Numerical and Experiment Investigation of the Friction Coefficient in Gas Turbine Impeller Dovetail Joints
- 作者: Sapron D.V.1, Gukasyan S.G.1, Mezentsev M.A.1
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隶属关系:
- P.I. Baranov Central Institute of Aviation Motors (CIAM)
- 期: 卷 62, 编号 3 (2019)
- 页面: 381-386
- 栏目: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/231018
- DOI: https://doi.org/10.3103/S1068799819030048
- ID: 231018
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详细
This paper proposes a numerical and experimental approach for determining the friction coefficient in gas turbine impeller dovetail joints. The approach involves comparing the results of numerical simulation of the impeller rotation at different friction coefficients and the experiment data from strain-gauge measurement of the structure characteristic areas.
作者简介
D. Sapron
P.I. Baranov Central Institute of Aviation Motors (CIAM)
编辑信件的主要联系方式.
Email: sapronov@ciam.ru
俄罗斯联邦, ul. Aviamotornaya 2, Moscow, 111116
S. Gukasyan
P.I. Baranov Central Institute of Aviation Motors (CIAM)
Email: sapronov@ciam.ru
俄罗斯联邦, ul. Aviamotornaya 2, Moscow, 111116
M. Mezentsev
P.I. Baranov Central Institute of Aviation Motors (CIAM)
Email: sapronov@ciam.ru
俄罗斯联邦, ul. Aviamotornaya 2, Moscow, 111116
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