology, the purpose of this utility model is to provide a multi-rotor drone arm and fuselage connection component, which aims to solve the technical problem that the connection component of the drone arm is not easy to install and disassemble.

[0005] To achieve the above objectives, the present invention adopts the following technical solution:

[0006] A multi-rotor unmanned aerial vehicle (UAV) arm-fuselage connection assembly includes a body and a support block, the support block being fixedly connected to the body; it further includes: two support sleeves symmetrically arranged on the support block and fixedly connected to it; a support column disposed within the support sleeves and rotatably connected to them; a support plate disposed on the support column and rotatably connected to it; a support shaft slidably connected to the support plate; and multiple support blades evenly arranged on the support shaft and rotating with it. Connection; connecting plates, having two plates symmetrically arranged on the body and fixedly connected to the body; clamping mechanism, arranged on the support column, for clamping the support column; clamping groove, formed on the support column; clamping rings, having two rings symmetrically arranged in the clamping groove, slidably connected to the clamping groove; clamping column, arranged on the clamping ring, fixedly connected to the clamping ring; driving component, arranged on the support block; fixing mechanism, arranged on the support plate, for fixing the support shaft.

[0007] Preferably, the driving component includes: a driving shaft disposed on the support block and fixedly connected to the support block; a driving block disposed on the driving shaft and fixedly connected to the driving shaft; and a sliding component disposed within the support block.

[0008] Preferably, the sliding component includes: a sliding groove formed within the support block; and two sliding plates symmetrically arranged within the sliding groove, slidably connected to the sliding groove, and threadedly connected to the drive shaft.

[0009] Preferably, the sliding plate is fixedly connected to the clamping column.

[0010] Preferably, the fixing mechanism includes: a fixing column disposed on the support plate and fixedly connected to the support plate; a fixing plate fixedly connected to the fixing column; a fixing ring disposed on the fixing column and rotatably connected to the fixing column; and a rotating component disposed on the fixing column.

[0011] Preferably, the rotating component includes: a rotating ring disposed on the fixed column and fixedly connected to the fixed column; a rotating groove formed on the rotating ring; a rotating column disposed in the rotating groove, slidably connected to the rotating groove, and fixedly connected to the fixed ring; and a transmission component disposed within the support plate.

[0012] Preferably, the transmission component includes: a transmission groove formed within the support plate; a transmission block disposed within the transmission groove, slidably connected to the transmission groove, and fixedly connected to the rotating column; a transmission plate fixedly connected to the transmission block; and a fixing groove formed on the support shaft.

[0013] Preferably, the transmission plate is slidably connected to the fixing groove.

[0014] In summary, due to the adoption of the above technical solution, the beneficial effects of this utility model are:

[0015] By setting up a clamping mechanism and a driving component, the support column can be clamped, making the replacement of the support column more convenient; by setting up a fixing mechanism, the support shaft can be clamped and fixed, avoiding the difficulty of disassembly when the support blade is damaged. Attached Figure Description

[0016] 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.

[0017] Figure 1 A three-dimensional structural schematic diagram of a multi-rotor drone arm-fuselage connection assembly is shown.

[0018] Figure 2A top view of a multi-rotor unmanned aerial vehicle (UAV) arm-fuselage connection assembly is shown.

[0019] Figure 3 It shows Figure 2 A schematic diagram of the cross-sectional structure of AA.

[0020] Figure 4 An exploded view of the fixing mechanism of a multi-rotor drone arm-fuselage connection assembly is shown.

[0021] Figure 5 An exploded view of the clamping mechanism of a multi-rotor drone arm-fuselage connection assembly is shown.

[0022] Legend:

[0023] 1. Body; 2. Support block; 3. Support sleeve; 4. Support column; 5. Support plate; 6. Support shaft; 7. Support blade; 8. Connecting plate; 9. Clamping groove; 10. Clamping ring; 11. Clamping column; 12. Drive shaft; 13. Drive block; 14. Sliding groove; 15. Sliding plate; 16. Fixed column; 17. Fixed plate; 18. Fixed ring; 19. Rotating ring; 20. Rotating groove; 21. Rotating column; 22. Transmission groove; 23. Transmission block; 24. Transmission plate; 25. Fixed groove. Detailed Implementation

[0024] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of the present utility model.

[0025] In the description of this utility model, it should be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0026] It should be noted that when a component is described as "fixed to" another component, it can be directly on the other component or may have a component in between. When a component is considered "connected to" another component, it can be directly connected to the other component or may have a component in between. When a component is considered "set on" another component, it can be directly set on the other component or may have a component in between. The terms "vertical," "horizontal," "left," "right," and similar expressions used in this document are for illustrative purposes only.

[0027] Furthermore, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of this utility model, "a plurality of" means two or more, unless otherwise explicitly specified.

[0028] Reference Figures 1 to 5 The present invention provides a further description of an embodiment of a multi-rotor unmanned aerial vehicle (UAV) arm-fuselage connection component.

