Journal
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES
Volume 32, Issue 2, Pages 193-197Publisher
WALTER DE GRUYTER GMBH
DOI: 10.1515/tjj-2014-0020
Keywords
squeeze film damper; maneuver flight; centrifugal force; gyroscopic moment; performance of attenuating vibration
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The rotor systems of an aero engine will endure additional centrifugal force and gyroscopic moment during maneuver flight. A maneuver fly mechanical simulator is designed and experimental investigations on dynamics of squeeze film damper (SFD) under the different additional centrifugal force and gyroscopic moment are carried out. The results show that the maneuver flight weaken effectiveness of the SFD, the additional centrifugal force and gyroscopic moment caused by maneuver flight will change film damping, film stiffness. And the influence of maneuver flight can be effective relieved by increasing the film clearance.
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