海军航空工程学院学报Issue(3)：252-256,5.DOI:10.7682/j.issn.1673-1522.2014.03.012
基于弹性起落架的直升机系留载荷计算
Calculation of Mooring Tension of the Ship-based Helicopter with Elastic Landing Gear
吴靖 1胡国才1
作者信息
- 1. 海军航空工程学院飞行器工程系，山东烟台264001
- 折叠
摘要
Abstract
According to analyzing the force situation of the ship-based helicopter moored on the ship, a equation set of verti-cal deformation of landing gear based on virtual work principle was derived. Then, the mooring tension was calculated by deformation of landing gear. Newton iterative method was used to solve the equation set. It was found that the mooring ten-sion were mainly distributed to main landing gear’s cable when roll amplitude were bigger than pitch amplitude and wind load couldn’t be ignored. Finally, the influence of tyre’s rigidity was analyzed. The results showed that the biggest tension decreased 7.43%when the tyre’s rigidity increased from 300 N/mm to 800 N/mm tyre’s. That was to say it could improved the safety of the moored helicopter.关键词
直升机/系留/起落架/虚位移原理Key words
helicopter/mooring/landing gear/virtual work principle分类
航空航天引用本文复制引用
吴靖,胡国才..基于弹性起落架的直升机系留载荷计算[J].海军航空工程学院学报,2014,(3):252-256,5.
