[1]
Xu X., Li H., Feng G., Applications of structural fuse design on fan blade off of high bypass ratio turbofan engine. Aeroengine, 2018, 44(2): 1–8.
[2]
CCAR-33R2 Airworthiness standards: Aircraft engines. Civil Aviation Administration of China, Beijing, China, 2011.
[3]
Federal aviation administration: turbine engine rotor blade containment/durability: advisory circular 33–5. United States Department of Transportation, Washington D.C., U.S., 1990.
[4]
CS-25 certification specifications for large aeroplanes. European Aviation Safety Agency, Cologne, Germany, 2013.
[5]
Sinha S., Dynamic characteristics of a flexible bladed-rotor with coulomb damping due to tip-rub. Journal of Sound and Vibration, 2004, 273: 875–919.
[6]
Ma Y., Liang Z., Wang G., et al., Review on fan blade out event analysis for aero-engine. Journal of Aerospace Power, 2016, (3): 513–526.
[7]
Sinha S., Rotordynamic analysis of asymmetric turbofan rotor due to fan blade-loss event with contact-impact rub load. Journal of Sound and Vibration, 2013, 332: 2253–2283.
[8]
Williams R., Simulation of blade casing inter-action phenomena in gas turbines resulting from heavy tip rubs using an implicit time marching method. ASME Paper 2011, GT2011-45495.
[9]
Hong J., Li T., Wang Y., et al., Dynamic response of aero-engine flexible rotor system under the blade-off. Journal of Aerospace Power, 2018, 33(2): 257–264.
[10]
Liu L., Zhao Z., Chen W., et al., Simulated test and numerical simulation of aero-engine whole engine response during blade out event. Journal of Aerospace Power, 2018, 33(2): 290–298.
[11]
Airbus A330–343, registration B-HLM engine fire event final report. Air Accident Investigation Bureau of Singapore, Ministry of Transport Singapore, Singapore, 2014.
[12]
Nicolas C., David C., Jerome B., Prediction of transient engine loads and damage due to hollow fan blade-off. Revue Européenne des Éléments Finis, 2002, 11(5): 651–666.
[13]
Ma C., Liu L., Chen W., et al., Response of aeroengine with fusing design suffering FBO. International Journal of Aerospace Engineering, 2019, 11(5): 1155–1172.
[14]
Xu X., The position of a location bearing for the low pressure shaft of a 3-shaft turbofan engine and its influence. Cranfield University, Bedford, UK, 2010.
[15]
Xu X., Li H., Feng G., Low pressure shaft and structural fuse dynamic behavior simulation for Trent 900 engine after a fan blade out event. Journal of Aerospace Power, 2020, 35(4): 1–13.
[16]
Su X., Ma C., Yuan X., Adjoint-based geometrically constrained aerodynamic optimization of a transonic compressor stage. Journal of Thermal Science, 2019, 28: 850–861.
[17]
Wang Y., Kang D., Zhong J., Reconstruction method for running shape of rotor blade considering nonlinear stiffness and loads. Journal of Thermal Science, 2017, 26: 431–439.
[18]
Liu X., Dynamic constitutive relationship of TC4 titanium alloy. Nanjing University of Aeronautics and Astronautics, Nanjing, 2010.
[19]
Chen G., Aeroengine structural design and analysis. BUAA press, Beijing, 2009.
