导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2012, Vol. 33 ›› Issue (2): 369.

• Material Engineering and Mechanical Manufacturing • Previous Articles     Next Articles

Study of Residual Stress of Thermal Barrier Coatings by Raman Spectroscopy and Numerical Analysis

HAN Zhiyong, ZHANG Hua, WANG Zhiping   

  1. Tianjin Key Laboratory for Civil Aircraft Airworthiness and Maintenance, Civil Aviation University of China, Tianjin 300300, China
  • Received:2011-10-12 Revised:2011-11-03 Online:2012-02-25 Published:2012-02-24

Abstract: Residual stress of thermal barrier coatings (TBCs) is investigated by experiment and numerical method. Thermal barrier coatings, which consist of CoCrAlY bond coating (BC) and ZrO2 thermat ceramic coating (TCC) are fabricated on the GH99 superalloy by air plasma spray (APS). Meanwhile, residual stress in TBCs during the cooling process is measured by 100-3 500 cm-1 Raman spectroscopy and simulated using finite element method (FEM). The distributions of vertical stresses are analyzed; meanwhile, the results of Raman shift and numerical simulation are compared. The results show that in the vertical direction, there appears compressive stress in TCC, and to the interface of TCC/BC there shows the maximum compressive stress, 14.8 MPa. There appears tensile stress in BC. The results of the simulation are consistent with experimental measurements obtained with micro-Raman spectroscopy.

Key words: thermal barrier coatings, Raman spectroscopy, Raman shift, finite elment method, residual stress

CLC Number: