|
DE2121711A1
(en)
|
1970-07-31 |
1972-02-03 |
Thaelmann Schwermaschbau Veb |
Wire press automatic cut out
|
|
JPS5114519A
(ja)
*
|
1974-07-25 |
1976-02-05 |
Mitsui Shipbuilding Eng |
Reikyakutaabindoyoku
|
|
DE2821691A1
(de)
|
1977-05-23 |
1978-12-21 |
Pavel Dipl Ing Chem Buncak |
Verfahren und vorrichtung zum anzeigen der stellung der gelenkten raeder von zwei- und mehrspurigen fahrzeugen
|
|
US4147513A
(en)
|
1977-09-26 |
1979-04-03 |
Bendix Autolite Corporation |
Method and apparatus for measuring the O2 content of a gas
|
|
DE2821681A1
(de)
|
1978-05-18 |
1979-11-22 |
Moto Meter Ag |
Lichtschrankensystem
|
|
FR2432876A1
(fr)
|
1978-08-08 |
1980-03-07 |
Dotson Donald |
Planche de patinage, notamment de patinage sur la neige
|
|
DE2834641A1
(de)
|
1978-08-08 |
1980-02-28 |
Bosch Gmbh Robert |
Mehrstufiger transistorverstaerker
|
|
SE438907B
(sv)
|
1978-09-22 |
1985-05-13 |
Kawaguchiya Firearms |
Sperranornding for patron och patronforare i automatvapen
|
|
US4474532A
(en)
|
1981-12-28 |
1984-10-02 |
United Technologies Corporation |
Coolable airfoil for a rotary machine
|
|
GB2121483B
(en)
|
1982-06-08 |
1985-02-13 |
Rolls Royce |
Cooled turbine blade for a gas turbine engine
|
|
JPH06102963B2
(ja)
*
|
1983-12-22 |
1994-12-14 |
株式会社東芝 |
ガスタ−ビン空冷翼
|
|
JPS61279702A
(ja)
*
|
1985-06-06 |
1986-12-10 |
Toshiba Corp |
ガスタ−ビン空冷案内羽根
|
|
US4753575A
(en)
*
|
1987-08-06 |
1988-06-28 |
United Technologies Corporation |
Airfoil with nested cooling channels
|
|
US5813835A
(en)
|
1991-08-19 |
1998-09-29 |
The United States Of America As Represented By The Secretary Of The Air Force |
Air-cooled turbine blade
|
|
US5296308A
(en)
|
1992-08-10 |
1994-03-22 |
Howmet Corporation |
Investment casting using core with integral wall thickness control means
|
|
US5403159A
(en)
*
|
1992-11-30 |
1995-04-04 |
United Technoligies Corporation |
Coolable airfoil structure
|
|
US5853044A
(en)
|
1996-04-24 |
1998-12-29 |
Pcc Airfoils, Inc. |
Method of casting an article
|
|
US6220817B1
(en)
*
|
1997-11-17 |
2001-04-24 |
General Electric Company |
AFT flowing multi-tier airfoil cooling circuit
|
|
GB9901218D0
(en)
|
1999-01-21 |
1999-03-10 |
Rolls Royce Plc |
Cooled aerofoil for a gas turbine engine
|
|
US6196792B1
(en)
|
1999-01-29 |
2001-03-06 |
General Electric Company |
Preferentially cooled turbine shroud
|
|
US6416284B1
(en)
|
2000-11-03 |
2002-07-09 |
General Electric Company |
Turbine blade for gas turbine engine and method of cooling same
|
|
US6491496B2
(en)
*
|
2001-02-23 |
2002-12-10 |
General Electric Company |
Turbine airfoil with metering plates for refresher holes
|
|
US6478535B1
(en)
|
2001-05-04 |
2002-11-12 |
Honeywell International, Inc. |
Thin wall cooling system
|
|
FR2829175B1
(fr)
|
2001-08-28 |
2003-11-07 |
Snecma Moteurs |
Circuits de refroidissement pour aube de turbine a gaz
|
|
FR2829174B1
(fr)
|
2001-08-28 |
2006-01-20 |
Snecma Moteurs |
Perfectionnement apportes aux circuits de refroidissement pour aube de turbine a gaz
|
|
US6974308B2
(en)
|
2001-11-14 |
2005-12-13 |
Honeywell International, Inc. |
High effectiveness cooled turbine vane or blade
|
|
US7217097B2
(en)
|
2005-01-07 |
2007-05-15 |
Siemens Power Generation, Inc. |
Cooling system with internal flow guide within a turbine blade of a turbine engine
|
|
US7303376B2
(en)
|
2005-12-02 |
2007-12-04 |
Siemens Power Generation, Inc. |
Turbine airfoil with outer wall cooling system and inner mid-chord hot gas receiving cavity
|
|
US7686581B2
(en)
|
2006-06-07 |
2010-03-30 |
General Electric Company |
Serpentine cooling circuit and method for cooling tip shroud
|
|
US7780413B2
(en)
|
2006-08-01 |
2010-08-24 |
Siemens Energy, Inc. |
Turbine airfoil with near wall inflow chambers
|
|
US7527475B1
(en)
|
2006-08-11 |
2009-05-05 |
Florida Turbine Technologies, Inc. |
Turbine blade with a near-wall cooling circuit
|
|
US7625178B2
(en)
|
2006-08-30 |
2009-12-01 |
Honeywell International Inc. |
