CN1087046C
(zh)
*
|
1995-01-10 |
2002-07-03 |
普罗克特和甘保尔公司 |
平滑,穿透热风干燥的薄页纸和制造方法
|
US6431476B1
(en)
|
1999-12-21 |
2002-08-13 |
Cepheid |
Apparatus and method for rapid ultrasonic disruption of cells or viruses
|
US20040200909A1
(en)
*
|
1999-05-28 |
2004-10-14 |
Cepheid |
Apparatus and method for cell disruption
|
US6619030B1
(en)
|
2002-03-01 |
2003-09-16 |
General Electric Company |
Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors
|
US6732502B2
(en)
|
2002-03-01 |
2004-05-11 |
General Electric Company |
Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor
|
US6739120B2
(en)
|
2002-04-29 |
2004-05-25 |
General Electric Company |
Counterrotatable booster compressor assembly for a gas turbine engine
|
US6684626B1
(en)
|
2002-07-30 |
2004-02-03 |
General Electric Company |
Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines
|
US6711887B2
(en)
|
2002-08-19 |
2004-03-30 |
General Electric Co. |
Aircraft gas turbine engine with tandem non-interdigitated counter rotating low pressure turbines
|
US6763652B2
(en)
|
2002-09-24 |
2004-07-20 |
General Electric Company |
Variable torque split aircraft gas turbine engine counter rotating low pressure turbines
|
US6763653B2
(en)
|
2002-09-24 |
2004-07-20 |
General Electric Company |
Counter rotating fan aircraft gas turbine engine with aft booster
|
US6763654B2
(en)
|
2002-09-30 |
2004-07-20 |
General Electric Co. |
Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans
|
US7063505B2
(en)
|
2003-02-07 |
2006-06-20 |
General Electric Company |
Gas turbine engine frame having struts connected to rings with morse pins
|
US6866479B2
(en)
*
|
2003-05-16 |
2005-03-15 |
Mitsubishi Heavy Industries, Ltd. |
Exhaust diffuser for axial-flow turbine
|
FR2858649B1
(fr)
*
|
2003-08-05 |
2005-09-23 |
Snecma Moteurs |
Turbine basse-pression de turbomachine
|
FR2866073B1
(fr)
*
|
2004-02-11 |
2006-07-28 |
Snecma Moteurs |
Turboreacteur ayant deux soufflantes contrarotatives solidaires d'un compresseur a basse pression contrarotatif
|
US7185484B2
(en)
*
|
2004-08-11 |
2007-03-06 |
General Electric Company |
Methods and apparatus for assembling a gas turbine engine
|
US7409819B2
(en)
*
|
2004-10-29 |
2008-08-12 |
General Electric Company |
Gas turbine engine and method of assembling same
|
US7195447B2
(en)
*
|
2004-10-29 |
2007-03-27 |
General Electric Company |
Gas turbine engine and method of assembling same
|
EP1825170B1
(de)
|
2004-12-01 |
2009-03-18 |
United Technologies Corporation |
Schmiermittel-versorgungssystem für das getriebe eines tip-turbinen-triebwerks
|
US7980054B2
(en)
*
|
2004-12-01 |
2011-07-19 |
United Technologies Corporation |
Ejector cooling of outer case for tip turbine engine
|
WO2006059971A2
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine integral fan, combustor, and turbine case
|
WO2006110122A2
(en)
|
2004-12-01 |
2006-10-19 |
United Technologies Corporation |
Inflatable bleed valve for a turbine engine and a method of operating therefore
|
WO2006059985A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Axial compressor for tip turbine engine
|
US7921635B2
(en)
*
|
2004-12-01 |
2011-04-12 |
United Technologies Corporation |
Peripheral combustor for tip turbine engine
|
DE602004023769D1
(de)
*
|
2004-12-01 |
2009-12-03 |
United Technologies Corp |
Gestapelte ringförmige bauteile für turbinenmotoren
|
WO2006060014A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Starter generator system for a tip turbine engine
|
WO2006059973A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine with a heat exchanger
|
US9003759B2
(en)
|
2004-12-01 |
