Research Article

Response of Aeroengine with Fusing Design Suffering FBO

Table 8

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

PositionPeak value of transient response (mm)Amplitude of steady response (mm)

Fusing structure activated (mm)103.926.3
Fusing structure not activated (mm)72.833.6
Relative deviation (%)42.7%21.7%