US3412979A
(en)
*
|
1965-12-10 |
1968-11-26 |
Rolls Royce |
Aerofoil-shaped blade for use in a fluid flow machine such as a turbine
|
GB1070480A
(en)
*
|
1966-02-01 |
1967-06-01 |
Rolls Royce |
Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine
|
US3963368A
(en)
*
|
1967-12-19 |
1976-06-15 |
General Motors Corporation |
Turbine cooling
|
US3574481A
(en)
*
|
1968-05-09 |
1971-04-13 |
James A Pyne Jr |
Variable area cooled airfoil construction for gas turbines
|
US3529903A
(en)
*
|
1968-11-29 |
1970-09-22 |
Westinghouse Electric Corp |
Nozzle blade structure
|
US3715170A
(en)
*
|
1970-12-11 |
1973-02-06 |
Gen Electric |
Cooled turbine blade
|
US3920947A
(en)
*
|
1972-01-27 |
1975-11-18 |
Chromalloy American Corp |
Turbine-nozzle manufacturing apparatus and method
|
US3802046A
(en)
*
|
1972-01-27 |
1974-04-09 |
Chromalloy American Corp |
Method of making or reconditioning a turbine-nozzle or the like assembly
|
US3858290A
(en)
*
|
1972-11-21 |
1975-01-07 |
Avco Corp |
Method of making inserts for cooled turbine blades
|
US4288201A
(en)
*
|
1979-09-14 |
1981-09-08 |
United Technologies Corporation |
Vane cooling structure
|
DE3629910A1
(de)
*
|
1986-09-03 |
1988-03-17 |
Mtu Muenchen Gmbh |
Metallisches hohlbauteil mit einem metallischen einsatz, insbesondere turbinenschaufel mit kuehleinsatz
|
FR2659689B1
(fr)
*
|
1990-03-14 |
1992-06-05 |
Snecma |
Circuit de refroidissement interne d'une aube directrice de turbine.
|
US5145315A
(en)
*
|
1991-09-27 |
1992-09-08 |
Westinghouse Electric Corp. |
Gas turbine vane cooling air insert
|
US5493855A
(en)
*
|
1992-12-17 |
1996-02-27 |
Alfred E. Tisch |
Turbine having suspended rotor blades
|
US5611662A
(en)
*
|
1995-08-01 |
1997-03-18 |
General Electric Co. |
Impingement cooling for turbine stator vane trailing edge
|
US6237344B1
(en)
|
1998-07-20 |
2001-05-29 |
General Electric Company |
Dimpled impingement baffle
|
US6193465B1
(en)
*
|
1998-09-28 |
2001-02-27 |
General Electric Company |
Trapped insert turbine airfoil
|
DE10004128B4
(de)
|
2000-01-31 |
2007-06-28 |
Alstom Technology Ltd. |
Luftgekühlte Turbinenschaufel
|
FR2872541B1
(fr)
*
|
2004-06-30 |
2006-11-10 |
Snecma Moteurs Sa |
Aube fixe de turbine a refroidissement ameliore
|
FR2877390B1
(fr)
*
|
2004-10-29 |
2010-09-03 |
Snecma Moteurs |
Secteur de distribution de turbine alimente en air de refroidissement
|
US20060099073A1
(en)
*
|
2004-11-05 |
2006-05-11 |
Toufik Djeridane |
Aspherical dimples for heat transfer surfaces and method
|
FR2899271B1
(fr)
*
|
2006-03-29 |
2008-05-30 |
Snecma Sa |
Ensemble d'une aube et d'une chemise de refroidissement, distributeur de turbomachine comportant l'ensemble, turbomachine, procede de montage et de reparation de l'ensemble
|
US7930891B1
(en)
*
|
2007-05-10 |
2011-04-26 |
Florida Turbine Technologies, Inc. |
Transition duct with integral guide vanes
|
FR2922597B1
(fr)
*
|
2007-10-19 |
2012-11-16 |
Snecma |
Aube refroidie de turbomachine
|
FR2928962B1
(fr)
*
|
2008-03-19 |
2013-10-18 |
Snecma |
Distributeur de turbine a pales creuses.
|
US8109724B2
(en)
*
|
2009-03-26 |
2012-02-07 |
United Technologies Corporation |
Recessed metering standoffs for airfoil baffle
|
US8449249B2
(en)
|
2010-04-09 |
2013-05-28 |
Williams International Co., L.L.C. |
Turbine nozzle apparatus and associated method of manufacture
|
JP2015527530A
(ja)
*
|
2012-08-20 |
2015-09-17 |
アルストム テクノロジー リミテッドALSTOM Technology Ltd |
回転機械用の内部冷却される翼
|
EP2949871B1
(en)
*
|
2014-05-07 |
2017-03-01 |
United Technologies Corporation |
Variable vane segment
|
US10781715B2
(en)
*
|
2015-12-21 |
2020-09-22 |
Raytheon Technologies Corporation |
Impingement cooling baffle
|
JP6651378B2
(ja)
|
2016-02-22 |
2020-02-19 |
三菱日立パワーシステムズ株式会社 |
インサート組品、翼、ガスタービン、および、翼の製造方法
|
EP3236009A1
(de)
|
2016-04-21 |
2017-10-25 |
Siemens Aktiengesellschaft |
Leitschaufel mit einem verbindungsrohr
|
US10450880B2
(en)
*
|
2016-08-04 |
2019-10-22 |
United Technologies Corporation |
Air metering baffle assembly
|
US10309242B2
(en)
*
|
2016-08-10 |
2019-06-04 |
General Electric Company |
Ceramic matrix composite component cooling
|
US10662783B2
(en)
*
|
2018-08-29 |
2020-05-26 |
United Technologies Corporation |
Variable heat transfer collector baffle
|
US11702941B2
(en)
*
|
2018-11-09 |
2023-07-18 |
Raytheon Technologies Corporation |
Airfoil with baffle having flange ring affixed to platform
|
US10711620B1
(en)
*
|
2019-01-14 |
2020-07-14 |
General Electric Company |
Insert system for an airfoil and method of installing same
|
US11371360B2
(en)
*
|
2019-06-05 |
2022-06-28 |
Raytheon Technologies Corporation |
Components for gas turbine engines
|
US11448075B2
(en)
*
|
2020-11-02 |
2022-09-20 |
Raytheon Technologies Corporation |
CMC vane arc segment with cantilevered spar
|
US11428166B2
(en)
*
|
2020-11-12 |
2022-08-30 |
Solar Turbines Incorporated |
Fin for internal cooling of vane wall
|
FR3116466B1
(fr)
*
|
2020-11-25 |
2022-11-25 |
Safran Ceram |
Préforme fibreuse d'un profil aérodynamique d'aube de turbomachine
|
US12234744B2
(en)
*
|
2022-06-17 |
2025-02-25 |
Rtx Corporation |
Flow guides for internal cooling of a CMC airfoil
|
GB202216827D0
(en)
*
|
2022-11-11 |
2022-12-28 |
Rolls Royce Plc |
A method of manufacturing a turbine component
|
US12281597B2
(en)
|
2023-08-21 |
2025-04-22 |
Rtx Corporation |
CMC vane with rotatable baffle design to accommodate re-stagger
|
US12326099B2
(en)
|
2023-08-21 |
2025-06-10 |
Rtx Corporation |
Bathtub seal integrated into CMC vane load path
|
US12025029B1
(en)
|
2023-08-21 |
2024-07-02 |
Rtx Corporation |
Bathtub seal for damping CMC vane platform
|