The development history of 33.87 endurance test in aero-engine airworthiness standards CCAR-33R2 was comprehensively reviewed. Based on the interpretation of airworthiness regulation requirements
the current research of 33.87 endurance test in the world was deeply tracked. It showed the endurance test requirement remained essentially unchanged since 1 957 when the current 6 hour×25 cycles formats were implemented
but turbine engine designs had evolved significantly. The progress of engine design technology brought incompatibility with airworthiness regulations
so exploratory research and application on alternative test of 150 hour endurance test was carried out in the world. Despite of some existing issues for clarifications
the relevant research can provide reference for the accepted compliance method research and the airworthiness standard formulation and revision in China. It is of great significance for improving the compilation and revision ability about China's airworthiness technical regulations to track domestic and international airworthiness technology trends continuously and deeply
and then take positive response strategies timely and carry out targeted research on relevant provisions.
Speed prediction for power turbine rotors of turboshaft engine on loss-of-load
Aero-engine stall/surge airworthiness certification method under the influence of crosswind
Civil turboshaft engine induction system icing test
Risk model in conceptual design phase of civil aero-engine type certification
Compliance verification method for pressurized engine static parts of aircraft engine airworthiness
Related Author
FU Qiuju
LUO Mingzhi
XIONG Qingyong
GONG Lifeng
ZHANG Peng
ZHU Xingyu
LI Zhiping
SONG Jianyu
Related Institution
School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Collaborative Innovation Center for Advanced Aero-Engine
Department of Aircraft Airworthiness Certification, Civil Aviation Management Institute of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Engine Certification Center, Civil Aviation Administration of China