Oil-electric hybrid multi-rotor wing unmanned aerial vehicle capable of mounting multiple loads

A multi-rotor unmanned aerial vehicle and mounting technology, which is applied to aircraft parts, fuselage frames, equipment for loading and unloading goods, etc. problems, to achieve the effect of convenient transportation and storage, convenient and quick disassembly and replacement, and reduced weight

Pending Publication Date: 2019-05-21
山东蜂巢航空科技有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] To this end, the embodiment of the present invention provides an oil-electric hybrid multi-rotor UAV that can mount various loads, so as to solve the problem that existing rotor UAVs cannot mount various loads, and the UAV occupies a large space. The problem of inconvenient transportation

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  • Oil-electric hybrid multi-rotor wing unmanned aerial vehicle capable of mounting multiple loads
  • Oil-electric hybrid multi-rotor wing unmanned aerial vehicle capable of mounting multiple loads
  • Oil-electric hybrid multi-rotor wing unmanned aerial vehicle capable of mounting multiple loads

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Embodiment Construction

[0029] The implementation mode of the present invention is illustrated by specific specific examples below, and those who are familiar with this technology can easily understand other advantages and effects of the present invention from the contents disclosed in this description. Obviously, the described embodiments are a part of the present invention. , but not all examples. 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.

[0030] Such as figure 1 , 2 , 3 and 4, the oil-electric hybrid multi-rotor UAV that can mount various loads includes a fuselage 100, six arm assemblies 200 and a mounting plate 300. Of course, the number of arm assemblies 200 is not limited to six.

[0031] The fuselage 100 adopts a streamlined fuselage to reduce the flight resistance of the drone during cruising flight. The upper surface of t...

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Abstract

The embodiment of the invention discloses an oil-electric hybrid multi-rotor wing unmanned aerial vehicle capable of mounting multiple loads, and relates to the field of unmanned aerial vehicles. Theoil-electric hybrid multi-rotor wing unmanned aerial vehicle comprises a vehicle body, six vehicle arm assemblies and a mounting plate, undercarriages are arranged on the two sides of the lower portion of the vehicle body respectively, an oil-electric hybrid engine is arranged at the rear end of the lower portion of the vehicle body, and a mounting plate installing hole is formed in the front endof the lower portion of the vehicle body; a mounting equipment installing hole is formed in the middle of the mounting plate, multiple fixing holes are formed in the edge of the mounting plate, the mounting plate and the edge of the mounting plate installing hole are connected through screws, and a shock-absorption ball abuts against the edge of the mounting plate installing hole. By using the mounting plate, different sets of equipment can be mounted, and rapid detaching and installing are realized; since the mounting plate is made from carbon fiber materials, the weight of the unmanned aerial vehicle is reduced greatly; by using the detachable vehicle arms, space occupied during transportation and storage of the unmanned aerial vehicle is effectively shrunk, and therefore transportationand storage are convenient; the undercarriages and the vehicle body are connected through connecting parts, so that the undercarriages are conveniently and rapidly detached and replaced.

Description

technical field [0001] The embodiments of the present invention relate to the field of unmanned aerial vehicles, in particular to an oil-electric hybrid multi-rotor unmanned aerial vehicle capable of carrying various loads. Background technique [0002] The six-rotor UAV is a small unmanned aerial vehicle with flexible flight performance advantages such as vertical lift and hovering. In some environments, it has better practicability than fixed-wing UAVs. It provides lift through six circularly arranged motors, adjusts the attitude by changing the rotor speed, and further realizes position control by adjusting the attitude. It has the advantages of excellent hovering performance, flexible movement, compact mechanical structure, and high reliability of parts. Both military and civilian fields have broad application prospects. After several years of development, the six-rotor UAV has appeared in various forms, but there are still the following problems. The task load mounted ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D9/00B64C1/06
CPCY02T50/40
Inventor 李威尤冰冰温小青冉德伟
Owner 山东蜂巢航空科技有限公司
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