US6508630B2
(en)
|
2001-03-30 |
2003-01-21 |
General Electric Company |
Twisted stator vane
|
JP3927886B2
(ja)
*
|
2002-08-09 |
2007-06-13 |
本田技研工業株式会社 |
軸流圧縮機
|
US8550775B2
(en)
|
2002-08-13 |
2013-10-08 |
Honeywell International Inc. |
Compressor
|
FR2851798B1
(fr)
|
2003-02-27 |
2005-04-29 |
Snecma Moteurs |
Aube en fleche de turboreacteur
|
DE10352253A1
(de)
*
|
2003-11-08 |
2005-06-09 |
Alstom Technology Ltd |
Verdichterlaufschaufel
|
EP1760257B1
(en)
*
|
2004-09-24 |
2012-12-26 |
IHI Corporation |
Wall shape of axial flow machine and gas turbine engine
|
US7217096B2
(en)
*
|
2004-12-13 |
2007-05-15 |
General Electric Company |
Fillet energized turbine stage
|
US7195456B2
(en)
*
|
2004-12-21 |
2007-03-27 |
United Technologies Corporation |
Turbine engine guide vane and arrays thereof
|
US7134842B2
(en)
*
|
2004-12-24 |
2006-11-14 |
General Electric Company |
Scalloped surface turbine stage
|
US7249933B2
(en)
*
|
2005-01-10 |
2007-07-31 |
General Electric Company |
Funnel fillet turbine stage
|
US20060198726A1
(en)
*
|
2005-03-07 |
2006-09-07 |
General Electric Company |
Apparatus for eliminating compressor stator vibration induced by tip leakage vortex bursting
|
GB0506685D0
(en)
*
|
2005-04-01 |
2005-05-11 |
Hopkins David R |
A design to increase and smoothly improve the throughput of fluid (air or gas) through the inlet fan (or fans) of an aero-engine system
|
US7476086B2
(en)
*
|
2005-04-07 |
2009-01-13 |
General Electric Company |
Tip cambered swept blade
|
US7374403B2
(en)
*
|
2005-04-07 |
2008-05-20 |
General Electric Company |
Low solidity turbofan
|
US7220100B2
(en)
*
|
2005-04-14 |
2007-05-22 |
General Electric Company |
Crescentic ramp turbine stage
|
US20060237168A1
(en)
*
|
2005-04-21 |
2006-10-26 |
Belady Christian L |
Air mover with thermally coupled guide vanes
|
US7811053B2
(en)
*
|
2005-07-22 |
2010-10-12 |
United Technologies Corporation |
Fan rotor design for coincidence avoidance
|
GB0620769D0
(en)
*
|
2006-10-19 |
2006-11-29 |
Rolls Royce Plc |
A fan blade
|
FR2908152B1
(fr)
*
|
2006-11-08 |
2009-02-06 |
Snecma Sa |
Aube en fleche de turbomachine
|
US8413709B2
(en)
*
|
2006-12-06 |
2013-04-09 |
General Electric Company |
Composite core die, methods of manufacture thereof and articles manufactured therefrom
|
US20080135721A1
(en)
*
|
2006-12-06 |
2008-06-12 |
General Electric Company |
Casting compositions for manufacturing metal casting and methods of manufacturing thereof
|
US7624787B2
(en)
*
|
2006-12-06 |
2009-12-01 |
General Electric Company |
Disposable insert, and use thereof in a method for manufacturing an airfoil
|
US7938168B2
(en)
*
|
2006-12-06 |
2011-05-10 |
General Electric Company |
Ceramic cores, methods of manufacture thereof and articles manufactured from the same
|
US8884182B2
(en)
|
2006-12-11 |
2014-11-11 |
General Electric Company |
Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom
|
US7487819B2
(en)
*
|
2006-12-11 |
2009-02-10 |
General Electric Company |
Disposable thin wall core die, methods of manufacture thereof and articles manufactured therefrom
|
GB0712561D0
(en)
*
|
2007-06-28 |
2007-08-08 |
Rolls Royce Plc |
A blade mounting
|
EP2146053A1
(de)
*
|
2008-07-17 |
2010-01-20 |
Siemens Aktiengesellschaft |
Axialturbomaschine mit geringen Spaltverlusten
|
EP2146054A1
(de)
*
|
2008-07-17 |
2010-01-20 |
Siemens Aktiengesellschaft |
Axialturbine für eine Gasturbine
|
US8061980B2
(en)
*
|
2008-08-18 |
2011-11-22 |
United Technologies Corporation |
Separation-resistant inlet duct for mid-turbine frames
|
FR2940374B1
(fr)
*
|
2008-12-23 |
2015-02-20 |
Snecma |
Carter de compresseur a cavites optimisees.
