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Indexed by:期刊论文

Date of Publication:2016-11-01

Journal:AEROSPACE SCIENCE AND TECHNOLOGY

Included Journals:SCIE、EI、Scopus

Volume:58

Page Number:248-257

ISSN No.:1270-9638

Key Words:Integrally bladed disk; Damping hard coating; Vibration analysis; Complex modulus; Loss factor; Rayleigh-Ritz method

Abstract:For the blisk (integrally bladed disk) with damping hard coating on blades, an analytical approach is developed to calculate its free vibration characteristics and damping effect, based on the constitutive model of complex modulus and Rayleigh-Ritz method. Firstly, by using the Oberst beam theory, equivalent elastic modulus and loss factor of the coated blade are derived. Then energy equations of the bladed disk on basis of complex modulus are given. By employing a set of orthogonal polynomials as the admissible function, the Rayleigh-Ritz method is used to formulate the equations of motion. Solutions are obtained as complex eigenvalues, whose real parts are undamped frequencies and imaginary parts represent the damping coefficient. Further, frequency response function can be achieved, by using of proportional damping model to obtain damping matrix. An academic bladed disk made of stainless steel is taken as example to conduct numerical calculation, and compared with the experimental results by both natural frequencies and modal shapes. NiCrA1Y coating is deposited on single side of the blades to investigate its effect on the natural frequencies, modal loss factors and frequency responses. At last, influence of the coating thickness on the variation of natural frequencies and damping capacity is discussed. (C) 2016 Elsevier Masson SAS. All rights reserved.