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1974-11-11 |
1978-08-02 |
Rolls Royce |
Gas turbine engine
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1975-07-16 |
1979-08-15 |
Rolls Royce |
Laminated materials
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1975-10-14 |
1977-03-15 |
United Technologies Corporation |
Turbomachinery vane or blade with cooled platforms
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1975-10-14 |
1977-04-21 |
United Technologies Corp |
Schaufel mit gekuehlter plattform fuer eine stroemungsmaschine
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1975-10-14 |
1977-04-12 |
United Technologies Corporation |
Turbomachinery vane or blade with cooled platforms
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1976-07-29 |
1982-10-12 |
General Electric Company |
Fluid-cooled element
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1976-08-11 |
1978-10-03 |
United Technologies Corporation |
Coolable wall
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1976-11-22 |
1978-05-02 |
General Electric Company |
Ceramic turbine shroud assembly
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1978-04-20 |
1980-07-29 |
General Electric Company |
Structural cooling air manifold for a gas turbine engine
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1978-04-20 |
1980-02-05 |
General Electric Company |
Turbine band cooling system
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1978-09-27 |
1980-04-25 |
Snecma |
Perfectionnements aux joints a labyrinthe
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1979-02-09 |
1981-07-28 |
Avco Corporation |
Air-cooled turbine rotor shroud with restraints
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1982-03-17 |
1984-07-17 |
A/S Kongsberg Vapenfabrikk |
Heat shield for radial gas turbine
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1985-06-05 |
Rolls Royce |
Shroud assembly for a gas turbine engine
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1987-02-17 |
United Technologies Corporation |
Stator structure for supporting an outer air seal in a gas turbine engine
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1985-11-19 |
United Technologies Corporation |
Stator structure for a gas turbine engine
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MTU Motoren- und Turbinen-Union München GmbH, 8000 München |
Verfahren und mittel zur vermeidung der entstehung von titanfeuer
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1984-03-03 |
1985-09-05 |
MTU Motoren- und Turbinen-Union München GmbH, 8000 München |
Einrichtung zur verhinderung der ausbreitung von titanfeuer bei turbomaschinen, insbesondere gasturbinen- bzw. gasturbinenstrahltriebwerken
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1991-03-05 |
Minnesota Mining And Manufacturing Company |
Heat exchanger
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1993-03-30 |
General Electric Company |
Nozzle band overhang cooling
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1991-02-22 |
1992-09-01 |
Solar Turbines, Incorporated |
Turbine cooling system
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1991-05-20 |
1992-11-24 |
General Electric Company |
Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines
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1992-12-08 |
General Electric Company |
Shroud cooling assembly for gas turbine engine
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1993-08-03 |
General Electric Company |
Finned structural disk spacer arm
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General Electric Company |
Enhanced impingement cooled components
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1994-09-06 |
United Technologies Corporation |
Turbine vane having dedicated inner platform cooling
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1997-07-22 |
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United Technologies Corporation |
Turbine vane with a platform cavity having a double feed for cooling fluid
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1994-10-31 |
1996-12-17 |
General Electric Company |
Cooled shroud
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1994-11-10 |
2000-08-03 |
Siemens Westinghouse Power Corp., Orlando |
Gasturbinenschaufel mit einer gekühlten plattform
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2000-02-01 |
Siemens Westinghouse Power Corporation |
Combustion turbine modular cooling panel
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General Electric Company |
Method and apparatus for increasing heat transfer from combustors
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2002-07-30 |
General Electric Company |
Salvaged castings and methods of salvaging castings with defective cast cooling bumps
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2002-11-12 |
General Electric Company |
Bucket platform cooling scheme and related method
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2001-09-05 |
Siemens Ag |
Coolable segment for a turbomachinery and combustion turbine
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2004-08-06 |
Snecma Moteurs |
Plate-forme d'aube de distributeur pour moteur a turbine a gaz
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2007-06-26 |
Pratt & Whitney Canada Corp |
Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine
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2004-06-15 |
2006-01-05 |
Rolls-Royce Deutschland Ltd & Co Kg |
Plattformkühlanordnung für den Leitschaufelkranz einer Gasturbine
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2004-07-09 |
2006-01-11 |
Siemens Aktiengesellschaft |
Roue de turbine comprenant des aubes de turbine avec turbulateurs sur la surface radiale interne de la plate-forme
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2006-03-23 |
Alstom Technology Ltd |
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Turbine airfoil platform cooling circuit
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General Electric Company |
Turbine bucket tip cap
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2007-07-12 |
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Tilted turbine vane with impingement cooling
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Turbine airfoil with integral chordal support ribs
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Heat transfer system and method for turbine engine using heat pipes
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Turbine vane with endwall cooling
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Passage obstruction for improved inlet coolant filling
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Gekühltes bauelement für eine gasturbine.
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An impingement cooling arrangement for a gas turbine engine
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Sealing for vane segments
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General Electric Company |
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Hot gas path component
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Turbine endwall with grooved recess cavity
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Combustor panel with increased durability
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Hot gas path component with impingement and pedestal cooling
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Industrial gas turbine exhaust system diffuser inlet lip
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Turbine endwall with micro-circuit cooling
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Turbine engine blade outer air seal with load-transmitting cover plate
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Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse
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Endwall cooling system
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Turbine engine airfoil assembly
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2023-11-14 |
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Internally cooled turbine tip shroud component
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2022-12-27 |
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Endwall cooling scheme
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Endwall directional cooling
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Stator plenum with collet seal
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