Civil minitype unmanned verticraft jet landing gear

A small unmanned aerial vehicle, jet-type technology, applied in the field of unmanned aerial vehicles, can solve problems such as unbalanced fuselage weight, unmanned aerial vehicle falling, and fuselage tilting, and achieve the effect of reasonable structure and improved safety and practical performance

Inactive Publication Date: 2018-06-29
成都市煜沣科技有限公司
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  • Abstract
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  • Claims
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AI Technical Summary

Problems solved by technology

[0002] The UAV market has developed rapidly in recent years. As the civilian use of UAVs continues to expand, more and more home users choose to use UAVs. The propellers provide lifting force, and the weight of the fuselage is unbalanced, which leads to the problem that the fuselage is prone to tilt during take-off and landing, and sometimes the tilt of the fuselage is likely to cause the drone to fall and cause serious consequences. How to solve it Existing technical problems have become an urgent need for technical personnel in related fields to solve

Method used

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  • Civil minitype unmanned verticraft jet landing gear
  • Civil minitype unmanned verticraft jet landing gear

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Embodiment Construction

[0016] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0017] In the description of the present invention, it should be noted that the orientation or positional relationship indicated by the terms "vertical", "upper", "lower" and "horizontal" are based on the orientation or positional relationship shown in the drawings, and are only for It is convenient to describe the utility and simplify the description, but does not indicate or imply that the device or element referred to must have a specific orientation, be con...

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Abstract

The invention discloses a civil minitype unmanned verticraft jet landing gear, which comprises a first supporting leg and a second supporting leg; a transverse supporting rod is fixedly connected between the first supporting leg and the second supporting leg; the first supporting leg is internally provided with a second placement cavity which is communicated with a first ventilation hole; a distance induction controller and a first controller are sequentially installed above a first minitype turbine motor; a second communicating pipe is fixedly connected to the upper end of a second air nozzle; and a second controller and a power supply component are sequentially installed above a second minitype turbine motor. The civil minitype unmanned verticraft jet landing gear is reasonable in structure and exerts the boosting effect through the minitype turbine motors in the landing gear, so that the unmanned verticraft can be smoother and rapider during rising or landing; and meanwhile, the equipped distance inductor can automatically control the turbine motors when landing to a certain height from the ground, the possibility of controlling rapid falling is realized, and the safety and practicability of the unmanned verticraft is improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a jet landing gear of a civilian small unmanned aerial vehicle. Background technique [0002] The UAV market has developed rapidly in recent years. As the civilian use of UAVs continues to expand, more and more home users choose to use UAVs. The propellers provide lifting force, and the weight of the fuselage is unbalanced, which leads to the problem that the fuselage is prone to tilt during take-off and landing, and sometimes the tilt of the fuselage is likely to cause the drone to fall and cause serious consequences. How to solve it Existing technical problems have become urgent needs for those skilled in the art to solve. Contents of the invention [0003] The object of the present invention is to provide a jet landing gear of a civil small unmanned aerial vehicle, to solve the problems raised in the above-mentioned background technology. [0004] In order...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C25/02
CPCB64C25/02
Inventor 郑向东
Owner 成都市煜沣科技有限公司
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