|
|||||
|
|
| 某型尾桨叶受载分析及叶根改进 | |
| 引用本文： | 鲁伟,蒋建军,王安平.某型尾桨叶受载分析及叶根改进[J].直升机技术,2009(2). |
| 作者姓名： | 鲁伟 蒋建军 王安平 |
| 作者单位： | 1. 兵器工业集团公司第二一二研究所,西安,710065 2. 陆航驻西安地区军事代表室,西安,710068 3. 陆航驻景德镇地区军事代表室,景德镇,333001 |
| 摘 要： | 结合近年来某型直升机在飞行训练中尾桨叶出现了叶尖外偏现象,外偏尺寸较大,并且在根部非工作面上出现了起皱、漆裂的现象。本文就尾桨叶的受力和故障原因进行分析探讨,并给出改进方案。 |
| 关 键 词： | 尾桨叶 起皱 漆裂 叶根改进 受载分析 |
The Endurance Analysis and Oar Base Improvement on a Stroke Oar |
|
| Authors: | LU Wei JIANG Jianjun WANG Anping |
| Institution: | 1.The 212 Institute of Bingqi Corp.; Xi'an; 710065; 2.The PLA General Staff's Army Aviation Bureau and Work in the Xi'an Delegation Office; 710068; 3.The PLA General Staff's Army Aviation Bureau and Work in the Jingdezhen Delegation Office; 333001); |
| Abstract: | Because of the phenomena that outside slanting largely occurs in the oar top and the phenomena that crinkle and lacquer crack appear in the base of the non-working face recently,an improved method which based on the endurance analysis and fault reason was provided. |
| Keywords: | stroke oar crinkle lacquer crack oar base improvement endurance analysis |
| 本文献已被 维普 万方数据 等数据库收录！ | |