Foldable six-axis multi-rotor aircraft

A multi-rotor aircraft and six-axis technology, applied in the field of aviation aircraft, can solve the problems of large geometric size, difficult to carry and transport, etc., to achieve the effect of reducing geometric size, solving the problem of being difficult to carry and transport, and easy to store

Active Publication Date: 2011-03-30
CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] In view of the above content, in order to solve the defects of the prior art, the object of the present invention is to provide a foldable six-axis multi-rotor aircraft, which can effectively solve the problem that the current six-axis multi-rotor aircraft has a large geometric size and is not easy to carry and transport. question

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  • Foldable six-axis multi-rotor aircraft
  • Foldable six-axis multi-rotor aircraft
  • Foldable six-axis multi-rotor aircraft

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Embodiment Construction

[0019] The specific implementation manners of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0020] Depend on Figures 1 to 5 , shown in 9 to 11, a kind of foldable six-axis multi-rotor aircraft of the present invention comprises body 1, motor, six groups of motor installation covers 2, rotor 5 and six support arms, and motor installation cover 2 li is housed , the rotor 5 is placed outside the motor installation cover and connected to the motor, the body 1 is connected to the motor installation cover 2 through the support arm, and the aircraft control system, sensors, batteries and fuel supply system are installed inside the body 1, and it is characterized in that, The six supporting arms include two fixed supporting arms 3 and four rotating supporting arms 4, one end of the fixed supporting arm 3 is fixed on one side of the body 1 by a fastener, and one end of the rotating supporting arm 3 is passed through The faste...

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Abstract

The invention relates to a foldable six-axis multi-rotor c belonging to the field of aviation aircrafts. The foldable six-axis multi-rotor aircraft comprises an aircraft body, motors, six groups of motor mounting hoods, rotors and six supporting arms, wherein a motor is mounted in each motor mounting hood, rotors are arranged outside the motor mounting hood and connected with the motor, the aircraft body is connected with each motor mounting hood through the supporting arms, an aircraft control system, a sensor, a batter and an oil supply system are mounted in the aircraft body, and the six supporting arms comprise two fixed supporting arms and four rotary supporting arms. Through the dual folding structure comprising the horizontal rotary folding of the four supporting arms and the vertical rotary folding of the six supporting arms, the aircraft has smaller geometrical size, is convenient to store and effectively solves the problems of inconvenient carrying and transportation of the multi-axis multi-rotor aircraft.

Description

technical field [0001] The invention relates to the field of aviation aircraft, in particular to a foldable six-axis multi-rotor aircraft. Background technique [0002] Rotor-type aircraft with vertical take-off and landing and hovering functions not only play an important role in the military field, but also show great application potential in disaster scene rescue, dangerous environment detection, traffic surveillance or aerial photography, and have attracted widespread attention. [0003] Currently, rotorcraft mainly include single-rotor (main rotor + tail rotor) helicopters, dual-rotor (coaxial inversion and non-coaxial inversion) helicopters, and multi-rotor aircraft. For example, the MH- 16 helicopters, Russia's Ka-29 helicopter, Germany's Microdrone company, Canada's Dranganflyer company's quadrotor aircraft, etc. The single-rotor helicopter generates lift, side force and required moment through the main rotor, and overcomes the anti-torque torque of the main rotor t...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/08B64C27/37
Inventor 白越高庆嘉孙强续志军
Owner CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI
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