US7399159B2
(en)
*
|
2003-06-25 |
2008-07-15 |
Florida Turbine Technologies, Inc |
Detachable leading edge for airfoils
|
EP1828567B1
(de)
*
|
2004-12-01 |
2011-10-12 |
United Technologies Corporation |
Diffusor-ansaugung für einen spitzenturbinenmotor
|
US20090148273A1
(en)
*
|
2004-12-01 |
2009-06-11 |
Suciu Gabriel L |
Compressor inlet guide vane for tip turbine engine and corresponding control method
|
US8641367B2
(en)
|
2004-12-01 |
2014-02-04 |
United Technologies Corporation |
Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method
|
US8087885B2
(en)
*
|
2004-12-01 |
2012-01-03 |
United Technologies Corporation |
Stacked annular components for turbine engines
|
WO2006060013A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan rotor of a tip turbine engine
|
DE602004027766D1
(de)
|
2004-12-01 |
2010-07-29 |
United Technologies Corp |
Hydraulische dichtung für ein getriebe eines spitzenturbinenmotors
|
WO2006110123A2
(en)
*
|
2004-12-01 |
2006-10-19 |
United Technologies Corporation |
Vectoring transition duct for turbine engine
|
WO2006060001A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Fan rotor assembly for a tip turbine engine
|
US8561383B2
(en)
|
2004-12-01 |
2013-10-22 |
United Technologies Corporation |
Turbine engine with differential gear driven fan and compressor
|
EP1834067B1
(de)
|
2004-12-01 |
2008-11-26 |
United Technologies Corporation |
Gebläseschaufelanordnung für ein tip-turbinentriebwerk und montageverfahren
|
US9845727B2
(en)
|
2004-12-01 |
2017-12-19 |
United Technologies Corporation |
Tip turbine engine composite tailcone
|
WO2006060011A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine comprising a nonrotable compartment
|
US8083030B2
(en)
|
2004-12-01 |
2011-12-27 |
United Technologies Corporation |
Gearbox lubrication supply system for a tip engine
|
US7980054B2
(en)
*
|
2004-12-01 |
2011-07-19 |
United Technologies Corporation |
Ejector cooling of outer case for tip turbine engine
|
US8152469B2
(en)
|
2004-12-01 |
2012-04-10 |
United Technologies Corporation |
Annular turbine ring rotor
|
WO2006112807A2
(en)
|
2004-12-01 |
2006-10-26 |
United Technologies Corporation |
Turbine engine and method for starting a turbine engine
|
WO2006059985A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Axial compressor for tip turbine engine
|
US8365511B2
(en)
|
2004-12-01 |
2013-02-05 |
United Technologies Corporation |
Tip turbine engine integral case, vane, mount and mixer
|
WO2006059973A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine with a heat exchanger
|
WO2006059994A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Seal assembly for a fan-turbine rotor of a tip turbine engine
|
WO2006059977A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine and corresponding orepating method
|
WO2006060000A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Variable fan inlet guide vane assembly, turbine engine with such an assembly and corresponding controlling method
|
WO2006059987A1
(en)
|
2004-12-01 |
2006-06-08 |
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
|
WO2006059986A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine and operating method with reverse core airflow
|
EP1841960B1
(de)
|
2004-12-01 |
2011-05-25 |
United Technologies Corporation |
Starter-generatorsystem für einen spitzenturbinenmotor
|
DE602004032186D1
(de)
|
2004-12-01 |
2011-05-19 |
United Technologies Corp |
Turbinenschaufelgruppe eines Fanrotors sowie Verfahren zur Montage einer solchen Gruppe
|
US7887296B2
(en)
|
2004-12-01 |
2011-02-15 |
United Technologies Corporation |
Fan blade with integral diffuser section and tip turbine blade section for a tip turbine engine
|
US8033094B2
(en)
|
2004-12-01 |
2011-10-11 |
United Technologies Corporation |
Cantilevered tip turbine engine
|
EP1828683B1
(de)
|
2004-12-01 |
2013-04-10 |
United Technologies Corporation |
Brennkammer für turbinenmotor
|
WO2006059996A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Balanced turbine rotor fan blade for a tip turbine engine
|
US8061968B2
(en)
|
2004-12-01 |
2011-11-22 |
United Technologies Corporation |
Counter-rotating compressor case and assembly method for tip turbine engine
|
WO2006059972A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Compressor variable stage remote actuation for turbine engine
