|
| High Stress Vibration Fatigue Test Technology of Aeroengine Blade |
| Received:February 06, 2013 Revised:July 01, 2013 |
| View Full Text View/Add Comment Download reader |
| DOI：10.7643/issn.1672-9242.2013.04.011 |
| KeyWord:vibration fatigue test aeroengine blade resonance magnification electric shaker vibration stress |
| Author | Institution |
| HE Sheng-shuai |
Beijing Institute of Structure and Environment Engineering，Beijing，China |
| CHEN Li-wei |
Beijing Institute of Structure and Environment Engineering，Beijing，China |
| QIANG Xiao-hui |
Beijing Institute of Structure and Environment Engineering，Beijing，China |
| DENG Ying |
AVIC Beijing Aeronautical Manufacturing Technology Research Institute，Beijing，China |
|
| Hits: |
| Download times: |
| Abstract: |
| High stress vibration fatigue test of several aeroengine blades were carried out on electric shaker and the test mechanism was studied. New test methods were put forward, which were blade maximal vibration stress monitoring using assisting points and fixed frequency excitation after resonance frequency. Open loop control technology of vibrating table was successfully applied to stabilize vibration stress and reliable fatigue data were obtained. The relation between the excitation of electric shaker and the vibration response of blade was discussed. |
| Close |