[0029] A multi-rotor unmanned aerial vehicle (UAV) arm-fuselage connection assembly includes a body 1 and a support block 2, the support block 2 being fixedly connected to the body 1; it also includes: two support sleeves 3, symmetrically arranged on the support block 2 and fixedly connected to it; a support column 4, disposed within the support sleeves 3 and rotatably connected to them; a support plate 5, disposed on the support column 4 and rotatably connected to it; a support shaft 6, slidably connected to the support plate 5; and multiple support blades 7, evenly arranged on the support shaft 6 and rotatably connected to it. The system includes: a connecting plate 8 (two plates 8 symmetrically arranged on the body 1 and fixedly connected to the body 1); a clamping mechanism on the support column 4 for clamping the support column 4; a clamping groove 9 on the support column 4; two clamping rings 10 symmetrically arranged in the clamping groove 9 and slidably connected to the clamping groove 9; a clamping column 11 on the clamping ring 10 and fixedly connected to the clamping ring 10; a driving component on the support block 2; and a fixing mechanism on the support plate 5 for fixing the support shaft 6.

[0030] Reference Figure 5 In a preferred embodiment, the driving component includes: a driving shaft 12, which is disposed on the support block 2 and fixedly connected to the support block 2; a driving block 13, which is disposed on the driving shaft 12 and fixedly connected to the driving shaft 12; and a sliding component disposed within the support block 2.

[0031] This configuration allows the rotating drive block 13 to rotate the drive shaft 12, which is fixedly connected to the drive block 13, on the support block 2, thereby driving the sliding component to run.

[0032] Reference Figure 3 and Figure 5 In a preferred embodiment, the sliding component includes: a sliding groove 14, which is formed in the support block 2; and two sliding plates 15, which are symmetrically arranged in the sliding groove 14, slidably connected to the sliding groove 14, and threadedly connected to the drive shaft 12.

[0033] Reference Figure 5 In a preferred embodiment, the sliding plate 15 is fixedly connected to the clamping column 11.

[0034] This configuration causes the sliding plate 15, which is threadedly connected to the drive shaft 12, to rotate, thereby causing the sliding plate 15 to slide within the sliding groove 14. This causes the sliding plates 15 to move away from each other, which in turn causes the clamping column 11, which is fixedly connected to the sliding plate 15, to move. This causes the clamping ring 10, which is fixedly connected to the clamping column 11, to slide within the clamping groove 9, thereby causing the clamping rings 10 to move away from each other until the clamping rings 10 are completely disengaged from the clamping groove 9, thus enabling the disassembly of the support column 4.

[0035] Reference Figure 4 In a preferred embodiment, the fixing mechanism includes: a fixing column 16, which is disposed on the support plate 5 and fixedly connected to the support plate 5; a fixing plate 17, which is fixedly connected to the fixing column 16; a fixing ring 18, which is disposed on the fixing column 16 and rotatably connected to the fixing column 16; and a rotating component, which is disposed on the fixing column 16.

[0036] This configuration allows the rotating fixed ring 18 to rotate on the fixed column 16, thereby driving the rotating component to operate.

[0037] Reference Figure 4 In a preferred embodiment, the rotating component includes: a rotating ring 19, which is disposed on the fixed column 16 and fixedly connected to the fixed column 16; a rotating groove 20, which is formed on the rotating ring 19; a rotating column 21, which is disposed in the rotating groove 20, slidably connected to the rotating groove 20, and fixedly connected to the fixed ring 18; and a transmission component, which is disposed in the support plate 5.

[0038] This configuration allows the rotating column 21, which is fixedly connected to the fixed ring 18, to slide within the rotating groove 20 of the rotating ring 19, thereby driving the transmission components to operate.

[0039] Reference Figure 4In a preferred embodiment, the transmission component includes: a transmission groove 22, which is formed in the support plate 5; a transmission block 23, which is disposed in the transmission groove 22, slidably connected to the transmission groove 22, and fixedly connected to the rotating column 21; a transmission plate 24, which is fixedly connected to the transmission block 23; and a fixing groove 25, which is formed on the support shaft 6.

[0040] Reference Figure 4 In a preferred embodiment, the transmission plate 24 is slidably connected to the fixed groove 25.

[0041] This configuration allows the transmission block 23, which is fixedly connected to the rotating column 21, to slide within the transmission groove 22, causing the transmission blocks 23 to move away from each other and drive the transmission plate 24, which is fixedly connected to the transmission block 23, to move until the transmission plate 24 is completely disengaged from the fixed groove 25, thereby enabling the disassembly of the support shaft 6.

