发明名称 AIR SEAL FOR GAS TURBINE ENGINE, SEAL SYSTEM, AND METHOD FOR FORMING AIR SEAL FOR GAS TURBINE ENGINE
摘要 PROBLEM TO BE SOLVED: To provide a seal having no fear of firing occurring in a state to peel quantities of seal materials from a seal. SOLUTION: A seal is provided with a seal base 30 and a thermally sprayed metal adhesion layer 36. The metal adhesion layer 36 is formed at least at a part of the seal base 30. The metal adhesion layer 36 contains preferably thermally sprayed nickel and aluminum, and up to 1 wt.% of each of iron, copper, zinc, manganese, and magnesium. The seal layer further has a wear layer 38 and the seal layer is applied on the metal adhesion layer 36. The seal layer is that aluminum powder and silicon powder, forming a metallic substrate, are thermally sprayed on the seal layer, and a polymer buried in the substrate, for example, filler particles of methyl methacrylate, buried in the substrate, is accumulated simultaneously therewith. Firing ability in a state that an extremely large quantity of seal materials are peeled from a seal is lowered by filler particle.
申请公布号 JP2000186574(A) 申请公布日期 2000.07.04
申请号 JP19990360514 申请日期 1999.12.20
申请人 UNITED TECHNOL CORP <UTC> 发明人 WALDEN FREDERICK CLELL;CRAWFORD GEORGE LEE;DALZELL WILLIAM JOHN JR
分类号 F02C7/28;C23C4/04;C23C4/18;F01D5/28;F01D11/12;F16J15/40;(IPC1-7):F02C7/28 主分类号 F02C7/28
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