会议专题

Certification Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor Failure

This paper sets forth a method of compliance with the requirements of CCAR 25.901(d) and 25.903(d)(1) 1 of the Civil Aviation Administration of China(CAAC) pertaining to design precautions taken to minimize the hazards to an airplane in the event of uncontained engine or auxiliary power unit (APU) rotor failures.A general methodology including the safety and risk analysis to deal with this issue is proposed.The principles to determine the risk factors are also discussed in order to provide a practical method to decide this key factor for risk analysis use.

Uncontained engine failure design precautions rotor burst failure models risk factor turbine CAAC APU

ZHANG Haitao LI Xin

Powerplant System,Shanghai Aircraft Airworthiness Certification Center of CAAC,No. 128 Konggang Yi RD,Shanghai,200335,P.R. China

国际会议

航空器适航技术与管理国际会议 ISAA 2011

北京

英文

521-528

2011-10-01(万方平台首次上网日期,不代表论文的发表时间)