摘要
为消除飞行人员对副翼人力操纵的疑虑 ,在建立副翼人力操纵可行性分析模型的基础上 ,应用飞行力学的基本原理 ,对某型歼击机因液压系统正常供压部分失效 ,副翼助力器转换为人力操纵后所需的压杆力进行了定量分析计算。结果表明 ,在应急情况下 ,只要处理得当 。
In order to eliminate the suspense of aileron manpower control, the model of feasibility analysis of aileron manpower control was built. Make use of the flying mechanics base principle,this paper analyzed the required power when aileron hydromechanical servomechanism switch to manpower control because of the failure of normal hydraulic power supply in a fighter.Based on it, the article analysed the feasibility of aileron manpower control.The result is,take the suitable process, aileron manpower control is feasible.
出处
《飞行力学》
CSCD
2001年第1期75-77,共3页
Flight Dynamics