Unmanned aircraft

An unmanned and aircraft technology, applied in the field of aircraft, can solve the problems of high speed and high endurance, short flight time and range, and low speed of the quadcopter, and achieves light weight, high speed and structure. simple effect

Active Publication Date: 2016-11-16
CHINA AVIATION MARINE EQUIP YANTAI TECH CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0003] However, the quadcopter also has many disadvantages, for example, the quadcopter has low speed, flight time and short ran

Method used

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[0050] The implementation of the present invention will be described in detail below with reference to the accompanying drawings and embodiments, so as to fully understand how the present invention applies technical means to solve technical problems and achieve the realization process of technical effects and implement them accordingly. It should be noted that, as long as there is no conflict, each embodiment of the present invention and each feature in each embodiment can be combined with each other, and the technical solutions formed are all within the protection scope of the present invention.

[0051] Meanwhile, in the following description, many specific details are set forth for the purpose of explanation to provide a thorough understanding of the embodiments of the present invention. However, it is obvious to those skilled in the art that the present invention can be implemented without the specific details or the specific manner described herein.

[0052] In addition, the s...

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Abstract

An unmanned aircraft comprises an aircraft body, fixed wings fixed to the two sides of the aircraft body and multiple rotors connected to the two sides of each fixed wing through rotor supporting parts. Rotor shafts of the unmanned aircraft do not need to rotate relative to the wings, so that complex mechanical components for controlling and adjusting rotation of the rotor shafts do not need to be configured, and compared with an existing tilting rotor aircraft, the aircraft is simpler in structure and smaller in weight. Meanwhile, a set of power devices, namely the rotors and motors corresponding to the rotors are adopted in the unmanned aircraft to achieve the functions of vertical take-off and landing and fixed wing modal cruising, and compared with an existing aircraft, the unmanned aircraft can supply larger weight and meet the requirements for the task load and the voyage endurance.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to an unmanned aircraft. Background technique [0002] Due to the advantages of small size, light weight, and easy portability, the quadcopter has been more and more widely used in various fields. Quadcopters can easily enter special environments that humans cannot enter. Therefore, in addition to being used to make models, quadcopters can also be used to perform flight tasks such as aerial photography, real-time monitoring, and terrain exploration. [0003] However, the quadcopter also has many disadvantages, for example, the quadcopter has low speed, short flight time and short range, which makes the quadcopter unsuitable for application scenarios with strict requirements on high speed and high battery life. Contents of the invention [0004] In order to solve the above problems, the present invention provides an unmanned aerial vehicle, which comprises: [0005] aircraft bod...

Claims

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Application Information

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IPC IPC(8): B64C29/02B64C27/26G05D1/10
CPCB64C27/26B64C29/02G05D1/102B64C29/0025B64C39/024G05D1/042B64U70/00B64U30/10B64U10/25B64U30/20
Inventor 于进勇
Owner CHINA AVIATION MARINE EQUIP YANTAI TECH CO LTD
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