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Aircraft and aircraft control method

A technology for an aircraft and a rotor arm, applied in the field of aircraft, can solve problems such as poor safety performance of aircraft, and achieve the effect of avoiding crashes and hazards to the ground and improving safety

Pending Publication Date: 2018-03-20
刘红军
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide an aircraft to solve the technical problem of poor aircraft safety performance in the prior art

Method used

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  • Aircraft and aircraft control method
  • Aircraft and aircraft control method
  • Aircraft and aircraft control method

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Embodiment Construction

[0039] The technical solutions of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are some of the embodiments of the present invention, but not all of them. 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.

[0040] In the description of the present invention, it should be noted that if the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer" appear ", etc., the indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specif...

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Abstract

The invention provides an aircraft and aircraft control method, and relates to the aircraft technical field. The aircraft includes at least four rotor arms; one end of each rotor arm is connected witheach other to form a connection point, and the multiple rotor arms are distributed along the circumferential direction of the connection point in a horizontal plane. Each rotor arm is provided with arotor. The rotor can rotate around the axis of the rotor arm in a vertical plane for adjustment of the working surface of the rotor. When the rotor on any one or more rotor arms fails, the rotor armon which a non-failure rotor is can rotate in the horizontal plane around the connection point, and is fixed at a position to ensure the aircraft can stably fly. In actual use, the aircraft adopting the air-changing technology can rapidly recover to a stable flight state through deformation when power failure causes instability, air crash and hazard to the ground can be avoided, and the safety ofthe aircraft can be improved.

Description

technical field [0001] The present invention relates to the technical field of aircraft, in particular to an aircraft and an aircraft control method for controlling the aircraft. Background technique [0002] Unmanned aircraft, referred to as "aircraft", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by re...

Claims

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Application Information

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IPC IPC(8): B64C39/02B64C27/08
CPCB64C27/08B64C39/02B64U50/19B64U30/20
Inventor 刘红军
Owner 刘红军
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