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公开(公告)号:CA1152340A
公开(公告)日:1983-08-23
申请号:CA370319
申请日:1981-02-06
Applicant: UNITED TECHNOLOGIES CORP
Inventor: FAUCHER JOSEPH E , WRIGHT RICHARD R , PANE FRANCIS C JR , KWOKA DAVID
Abstract: Anti-Coke Fuel Nozzle Coke hereinbefore known to form in the secondary passage of a dual orifice fuel nozzle for the combustor of a turbine type power plant is prevented from forming by imposing increased air pressure in the secondary passage during its inoperative mode and when the primary fuel passage is in the operative mode, without relying on purging or requiring an external air source.
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公开(公告)号:CA1170843A
公开(公告)日:1984-07-17
申请号:CA390190
申请日:1981-11-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor: FAUCHER JOSEPH E , WRIGHT RICHARD R , PANE FRANCIS C JR , KWOKA DAVID , STRIEBEL EDMUND E
Abstract: Fuel Nozzle For Gas Turbine Engine A fuel nozzle designed to reduce pollutant emissions and minimize the buildup of coke in the secondary fuel passage of a dual orifice fuel nozzle for the combustor of a gas turbine engine sizes the orifices and passages of the air and fuel so as to increase the pressure in the secondary passage during its inoperative mode and when the primary fuel passage is in the operative mode and having the air and fuel issuing from both the primary and secondary orifices swirl in the same direction.
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公开(公告)号:CA1280611C
公开(公告)日:1991-02-26
申请号:CA560730
申请日:1988-03-07
Applicant: UNITED TECHNOLOGIES CORP
Inventor: WRIGHT RICHARD R , PANE FRANCIS C JR , MATTHEWS JOHN A , STRIEBEL EDMUND E
Abstract: Airblast Fuel Injector A fuel injector assembly for a gas turbine combustor projects a hollow conical spray of fuel. A plurality of discrete surrounding air nozzles 42 project air directly toward the axis 46 of the injector at an angle of 15 degrees, establishing a fuel rich external recirculation zone 52.
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公开(公告)号:CA1179155A
公开(公告)日:1984-12-11
申请号:CA390192
申请日:1981-11-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor: STRIEBEL EDMUND E , PANE FRANCIS C JR
Abstract: Fuel Nozzle With Water Injection For Gas Turbine Engines A pressure atomizing fuel nozzle of the type that has a primary and secondary fuel system for a gas turbine engine and includes air swirl means and water injection is designed so that the water laden airstream is swirling in the same direction as both the fuels egressing from the primary fuel system and the secondary fuel system.
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