摘要
助力器小轴材料在低温试验时发生相变,因残余奥氏体较多导致小轴尺寸变大,引起操纵力变大.通过原理分析,查明原因排除故障,并对故障的发生进行了思考,从技术和管理两个方面提出了改进建议.
When the assistance organ＇s spare parts are heat treated, there will be much more the remnant Aoshiti. In low temperature test they change, their size changes, revoking the airplane assistance organ＇s control power increase. By analyzing its principle, the matter of trouble is found out and removed. At last, some prophylaxis advices are raised.
出处
《海军航空工程学院学报》
2005年第6期676-677,680,共3页
Journal of Naval Aeronautical and Astronautical University
关键词
助力器
低温试验
操纵力
assistance organ
low temperature test
control power
