Environment-adaptive unmanned aerial vehicle undercarriage

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an environment-adaptive unmanned aerial vehicle undercarriage. According to the environment-adaptive unmanned aerial vehicle undercarriage, the height and the angle of the soft cushion can be adjusted, so that the unmanned aerial vehicle can stably land in different terrain environments, and the unmanned aerial vehicle is prevented from being damaged. The environment-adaptive unmanned aerial vehicle undercarriage comprises a mounting frame, fixing blocks, motors and the like, the fixing blocks are connected to the front side and the rear side of the mounting frame, and the motors are connected to the left sides and the right sides of the fixing blocks. The height of the soft cushion can be adjusted by starting the electric push rod on the mounting block, meanwhile, when the soft cushion makes contact with the ground, the soft cushion can rotate on the universal shaft, the soft cushion makes parallel contact with the landing ground, and the purpose that the height and the angle of the soft cushion can be adjusted, so that the height and the angle of the soft cushion can be adjusted is achieved. Therefore, the unmanned aerial vehicle can stably land in different terrain environments, and the unmanned aerial vehicle is prevented from being damaged.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to an environmentally adaptable UAV landing gear. Background Art

[0002] The drone landing gear is a vital component of the drone system. Its main function is to support the weight of the drone and ensure stable parking. At the same time, it absorbs impact energy during takeoff and landing, protects the fuselage and internal equipment, and improves flight safety and reliability. Existing drones are fixed in structure and often show insufficient adaptability when facing complex and changeable outdoor environments. Especially on uneven ground conditions, drones are prone to tipping over due to unstable landing gear support, causing damage to external components such as blades and cameras, which not only affects the smooth progress of the mission but may also cause unnecessary economic losses.

[0003] Therefore, an environmentally adaptable UAV landing gear has been developed that can adjust the height and angle of the soft cushion to adapt to smooth landing in different terrain environments and avoid damage to the UAV. Utility Model Content

[0004] In order to overcome the shortcomings of existing drones, which are fixed in structure and often lack adaptability when facing complex and changeable outdoor environments, and which easily lead to damage to the drone, the utility model provides an environmentally adaptable drone landing gear that can adjust the height and angle of the soft cushion to facilitate smooth landing in different terrain environments and avoid damage to the drone.

[0005] Technical solution: An environmentally adaptive UAV landing gear includes a mounting frame, a fixed block, a motor, a rotating shaft, a bevel gear set, an adjustment component, a buffer component and a rotating component. The front and rear sides of the mounting frame are connected to fixed blocks, the left and right sides of the fixed block are connected to motors, the left and right sides of the lower part of the mounting frame are rotatably connected to the rotating shaft, and bevel gear sets are connected between the motors and adjacent rotating shafts. The rotating shaft is provided with an adjustment component that can be adjusted to adapt to take-off and landing on terrains of different heights, the adjustment component is provided with a buffer component that can perform buffering, and the buffer component is provided with a rotating component that can be adjusted to adapt to different angles.

[0006] Furthermore, a plurality of mounting holes are provided on the mounting frame.

[0007] Furthermore, the adjustment component includes a mounting block, an electric push rod and a connecting block. The front and rear sides of the rotating shaft are connected to the mounting blocks, the electric push rods are on the mounting blocks, and the telescopic ends of the electric push rods are connected to the connecting blocks.

[0008] Furthermore, the buffer assembly includes a sleeve, a sliding frame and a telescopic spring. The lower side of the connecting block is connected to the sleeve, the sliding frame is slidably connected inside the sleeve, and the sliding frame is connected to the adjacent sleeve with a telescopic spring.

[0009] Furthermore, the rotating assembly includes a universal shaft and a soft pad. The lower side of the sliding frame is rotatably connected to the universal shaft, and the lower side of the universal shaft is connected to the soft pad.

[0010] Furthermore, the cushions are all made of rubber.

[0011] The utility model has the following advantages: the utility model can adjust the height of the cushion by starting the electric push rod on the mounting block, and at the same time, when the cushion contacts the ground, the cushion can rotate on the universal shaft, so that the cushion maintains parallel contact with the landing ground, thereby achieving the effect of being able to adjust the height and angle of the cushion to adapt to smooth landing in different terrain environments and avoid damage to the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model.

[0013] Figure 2 This is a schematic diagram of the first three-dimensional structure of the utility model.

[0014] Figure 3 This is a schematic diagram of a second partial cross-sectional three-dimensional structure of the present invention.

[0015] In the above figures: 1: mounting frame, 2: fixing block, 3: motor, 4: rotating shaft, 5: bevel gear set, 6: mounting block, 7: electric push rod, 8: connecting block, 9: sleeve, 10: sliding frame, 11: telescopic spring, 12: universal shaft, 13: cushion. DETAILED DESCRIPTION

[0016] The following will be combined with the accompanying drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0017] An environmentally adaptable UAV landing gear, such as Figure 1 and Figure 2As shown, it includes a mounting frame 1, a fixed block 2, a motor 3, a rotating shaft 4, a bevel gear set 5, an adjustment component, a buffer component and a rotating component. The front and rear sides of the mounting frame 1 are connected to the fixed block 2. The mounting frame 1 has six mounting holes for easy installation on the drone. The left and right sides of the fixed block 2 are connected to the motor 3. The left and right sides of the lower part of the mounting frame 1 are rotatably connected to the rotating shaft 4. The motor 3 is connected to the adjacent rotating shaft 4 with a bevel gear set 5. The rotating shaft 4 is provided with an adjustment component, the adjusting component is provided with a buffer component, and the buffer component is provided with a rotating component.

