| 直升机自转进入和退出发动机控制逻辑的设计 |
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| 引用本文： | 左丽华,胡招才,阮红霞.直升机自转进入和退出发动机控制逻辑的设计[J].直升机技术,2009(3). |
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| 作者姓名： | 左丽华 胡招才 阮红霞 |
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| 作者单位： | 中国直升机设计研究所,景德镇,333001 |
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| 摘 要： | 直升机自转进入和退出是直升机机动飞行经常遇到的状态,它的特性是由直升机旋翼和发动机的安装特性共同决定的,该状态的发动机控制是典型的直升机与发动机的综合控制。本文介绍了直升机自转进入和退出发动机控制逻辑的设计和验证。
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| 关 键 词： | 直升机 发动机控制 自转 |
Engine Control Logic Design of Autorotation Entry and Recovery |
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| Authors: | ZUO Lihua HU Zhaocai RUAN Hongxia |
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| Institution: | ZUO Lihua; HU Zhaocai; RUAN Hongxia(China Helicopter Research and Development Institute; Jingdezhen; 333001); |
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| Abstract: | Helicopter autorotation entry and recovery occurs regularly during manoeuvring and autorotation training.It is a characteristic of the helicopter rotor and its engine installation,and the engine control in this condition is a typical integration control of the helicopter and the engine.The engine control law design of autorotation entry and recovery as well as its verification is described in this paper. |
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| Keywords: | helicopter engine control autorotation |
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