Research Article

Response of Aeroengine with Fusing Design Suffering FBO

Table 5

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

PositionPeak value of transient responseAmplitude of steady response

Fusing structure activated77.2 mm29.4 mm
Fusing structure not activated72.8 mm33.6 mm
Relative deviation6.04%12.5%