[0018] like Figure 2 and Figure 3 As shown, the adjustment assembly includes a mounting block 6, an electric push rod 7 and a connecting block 8. The front and rear sides of the rotating shaft 4 are connected to the mounting blocks 6. The mounting blocks 6 are each equipped with an electric push rod 7. The telescopic ends of the electric push rod 7 are each connected to a connecting block 8.

[0019] like Figure 1 and Figure 3 As shown, the buffer assembly includes a sleeve 9, a sliding frame 10 and a telescopic spring 11. The sleeve 9 is connected to the lower side of the connecting block 8, the sliding frame 10 is slidably connected inside the sleeve 9, and the telescopic spring 11 is connected between the sliding frame 10 and the adjacent sleeve 9.

[0020] like Figure 1 and Figure 3 As shown, the rotating assembly includes a universal shaft 12 and a soft pad 13. The lower side of the sliding frame 10 is rotatably connected to the universal shaft 12, and the lower side of the universal shaft 12 is connected to the soft pad 13. The soft pad 13 is made of rubber material to facilitate impact buffering.

[0021] When using the present invention, first install the device on the drone through the mounting frame 1. When the drone takes off and lands, the soft pad 13 contacts the landing ground, squeezing the soft pad 13 upward, causing the sliding frame 10 to slide upward on the sleeve 9. Under the action of the telescopic spring 11, the impact force of the drone landing is buffered. The electric push rod 7 on the mounting block 6 is started, so that the telescopic end of the electric push rod 7 is pushed out, and the height of the soft pad 13 can be adjusted. At the same time, when the soft pad 13 contacts the ground, the soft pad 13 can be rotated on the universal shaft 12, so that the soft pad 1 3 maintains parallel contact with the landing ground, thereby achieving the effect of being able to adjust the height and angle of the soft cushion 13 to adapt to a smooth landing in different terrain environments and avoid damage to the drone. After the drone is used, the motor 3 on the starting fixing block 2 can be controlled to rotate the rotating shaft 4, and the meshing movement of the bevel gear set 5 can rotate the rotating shaft 4, driving the mounting block 6 to rotate, so that the electric push rod 7 can be rotated and retracted, reducing the space occupied by the device, thereby facilitating the storage of the drone.

[0022] It should be understood that the embodiments are only used for illustrating the present application and are not used for limiting the scope of the present application. In addition, it should be understood that after reading the content taught by the present application, those skilled in the art can make various changes or modifications to the present application, and these equivalent forms also fall within the scope defined by the appended claims of the present application.

Claims

1. An environmentally adaptable UAV landing gear, characterized by: The invention comprises a mounting frame (1), a fixing block (2), a motor (3), a rotating shaft (4), a bevel gear set (5), an adjusting component, a buffer component and a rotating component. The fixing blocks (2) are connected to the front and rear sides of the mounting frame (1), the motors (3) are connected to the left and right sides of the fixing blocks (2), the rotating shafts (4) are rotatably connected to the left and right sides of the lower part of the mounting frame (1), the bevel gear set (5) is connected between the motors (3) and the adjacent rotating shafts (4), the rotating shaft (4) is provided with an adjusting component capable of adjusting and adapting to take-off and landing on terrains of different heights, the adjusting component is provided with a buffer component capable of performing buffering, and the buffer component is provided with a rotating component capable of adjusting and adapting to different angles.

2. The environmentally adaptable UAV landing gear according to claim 1, characterized in that: The mounting frame (1) is provided with a plurality of mounting holes.

3. The environmentally adaptable UAV landing gear according to claim 1, characterized in that: The adjustment component comprises a mounting block (6), an electric push rod (7) and a connecting block (8); the front and rear sides of the rotating shaft (4) are both connected with the mounting block (6); the electric push rod (7) is on the mounting block (6); and the telescopic end of the electric push rod (7) is both connected with the connecting block (8).

4. The environmentally adaptable UAV landing gear according to claim 1, characterized in that: The buffer assembly comprises a sleeve (9), a sliding frame (10) and a telescopic spring (11); the lower side of the connecting block (8) is connected to the sleeve (9); the inside of the sleeve (9) is slidably connected to the sliding frame (10); and the telescopic spring (11) is connected between the sliding frame (10) and the adjacent sleeve (9).

5. The environmentally adaptable UAV landing gear according to claim 1, characterized in that: The rotating assembly comprises a universal shaft (12) and a soft pad (13); the lower side of the sliding frame (10) is rotatably connected to the universal shaft (12); and the lower side of the universal shaft (12) is connected to the soft pad (13).

6. The environmentally adaptable UAV landing gear according to claim 5, characterized in that: The cushion (13) is made of rubber.

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