罗刚1,张海洋2,吴春波1,陈伟1,丁振东1.航空发动机吞鸟与鸟撞飞机适航通用分析方法[J].航空发动机,2019,45(6):90-96
航空发动机吞鸟与鸟撞飞机适航通用分析方法
General Airworthiness Analysis Method of Aeroengine Bird Ingestion and Aircraft Bird Impact
  
DOI:
中文关键词:  吞鸟  鸟撞  适航  通用分析方法  航空发动机
英文关键词:bird ingestion  bird impact  airworthiness  general analysis method  aeroengine
基金项目:国家自然科学基金(51575262、51475227)资助
作者单位E-mail
罗刚1,张海洋2,吴春波1,陈伟1,丁振东1 1.南京航空航天大学能源与动力学院南京210016 2.中国航发沈阳发动机研究所辽宁省航空发动机冲击动力学重点实验室沈阳110015 mevislab@nuaa.edu.cn 
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中文摘要:
      针对现行有效的14 CFR 中Part33 有关发动机吞鸟和Part25 有关飞机鸟撞的适航规章,分析和对比了相关规章的发展 历史、实施范畴和实施重点,掌握了相关规章的内涵和外延,根据规章中验证方法的内容和特点,揭示了相关规章的设置目的、验证 方法、设备需求等关键技术问题,梳理了相应技术体系,提出了可借鉴的通用适航符合性分析方法与流程。
英文摘要:
      The development history,the implementation category and the implementation focus of the relevant regulations were analyzed and compared with respect to the current valid 14 CFR airworthiness regulations of part 33 related to engine bird ingestion and Part25 related to the aircraft bird impact. The connotation and extension of the relevant regulations were mastered. According to the contents and characteristics of the verification method in the regulations,the key technology problems such as the setting purpose,the verification method and the equipment demand of the relevant regulations were revealed,the corresponding technical system was sorted out,and the applicable general airworthiness analysis method and process could be used for reference.
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