High effectiveness cooled turbine blade
|
|
US7722324B2
(en)
|
2006-09-05 |
2010-05-25 |
United Technologies Corporation |
Multi-peripheral serpentine microcircuits for high aspect ratio blades
|
|
US7607891B2
(en)
|
2006-10-23 |
2009-10-27 |
United Technologies Corporation |
Turbine component with tip flagged pedestal cooling
|
|
US8591189B2
(en)
|
2006-11-20 |
2013-11-26 |
General Electric Company |
Bifeed serpentine cooled blade
|
|
US8047790B1
(en)
|
2007-01-17 |
2011-11-01 |
Florida Turbine Technologies, Inc. |
Near wall compartment cooled turbine blade
|
|
US7780415B2
(en)
*
|
2007-02-15 |
2010-08-24 |
Siemens Energy, Inc. |
Turbine blade having a convergent cavity cooling system for a trailing edge
|
|
US7819629B2
(en)
|
2007-02-15 |
2010-10-26 |
Siemens Energy, Inc. |
Blade for a gas turbine
|
|
US7862299B1
(en)
|
2007-03-21 |
2011-01-04 |
Florida Turbine Technologies, Inc. |
Two piece hollow turbine blade with serpentine cooling circuits
|
|
US7785072B1
(en)
|
2007-09-07 |
2010-08-31 |
Florida Turbine Technologies, Inc. |
Large chord turbine vane with serpentine flow cooling circuit
|
|
US8087891B1
(en)
|
2008-01-23 |
2012-01-03 |
Florida Turbine Technologies, Inc. |
Turbine blade with tip region cooling
|
|
CN101586477B
(zh)
*
|
2008-05-23 |
2011-04-13 |
中国科学院工程热物理研究所 |
一种具有射流冲击作用的扰流挡板强化传热装置
|
|
US8192146B2
(en)
|
2009-03-04 |
2012-06-05 |
Siemens Energy, Inc. |
Turbine blade dual channel cooling system
|
|
US8157505B2
(en)
|
2009-05-12 |
2012-04-17 |
Siemens Energy, Inc. |
Turbine blade with single tip rail with a mid-positioned deflector portion
|
|
US8292582B1
(en)
|
2009-07-09 |
2012-10-23 |
Florida Turbine Technologies, Inc. |
Turbine blade with serpentine flow cooling
|
|
US8616845B1
(en)
|
2010-06-23 |
2013-12-31 |
Florida Turbine Technologies, Inc. |
Turbine blade with tip cooling circuit
|
|
US8794921B2
(en)
|
2010-09-30 |
2014-08-05 |
General Electric Company |
Apparatus and methods for cooling platform regions of turbine rotor blades
|
|
CN102182518B
(zh)
|
2011-06-08 |
2013-09-04 |
河南科技大学 |
一种涡轮冷却叶片
|
|
US8734108B1
(en)
|
2011-11-22 |
2014-05-27 |
Florida Turbine Technologies, Inc. |
Turbine blade with impingement cooling cavities and platform cooling channels connected in series
|
|
US9109454B2
(en)
*
|
2012-03-01 |
2015-08-18 |
General Electric Company |
Turbine bucket with pressure side cooling
|
|
US8678766B1
(en)
|
2012-07-02 |
2014-03-25 |
Florida Turbine Technologies, Inc. |
Turbine blade with near wall cooling channels
|
|
US20140096538A1
(en)
|
2012-10-05 |
2014-04-10 |
General Electric Company |
Platform cooling of a turbine blade assembly
|
|
US8920123B2
(en)
*
|
2012-12-14 |
2014-12-30 |
Siemens Aktiengesellschaft |
Turbine blade with integrated serpentine and axial tip cooling circuits
|
|
CN104420887B
(zh)
*
|
2013-08-30 |
2016-06-15 |
哈尔滨汽轮机厂有限责任公司 |
一种燃气轮机的透平机
|
|
US9366194B2
(en)
|
2013-09-05 |
2016-06-14 |
General Electric Company |
Method and system for controlling gas turbine performance with a variable backflow margin
|
|
US20150152738A1
(en)
*
|
2013-12-02 |
2015-06-04 |
George Liang |
Turbine airfoil cooling passage with diamond turbulator
|
|
US9879547B2
(en)
|
2013-12-30 |
2018-01-30 |
General Electric Company |
Interior cooling circuits in turbine blades
|
|
US20150184538A1
(en)
|
2013-12-30 |
2015-07-02 |
General Electric Company |
Interior cooling circuits in turbine blades
|
|
US9995149B2
(en)
|
2013-12-30 |
2018-06-12 |
General Electric Company |
Structural configurations and cooling circuits in turbine blades
|
|
US10294799B2
(en)
*
|
2014-11-12 |
2019-05-21 |
United Technologies Corporation |
Partial tip flag
|
|
US9845694B2
(en)
|
2015-04-22 |
2017-12-19 |
United Technologies Corporation |
Flow directing cover for engine component
|
|
US9863538B2
(en)
|
2015-04-27 |
2018-01-09 |
United Technologies Corporation |
Gas turbine engine brush seal with supported tip
|