摘要
介绍了某型飞机座舱盖载荷谱编制中,采用包括飞行训练大纲和内厂、外场试飞大纲作为飞行剖面编制依据、以飞参数据作为温度载荷原始输入、温度计算以实测结果进行校对以及温度计算采用大气状态的几个应注意的问题。使座舱盖载荷谱更接近飞机使用的真实情况。
The fatigue loads of a fighter aircraft are affected by many factors.This paper describes a method of compiling loading spectrum.Through calculating service temperature by flight parameter and based on the flight training program,infield and outfield test-fly program,and compares the result with actual-measurement.In addition,different atmosphere parameters affect the canopy transparent temperature also.The loading spectrum with this method can reflect airplane fact usage very well.
出处
《飞机设计》
2010年第6期26-29,37,共5页
Aircraft Design
关键词
座舱盖
载荷谱
飞参数据
温度计算
大气状态
canopy transparent body
loading spectrum
flight parameter
temperature calculation
atmosphere parameter
