Research Article
Response of Aeroengine with Fusing Design Suffering FBO
Table 8
Response value of a dual-rotor system with fractured fusing structure.
| Position | Peak value of transient response (mm) | Amplitude of steady response (mm) |
| Fusing structure activated (mm) | 103.9 | 26.3 | Fusing structure not activated (mm) | 72.8 | 33.6 | Relative deviation (%) | 42.7% | 21.7% |
|
|