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Landing gear of unmanned aircraft

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: 2015-11-18
湖南省金峰机械科技有限公司
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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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  • Landing gear of unmanned aircraft

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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] Such as 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] Such as 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...

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Abstract

The invention discloses a landing gear of an unmanned aircraft. The landing gear comprises a first supporting column, a second supporting column, a third supporting column, a first buffering device, a first supporting device, a second buffering device, a second supporting device and a third buffering device, wherein a first rectangular groove, a rolling wheel and a first bracket are formed / arranged in / on the first supporting column; a first groove, a second groove, a first spring, a first movable block and a rectangular block are formed / arranged in / on the second supporting column; a first positioning rod and a second spring are arranged on the third supporting column; the first buffering device comprises a first fixed rod, a first rotary rod, a second rotary rod, a first fixed block, a third spring and a positioning part; the first supporting device comprises a second bracket, a first supporting rod, a first transverse rod and a third bracket; the second buffering device comprises a first horizontal plate, a second positioning rod, a second horizontal plate, a clamping part and an elastic part. Through the adoption of the landing gear disclosed by the invention, the unmanned aircraft can be well and firmly supported; besides, the landing gear has good buffering performance, so that the unmanned aircraft can be prevented from being damaged.

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 problem. [0005] For reaching the purpose of the present inve...

Claims

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Application Information

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