|
US7921635B2
(en)
*
|
2004-12-01 |
2011-04-12 |
United Technologies Corporation |
Peripheral combustor for tip turbine engine
|
WO2006059993A1
(en)
*
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine with multiple fan and turbine stages
|
WO2006110122A2
(en)
|
2004-12-01 |
2006-10-19 |
United Technologies Corporation |
Inflatable bleed valve for a turbine engine and a method of operating therefore
|
US7959406B2
(en)
|
2004-12-01 |
2011-06-14 |
United Technologies Corporation |
Close coupled gearbox assembly for a tip turbine engine
|
WO2006059968A1
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Counter-rotating gearbox for tip turbine engine
|
WO2006059971A2
(en)
|
2004-12-01 |
2006-06-08 |
United Technologies Corporation |
Tip turbine engine integral fan, combustor, and turbine case
|
US9109537B2
(en)
|
2004-12-04 |
2015-08-18 |
United Technologies Corporation |
Tip turbine single plane mount
|
US7537430B2
(en)
*
|
2005-11-11 |
2009-05-26 |
General Electric Company |
Stacked reaction steam turbine rotor assembly
|
US7578655B1
(en)
*
|
2006-05-20 |
2009-08-25 |
Florida Turbine Technologies, Inc. |
Composite gas turbine fan blade
|
US7758303B1
(en)
*
|
2006-07-31 |
2010-07-20 |
General Electric Company |
FLADE fan with different inner and outer airfoil stagger angles at a shroud therebetween
|
US7736450B2
(en)
*
|
2006-09-29 |
2010-06-15 |
General Electric Company |
Varying fluence as a function of thickness during laser shock peening
|
US8192141B1
(en)
*
|
2007-04-05 |
2012-06-05 |
The United States Of America As Represented By The Secretary Of The Air Force |
Dual compression rotor
|
FR2914943B1
(fr)
|
2007-04-13 |
2011-04-01 |
Snecma |
Aube de soufflante
|
US8967945B2
(en)
|
2007-05-22 |
2015-03-03 |
United Technologies Corporation |
Individual inlet guide vane control for tip turbine engine
|
CA2643587A1
(en)
*
|
2008-11-10 |
2010-05-10 |
Organoworld Inc. |
Turbine annular axial rotor
|
US8667774B2
(en)
|
2009-08-05 |
2014-03-11 |
The Boeing Company |
Coannular ducted fan
|
ITMI20120569A1
(it)
*
|
2012-04-06 |
2013-10-07 |
Franco Tosi Meccanica S P A |
Stadio rotorico di turbina assiale a rapporto corda/passo migliorato
|
US20140169972A1
(en)
*
|
2012-12-17 |
2014-06-19 |
United Technologies Corporation |
Fan with integral shroud
|
KR20160070079A
(ko)
*
|
2013-10-03 |
2016-06-17 |
프랑코 토시 메카니카 에세.피.아. |
향상된 익현/피치 비율을 가진 축 터빈의 로터 스테이지
|
WO2015057544A1
(en)
*
|
2013-10-16 |
2015-04-23 |
United Technologies Corporation |
Auxiliary power unit impeller blade
|
US10119403B2
(en)
|
2014-02-13 |
2018-11-06 |
United Technologies Corporation |
Mistuned concentric airfoil assembly and method of mistuning same
|
EP3012411A1
(de)
*
|
2014-10-23 |
2016-04-27 |
United Technologies Corporation |
Integral beschaufelter rotor mit axialem arm und tasche
|
US20160208613A1
(en)
*
|
2015-01-15 |
2016-07-21 |
United Technologies Corporation |
Gas turbine engine integrally bladed rotor
|
US10563516B2
(en)
*
|
2016-07-06 |
2020-02-18 |
General Electric Company |
Turbine engine and method of assembling
|
US10415403B2
(en)
*
|
2017-01-13 |
2019-09-17 |
Rolls-Royce North American Technologies Inc. |
Cooled blisk for gas turbine engine
|
US10876407B2
(en)
*
|
2017-02-16 |
2020-12-29 |
General Electric Company |
Thermal structure for outer diameter mounted turbine blades
|
GB2561837A
(en)
|
2017-04-24 |
2018-10-31 |
Hieta Tech Limited |
Turbine rotor, turbine, apparatus and method
|
US10619483B2
(en)
*
|
2017-11-21 |
2020-04-14 |
United Technologies Corporation |
Partially shrouded gas turbine engine fan
|
US10670037B2
(en)
*
|
2017-11-21 |
2020-06-02 |
General Electric Company |
Turbofan engine's fan blade and setting method thereof
|
US11060406B2
(en)
*
|
2019-10-11 |
2021-07-13 |
Pratt & Whitney Canada Corp. |
Rotor for gas turbine engine
|
US11428160B2
(en)
|
2020-12-31 |
2022-08-30 |
General Electric Company |
Gas turbine engine with interdigitated turbine and gear assembly
|
BE1030046B1
(fr)
*
|
2021-12-17 |
2023-07-17 |
Safran Aero Boosters |
Roue mobile a plusieurs rangees d’aubes
|
CN114542510A
(zh)
*
|
2022-02-23 |
2022-05-27 |
中国航发沈阳发动机研究所 |
一种自适应变循环发动机风扇转子结构
|
BE1030473B1
(fr)
*
|
2022-04-21 |
2023-11-27 |
Safran Aero Boosters |
Rotor a plusieurs rangees d’aubes
|