JPS5145728B2
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1972-08-21 |
1976-12-04 |
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GB1504129A
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1974-06-29 |
1978-03-15 |
Rolls Royce |
Matching differential thermal expansions of components in heat engines
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1974-11-27 |
1976-11-02 |
General Electric Company |
Labyrinth seal system
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1975-10-01 |
1978-08-01 |
United Technologies Corporation |
Rotary seal with pressurized air directed at fluid approaching the seal
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FR2437544A1
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1978-09-27 |
1980-04-25 |
Snecma |
Perfectionnements aux joints a labyrinthe
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GB2118629B
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1982-04-21 |
1985-07-17 |
Rolls Royce |
Device for passing a fluid flow eg. cooling air through a barrier eg. bolted joint
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1983-03-30 |
1985-09-17 |
United Technologies Corporation |
Clearance control in turbine seals
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1983-04-13 |
1985-12-10 |
Dresser Industries, Inc. |
Control of steam turbine shaft thrust loads
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1984-04-27 |
1985-04-30 |
General Electric Company |
Thermally responsive labyrinth seal
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FR2570763B1
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1984-09-27 |
1986-11-28 |
Snecma |
Dispositif de controle automatique du jeu d'un joint a labyrinthe de turbomachine
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1984-10-11 |
1988-04-26 |
United Technologies Corporation |
Cooling scheme for combustor vane interface
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1986-01-17 |
1988-05-31 |
United Technologies Corporation |
Transition duct seal
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1986-12-31 |
1988-03-15 |
General Electric Company |
Thrust bearing loading arrangement for gas turbine engines
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1987-07-02 |
1989-04-18 |
United Technologies Corporation |
Sealing and cooling arrangement for combustor vane interface
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1989-01-09 |
1990-02-20 |
General Motors Corporation |
Rotor for gas turbine engine
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1990-07-30 |
1992-08-04 |
General Electric Company |
Aft entry cooling system and method for an aircraft engine
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1991-08-28 |
1993-07-06 |
General Electric Company |
Labyrinth seal with recirculating means for reducing or eliminating parasitic leakage through the seal
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GB2263946A
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1992-02-04 |
1993-08-11 |
Bmw Rolls Royce Gmbh |
An arrangement for supplying cooling air to a gas turbine casing.
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1992-05-14 |
2002-10-15 |
William Miller Farrell |
Intercooled gas turbine engine
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1993-11-17 |
1995-09-19 |
Alliedsignal, Inc. |
Gas turbine engine rear magnetic or foil bearing cooling using exhaust eductor
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1994-06-16 |
1995-12-21 |
Abb Management Ag |
Wellendichtung einer thermischen Turbomaschine
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1995-11-22 |
1998-07-07 |
General Electric Company |
Variable size gas turbine engine
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2000-12-08 |
2002-11-05 |
General Electric Company |
Variable stator vane bushing
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JP4773810B2
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2005-11-28 |
2011-09-14 |
三菱重工業株式会社 |
ガスタービン
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2007-09-18 |
2009-03-19 |
Honeywell International, Inc. |
Notched tooth labyrinth seals and methods of manufacture
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2009-05-01 |
2014-02-12 |
株式会社日立製作所 |
シール構造とその制御方法
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2010-02-10 |
2014-04-09 |
Rolls Royce Plc |
A seal arrangement
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2010-03-31 |
2016-05-24 |
United Technologies Corporation |
Turbine blade tip clearance control
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2016-02-24 |
2017-08-24 |
General Electric Company |
Turbine engine ejector throat control
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2016-05-31 |
2019-07-09 |
Rolls-Royce Corporation |
Labyrinth seal with lubricant directing projection
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2016-10-20 |
2020-08-04 |
General Electric Company |
Overhanging seal assembly for a gas turbine
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2020-05-20 |
2021-11-30 |
中国核动力研究设计院 |
一种超临界二氧化碳透平干气密封失效保护装置及方法
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