Volume 42 Issue 6
Nov.  2012
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YANG Li, ZHOU Yichun, QI Shasha. RESEARCH PROGRESS IN EROSION MECHANISMS OF THERMAL BARRIER COATINGS[J]. Advances in Mechanics, 2012, 42(6): 704-721. doi: 10.6052/1000-0992-12-003
Citation: YANG Li, ZHOU Yichun, QI Shasha. RESEARCH PROGRESS IN EROSION MECHANISMS OF THERMAL BARRIER COATINGS[J]. Advances in Mechanics, 2012, 42(6): 704-721. doi: 10.6052/1000-0992-12-003

RESEARCH PROGRESS IN EROSION MECHANISMS OF THERMAL BARRIER COATINGS

doi: 10.6052/1000-0992-12-003
Funds:  The project was supported by the National Natural Science Foundation of China (11272275, 51172192, 11002122), the Natural Science Foundation of Hunan Province for Innovation Group (09JJ7004),and the Natural Science Foundation of Hunan Province (11JJ4003), andthe Key Project of Scientific Research Conditions in Hunan Province (2012TT2040).
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  • Corresponding author: YANG Li; ZHOU Yichun
  • Received Date: 2012-01-16
  • Rev Recd Date: 2012-05-16
  • Publish Date: 2012-11-25
  • Thermal barrier coatings (TBCs) with high temperature durability and excellent heat insulation can reduce the metal surface temperature, which results in a significant improvement in performance and high efficiency of gas turbine engines. TBCs have been developed as a key heat protection technique. During flight, TBCs are unavoidably impacted and then eroded by particles from combustion chambers or foreign objects. Erosion of TBCs has become a severe problem in service life and reliability. In this paper, recent developments have been reviewed, including the experimental results, numerical simulations, theoretical analyses, experimental simulations and relevant measurement methods. Finally, development trend in TBCs erosion research is discussed.

     

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