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公开(公告)号:PT96011A
公开(公告)日:1991-09-13
申请号:PT9601190
申请日:1990-11-27
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W , SILEO GERARD A , BARRINGER HERBERT R , PATRY MICHAEL J
Abstract: Gas turbine engine coatings must often be removed during engine maintenance and repair. The techniques utilized to accomplish this task, machining, chemical stripping, machining followed by chemical stripping, or grit blasting, frequently result in component damage or destruction. Liquid jet erosion can be utilized to remove seals, coatings, or portions thereof without damaging the engine hardware.
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公开(公告)号:DE69407811T2
公开(公告)日:1998-04-23
申请号:DE69407811
申请日:1994-10-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SILEO GERARD A , APPLEBY JOHN W , NARSAVAGE STEPHEN T , ALENT FRANCIS X , DAVIS CHARLES G
Abstract: A gas turbine abradable seal is prepared by plasma spraying an oxidation resistant metallic material and boron nitride. The resultant structure comprises a metallic matrix encompassing a lubricating amount of boron nitride, with porosity of less than about 15 percent and a fabricated surface roughness of less than about 600 microinches. The reduced surface roughness and substantially reduced permeability of this seal provide substantially enhanced engine efficiency, and improved durability.
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公开(公告)号:DE60236393D1
公开(公告)日:2010-07-01
申请号:DE60236393
申请日:2002-03-14
Applicant: UNITED TECHNOLOGIES CORP
Inventor: ALLEN WILLIAM P , VERONESI WILLIAM A , APPLEBY JOHN W , HALL ROBERT J , MALONEY MICHAEL J , HAGUE DOUGLAS C , KHAN ABDUS
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公开(公告)号:DE69407811D1
公开(公告)日:1998-02-12
申请号:DE69407811
申请日:1994-10-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SILEO GERARD A , APPLEBY JOHN W , NARSAVAGE STEPHEN T , ALENT FRANCIS X , DAVIS CHARLES G
Abstract: A gas turbine abradable seal is prepared by plasma spraying an oxidation resistant metallic material and boron nitride. The resultant structure comprises a metallic matrix encompassing a lubricating amount of boron nitride, with porosity of less than about 15 percent and a fabricated surface roughness of less than about 600 microinches. The reduced surface roughness and substantially reduced permeability of this seal provide substantially enhanced engine efficiency, and improved durability.
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公开(公告)号:DE69020507D1
公开(公告)日:1995-08-03
申请号:DE69020507
申请日:1990-11-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W , SILEO GERARD A , BARRINGER HERBERT R , PATRY MICHAEL J
Abstract: Gas turbine engine coatings must often be removed during engine maintenance and repair. The techniques utilized to accomplish this task, machining, chemical stripping, machining followed by chemical stripping, or grit blasting, frequently result in component damage or destruction. Liquid jet erosion can be utilized to remove seals, coatings, or portions thereof without damaging the engine hardware.
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公开(公告)号:AT468425T
公开(公告)日:2010-06-15
申请号:AT02251839
申请日:2002-03-14
Applicant: UNITED TECHNOLOGIES CORP
Inventor: ALLEN WILLIAM P , VERONESI WILLIAM A , APPLEBY JOHN W , HALL ROBERT J , MALONEY MICHAEL J , HAGUE DOUGLAS C , KHAN ABDUS
Abstract: An article has a protective ceramic coating 26 which reduces radiation heat transport through the ceramic coating. The protective ceramic coating 26 includes one or more embedded reflective metallic layers 30', 30'', 30''' for reducing the radiation heat transport. The article may be a turbine component and the coating 26 may be a thermal barrier coating.
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公开(公告)号:DE69020507T2
公开(公告)日:1996-01-04
申请号:DE69020507
申请日:1990-11-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W , SILEO GERARD A , BARRINGER HERBERT R , PATRY MICHAEL J
Abstract: Gas turbine engine coatings must often be removed during engine maintenance and repair. The techniques utilized to accomplish this task, machining, chemical stripping, machining followed by chemical stripping, or grit blasting, frequently result in component damage or destruction. Liquid jet erosion can be utilized to remove seals, coatings, or portions thereof without damaging the engine hardware.
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