IT1063035B
(it)
*
|
1975-05-09 |
1985-02-11 |
Maschf Augsburg Nuernberg Ag |
Apparato per la realizzazione del procedimento per elevare il limite dinamico di potenza di turbine a vapore od a gas o di compressori
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JPS5338806A
(en)
*
|
1976-09-22 |
1978-04-10 |
Hitachi Ltd |
Seal device for nose part of movable vane
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US4390320A
(en)
*
|
1980-05-01 |
1983-06-28 |
General Electric Company |
Tip cap for a rotor blade and method of replacement
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US4526509A
(en)
*
|
1983-08-26 |
1985-07-02 |
General Electric Company |
Rub tolerant shroud
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FR2557208B1
(fr)
*
|
1983-12-21 |
1988-03-25 |
Snecma |
Moyen de liaison entre deux elements cylindriques coaxiaux, notamment fixation d'un joint labyrinthe sur l'arbre d'une turbomachine
|
JPS6123804A
(ja)
*
|
1984-07-10 |
1986-02-01 |
Hitachi Ltd |
タ−ビン段落構造
|
DE3505491A1
(de)
*
|
1985-02-16 |
1986-08-21 |
MTU Motoren- und Turbinen-Union München GmbH, 8000 München |
Dichtung fuer eine stroemungsmaschine
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US5639095A
(en)
*
|
1988-01-04 |
1997-06-17 |
Twentieth Technology |
Low-leakage and low-instability labyrinth seal
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US5244216A
(en)
*
|
1988-01-04 |
1993-09-14 |
The Texas A & M University System |
Labyrinth seal
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GB8925421D0
(en)
*
|
1989-11-10 |
1989-12-28 |
Boc Group Plc |
Shaft sealing arrangements
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US5037114A
(en)
*
|
1990-01-26 |
1991-08-06 |
Westinghouse Electric Corp. |
Labyrinth seal for steam turbines
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US5049032A
(en)
*
|
1990-04-30 |
1991-09-17 |
Brandon Ronald E |
Particulate seal for elastic fluid turbines
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GB2250789B
(en)
*
|
1990-12-12 |
1994-03-30 |
Rolls Royce Plc |
Brush seal arrangement
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US5632598A
(en)
*
|
1995-01-17 |
1997-05-27 |
Dresser-Rand |
Shrouded axial flow turbo machine utilizing multiple labrinth seals
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US5599026A
(en)
*
|
1995-09-06 |
1997-02-04 |
Innovative Technology, L.L.C. |
Turbine seal with sealing strip and rubbing strip
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US5735667A
(en)
*
|
1996-05-06 |
1998-04-07 |
Innovative Technology, L.L.C. |
Method and apparatus for minimizing leakage in turbine seals
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DE19619722A1
(de)
*
|
1996-05-15 |
1997-11-20 |
Siemens Ag |
Dichtungsanordnung und Turbinenschaufel, insbesondere für eine Dampfturbine
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US5910094A
(en)
*
|
1996-09-10 |
1999-06-08 |
The Boeing Company |
Aircraft labyrinth fire seal
|
US5771681A
(en)
*
|
1996-09-17 |
1998-06-30 |
The Boeing Company |
Aircraft turbofan engine mixing apparatus
|
US5779150A
(en)
*
|
1996-10-01 |
1998-07-14 |
The Boeing Company |
Aircraft engine ejector nozzle
|
US5794434A
(en)
*
|
1996-10-09 |
1998-08-18 |
The Boeing Company |
Aircraft thrust reverser system with linearly translating inner and outer doors
|
US5941065A
(en)
*
|
1996-11-04 |
1999-08-24 |
The Boeing Company |
Stowable mixer ejection nozzle
|
US5884843A
(en)
*
|
1996-11-04 |
1999-03-23 |
The Boeing Company |
Engine noise suppression ejector nozzle
|
US5908159A
(en)
*
|
1997-02-24 |
1999-06-01 |
The Boeing Company |
Aircraft chute ejector nozzle
|
US5826794A
(en)
*
|
1997-02-28 |
1998-10-27 |
The Boeing Company |
Aircraft scoop ejector nozzle
|
DE59710621D1
(de)
*
|
1997-09-19 |
2003-09-25 |
Alstom Switzerland Ltd |
Vorrichtung zur Spaltdichtung
|
EP0943849A1
(de)
*
|
1998-03-19 |
1999-09-22 |
Asea Brown Boveri AG |
Berührungsfreie Dichtung für Strömungsmaschinen
|
JP2003214113A
(ja)
*
|
2002-01-28 |
2003-07-30 |
Toshiba Corp |
地熱タービン
|
US6679681B2
(en)
*
|
2002-04-10 |
2004-01-20 |
General Electric Company |
Flush tenon cover for steam turbine blades with advanced sealing
|
US7059821B2
(en)
*
|
2003-05-07 |
2006-06-13 |
General Electric Company |
Method and apparatus to facilitate sealing within turbines
|
US7540709B1
(en)
|
2005-10-20 |
2009-06-02 |
Florida Turbine Technologies, Inc. |
Box rim cavity for a gas turbine engine
|
US7445213B1
(en)
|
2006-06-14 |
2008-11-04 |
Florida Turbine Technologies, Inc. |
Stepped labyrinth seal
|
US8181967B2
(en)
*
|
2006-06-27 |
2012-05-22 |
General Electric Company |
Variable clearance packing ring
|
US8333557B2
(en)
*
|
2009-10-14 |
2012-12-18 |
General Electric Company |
Vortex chambers for clearance flow control
|
US20110156359A1
(en)
*
|
2009-12-31 |
2011-06-30 |
General Electric Company |
Turbine engine seals
|
JP5558138B2
(ja)
*
|
2010-02-25 |
2014-07-23 |
三菱重工業株式会社 |
タービン
|
GB201013003D0
(en)
|
2010-08-03 |
2010-09-15 |
Rolls Royce Plc |
A seal assembly
|
GB201013004D0
(en)
*
|
2010-08-03 |
2010-09-15 |
Rolls Royce Plc |
A seal assembly
|
JP5517910B2
(ja)
*
|
2010-12-22 |
2014-06-11 |
三菱重工業株式会社 |
タービン、及びシール構造
|
ITTO20110448A1
(it)
*
|
2011-05-19 |
2012-11-20 |
Avio Spa |
Tenuta a labirinto, particolarmente per turbine a gas di motori aeronautici
|
JP5518022B2
(ja)
*
|
2011-09-20 |
2014-06-11 |
三菱重工業株式会社 |
タービン
|
US8807927B2
(en)
*
|
2011-09-29 |
2014-08-19 |
General Electric Company |
Clearance flow control assembly having rail member
|
EP2878771B1
(en)
*
|
2012-07-11 |
2017-10-11 |
Mitsubishi Hitachi Power Systems, Ltd. |
Axial flow fluid machine
|
JP5917329B2
(ja)
*
|
2012-08-02 |
2016-05-11 |
株式会社東芝 |
蒸気タービンのシール構造
|
US20140054863A1
(en)
*
|
2012-08-21 |
2014-02-27 |
General Electric Company |
Seal assembly for a turbine system
|
US10428670B2
(en)
*
|
2016-05-09 |
2019-10-01 |
United Technologies Corporation |
Ingestion seal
|
FR3069276B1
(fr)
*
|
2017-07-18 |
2019-08-02 |
Safran Aircraft Engines |
Ensemble d'etancheite pour turbomachine
|