| 小型航空发动机联轴器设计及应用 |
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| 引用本文： | 张旭东,李明强,孙奇,张娟. 小型航空发动机联轴器设计及应用[J]. 内燃机与配件, 2021, 0(3): 139-140 |
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| 作者姓名： | 张旭东 李明强 孙奇 张娟 |
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| 作者单位： | 西北工业大学365所,西安710065;西安航空制动科技有限公司,西安710065 |
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| 摘 要： | 发动机联轴器对主动轴和从动轴同轴度、重量以及换向和变速时要求传动轴不能受到冲击力等方面有着更高的要求.为进一步满足小型航空发动机减重、简洁、可靠、经济的发展要求,提供了一种小型航空发动机联轴器设计方案并应用.有效的解决了主动轴和从动轴同轴度、机构重量和在换向与变速时传动轴不能受到冲击力的要求,结构简单,消除了换向间隙,...
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| 关 键 词： | 联轴器 发动机 设计 |
Design and Application of Small Aero Engine Coupling |
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| ZHANG Xu-dong,LI Ming-qiang,SUN Qi,ZHANG Juan. Design and Application of Small Aero Engine Coupling[J]. Internal Combustion Engine & Parts, 2021, 0(3): 139-140 |
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| Authors: | ZHANG Xu-dong LI Ming-qiang SUN Qi ZHANG Juan |
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| Affiliation: | (Institute of 365,Northwestern Polytechnic University,Xi'an 710065,China;Xi'an Aviation Brake Technology Co.,Ltd.,Xi'an 710065,China) |
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| Abstract: | The engine coupling has higher requirements on coaxiality,weight of driving shaft and driven shaft,as well as the requirement that the transmission shaft should not be impacted when reversing and changing speed.In order to meet the development requirements of small aero-engine such as weight reduction,simplicity,reliability and economy,a design scheme of coupling for small aero-engine is provided and applied.It effectively solves the requirements of coaxiality of driving shaft and driven shaft,weight of mechanism and transmission shaft can not be impacted when reversing and changing speed.The structure is simple,eliminates the reversing clearance,improves the service life and reliability of coupling,and reduces the manufacturing cost. |
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| Keywords: | coupling engine design |
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