US3572970A
(en)
*
|
1969-01-23 |
1971-03-30 |
Gen Electric |
Turbomachinery blade spacer
|
US3653781A
(en)
*
|
1970-12-18 |
1972-04-04 |
Gen Electric |
Turbomachinery blade retainer
|
DE2155344A1
(de)
*
|
1971-11-08 |
1973-05-17 |
Motoren Turbinen Union |
Integrales turbinenrad mit offenen axialen durchbruechen am aeusseren kranz und kontrollierten kranzrissen
|
BE794573A
(fr)
*
|
1972-02-02 |
1973-05-16 |
Gen Electric |
Dispositif de fixation d'aubes
|
US3832092A
(en)
*
|
1973-10-19 |
1974-08-27 |
Gen Electric |
Device for locking turbomachinery blades
|
US3936234A
(en)
*
|
1975-02-10 |
1976-02-03 |
General Electric Company |
Device for locking turbomachinery blades
|
US4279572A
(en)
*
|
1979-07-09 |
1981-07-21 |
United Technologies Corporation |
Sideplates for rotor disk and rotor blades
|
FR2507679A1
(fr)
*
|
1981-06-12 |
1982-12-17 |
Snecma |
Dispositif de verrouillage d'une aube de rotor de turbomachine
|
US4451205A
(en)
*
|
1982-02-22 |
1984-05-29 |
United Technologies Corporation |
Rotor blade assembly
|
FR2535794A1
(fr)
*
|
1982-11-08 |
1984-05-11 |
Snecma |
Dispositif de retenue axiale et radiale d'aubes de soufflante
|
US4477226A
(en)
*
|
1983-05-09 |
1984-10-16 |
General Electric Company |
Balance for rotating member
|
US4505640A
(en)
*
|
1983-12-13 |
1985-03-19 |
United Technologies Corporation |
Seal means for a blade attachment slot of a rotor assembly
|
US4595340A
(en)
*
|
1984-07-30 |
1986-06-17 |
General Electric Company |
Gas turbine bladed disk assembly
|
US4778342A
(en)
*
|
1985-07-24 |
1988-10-18 |
Imo Delaval, Inc. |
Turbine blade retainer
|
US4797065A
(en)
*
|
1986-10-17 |
1989-01-10 |
Transamerica Delaval Inc. |
Turbine blade retainer
|
DE19516694C2
(de)
*
|
1995-05-06 |
2001-06-28 |
Mtu Aero Engines Gmbh |
Einrichtung zur Fixierung von Laufschaufeln am Laufrad, insbesondere einer Turbine eines Gasturbinentriebwerks
|
DE19603388C1
(de)
*
|
1996-01-31 |
1997-07-24 |
Mtu Muenchen Gmbh |
Einrichtung zur Fixierung der Laufschaufeln am Laufrad, insbesondere einer Turbine eines Gasturbinentriebwerks, durch Nietung
|
US5993160A
(en)
*
|
1997-12-11 |
1999-11-30 |
Pratt & Whitney Canada Inc. |
Cover plate for gas turbine rotor
|
US5984639A
(en)
*
|
1998-07-09 |
1999-11-16 |
Pratt & Whitney Canada Inc. |
Blade retention apparatus for gas turbine rotor
|
US6582195B2
(en)
*
|
2001-06-27 |
2003-06-24 |
General Electric Company |
Compressor rotor blade spacer apparatus
|
GB2408296A
(en)
*
|
2003-11-22 |
2005-05-25 |
Rolls Royce Plc |
Compressor blade root retainer with integral sealing means to reduce axial leakage
|
GB2410531B
(en)
|
2004-01-29 |
2006-03-01 |
Rolls Royce Plc |
Fan blade disk assembly
|
US7264448B2
(en)
*
|
2004-10-06 |
2007-09-04 |
Siemens Power Corporation, Inc. |
Remotely accessible locking system for turbine blades
|
US8708652B2
(en)
*
|
2007-06-27 |
2014-04-29 |
United Technologies Corporation |
Cover plate for turbine rotor having enclosed pump for cooling air
|
FR2945329B1
(fr)
*
|
2009-05-06 |
2011-06-03 |
Snecma |
Rotor de soufflante d'un turboracteur d'avion
|
US8439635B2
(en)
*
|
2009-05-11 |
2013-05-14 |
Rolls-Royce Corporation |
Apparatus and method for locking a composite component
|
US8979502B2
(en)
|
2011-12-15 |
2015-03-17 |
Pratt & Whitney Canada Corp. |
Turbine rotor retaining system
|
ES2630046T3
(es)
*
|
2013-04-09 |
2017-08-17 |
MTU Aero Engines AG |
Surtido de chapas de sujeción, turbina de gas correspondiente y método de ensamblaje
|
US9840922B2
(en)
*
|
2014-03-07 |
2017-12-12 |
United Technologies Corporation |
Fan blade spacer
|
GB201516657D0
(en)
|
2015-09-21 |
2015-11-04 |
Rolls Royce Plc |
Seal-plate anti-rotation in a stage of a gas turbine engine
|
CN106015093B
(zh)
*
|
2016-07-13 |
2018-06-29 |
上海电气燃气轮机有限公司 |
一种压气机动叶轮盘的锁紧结构
|