Study of uncontained turbine engine rotor failure airworthiness compliance verification method

摘要：

The safety design is very important to civil aircraft.In order to verify the civil aircraft design whether meet the requirement of airworthiness regulation about the hazards to an airplane in the event of uncontained turbine engine rotor failure, which require the design measures to minimize the hazards in the case of uncontained turbine engine rotor failure.Airworthiness compliance verification method is presented in this paper .Firstly, in the cause of uncontained rotor fragments bursting out, the hazards validation method is proposed based on the results of airplane level functional hazard analysis (FHA) and fault tree analysis (FTA) in this paper.Secondly, airworthiness compliance verification procedure is developed.Thirdly, quantitative assessment model of hazards caused is proposed and calculated.Finally, an example show the whole airworthiness compliance verification procedure include hazards validation, quantitative calculation and airworthiness compliance verdict Results show that the hazard combinations resulting in multiple systems failure can be identified, thus providing more sufficient basis for airplane design improvement to minimize the hazards caused by uncontained engine rotor failure.

关键词： Airworthiness Airworthiness compliance verification Airplane turbine engine Uncontained rotor failure Safety analysis Hazard identification

作者: WANG Fengchan SUN Youchao ZENG Haijun

作者单位: College of Civil Aviation,Nanjing University of Aeronautics and Astronautics,Nanjing,210016,China Zh College of Civil Aviation,Nanjing University of Aeronautics and Astronautics,Nanjing,210016,China

会议类型: 国际会议

会议名称: 航空器适航技术与管理国际会议 ISAA 2011

会议地点: 北京

会议语种:英文

页码: 531-541

在线出版日期: 2011-10-01（万方平台首次上网日期，不代表论文的发表时间）