|
US8657570B2
(en)
|
2009-06-30 |
2014-02-25 |
General Electric Company |
Rotor blade with reduced rub loading
|
US8662834B2
(en)
|
2009-06-30 |
2014-03-04 |
General Electric Company |
Method for reducing tip rub loading
|
EP2449216A1
(en)
*
|
2009-06-30 |
2012-05-09 |
General Electric Company |
Rotor blade and method for reducing tip rub loading
|
US8393872B2
(en)
*
|
2009-10-23 |
2013-03-12 |
General Electric Company |
Turbine airfoil
|
GB201006449D0
(en)
*
|
2010-04-19 |
2010-06-02 |
Rolls Royce Plc |
Blades
|
US8668459B2
(en)
*
|
2010-05-28 |
2014-03-11 |
Hamilton Sundstrand Corporation |
Turbine blade walking prevention
|
FR2961564B1
(fr)
|
2010-06-17 |
2016-03-04 |
Snecma |
Compresseur et turbomachine a rendement optimise
|
GB2483059A
(en)
*
|
2010-08-23 |
2012-02-29 |
Rolls Royce Plc |
An aerofoil blade with a set-back portion
|
US8668446B2
(en)
|
2010-08-31 |
2014-03-11 |
General Electric Company |
Supersonic compressor rotor and method of assembling same
|
US9022730B2
(en)
|
2010-10-08 |
2015-05-05 |
General Electric Company |
Supersonic compressor startup support system
|
JP5502695B2
(ja)
*
|
2010-10-14 |
2014-05-28 |
株式会社日立製作所 |
軸流圧縮機
|
US8864454B2
(en)
|
2010-10-28 |
2014-10-21 |
General Electric Company |
System and method of assembling a supersonic compressor system including a supersonic compressor rotor and a compressor assembly
|
US8657571B2
(en)
|
2010-12-21 |
2014-02-25 |
General Electric Company |
Supersonic compressor rotor and methods for assembling same
|
US8827640B2
(en)
|
2011-03-01 |
2014-09-09 |
General Electric Company |
System and methods of assembling a supersonic compressor rotor including a radial flow channel
|
US8777793B2
(en)
|
2011-04-27 |
2014-07-15 |
United Technologies Corporation |
Fan drive planetary gear system integrated carrier and torque frame
|
US8550770B2
(en)
|
2011-05-27 |
2013-10-08 |
General Electric Company |
Supersonic compressor startup support system
|
US8770929B2
(en)
|
2011-05-27 |
2014-07-08 |
General Electric Company |
Supersonic compressor rotor and method of compressing a fluid
|
EP2530330B1
(de)
*
|
2011-06-01 |
2016-05-25 |
MTU Aero Engines AG |
Laufschaufel für einen Verdichter einer Turbomaschine, Verdichter sowie Turbomaschine
|
US9102397B2
(en)
*
|
2011-12-20 |
2015-08-11 |
General Electric Company |
Airfoils including tip profile for noise reduction and method for fabricating same
|
FR2986285B1
(fr)
*
|
2012-01-30 |
2014-02-14 |
Snecma |
Aube pour soufflante de turboreacteur
|
US8863491B2
(en)
|
2012-01-31 |
2014-10-21 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US20130192198A1
(en)
|
2012-01-31 |
2013-08-01 |
Lisa I. Brilliant |
Compressor flowpath
|
US10400629B2
(en)
|
2012-01-31 |
