US3788763A
(en)
*
|
1972-11-01 |
1974-01-29 |
Gen Motors Corp |
Variable vanes
|
US4169692A
(en)
*
|
1974-12-13 |
1979-10-02 |
General Electric Company |
Variable area turbine nozzle and means for sealing same
|
US3966352A
(en)
*
|
1975-06-30 |
1976-06-29 |
United Technologies Corporation |
Variable area turbine
|
US4025227A
(en)
*
|
1975-06-30 |
1977-05-24 |
United Technologies Corporation |
Variable area turbine
|
US4053256A
(en)
*
|
1975-09-29 |
1977-10-11 |
United Technologies Corporation |
Variable camber vane for a gas turbine engine
|
US4013377A
(en)
*
|
1975-10-08 |
1977-03-22 |
Westinghouse Electric Corporation |
Intermediate transition annulus for a two shaft gas turbine engine
|
US3990810A
(en)
*
|
1975-12-23 |
1976-11-09 |
Westinghouse Electric Corporation |
Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine
|
DE2835349C2
(de)
*
|
1978-08-11 |
1979-12-20 |
Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen |
Verstelleitgitter für hochbelastete Verdichter, insbesondere von Gasturbinentriebwerken
|
CA2082709A1
(en)
*
|
1991-12-02 |
1993-06-03 |
Srinivasan Venkatasubbu |
Variable stator vane assembly for an axial flow compressor of a gas turbine engine
|
US5517817A
(en)
*
|
1993-10-28 |
1996-05-21 |
General Electric Company |
Variable area turbine nozzle for turbine engines
|
FR2850138A1
(fr)
*
|
2003-01-16 |
2004-07-23 |
Snecma Moteurs |
Dispositif anti-usure pour systeme de calage variable d'aube de turbomachine
|
FR2856750B1
(fr)
*
|
2003-06-26 |
2005-08-19 |
Snecma Moteurs |
Dispositif de guidage d'une aube a angle de calage variable
|
FR2894302B1
(fr)
*
|
2005-12-05 |
2008-01-18 |
Snecma Sa |
Dispositif de guidage d'une aube a angle de calage variable
|
EP1895106A1
(de)
*
|
2006-08-28 |
2008-03-05 |
ABB Turbo Systems AG |
Abdichtung verstellbarer Leitschaufeln
|
FR2913052B1
(fr)
*
|
2007-02-22 |
2011-04-01 |
Snecma |
Commande des aubes a angle de calage variable
|
US8033782B2
(en)
*
|
2008-01-16 |
2011-10-11 |
Elliott Company |
Method to prevent brinelling wear of slot and pin assembly
|
US8382436B2
(en)
|
2009-01-06 |
2013-02-26 |
General Electric Company |
Non-integral turbine blade platforms and systems
|
DE102009004933A1
(de)
*
|
2009-01-16 |
2010-07-29 |
Mtu Aero Engines Gmbh |
Leitschaufel für einen Stator eines Turboverdichters
|
US8262345B2
(en)
*
|
2009-02-06 |
2012-09-11 |
General Electric Company |
Ceramic matrix composite turbine engine
|
US8668445B2
(en)
|
2010-10-15 |
2014-03-11 |
General Electric Company |
Variable turbine nozzle system
|
CN102606223B
(zh)
*
|
2011-01-24 |
2014-12-17 |
中国石油化工集团公司 |
一种烟气轮机
|
EP2808495B1
(de)
*
|
2013-05-29 |
2016-03-23 |
MTU Aero Engines GmbH |
Lageranordnung für eine verstellbare Leitschaufel
|
DE102014215623A1
(de)
|
2014-08-07 |
2016-02-25 |
MTU Aero Engines AG |
Wälzlager, insbesondere Nadellager, zur Anordnung an einem Drehzapfen einer variablen Leitschaufel einer Strömungsmaschine
|
DE102018213604A1
(de)
*
|
2018-08-13 |
2020-02-13 |
Rolls-Royce Deutschland Ltd & Co Kg |
Leitschaufelbaugruppe mit Dichtelement
|
CN114526126B
(zh)
*
|
2022-04-24 |
2022-07-26 |
中国航发四川燃气涡轮研究院 |
一种可消除旋转凸台的进口可变弯度导叶结构
|