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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: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:NO865100D0
公开(公告)日:1986-12-17
申请号:NO865100
申请日:1986-12-17
Applicant: UNITED TECHNOLOGIES CORP
Inventor: NARSAVAGE STEPHEN T , HECHT RALPH J
IPC: C23C20060101 , C23C
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