2015-04-14 |
United Technologies Corporation |
Particle separator for tip turbine engine
|
WO2006059989A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine support structure
|
US8807936B2
(en)
|
2004-12-01 |
2014-08-19 |
United Technologies Corporation |
Balanced turbine rotor fan blade for a tip turbine engine
|
US7874802B2
(en)
|
2004-12-01 |
2011-01-25 |
United Technologies Corporation |
Tip turbine engine comprising turbine blade clusters and method of assembly
|
DE602004031986D1
(de)
|
2004-12-01 |
2011-05-05 |
United Technologies Corp |
Gebläse-turbinen-rotoranordnung für einen spitzenturbinenmotor
|
WO2006059970A2
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Turbine engine with differential gear driven fan and compressor
|
DE602004028528D1
(de)
*
|
2004-12-01 |
2010-09-16 |
United Technologies Corp |
Tip-Turbinentriebwerk mit mehreren Gebläse- und Turbinenstufen
|
US7883315B2
(en)
|
2004-12-01 |
2011-02-08 |
United Technologies Corporation |
Seal assembly for a fan rotor of a tip turbine engine
|
US8096753B2
(en)
|
2004-12-01 |
2012-01-17 |
United Technologies Corporation |
Tip turbine engine and operating method with reverse core airflow
|
WO2006059994A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan-turbine rotor of a tip turbine engine
|
EP1828547B1
(de)
|
2004-12-01 |
2011-11-30 |
United Technologies Corporation |
Turbofantriebwerk mit einer Mehrzahl von einzeln steuerbaren Einlassleitschaufeln und zugehöriges Steuerverfahren
|
US7882694B2
(en)
|
2004-12-01 |
2011-02-08 |
United Technologies Corporation |
Variable fan inlet guide vane assembly for gas turbine engine
|
WO2006060010A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Compressor inlet guide vane for tip turbine engine and corresponding control method
|
US7921636B2
(en)
*
|
2004-12-01 |
2011-04-12 |
United Technologies Corporation |
Tip turbine engine and corresponding operating method
|
US8061968B2
(en)
|
2004-12-01 |
2011-11-22 |
United Technologies Corporation |
Counter-rotating compressor case and assembly method for tip turbine engine
|
US7959406B2
(en)
|
2004-12-01 |
2011-06-14 |
United Technologies Corporation |
Close coupled gearbox assembly for a tip turbine engine
|
EP1825113B1
(de)
*
|
2004-12-01 |
2012-10-24 |
United Technologies Corporation |
Gegenläufiges getriebe für ein tip-turbinen-triebwerk
|
WO2006059972A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Compressor variable stage remote actuation for turbine engine
|
US7959532B2
(en)
|
2004-12-01 |
2011-06-14 |
United Technologies Corporation |
Hydraulic seal for a gearbox of a tip turbine engine
|
WO2006059990A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Regenerative turbine blade and vane cooling for a tip turbine engine
|
US7631480B2
(en)
|
2004-12-01 |
2009-12-15 |
United Technologies Corporation |
Modular tip turbine engine
|
WO2006060011A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine comprising a nonrotable compartment
|
US8468795B2
(en)
*
|
2004-12-01 |
2013-06-25 |
United Technologies Corporation |
Diffuser aspiration for a tip turbine engine
|
US8152469B2
(en)
|
2004-12-01 |
2012-04-10 |
United Technologies Corporation |
Annular turbine ring rotor
|
US7882695B2
(en)
|
2004-12-01 |
2011-02-08 |
United Technologies Corporation |
Turbine blow down starter for turbine engine
|
US8024931B2
(en)
|
2004-12-01 |
2011-09-27 |
United Technologies Corporation |
Combustor for turbine engine
|
WO2006060006A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine non-metallic tailcone
|
WO2006060003A2
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
