Research Article

Response of Aeroengine with Fusing Design Suffering FBO

Table 7

Response value of a dual-rotor system with varied-stiffness fusing structure.

Bearing numberPeak value of transient responseAmplitude of steady response

#1With fusing structure
Without fusing structure

#2With fusing structure
Without fusing structure

#3With fusing structure
Without fusing structure

#4With fusing structure
Without fusing structure