年次大会
Online ISSN : 2424-2667
ISSN-L : 2424-2667
セッションID: J1030203
会議情報
J1030203 ロケット用ターボポンプの磁気軸受を用いた制振
廣田 明井上 剛志藤原 浩幸内海 政春
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会議録・要旨集 フリー

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抄録
A damping device so called 'wire mesh damper' has been used between the ball bearing and the casing to increase the system damping. However, it has some disadvantages; it has moderate level of error from the nominal design, and it is difficult to achieve the designed damping performance, etc. In this study, active magnetic bearing is used as the damping device instead of wire mesh damper, and its vibration suppression effect is evaluated numerically. As a result, it is verified that the usage of the active magnetic bearing enables the turbopump system to suppress the vibration level at the third critical speed efficiently.
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