2019-09-03 |
United Technologies Corporation |
Gas turbine engine shaft bearing configuration
|
US9038366B2
(en)
|
2012-01-31 |
2015-05-26 |
United Technologies Corporation |
LPC flowpath shape with gas turbine engine shaft bearing configuration
|
US9085983B2
(en)
|
2012-03-29 |
2015-07-21 |
General Electric Company |
Apparatus and method for purging a gas turbine rotor
|
CN104246138B
(zh)
|
2012-04-23 |
2016-06-22 |
通用电气公司 |
具有局部壁厚控制的涡轮翼型件及涡轮叶片
|
US9121285B2
(en)
*
|
2012-05-24 |
2015-09-01 |
General Electric Company |
Turbine and method for reducing shock losses in a turbine
|
FR2993927B1
(fr)
*
|
2012-07-27 |
2014-08-22 |
Snecma |
Piece de modification du profil d'une veine aerodynamique
|
CN103062113A
(zh)
*
|
2013-01-23 |
2013-04-24 |
薛文义 |
一种用于涡轮风扇发动机的风扇机构
|
WO2014163673A2
(en)
|
2013-03-11 |
2014-10-09 |
Bronwyn Power |
Gas turbine engine flow path geometry
|
US9879540B2
(en)
|
2013-03-12 |
2018-01-30 |
Pratt & Whitney Canada Corp. |
Compressor stator with contoured endwall
|
JP6012519B2
(ja)
*
|
2013-03-21 |
2016-10-25 |
三菱重工業株式会社 |
タービン、及びこれを備えた回転機械
|
US9245851B2
(en)
*
|
2013-07-18 |
2016-01-26 |
Fuji Electric Co., Ltd. |
Semiconductor device and method of manufacturing semiconductor device
|
FR3021706B1
(fr)
*
|
2014-05-28 |
2020-05-15 |
Safran Aircraft Engines |
Turbopropulseur d'aeronef comportant deux helices coaxiales.
|
US9470093B2
(en)
|
2015-03-18 |
2016-10-18 |
United Technologies Corporation |
Turbofan arrangement with blade channel variations
|
BR112017020559B1
(pt)
*
|
2015-04-15 |
2022-11-16 |
Robert Bosch Gmbh |
Conjunto de ventilador axial de ponta livre
|
JP6421091B2
(ja)
*
|
2015-07-30 |
2018-11-07 |
三菱日立パワーシステムズ株式会社 |
軸流圧縮機、それを備えたガスタービン、及び軸流圧縮機の静翼
|
US10808539B2
(en)
|
2016-07-25 |
2020-10-20 |
Raytheon Technologies Corporation |
Rotor blade for a gas turbine engine
|
US10458426B2
(en)
|
2016-09-15 |
2019-10-29 |
General Electric Company |
Aircraft fan with low part-span solidity
|
US11092163B2
(en)
|
2017-02-08 |
2021-08-17 |
Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. |
Compressor and turbocharger
|
USD911512S1
(en)
|
2018-01-31 |
2021-02-23 |
Carrier Corporation |
Axial flow fan
|
US11739766B2
(en)
|
2019-05-14 |
2023-08-29 |
Carrier Corporation |
Centrifugal compressor including diffuser pressure equalization feature
|
IT201900007935A1
(it)
*
|
2019-06-04 |
2020-12-04 |
R E M Holding S R L |
Ventilatore con virola migliorata
|
DE102020203966A1
(de)
|
2020-03-26 |
2021-09-30 |
MTU Aero Engines AG |
Verdichter für eine Gasturbine und Gasturbine
|
GB202112576D0
(en)
*
|
2021-09-03 |
2021-10-20 |
Cummins Ltd |
Impeller element for compressor
|
CN114251130B
(zh)
*
|
2021-12-22 |
2022-12-02 |
清华大学 |
一种用于控制叶顶泄漏流的鲁棒性转子结构和动力系统
|