US4033705A
(en)
*
|
1976-04-26 |
1977-07-05 |
The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration |
Blade retainer assembly
|
FR2404212A1
(fr)
*
|
1977-09-23 |
1979-04-20 |
Snecma |
Dispositif d'equilibrage d'un rotor
|
US4275990A
(en)
*
|
1977-12-17 |
1981-06-30 |
Rolls-Royce Limited |
Disc channel for cooling rotor blade roots
|
US4221542A
(en)
*
|
1977-12-27 |
1980-09-09 |
General Electric Company |
Segmented blade retainer
|
GB2054058B
(en)
*
|
1979-06-16 |
1983-04-20 |
Rolls Royce |
Reducing rotor noise
|
US4344740A
(en)
*
|
1979-09-28 |
1982-08-17 |
United Technologies Corporation |
Rotor assembly
|
US4347040A
(en)
*
|
1980-10-02 |
1982-08-31 |
United Technologies Corporation |
Blade to blade vibration damper
|
USRE32339E
(en)
*
|
1980-10-02 |
1987-01-27 |
United Technologies Corporation |
Blade to blade vibration damper
|
FR2499652A1
(fr)
*
|
1981-02-11 |
1982-08-13 |
Snecma |
Dispositif de correction de balourd de rotor de turbomachines
|
US4355957A
(en)
*
|
1981-06-18 |
1982-10-26 |
United Technologies Corporation |
Blade damper
|
US4477226A
(en)
*
|
1983-05-09 |
1984-10-16 |
General Electric Company |
Balance for rotating member
|
US4926710A
(en)
*
|
1987-09-08 |
1990-05-22 |
United Technologies Corporation |
Method of balancing bladed gas turbine engine rotor
|
US4848182A
(en)
*
|
1987-09-08 |
1989-07-18 |
United Technologies Corporation |
Rotor balance system
|
US4803893A
(en)
*
|
1987-09-24 |
1989-02-14 |
United Technologies Corporation |
High speed rotor balance system
|
US4898514A
(en)
*
|
1987-10-27 |
1990-02-06 |
United Technologies Corporation |
Turbine balance arrangement with integral air passage
|
FR2639402B1
(fr)
*
|
1988-11-23 |
1990-12-28 |
Snecma |
Disque ailete de rotor de turbomachine
|
US4890981A
(en)
*
|
1988-12-30 |
1990-01-02 |
General Electric Company |
Boltless rotor blade retainer
|
US5018943A
(en)
*
|
1989-04-17 |
1991-05-28 |
General Electric Company |
Boltless balance weight for turbine rotors
|
DE4136293B4
(de)
*
|
1990-11-03 |
2004-08-26 |
Papst Licensing Gmbh & Co. Kg |
Laufrad für ein Gebläse, insbesondere Radialgebläse
|
US5151013A
(en)
*
|
1990-12-27 |
1992-09-29 |
United Technologies Corporation |
Blade lock for a rotor disk and rotor blade assembly
|
GB9302064D0
(en)
*
|
1993-02-03 |
1993-03-24 |
Rolls Royce Plc |
Balanced rotor
|
US5350279A
(en)
*
|
1993-07-02 |
1994-09-27 |
General Electric Company |
Gas turbine engine blade retainer sub-assembly
|
FR2716931B1
(fr)
*
|
1994-03-03 |
1996-04-05 |
Snecma |
Système d'équilibrage et d'amortissement d'un dique de turbomachine.
|
US6494679B1
(en)
*
|
1999-08-05 |
2002-12-17 |
General Electric Company |
Apparatus and method for rotor damping
|
US6390777B1
(en)
|
1999-09-01 |
2002-05-21 |
Angelo Fan Brace Licensing, L.L.C. |
Quick-connect fan blade mounting assembly
|
US6951448B2
(en)
*
|
2002-04-16 |
2005-10-04 |
United Technologies Corporation |
Axial retention system and components thereof for a bladed rotor
|
US6908285B2
(en)
*
|
2003-04-08 |
2005-06-21 |
General Electric Company |
Methods and apparatus for assembling rotatable machines
|
US6976827B2
(en)
*
|
2003-10-14 |
2005-12-20 |
Pratt & Whitney Canada Corp. |
Rotor balancing device and method
|
FR2866057B1
(fr)
*
|
2004-02-06 |
2006-04-28 |
Snecma Moteurs |
Dispositif d'equilibrage d'un disque de rotor, disque equipe d'un tel dispositif, et rotor ayant un tel disque
|
US7287958B2
(en)
*
|
2005-01-10 |
2007-10-30 |
General Electric Company |
Methods and apparatus for assembling rotatable machines
|
US7530791B2
(en)
*
|
2005-12-22 |
2009-05-12 |
Pratt & Whitney Canada Corp. |
Turbine blade retaining apparatus
|
JP2007247406A
(ja)
*
|
2006-03-13 |
2007-09-27 |
Ihi Corp |
ファンブレードの保持構造
|
FR2918106B1
(fr)
*
|
2007-06-27 |
2011-05-06 |
Snecma |
Dispositif de retenue axiale d'aubes montees sur un disque de rotor de turbomachine.
|
DE102007059220A1
(de)
*
|
2007-12-07 |
2009-06-10 |
Rolls-Royce Deutschland Ltd & Co Kg |
Leitschaufelkranz für thermische Strömungsmaschinen, insbesondere Flugtriebwerke
|
FR2939832B1
(fr)
*
|
2008-12-11 |
2011-01-07 |
Turbomeca |
Roue de turbine equipee d'un dispositif de retenue axiale verrouillant des pales par rapport a un disque.
|
FR2951224B1
(fr)
*
|
2009-10-13 |
2011-12-09 |
Turbomeca |
Roue de turbine equipee d'un jonc de retenue axiale verrouillant des pales par rapport a un disque
|
RU2516722C1
(ru)
*
|
2012-11-15 |
2014-05-20 |
Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" |
Ротор с компенсатором дисбаланса
|
US9404367B2
(en)
*
|
2012-11-21 |
2016-08-02 |
Solar Turbines Incorporated |
Gas turbine engine compressor rotor assembly and balancing system
|
FR3000763B1
(fr)
*
|
2013-01-04 |
2016-07-15 |
Snecma |
Disque de rotor muni d’une pluralite de crochets
|
EP3006667A1
(fr)
*
|
2014-10-09 |
2016-04-13 |
Siemens Aktiengesellschaft |
Aube directrice de turbine, système composé d'un arbre de turbine, d'un disque de roue de turbine, d'une multitude d'aubes directrices de turbines, ainsi que d'un équilibrage et d'une turbine
|
US10436224B2
(en)
|
2016-04-01 |
2019-10-08 |
General Electric Company |
Method and apparatus for balancing a rotor
|
US10883370B2
(en)
*
|
2018-08-14 |
2021-01-05 |
Raytheon Technologies Corporation |
Dovetail weight system for rotor balance
|
CN112160794B
(zh)
*
|
2020-09-18 |
2023-02-17 |
中国航发四川燃气涡轮研究院 |
定位组件及其涡轮盘或压气机盘、航空发动机
|
RU209925U1
(ru)
*
|
2021-12-27 |
2022-03-23 |
Публичное Акционерное Общество "Одк-Сатурн" |
Узел ротора турбины большой мощности
|