|
US4022545A
(en)
*
|
1974-09-11 |
1977-05-10 |
Avco Corporation |
Rooted aerodynamic blade and elastic roll pin damper construction
|
|
US4480958A
(en)
*
|
1983-02-09 |
1984-11-06 |
The United States Of America As Represented By The Secretary Of The Air Force |
High pressure turbine rotor two-piece blade retainer
|
|
US4725200A
(en)
*
|
1987-02-24 |
1988-02-16 |
Westinghouse Electric Corp. |
Apparatus and method for reducing relative motion between blade and rotor in steam turbine
|
|
GB2236809B
(en)
*
|
1989-09-22 |
1994-03-16 |
Rolls Royce Plc |
Improvements in or relating to gas turbine engines
|
|
US5191711A
(en)
*
|
1991-12-23 |
1993-03-09 |
Allied-Signal Inc. |
Compressor or turbine blade manufacture
|
|
US5358262A
(en)
*
|
1992-10-09 |
1994-10-25 |
Rolls-Royce, Inc. |
Multi-layer seal member
|
|
US5605438A
(en)
|
1995-12-29 |
1997-02-25 |
General Electric Co. |
Casing distortion control for rotating machinery
|
|
US5630700A
(en)
*
|
1996-04-26 |
1997-05-20 |
General Electric Company |
Floating vane turbine nozzle
|
|
US6126389A
(en)
|
1998-09-02 |
2000-10-03 |
General Electric Co. |
Impingement cooling for the shroud of a gas turbine
|
|
US6190120B1
(en)
|
1999-05-14 |
2001-02-20 |
General Electric Co. |
Partially turbulated trailing edge cooling passages for gas turbine nozzles
|
|
US6446979B1
(en)
*
|
1999-07-09 |
2002-09-10 |
The United States Of America As Represented By The United States National Aeronautics And Space Administration |
Rocket motor joint construction including thermal barrier
|
|
US6343911B1
(en)
|
2000-04-05 |
2002-02-05 |
General Electric Company |
Side wall cooling for nozzle segments for a gas turbine
|
|
US6331096B1
(en)
|
2000-04-05 |
2001-12-18 |
General Electric Company |
Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment
|
|
US6386825B1
(en)
|
2000-04-11 |
2002-05-14 |
General Electric Company |
Apparatus and methods for impingement cooling of a side wall of a turbine nozzle segment
|
|
US6453557B1
(en)
|
2000-04-11 |
2002-09-24 |
General Electric Company |
Method of joining a vane cavity insert to a nozzle segment of a gas turbine
|
|
US6419445B1
(en)
|
2000-04-11 |
2002-07-16 |
General Electric Company |
Apparatus for impingement cooling a side wall adjacent an undercut region of a turbine nozzle segment
|
|
US6418618B1
(en)
|
2000-04-11 |
2002-07-16 |
General Electric Company |
Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling
|
|
US6375415B1
(en)
|
2000-04-25 |
2002-04-23 |
General Electric Company |
Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment
|
|
US6390769B1
(en)
|
2000-05-08 |
2002-05-21 |
General Electric Company |
Closed circuit steam cooled turbine shroud and method for steam cooling turbine shroud
|
|
US6435814B1
(en)
|
2000-05-16 |
2002-08-20 |
General Electric Company |
Film cooling air pocket in a closed loop cooled airfoil
|
|
US6402466B1
(en)
|
2000-05-16 |
2002-06-11 |
General Electric Company |
Leaf seal for gas turbine stator shrouds and a nozzle band
|
|
US6422810B1
(en)
|
2000-05-24 |
2002-07-23 |
General Electric Company |
Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
|
|
US6413040B1
(en)
|
2000-06-13 |
2002-07-02 |
General Electric Company |
Support pedestals for interconnecting a cover and nozzle band wall in a gas turbine nozzle segment
|
|
US6464453B2
(en)
*
|
2000-12-04 |
2002-10-15 |
General Electric Company |
Turbine interstage sealing ring
|
|
US6375429B1
(en)
*
|
2001-02-05 |
2002-04-23 |
General Electric Company |
Turbomachine blade-to-rotor sealing arrangement
|
|
US6398489B1
(en)
|
2001-02-08 |
2002-06-04 |
General Electric Company |
Airfoil shape for a turbine nozzle
|
|
US6464456B2
(en)
*
|
2001-03-07 |
2002-10-15 |
General Electric Company |
Turbine vane assembly including a low ductility vane
|