某型民用飞机电源系统负加速度试飞研究  

Research of Electrical Power System Negative Acceleration Flight Test for a Civil Aircraft

作　　者：曹涛[1] 

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《航空科学技术》2015年第3期67-69,共3页Aeronautical Science & Technology

摘　　要：首先对民用飞机电源系统负加速度试飞进行简要说明,提出民用飞机电源系统负加速度试飞的原因和目的。其次对电源系统负加速度试飞条件、试飞方法和试飞程序进行说明。对电源系统负加速试飞结果进行分析评估,表明电源系统设计是满足设计要求和民用航空标准要求的。最后对负加速度试飞中注意事项进行了详细说明,为其它机型飞机进行负加速度试飞提供借鉴。Firstly, brielfy introduced the electrical power system negative acceleration lfight test of civil aircraft, and illustrated the negative acceleration lfight test causation and purpose. Secondly, introduced the electrical power system negative acceleration lfight test conditions and methods and procedure. The lfight test data was analyzed to conifrm the electrical power system design can meet the design requirements and the civil aircraft standard requirements. Lastly, detail illustrated the attention items of negative acceleration lfight test to conduce to negative acceleration lfight test in other type aircraft.

关 键 词：民用飞机 电源系统 负加速度 试飞 

分 类 号：V328[航空宇航科学与技术—人机与环境工程]