Details
Title
Equivalent Heat Load Test on Hot Aircraft Engine ComponentsJournal title
Archives of Foundry EngineeringYearbook
2023Volume
vol. 23Issue
No 1Authors
Affiliation
Mróz, M. : Rzeszow University of Technology, Al. Powstańców Warszawy 12, 35-959 Rzeszów, Poland ; Orłowicz, A.W. : Rzeszow University of Technology, Al. Powstańców Warszawy 12, 35-959 Rzeszów, Poland ; Tupaj, M. : Rzeszow University of Technology, Al. Powstańców Warszawy 12, 35-959 Rzeszów, Poland ; Lenik, M. : Rzeszow University of Technology, Al. Powstańców Warszawy 12, 35-959 Rzeszów, PolandKeywords
Heat load ; Heat barrier ; Aircraft enginesDivisions of PAS
Nauki TechniczneCoverage
34-36Publisher
The Katowice Branch of the Polish Academy of SciencesBibliography
[1] Hejwowski, T., Weroński, A. (2000). Manufacture of wear-resistant coatings. Lublin: Politechnika Lubelska. (in Polish).[2] Research stand in WSK PZL Rzeszów.
[3] Chaur, - Jeng Wang, & Jiaun, - Sheng Lin (2002). The oxidation of MAR M247 superalloy with Na2SO4 coating. Materials Chemistry and Physics. 76, 123-129. DOI: 10.1016/S0254-0584(01)00527-2.
[4] Goebel, J.A., Petit, F.S. & Howard, G.W. (1973). Mechanism for the hot corrosion of nickel base alloys. Metallurgical Transactions. 4, 261-270. https://doi.org/10.1007/BF02649626.
[5] Su, C.Y., Lih, W.C., Chou, C.P. & Tsai, H.C. (2001). Activated diffusion brased repair for IN 738 hot section components of gas turbine. Journal of Materials Processing Technology. 115(3), 326-332.