首页> 外文会议>International conference on measuring technology and mechatronics automation >Research of Flow and Pressure Pulsation in Aircraft eicing System
【24h】

Research of Flow and Pressure Pulsation in Aircraft eicing System

机译:飞机除冰系统流量和压力脉动的研究

获取原文

摘要

Aiming at the flow and pressure pulsation caused by the reciprocating pump in aircraft deicing system, two solutions are presented in the paper. First, based on computational fluid dynamics and finite element analysis theory, the assembled ways of rigid and flexible accumulators are applied to absorb vibration in order to inhibit the pulse. Then, the control algorithm for multiple phases of three pumps is used to offset the pulse energy among the pumps. At last, simulation results show that both methods have effectively reduced the pulsation in the aircraft deicing system.
机译:针对飞机除冰系统中往复泵引起的流量和压力脉动,提出了两种解决方案。首先,基于计算流体动力学和有限元分析理论,采用刚性和柔性蓄能器的组合方式吸收振动,以抑制脉冲。然后,使用三个泵的多相控制算法来抵消泵之间的脉冲能量。最后,仿真结果表明,两种方法均有效地降低了飞机除冰系统中的脉动。

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