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 number | Peak value of transient response | Amplitude of steady response |
| #1 | With fusing structure | | | Without fusing structure | | |
| #2 | With fusing structure | | | Without fusing structure | | |
| #3 | With fusing structure | | | Without fusing structure | | |
| #4 | With fusing structure | | | Without fusing structure | | |
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