摘要
针对民用支线飞机辅助动力装置(APU)适航条款开展初步研究。从APU在航空器系统中的层级出发,确定其核心适航要求CTSO-C77b,并结合FAA TSO-C77b分析CTSO-C77b的产生和衍变历史,从而依据条款内容和技术特点进行重新分类。通过对比分析FAR-33/CCAR-33R2与CTSO-C77b条款要求的关联性,提出并表明借鉴FAR-33/CCAR-33R2的技术资料及相关研究成果来分析研究APU的适航要求是合理且充分的,上述研究结果可对我国APU适航体系建设提供一定的依据和参考。
The airworthiness regulation for Auxiliary Power Unit(APU)of civil regional aircraft was stud-ied.For the level of APU in aircraft system,the Technical Standard Order CTSO-C77b was determined as the key airworthiness technical requirement.The production and evolution history was analyzed along with the Federal Aviation Administration(FAA)TSO-C77b,and the airworthiness clauses were reclassified based on the specific content and technical characteristics.Through the contrastive analysis and correlation between aero engine airworthiness regulation FAR-33/CCAR-33R2and CTSO-C77b,it is proposed that the technical documents and related research results of FAR-33/CCAR-33R2can be used for APU airwor-thiness technical requirement study and the reasonability and sufficiency are proved.The results are refer-ential for the construction and development of the APU airworthiness system in China.
作者
鲍梦瑶
李果
徐亮
BAO Mengyao;LI Guo;XU Liang(Department of Aircraft Airworthiness Certification,Civil Aviation Management Institute of China,Beijing 100102,China;International Civil Aviation Organization,Air Navigation Bureau Operations Safety Section Airworthiness Panel,Montreal H3C5H7,Canada;Aircraft/Engine Integrated System Safety Beijing Key Laboratory,Beijing University of Aeronautics and Astronautics,Beijing 100191,China;AVIC Nanjing Jincheng Engineering Institute of Aircraft Systems,Nanjing 211106,China)
出处
《燃气涡轮试验与研究》
北大核心
2017年第6期43-48,55,共7页
Gas Turbine Experiment and Research
