| タイトル | Critical speeds and forced response solutions for active magnetic bearing turbomachinery, part 1 |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910011896 |
| 著者（英） | Kirk, R. Gordon; Keesee, J.; Rawal, D. |
| 著者所属（英） | Virginia Polytechnic Inst. and State Univ. |
| 発行日 | 1991-03-01 |
| 言語 | eng |
| 内容記述 | The prediction of critical speeds and forced response of active magnetic bearing turbomachinery is of great interest due to the increased use of this new and promising technology. Calculating the system undamped critical speeds and forced response is important to all those who are involved in the design of the active magnetic bearing system. An extended Jeffcott model which was used as an approximate solution to a more accurate transfer matrix procedure is presented. Theory behind a two-degree-of freedom extended Jeffcoat model is presented. Results of the natural frequency calculation are shown followed by the results of the forced response calculation. The system response was predicted for two types of forcing. A constant magnitude excitation with a wide frequency variation was applied at the bearings as one forcing function. The normal unbalance force at the midspan was the second source of excitation. The results of this extended Jeffcott solution gives useful design guidance for the influence of the first and third modes of a symmetric rotor system. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 91N21209 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/133232 |
