摘要
辅助动力装置(APU)是一个小型的动力装置,其适航要求与动力装置有所不同。对比了TSO-C77b与TSO-C77a的条款要求,分析了APU适航标准的发展趋势,总结了APU本体在TSO验证时,需考虑的飞机级安装条件;通过对比FAR25部部分条款与TSO-C77b的要求的差异性,分析了直接采用TSO-C77b的验证结果来表明符合性的FAR25部相关条款。
Auxiliary power unit（APU） is a small power plant, which is different from the power plant. Compared to the terms and TSO-C77 a TSO-C77 b APU airworthiness standards development trend are analyzed and summed up the APU ontology in the validation of the Tso, the need to consider the aircraft grade installation conditions,by contrast FAR25 part of the terms and TSO-C77 b differences analysis directly by TSO-C77 b verification results to indicate compliance with the FAR25 department related terms requirements.
出处
《装备制造技术》
2015年第7期201-203,共3页
Equipment Manufacturing Technology
关键词
辅助动力装置
适航标准
验证方法
auxiliary power unit
certification standard
compliance method
