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contributor authorDu, Chenhong
contributor authorWang, Yanrong
contributor authorJiang, Xianghua
date accessioned2025-08-20T09:47:32Z
date available2025-08-20T09:47:32Z
date copyright5/12/2025 12:00:00 AM
date issued2025
identifier issn0742-4795
identifier othergtp_147_11_111004.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4308859
description abstractBlisks are utilized by most modern aircraft turbine engines to reduce the weight of rotors and eliminate air leakage between platforms. Ring dampers are widely used to reduce the vibration of blisks and avoid high-cycle fatigue. Two methods are proposed to calculate the damping caused by the radial displacement of the ring damper. First, the analytic method was provided by previous researchers. It is improved to increase the precision on calculating the range of slipping region. Second, a one-dimensional (1D) finite element method with novel iteration process is introduced by us. In this method, the ring damper is modeled using rod elements, and the energy dissipation due to friction is calculated through maximum displacement or time-marching. The damping ratio of the ring damper under arbitrary standing wave modes can be calculated using this novel method. The simulation results show that the 1D finite element method has good mesh independence. Both methods show good agreement in terms of damping ratio and the position of the slipping region.
publisherThe American Society of Mechanical Engineers (ASME)
titleMethod for Predicting the Damping Ratio of Ring Dampers in Radial Standing Waves
typeJournal Paper
journal volume147
journal issue11
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4068388
journal fristpage111004-1
journal lastpage111004-9
page9
treeJournal of Engineering for Gas Turbines and Power:;2025:;volume( 147 ):;issue: 011
contenttypeFulltext


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