Research Status of Aero-Engine Blade Fly-off

Author:

Zhang Longfei,Li Jing,Kou Ying

Abstract

Abstract The research of aero engine blade out (Fan Blade Out, FBO) is an important problem that must be solved in the design stage of the reliability and safety of the whole structure. The turbofan blades are broken due to fatigue fracture or foreign object impact, and the rotor system produces large vortex under the action of huge unbalanced force, which causes the tip of the blade to collide with the casing and friction in turn. This paper analyzes the aero-engine FBO, and provides a systematic basic theory for the design, innovation and development, which has certain reference value.

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Reference19 articles.

1. Review of research on the loss of aero-engine blades [J];Ma;Journal of Aerospace Power,2016

2. Non-linear Transient Rotor-dynamics Analysis of Fan Blade Out;Liu;State Key Lab of Mechanical System and Vibration, Shanghai Jiao Tong University.,2019

3. Study on the transient response characteristics of a single-disk rotor with sudden imbalance [J];Li;Mechanical Science and Technology for Aerospace Engineering,2012

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