发明名称 Anisotropic support damper for gas turbine bearing
摘要 An apparatus and method that provides a flexible anisotropic support, which may accommodate open, closed, or re-circulating squeeze film damper in parallel, has improved internal rolling element clearances, limits maneuver and blade loss responses by limiting rotor excursion, and has a rotor centering feature. This is accomplished through the combination of beam and ring arrangement, which provides support anisotropy that produces beneficial cross-coupling stiffness for the support to control synchronous and non-synchronous vibration.
申请公布号 US6682219(B2) 申请公布日期 2004.01.27
申请号 US20020115823 申请日期 2002.04.03
申请人 HONEYWELL INTERNATIONAL INC. 发明人 ALAM MOHSIUL;SPENCER DOUG K.
分类号 F01D25/16;F16C27/04;(IPC1-7):F16C27/04 主分类号 F01D25/16
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