首页> 外文会议>CSAA/IET International Scientific-Technical Conference on Actual Problems of Electronics Instrument Engineering >Research on the pressure peak of landing gear uplock opening for civil aircraft
【24h】

Research on the pressure peak of landing gear uplock opening for civil aircraft

机译:民用飞机起落架上锁开启压力峰值的研究

获取原文

摘要

This paper do a research on the pressure peak of landing gear uplock unlocking for civil aircraft. This paper first do a theory analysis and find out relevant factors like valve opening time, tube length, tube diameter and a restrictor. Then based on the AMEsim platform, a simulation model is built. From the simulation results, it can be known that the valve opening time, tube length, tube diameter and a restrictor all can have an obvious effect on the uplock pressure peak. An optimize solution is found after a trade-off analysis.
机译:本文对民用飞机起落架上锁解锁的压力峰值进行了研究。本文首先进行理论分析,并找出相关因素,如阀门开启时间,管长,管径和节流阀。然后基于AMEsim平台,建立了仿真模型。从模拟结果可以看出,阀门开启时间,管长,管径和节流阀都可以对上锁压力峰值产生明显影响。经过权衡分析后,找到了一个优化解决方案。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号