摘要
飞机全静压系统采集空气全压及静压数据用于计算空速、高度等飞行参数。本文旨在通过对全静压系统的介绍及测试原理分析,总结一些实际工作中的注意要点。
Aircraft pitot-static pressure system collects air total pressure and static pressure data for calculation of airspeed, altitude and other flight parameters. This paper aims to summarize some of noted points in the practical work by introducing the pitot-static pressure system and analyzing the test principle.
出处
《价值工程》
2015年第5期64-65,共2页
Value Engineering
关键词
全静压
皮托管
静压孔
渗漏
密封性
pitot-static pressure
pitot tube
static pressure ports
leakage
tightness
