Environmental resistance of ceramic matrix composite materials for gas turbine applications

Key Engineering Materials

Volumn , Issue 136 PART 3, 1997, Pages 1637-1640

  De Gaudenzi, G P ^a   Taut, C ^b   Ifflander K ^c   Corcoruto, S ^c  

^a CISE SpA   (Italy)

^b SIEMENS AG   (Germany)

^c ANSALDO ENERGIA   (Italy)

Author keywords

Ceramic matrix composites; Gas turbine; High pressure high temperature corrosion; Oxidation; Thermal cycling; Thermal shock

Indexed keywords

ALUMINA; CERAMIC COATINGS; CORROSION; GAS TURBINES; HIGH TEMPERATURE EFFECTS; OXIDATION; SCANNING ELECTRON MICROSCOPY; SILICA; SILICON CARBIDE; THERMAL CYCLING;

HIGH PRESSURE CORROSION; HIGH TEMPERATURE CORROSION; THERMAL SHOCK;

CERAMIC MATRIX COMPOSITES;

EID: 4243452695     PISSN: 10139826     EISSN: 16629795     Source Type: Book Series    
DOI: None     Document Type: Article

References (6)

1. K.L. Luthra, J. Am. Ceram. Soc., 71, 12 (1988), p. 1114
2. M. Maeda et al., J. Am. Ceram. Soc., 72, 3 (1989), p. 512
3. J. Sawyer et al., J. Eng. Gas Turb. Power, Trans. ASME, 113, 10 (1991), p. 602
4. Y.J. Stockmann et al., Key Eng. Mats., 113 (1996), p. 113
5. F.E. Heredia, A.G. Evans, C.A. Andersson, J. Am. Ceram. Soc., 78, 10 (1995), p. 2790
6. H. Hald, Proc. 2nd Eur. Workshop High Temp. Behaviour of Advanced Materials, Béziers, France (1993), p. 15