摘要
本文从飞机型号单机寿命管理的需求出发,着眼于解决单机寿命管理中两大难点之一的飞行载荷分散性问题,通过对飞行参数的解析并结合飞机设计使用的气动载荷数据库、质量分布数据,开发了一套载荷即时分析计算方法。
Based on the requirements of single aircraft life management,this paper focuses on solving the problem of flight load dispersion,which is one of the two difficulties in single aircraft life management.Through the analysis on flight parameters,combined with the aerodynamic load database and mass distribution data used in aircraft design,a set of real-time load analysis and calculation method is developed.
作者
任智勇
马经忠
王国良
Ren Zhiyong;Ma Jingzhong;Wang Guoliang(AVIC Hongdu,Nanchang,Jiangxi,330024)
出处
《教练机》
2020年第4期9-12,共4页
Trainer
关键词
单机寿命管理
飞行载荷
疲劳
Single aircraft life management
Flight load
Fatigue