The Experimental Research on the Vibration Performance of SFD in Maneuver Right

摘要：

The rotor system of an aero-engine endures additional centrifugal force and gyroscopic moment in maneuver flight. This paper studies the SFDs performance of attenuating the vibration with different additional centrifugal forces and gyroscopic moments applied on the rotor system. The result shows that the influence of maneuver flight on the SFDs damping performance significant. The effect of maneuver flight is relieved by increasing the film clearance.

关键词： squeeze film damper maneuver flight centrifugal forcet gyroscopic moment performance of attenuating vibration

作者: LI Wei LIAOMing-fu WANG Si-ji

作者单位: School of Power and Energy, Northwestern Polytechnical University, Xian , China

会议类型: 国际会议

会议名称: 4th International Symposium on Jet Propulsion and Power Engineering(第四届喷气推进与动力工程国际会议 ISJPPE2012)

会议地点: 西安

会议语种:英文

页码: 447-451

在线出版日期: 2012-09-10（万方平台首次上网日期，不代表论文的发表时间）