发明名称 |
Beschichtungssystem zum Zurückhalten geschmolzenen Materials bei Feuer in Gasturbinen |
摘要 |
In a gas turbine engine, a method and apparatus for containing molten materials and ignited titanium and titanium alloys within the confines of the turbine engine environment. The method includes the step of first applying a bond coating 52 to the inner surface 44 of the outer compressor casing 36. The bond coating 52 is then plasma oversprayed with a non-reactive thermally insulative ceramic top coating 54. The apparatus includes a substrate 48 having a bond coating and a ceramic top coating, surrounding at least a portion of the gas turbine engine, for containing turbine engine fires within the turbine engine environment. Preferably, the bond coating 52 is a Ni-Co-Cr-Al-Y alloy, and the top coat 54 is stabilized zirconia. <IMAGE>
|
申请公布号 |
DE19505303(A1) |
申请公布日期 |
1995.08.17 |
申请号 |
DE1995105303 |
申请日期 |
1995.02.16 |
申请人 |
UNITED TECHNOLOGIES CORP. (N.D.GES.D.STAATES DELAWARE), EAST HARTFORD, US |
发明人 |
FRELING, MELVIN, WEST HARTFORD, CONN., US;GUPTA, DINESH K., SOUTH WINDSOR, CONN., US |
分类号 |
F02C7/00;B64C1/40;C23C4/02;F01D21/04;F02C7/24;F02C7/25;(IPC1-7):F02C7/24;C23C4/04;F16L59/02 |
主分类号 |
F02C7/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|