直升机操纵范围研究 |
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引用本文: | 张雅铭.直升机操纵范围研究[J].直升机技术,2000(1):1-6. |
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作者姓名: | 张雅铭 |
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作者单位: | 中国直升机设计研究所 景德镇 |
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摘 要: | 本文根据理论研究和飞行实测结果,探讨确定直升机四个操纵,即总距、纵向和横向周期操纵、尾桨距操纵范围的方法,以及应考虑的飞行状态。
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关 键 词: | 直升机 操纵范围 总距 变距 尾桨距 飞行状态 |
THE HELICOPTER CONTROL RANGE RESEARCH |
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Authors: | Zhang Yaming |
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Abstract: | The paper, based on theoretic resarch and flight tesl results, studies how to determine four controls of helicopter, it control range method of collective pitch. Longitudinal and lateral control, tail rotor collective pitch,and flight conditions that should be considered. |
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Keywords: | helicopter control range |
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