本文介绍了直11型直升机旋翼系统动部件飞行载荷测量技术及方案。
This text introduces test technology solutions of Z11 flight load test of rotor system dynamic components.
某型共轴双旋翼直升机计算实例表明，所得结果与该型直升机飞行特性一致。
Calculation example given indicates that the equations of dynamic response proposed for vertical movement and direction rotation reflect flight characteristics of this helicopter.
该设计用于“一驱二”图形发生器，已成功应用于某型直升机玻璃座舱显示系统。
This kind of video controller has been used in the glass cockpit display system of a helicopter.
应用推荐