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公开(公告)号:US3918925A
公开(公告)日:1975-11-11
申请号:US46927074
申请日:1974-05-13
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C
CPC classification number: F01D11/122 , B22F7/02 , C09K3/1028 , C09K2200/0213 , C09K2200/0239 , C09K2200/0243 , C09K2200/0278 , C23C28/321 , C23C28/345 , C23C28/3455 , C23C28/347 , Y10S277/94 , Y10S277/941 , Y10S428/926 , Y10T428/12042 , Y10T428/12049 , Y10T428/1234 , Y10T428/12472 , Y10T428/12764
Abstract: An abradable seal for use between relatively rotatable members in elevated temperature operating apparatus comprising a nickel aluminide coating approximately 0.005-0.010 inch thick bonded to one of said members, a voidless, inorganic water insoluble spinel compound layer approximately 0.005-0.05 inch thick bonded to the nickel aluminide coating consisting essentially of the air cured reaction product of, by weight, 20-40% sodium silicate, 55-75% aluminum and 2-8% zinc oxide, and an abradable material bonded to the inorganic coating selected from the group consisting of sintered metallic fiber, sintered metallic powder and metallic honeycomb.
Abstract translation: 一种用于在高温操作装置中的可相对旋转的构件之间使用的耐磨密封件,其包括约0.005-0.010英寸厚的镍铝化物涂层,其结合到所述构件中的一个构件上,大约0.005-0.05英寸厚的无孔水无定形尖晶石化合物层, 主要由空气固化的反应产物,重量比为20-40%的硅酸钠,55-75%的铝和2-8%的氧化锌组成的镍铝化物涂层,以及与无机涂层结合的可磨损材料,所述无机涂层选自 烧结金属纤维,烧结金属粉末和金属蜂窝。
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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:AU642928B2
公开(公告)日:1993-11-04
申请号:AU6697290
申请日:1990-11-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W JR , 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:AU6697290A
公开(公告)日:1991-05-30
申请号:AU6697290
申请日:1990-11-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W JR , 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:CA1161314A
公开(公告)日:1984-01-31
申请号:CA348289
申请日:1980-03-24
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SOKOL LARRY S , MCCOMAS CHARLES C , HANNA EARL M
Abstract: PLASMA SPRAY METHOD AND APPARATUS A plasma spray method capable of directing plasticized powders against a substrate for deposition of a protective coating thereon is disclosed. Various structural details of the apparatus described enable the attainment of high particle velocities without melting the particles. The technical concepts employed are directed to normalizing the temperature of the plasma stream at a reduced value prior to the injection of coating particles. A general reduction in temperature and substantial elimination of a thermal spike at the core of the stream are achieved. Coating particles are injected into the plasma stream only after the plasma is first cooled and then accelerated. In detailed embodiments, a nozzle extension assembly having a plasma cooling zone, a plasma acceleration zone, a powder injection zone and a plasma/powder discharge zone is affixed to the downstream end of a conventional plasma generator. F-4451
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公开(公告)号:IE68059B1
公开(公告)日:1996-05-15
申请号:IE426890
申请日:1990-11-27
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W JR , 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:NO905116L
公开(公告)日:1991-05-28
申请号:NO905116
申请日:1990-11-27
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C , APPLEBY JOHN W JR , 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:EG19442A
公开(公告)日:1995-03-30
申请号:EG3391
申请日:1991-01-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MCCOMAS CHARLES C
IPC: B08B9/08
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公开(公告)号:MX172981B
公开(公告)日:1994-01-26
申请号:MX2350590
申请日:1990-11-27
Applicant: UNITED TECHNOLOGIES CORP
Inventor: BARRINGER HERBERT R , PATRY MICHAEL J , MCCOMAS CHARLES C , APPLEBY JOHN W JR , SILEO GERARD A
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: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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