摘要

Aluminide coatings are applied on gas turbine components to improve oxidation and corrosion resistance or as bond coats for thermal barrier coatings (TBC). In the present study, coatings produced on a CMSX-4 superalloy by pack gas phase aluminising and subsequently annealed at 1050 degrees C for 2 h were investigated. Microstructure, morphology and phase composition of the coating were characterised using light microscopy, X-ray diffraction, scanning electron microscopy and analytical transmission electron microscopy (TEM). Scanning electron microscopy (SEM) investigations of the 39 mu m thick coating revealed a complex multilayered microstructure produced by diffusion at 1050 degrees C at the surface of CMSX-4 alloy. Detailed TEM phase analysis was performed on cross-section thin foils by electron diffraction and energy dispersive X-ray spectrometry (EDS). The outer zone (1) consisted of beta-NiAl phase. The interdifusion zone (2) contained two sublayers consisting of a Ni5Al3 matrix with precipitates of topologically close packed phases, most probably sigma and mu. Close to the surface of the CMSX-4 superalloy, a further zone (3) consisting of gamma+gamma ' with large precipitates (possibly mu and P phases) was observed.

  • 出版日期2008-9