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A drone landing gear

A technology for landing gear and drones, applied in the field of drones, can solve the problems of limited load capacity of drones, unsatisfactory demand, insufficient wing lift, etc., and achieve simple and stable structure, good buffering effect, and good buffering performance Effect

Active Publication Date: 2017-11-28
湖南省金峰机械科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0002] In recent years, with the continuous maturity of UAV technology and the advancement of supporting control equipment, it has the feasibility of various technical applications. At present, the structure of UAV itself is usually a fixed structure, and the main structure is fixed. The lift generated by the wings is insufficient, so that the load capacity of the UAV is limited, and its cushioning performance is poor, which cannot meet the demand

Method used

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  • A drone landing gear

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Embodiment Construction

[0018] Below will make clear and complete explanation to the UAV landing gear of the present invention in conjunction with accompanying drawing.

[0019] like figure 1 As shown, the UAV landing gear of the present invention includes a first support column 1, a second support column 2 above the first support column 1, a third support column 3 above the second support column 2, a The first buffer device 4 on the left side of the first support column 1, the first support device 5 above the first buffer device 4, the second buffer device 6 above the first support device 5, and the The second support device 7 on the right side of the second support column 2 and the third buffer device 8 below the second support device 7 .

[0020] like figure 1 As shown, the first support column 1 is a cuboid, and the first support column 1 is placed vertically. The roller 12 in the groove 11 and the first bracket 13 on the right surface. The first rectangular slot 11 is in the shape of a cuboi...

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Abstract

Landing gear for an unmanned aerial vehicle, comprising a first support column (1), a second support column (2), a third support column (3), a first damping apparatus (4), a first support apparatus (5), a second damping apparatus (6), a second support apparatus (7), and a third damping apparatus (8); a first rectangular groove (11), a roller (12), and a first support bracket (13) are disposed on the first support column (1); a first recessed groove (21), a second recessed groove (22), a first spring (24), a first moving block (23), and a rectangular block are disposed on the second support column (2); a first positioning rod (31) and a second spring (32) are disposed on the third support column (3); the first damping apparatus (4) comprises a first fixing rod (41), a first rotating rod (42), a second rotating rod (43), a first fixing block (41), a third spring (45), and a positioning part (46); the first support apparatus (5) comprises a second support bracket (51), a first support rod (52), a first crossbar (53), and a third support bracket (54); and the second damping apparatus (6) comprises a first horizontal plate (61), a second positioning rod (62), a second horizontal plate (63), a clamping part (64), and an elastic part (65). The present landing gear for an unmanned aerial vehicle provides better and more stable support for an unmanned vehicle, and also has a good damping function, thus preventing damage to the unmanned aerial vehicle.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle landing gear. Background technique [0002] In recent years, with the continuous maturity of UAV technology and the advancement of supporting control equipment, it has the feasibility of various technical applications. At present, the structure of UAV itself is usually a fixed structure, and the main structure is fixed. The lift generated by the wings is insufficient, so that the load capacity of the UAV is limited, and its cushioning performance is poor, which cannot meet the demand. [0003] Therefore, it is necessary to provide a new technical solution to overcome the above defects. Contents of the invention [0004] The object of the present invention is to provide a kind of unmanned aerial vehicle landing gear that can effectively solve the above-mentioned technical problems. [0005] For reaching the purpose of the present inv...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C25/02
CPCB64C25/02B64C25/62
Inventor 朱洪春
Owner 湖南省金峰机械科技有限公司
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