Research Article
Response of Aeroengine with Fusing Design Suffering FBO
Table 5
Response value of a dual-rotor system with varied-stiffness fusing structure.
| Position | Peak value of transient response | Amplitude of steady response |
| Fusing structure activated | 77.2 mm | 29.4 mm | Fusing structure not activated | 72.8 mm | 33.6 mm | Relative deviation | 6.04% | 12.5% |
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