Abstract
A model-based monitoring system is being developed. The concept allows an autonomous identification of different failures. In this paper, a reduced simulation model based on admissible shape functions is presented. It is restricted to faults without impacts or stick-slip-effects, but it is numerically more efficient. Additionally, the test rig in the undamaged state is examined with experimental modal analysis and the bow of the rotor is measured. The model-based monitoring is successfully tested for several failures at a rotor test rig. The amount of the failure is correctly identified, so this system gives useful information for evaluating the condition of the rotor.
Originalsprache | Englisch |
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Publikationsstatus | Veröffentlicht - 2012 |
Veranstaltung | 14th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2012 - Honolulu, HI, USA/Vereinigte Staaten Dauer: 27 Feb. 2012 → 2 März 2012 |
Konferenz
Konferenz | 14th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2012 |
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Land/Gebiet | USA/Vereinigte Staaten |
Ort | Honolulu, HI |
Zeitraum | 27/02/12 → 2/03/12 |