| 直升机旋翼/斜梁折叠控制系统原理与改进措施 |
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| 引用本文： | 邹小玲.直升机旋翼/斜梁折叠控制系统原理与改进措施[J].直升机技术,2011(3):20-24,19. |
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| 作者姓名： | 邹小玲 |
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| 作者单位： | 中航工业直升机设计研究所,江西景德镇,333001 |
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| 摘 要： | 旋翼、斜梁折叠是舰载直升机特定的基本功能。从直升机旋翼/斜梁折叠电气系统分析出发,通过分析折叠系统工作原理和电气故障原因,提出系统改进方法。
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| 关 键 词： | 直升机 旋翼 斜梁 折叠 |
The Analysis and Mend of the Helicopter Rotor/Pylon Folding System |
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| Authors: | ZHOU Xiaoling |
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| Institution: | ZHOU Xiaoling(AVIC Helicopter Research and Development Institute,Jingdezhen 333001,China) |
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| Abstract: | The folding system of main rotor and tail pylon is basic mission system for the shipborne helicopter.In order to bring forward folding system's improvement proposal,the operating principle and fault symptom of electronic equipment were analyzed. |
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| Keywords: | helicopter rotor pylon folding |
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