[0042] Working principle: When the support column 4 is damaged by a collision during flight, the disassembly tool is used to rotate the drive block 13, which drives the drive shaft 12 fixedly connected to the drive block 13 to rotate on the support block 2. This causes the sliding plate 15 threadedly connected to the drive shaft 12 to rotate, which in turn causes the sliding plate 15 to slide in the sliding groove 14, making the sliding plates 15 move away from each other. This causes the clamping column 11 fixedly connected to the sliding plate 15 to move, which in turn causes the clamping ring 10 fixedly connected to the clamping column 11 to slide in the clamping groove 9, making the clamping rings 10 move away from each other until the clamping rings 10 are completely disengaged from the clamping groove 9, thereby disassembling the support column 4.

[0043] Next, rotate the fixed ring 18, causing it to rotate on the fixed column 16. This causes the rotating column 21, which is fixedly connected to the fixed ring 18, to slide in the rotating groove 20 of the rotating ring 19. This causes the transmission block 23, which is fixedly connected to the rotating column 21, to slide in the transmission groove 22. This causes the transmission blocks 23 to move away from each other, and causes the transmission plate 24, which is fixedly connected to the transmission block 23, to move until the transmission plate 24 is completely disengaged from the fixed groove 25, thereby disassembling the support shaft 6.

[0044] The above description of the embodiments enables those skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention is not to be limited to the embodiments shown herein, but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. A multi-rotor unmanned aerial vehicle arm body connecting assembly, comprising a machine body (1) and a supporting block (2), the supporting block (2) is fixedly connected with the machine body (1); characterized in that, Also include: Supporting sleeve (3) has two, and two supporting sleeve (3) is symmetrically arranged on the supporting block (2), and is fixedly connected with the supporting block (2); Supporting column (4) is arranged in the supporting sleeve (3), and is rotatably connected with the supporting sleeve (3); Supporting plate (5) is arranged on the supporting column (4), and is rotatably connected with the supporting column (4); Supporting shaft (6) is slidably connected with the supporting plate (5); Supporting blade (7) has a plurality of, and a plurality of supporting blades (7) are uniformly arranged on the supporting shaft (6), and are rotatably connected with the supporting shaft (6); The connecting plate (8) has two, and two connecting plates (8) are symmetrically arranged on the machine body (1), and are fixedly connected with the machine body (1); The clamping mechanism is arranged on the supporting column (4), and is used for clamping the supporting column (4); Clamping groove (9) is arranged on the supporting column (4); The clamping ring (10) has two, and two clamping rings (10) are symmetrically arranged in the clamping groove (9), and are slidably connected with the clamping groove (9); Clamping column (11) is arranged on the clamping ring (10), and is fixedly connected with the clamping ring (10); The driving part is arranged on the supporting block (2); The fixing mechanism is arranged on the supporting plate (5), and is used for fixing the supporting shaft (6).

2. The multi-copter UAV arm-body connecting assembly according to claim 1 and wherein, The driving part includes: Driving shaft (12) is arranged on the supporting block (2), and is fixedly connected with the supporting block (2); Driving block (13) is arranged on the driving shaft (12), and is fixedly connected with the driving shaft (12); The sliding part is arranged in the supporting block (2).

3. The multi-copter UAV arm-body connecting assembly according to claim 2 and wherein: The sliding part includes: Sliding groove (14) is arranged in the supporting block (2); Sliding plate (15) has two, and two sliding plates (15) are symmetrically arranged in the sliding groove (14), and are slidably connected with the sliding groove (14), and are threadedly connected with the driving shaft (12).

4. The multi-copter UAV arm-body connecting assembly according to claim 3 and wherein: The sliding plate (15) is fixedly connected with the clamping column (11).

5. The multi-copter UAV arm-body connecting assembly according to claim 4 and wherein: The fixing mechanism includes: Fixed column (16) is arranged on the supporting plate (5), and is fixedly connected with the supporting plate (5); Fixed plate (17) is fixedly connected with the fixed column (16); Fixed ring (18) is arranged on the fixed column (16), and is rotatably connected with the fixed column (16); The rotating part is arranged on the fixed column (16).

6. The multi-copter UAV arm-body connecting assembly according to claim 5 and wherein: The rotating part includes: Rotating ring (19) is arranged on the fixed column (16), and is fixedly connected with the fixed column (16); Rotating groove (20) is arranged on the rotating ring (19); Rotating column (21) is arranged in the rotating groove (20), and is slidably connected with the rotating groove (20), and is fixedly connected with the fixed ring (18); The transmission part is arranged in the supporting plate (5).

7. The multi-copter UAV arm-body connecting assembly according to claim 6 and wherein: The transmission part includes: Transmission groove (22) is arranged in the supporting plate (5); Transmission block (23) is arranged in the transmission groove (22), and is slidably connected with the transmission groove (22), and is fixedly connected with the rotating column (21); Transmission plate (24) is fixedly connected with the transmission block (23); A fixed groove (25) is arranged on the support shaft (6).

8. The multi-copter UAV arm-body connecting assembly according to claim 7 and wherein: The transmission plate (24) is in sliding connection with the fixed groove (25).

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