A PHILOSOPHY FOR THERMAL BARRIER COATING DESIGN AND ITS CORROBORATION BY 10000-H SERVICE EXPERIENCE ON RB211 NOZZLE GUIDE VANES

被引：34

作者：

BENNETT, A ^{[1
]}

TORIZ, FC ^{[1
]}

THAKKER, AB ^{[1
]}

机构：

[1] ROLLS ROYCE INC,ATLANTA,GA 30349

来源：

关键词：

AERO GAS TURBINE ENGINES - JET ENGINE COMBUSTORS - NOZZLE GUIDE VANES - THERMAL BARRIER COATINGS;

D O I：

10.1016/0257-8972(87)90120-4

中图分类号：

TB3 [工程材料学];

学科分类号：

0805 ; 080502 ;

摘要：

引用

页码：359 / 375

页数：17

共 20 条

[1] BENNETT A, 1986, MATER SCI TECH SER, V2, P257, DOI 10.1179/026708386790123378
[2] BENNETT A, 1984, P BR CERAM SOC, V34, P207
[3] FAILURE DURING THERMAL CYCLING OF PLASMA-SPRAYED THERMAL BARRIER COATINGS
BERNDT, CC
HERMAN, H
[J]. THIN SOLID FILMS, 1983, 108 (04) : 427 - 437
[4] THERMAL SPRAYING OF CERAMICS.
Chagnon, P.
Fauchais, P.
[J]. Ceramics International, 1984, 10 (04) : 119 - 131
[5] CRAWLEY JD, 1984, NASA TP2286
[6] HANDSCHUH RF, 1985, 851219 AM I AER ASTR
[7] KNOTEK O, 1984, ASME84GT289 PAP
[8] LEVINE SR, 1978, 80TH ANN AM CER SOC
[9] LIEBERT CH, 1979, NASA TP1425
[10] LIEBERT CH, 1979, NASA TM79116