Aerial platform with escape power assisting system

An aerial platform and power assist system technology, applied in the field of helicopters, can solve the problems of poor endurance of multi-rotor helicopters, and achieve the effect of improving flight stability and sensitivity

Active Publication Date: 2019-03-12
辽宁同心圆科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006]Based on this, in order to solve the problem of poor endurance of the multi-rotor h

Method used

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  • Aerial platform with escape power assisting system
  • Aerial platform with escape power assisting system
  • Aerial platform with escape power assisting system

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Embodiment Construction

[0045] In order to better understand the purpose, technical solution and technical effect of the present invention, the present invention will be further explained below in conjunction with the accompanying drawings and embodiments. At the same time, it is stated that the embodiments described below are only used to explain the present invention, and are not intended to limit the present invention.

[0046] Please also refer to figure 1 and figure 2 , the motor-driven multi-rotor electric booster system includes: an engine 101, a motor / generator 102 and a propeller 100, the engine 101, a motor / generator 102, and the propeller 100 are coaxially connected, and the motor 101 Used to provide total power to the electric power assist system of the engine-driven multi-rotor.

[0047] In one of the embodiments, the engine 101 is also used to provide power for the propeller 100 .

[0048] In one of the embodiments, the engine 101 is also used to provide power for charging the stora...

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Abstract

Disclosed is an aerial platform with an escape power assisting system. The aerial platform with the escape power assisting system comprises n pairs of motors, n pairs of power driving/generating dual-purpose motors and n pairs of propellers, wherein the motors, the power driving/generating dual-purpose motors are in one-to-one correspondence with the impellers through coaxial connection; the engines provides total power for the aerial platform with the escape power assisting system. According to the escape power assisting system for an aero-engine, by means of a power balance controller, whena power assisting system for the aero-engine is inclined, the power balance controller can sensitively control to balance the power assisting system for the aero-engine to avoid crash landing and further improve the flight stability of the power assisting system for the aero-engine.

Description

technical field [0001] The present application relates to the technical field of helicopters, in particular to an aero-engine booster, an aero-engine escape booster, an aero-engine escape booster system and an aerial platform with an escape booster system. Background technique [0002] The difference between a multi-rotor helicopter and a single-blade helicopter is that the multi-rotor helicopter uses n pairs of propellers to fly, and the attitude balance of each pair of propellers needs to be controlled dynamically. The main blade of a single-blade helicopter is located on the axis of the center of gravity, which is naturally drooped to obtain balance. The pros and cons are: when one propeller fails, the remaining rotors of the multi-rotor helicopter can continue to complete the work of sailing or landing safely, while the single-rotor helicopter is destroyed. Obviously, the practicality of multi-rotor helicopters replacing single-blade helicopters is a technical expectati...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64D27/02B64D47/00
CPCB64C27/08B64D27/02B64D47/00B64D2027/026B64U50/11B64U10/10B64U50/19Y02T50/60
Inventor 王景生高峰李明赢商庆海周庆党商凯宇
Owner 辽宁同心圆科技有限公司
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