|
EP1825112B1
(de)
|
2004-12-01 |
2013-10-23 |
United Technologies Corporation |
Freigetragene tipturbinentriebwerk
|
WO2006059979A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine integral case, vane, mount, and mixer
|
WO2006110123A2
(en)
*
|
2004-12-01 |
2006-10-19 |
United Technologies Corporation |
Vectoring transition duct for turbine engine
|
EP1834076B1
(de)
|
2004-12-01 |
2011-04-06 |
United Technologies Corporation |
Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
|
WO2006062497A1
(en)
|
2004-12-04 |
2006-06-15 |
United Technologies Corporation |
Tip turbine engine mount
|
US7510371B2
(en)
*
|
2005-06-06 |
2009-03-31 |
General Electric Company |
Forward tilted turbine nozzle
|
US7594388B2
(en)
*
|
2005-06-06 |
2009-09-29 |
General Electric Company |
Counterrotating turbofan engine
|
US7513102B2
(en)
*
|
2005-06-06 |
2009-04-07 |
General Electric Company |
Integrated counterrotating turbofan
|
FR2912181B1
(fr)
*
|
2007-02-07 |
2009-04-24 |
Snecma Sa |
Turbine a gaz a turbines hp et bp contra-rotatives
|
US8038388B2
(en)
*
|
2007-03-05 |
2011-10-18 |
United Technologies Corporation |
Abradable component for a gas turbine engine
|
US8967945B2
(en)
|
2007-05-22 |
2015-03-03 |
United Technologies Corporation |
Individual inlet guide vane control for tip turbine engine
|
BR102013021427B1
(pt)
*
|
2013-08-16 |
2022-04-05 |
Luis Antonio Waack Bambace |
Turbomáquinas axiais de carcaça rotativa e elemento central fixo
|
KR101684778B1
(ko)
*
|
2015-04-16 |
2016-12-08 |
한양대학교 산학협력단 |
진동 특성 해석 시스템 및 진동 특성 해석 방법
|
PL415534A1
(pl)
*
|
2016-01-04 |
2017-07-17 |
General Electric Company |
Układ dla zespołu osłony i przegrody wstępnych łopatek kierowniczych
|
US10544734B2
(en)
*
|
2017-01-23 |
2020-01-28 |
General Electric Company |
Three spool gas turbine engine with interdigitated turbine section
|
US10655537B2
(en)
*
|
2017-01-23 |
2020-05-19 |
General Electric Company |
Interdigitated counter rotating turbine system and method of operation
|
US10539020B2
(en)
*
|
2017-01-23 |
2020-01-21 |
General Electric Company |
Two spool gas turbine engine with interdigitated turbine section
|
US10605168B2
(en)
|
2017-05-25 |
2020-03-31 |
General Electric Company |
Interdigitated turbine engine air bearing cooling structure and method of thermal management
|
US10718265B2
(en)
|
2017-05-25 |
2020-07-21 |
General Electric Company |
Interdigitated turbine engine air bearing and method of operation
|
US10787931B2
(en)
|
2017-05-25 |
2020-09-29 |
General Electric Company |
Method and structure of interdigitated turbine engine thermal management
|
US10669893B2
(en)
|
2017-05-25 |
2020-06-02 |
General Electric Company |
Air bearing and thermal management nozzle arrangement for interdigitated turbine engine
|
US10961850B2
(en)
*
|
2017-09-19 |
2021-03-30 |
General Electric Company |
Rotatable torque frame for gas turbine engine
|
US11085309B2
(en)
*
|
2017-09-22 |
2021-08-10 |
General Electric Company |
Outer drum rotor assembly
|
FR3101103B1
(fr)
*
|
2019-09-24 |
2022-04-22 |
Safran Aircraft Engines |
architecture améliorée de carter tournant de turbine contrarotative
|
US11268394B2
(en)
|
2020-03-13 |
2022-03-08 |
General Electric Company |
Nozzle assembly with alternating inserted vanes for a turbine engine
|
US11428160B2
(en)
|
2020-12-31 |
2022-08-30 |
General Electric Company |
Gas turbine engine with interdigitated turbine and gear assembly
|
DE102022113096A1
(de)
|
2022-05-24 |
2023-11-30 |
ConBotics GmbH |
Mobile Robotervorrichtungen und Verfahren zur bahnförmigen Oberflächenbearbeitung von Gebäudestrukturen
|