GB1423833A
(en)
*
|
1972-04-20 |
1976-02-04 |
Rolls Royce |
Rotor blades for fluid flow machines
|
US3810711A
(en)
*
|
1972-09-22 |
1974-05-14 |
Gen Motors Corp |
Cooled turbine blade and its manufacture
|
US3864199A
(en)
*
|
1973-07-26 |
1975-02-04 |
Gen Motors Corp |
Angular discharge porous sheet
|
JPS50121494U
(fr)
*
|
1974-03-20 |
1975-10-03 |
|
|
US4022542A
(en)
*
|
1974-10-23 |
1977-05-10 |
Teledyne Industries, Inc. |
Turbine blade
|
GB1530594A
(en)
*
|
1974-12-13 |
1978-11-01 |
Rolls Royce |
Perforate laminated material
|
US4004056A
(en)
*
|
1975-07-24 |
1977-01-18 |
General Motors Corporation |
Porous laminated sheet
|
GB2049152B
(en)
*
|
1979-05-01 |
1983-05-18 |
Rolls Royce |
Perforate laminated material
|
US4407632A
(en)
*
|
1981-06-26 |
1983-10-04 |
United Technologies Corporation |
Airfoil pedestaled trailing edge region cooling configuration
|
US4529358A
(en)
*
|
1984-02-15 |
1985-07-16 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Vortex generating flow passage design for increased film cooling effectiveness
|
FR2725474B1
(fr)
*
|
1984-03-14 |
1996-12-13 |
Snecma |
Aube de distributeur de turbine refroidie
|
US4587700A
(en)
*
|
1984-06-08 |
1986-05-13 |
The Garrett Corporation |
Method for manufacturing a dual alloy cooled turbine wheel
|
JPS6159274U
(fr)
*
|
1984-09-21 |
1986-04-21 |
|
|
FR2608674B1
(fr)
*
|
1986-12-17 |
1991-04-19 |
Snecma |
Roue de turbine a aubes ceramique
|
JPH0366585A
(ja)
*
|
1989-08-02 |
1991-03-22 |
Fujitsu Ltd |
関節型ロボット
|
US5295530A
(en)
|
1992-02-18 |
1994-03-22 |
General Motors Corporation |
Single-cast, high-temperature, thin wall structures and methods of making the same
|
US5810552A
(en)
*
|
1992-02-18 |
1998-09-22 |
Allison Engine Company, Inc. |
Single-cast, high-temperature, thin wall structures having a high thermal conductivity member connecting the walls and methods of making the same
|
DE4430302A1
(de)
*
|
1994-08-26 |
1996-02-29 |
Abb Management Ag |
Prallgekühltes Wandteil
|
US6193465B1
(en)
*
|
1998-09-28 |
2001-02-27 |
General Electric Company |
Trapped insert turbine airfoil
|
US6932570B2
(en)
*
|
2002-05-23 |
2005-08-23 |
General Electric Company |
Methods and apparatus for extending gas turbine engine airfoils useful life
|
US7464554B2
(en)
*
|
2004-09-09 |
2008-12-16 |
United Technologies Corporation |
Gas turbine combustor heat shield panel or exhaust panel including a cooling device
|
GB2439330B
(en)
|
2006-06-22 |
2008-09-17 |
Rolls Royce Plc |
Aerofoil
|
US7850497B2
(en)
*
|
2008-09-03 |
2010-12-14 |
Alan H. I. Kang |
Method and system for providing and using a power paddle
|
US8510925B2
(en)
|
2008-09-04 |
2013-08-20 |
Rolls-Royce Corporation |
System and method for sealing vacuum in hollow fan blades
|
US9334741B2
(en)
*
|
2010-04-22 |
2016-05-10 |
Siemens Energy, Inc. |
Discreetly defined porous wall structure for transpirational cooling
|
US8651805B2
(en)
*
|
2010-04-22 |
2014-02-18 |
General Electric Company |
Hot gas path component cooling system
|
US8894363B2
(en)
|
2011-02-09 |
2014-11-25 |
Siemens Energy, Inc. |
Cooling module design and method for cooling components of a gas turbine system
|
US20120067054A1
(en)
|
2010-09-21 |
2012-03-22 |
Palmer Labs, Llc |
High efficiency power production methods, assemblies, and systems
|
GB201016335D0
(en)
*
|
2010-09-29 |
2010-11-10 |
Rolls Royce Plc |
Endwall component for a turbine stage of a gas turbine engine
|
EP2778345A1
(fr)
*
|
2013-03-15 |
2014-09-17 |
Siemens Aktiengesellschaft |
Feuilles composites de refroidissement pour turbine à gaz
|
US9476306B2
(en)
*
|
2013-11-26 |
2016-10-25 |
General Electric Company |
Components with multi-layered cooling features and methods of manufacture
|
US10934853B2
(en)
*
|
2014-07-03 |
2021-03-02 |
Rolls-Royce Corporation |
Damage tolerant cooling of high temperature mechanical system component including a coating
|
RU2568600C1
(ru)
*
|
2014-09-24 |
2015-11-20 |
Акционерное общество "Инжиниринговая компания "АЭМ-технологии" (АО "АЭМ-технологии") |
Охлаждаемая лопатка газотурбинного двигателя
|
US10458251B2
(en)
*
|
2016-04-15 |
2019-10-29 |
General Electric Company |
Airfoil cooling using non-line of sight holes
|
CN114718657A
(zh)
*
|
2022-04-08 |
2022-07-08 |
中国航发沈阳发动机研究所 |
一种涡轮叶片叶背局部高效冷却结构
|