Metal-glass based composites for application in TBC-Systems

被引:23
作者
Mack, D. E.
Gross, S. -M.
Vassen, R.
Stoever, D.
机构
[1] Forschungszentrum Julich GmbH, Inst Energy Res, Julich, Germany
[2] Forschungszentrum Julich GmbH, Cent Dept Technol, ZAT, Julich, Germany
关键词
coatings for engine components; coatings for gas turbine components; composite materials; heat treatment of coatings; high temperature oxidation; TBC topcoats;
D O I
10.1361/105996306X146983
中图分类号
TB3 [工程材料学];
学科分类号
0805 [材料科学与工程]; 080502 [材料学];
摘要
A new type of thermal barrier coating (TBC) based on metal-glass composite (MGC) consisting of an ordinary container glass and a NiCoCrAIY-alloy has been recently presented. This TBC material provides the possibility to easily adjust its thermal expansion coefficient to match the substrate by changing the metal to glass ratio of the composite. Vacuum plasma spraying (VPS) has been applied as a possible technologies for deposition of MGC coatings. Isothermal oxidation tests were carried out in air at temperatures of 950, 1000, and 1050 degrees C, respectively. Thermal cycling tests were carried out by applying a temperature gradient across the sample thickness by heating with an open flame of natural gas followed by removal of the burner and air cooling. Changes in the microstructure were examined by means of microscopy, microanalysis, and x-ray powder diffraction. For long-time annealing at high temperatures, a progressive degradation of the glass matrix as well as oxidation of the metal phases cannot be fully suppressed up to now. By lowering the effective temperature at the MGC layer when used as an intermediate layer, the degradation of the MGC can be reduced without losing its advanced features with respect to creeping and gas-tightness. Additional concepts for improved oxidation resistance of the MGC based on suitable heat treatments and on alternative glass compositions have been developed, and primary results are shown. Evaluation of results from isothermal oxidation experiments and from thermal cycling in burner-rig facilities validates a clear improvement of the lifetime of the coatings compared with earlier results.
引用
收藏
页码:652 / 656
页数:5
相关论文
共 13 条
[1]
Thermal barrier coatings for aircraft turbine airfoils :: thermal challenge and materials [J].
Arnault, V ;
Mévrel, R ;
Alpérine, S ;
Jaslier, Y .
REVUE DE METALLURGIE-CAHIERS D INFORMATIONS TECHNIQUES, 1999, 96 (05) :585-597
[2]
Dietrich M., 2002, Ceramic Engineering and Science Proceedings, V23, P449
[3]
Dietrich M, 2001, MATERIALWISS WERKST, V32, P669
[4]
PREPARATION, PROPERTIES AND CHEMISTRY OF GLASS-CERAMIC-TO-METAL AND GLASS-CERAMIC-TO-METAL SEALS AND COATINGS [J].
DONALD, IW .
JOURNAL OF MATERIALS SCIENCE, 1993, 28 (11) :2841-2886
[5]
Mechanisms controlling the durability of thermal barrier coatings [J].
Evans, AG ;
Mumm, DR ;
Hutchinson, JW ;
Meier, GH ;
Pettit, FS .
PROGRESS IN MATERIALS SCIENCE, 2001, 46 (05) :505-553
[6]
Gross SM, 2005, CERAM ENG SCI PROC, V26, P239
[7]
Miller R.A., 1982, ADV CERAM, P241, DOI DOI 10.1098/RSPA.2007.1829
[8]
OXIDATION-BASED MODEL FOR THERMAL BARRIER COATING LIFE [J].
MILLER, RA .
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 1984, 67 (08) :517-521
[9]
STECURA S, 1986, ADV CERAM MATER, V1, P68
[10]
New material concepts for the next generation of plasma-sprayed thermal barrier coatings [J].
Stöver, D ;
Pracht, G ;
Lehmann, H ;
Dietrich, M ;
Döring, JE ;
Vassen, R .
JOURNAL OF THERMAL SPRAY TECHNOLOGY, 2004, 13 (01) :76-83