| 直升机尾桨毂拉扭条的设计与制造 |
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| 引用本文： | 覃海鹰,洪蛟.直升机尾桨毂拉扭条的设计与制造[J].直升机技术,2003(1):15-17. |
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| 作者姓名： | 覃海鹰 洪蛟 |
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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： | 拉扭条结构件是直升机主桨毂、尾桨毂通常采用的一种结构承载受力件。本文以直11型机尾桨毂拉扭条为例，详细介绍了直升机尾桨毂拉扭条的结构设计、材料选择、设计计算和加工工艺，对相关的试验情况也进行了介绍。
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| 关 键 词： | 直升机 尾桨毂 拉扭条 结构设计 材料选择 加工工艺 |
THE DESIGN AND MANUFACTURE OF STAINLESS LAMINATED STRIPS OF HELICOPTER TAIL ROTOR HUB |
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| Authors: | QIN Hai-ying HONG Jiao |
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| Abstract: | Stainless laminated strips has usually been selected as a load - bearing structure in main rotor hub and tail rotor hub of a helicopter. With the example of stainless laminated strips used in Z11 tail rotor, this paper presents the configuration design, material selection, design calculation and manufacture method of stainless laminated strips as well as the test instance of stainless laminated strips. |
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| Keywords: | tail rotor hub stainless laminated strips design manufacture |
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