US3536365A
(en)
*
|
1968-05-31 |
1970-10-27 |
Caterpillar Tractor Co |
Sealing means for high speed shafts
|
US3529906A
(en)
*
|
1968-10-30 |
1970-09-22 |
Westinghouse Electric Corp |
Static seal structure
|
BE756582A
(fr)
*
|
1969-10-02 |
1971-03-01 |
Gen Electric |
Ecran circulaire et support d'ecran avec dispositif de reglage de la temperature pour turbomachine
|
GB1308963A
(en)
*
|
1970-05-30 |
1973-03-07 |
Secr Defence |
Gap control apparatus
|
GB1316452A
(en)
*
|
1970-08-14 |
1973-05-09 |
Secr Defence |
Gas turbine engine
|
DE2054926B2
(de)
*
|
1970-11-07 |
1972-02-03 |
Motoren und Turbinen Union München GmbH, 8000 München |
Halterung eines turbinenleitkranzes
|
US3742705A
(en)
*
|
1970-12-28 |
1973-07-03 |
United Aircraft Corp |
Thermal response shroud for rotating body
|
US3807891A
(en)
*
|
1972-09-15 |
1974-04-30 |
United Aircraft Corp |
Thermal response turbine shroud
|
US3893786A
(en)
*
|
1973-06-07 |
1975-07-08 |
Ford Motor Co |
Air cooled shroud for a gas turbine engine
|
GB1484936A
(en)
*
|
1974-12-07 |
1977-09-08 |
Rolls Royce |
Gas turbine engines
|
GB1605255A
(en)
*
|
1975-12-02 |
1986-08-13 |
Rolls Royce |
Clearance control apparatus for bladed fluid flow machine
|
US4213296A
(en)
*
|
1977-12-21 |
1980-07-22 |
United Technologies Corporation |
Seal clearance control system for a gas turbine
|
FR2416345A1
(fr)
*
|
1978-01-31 |
1979-08-31 |
Snecma |
Dispositif de refroidissement par impact des segments d'etancheite de turbine d'un turboreacteur
|
US4251185A
(en)
*
|
1978-05-01 |
1981-02-17 |
Caterpillar Tractor Co. |
Expansion control ring for a turbine shroud assembly
|
US4230439A
(en)
*
|
1978-07-17 |
1980-10-28 |
General Electric Company |
Air delivery system for regulating thermal growth
|
US4230436A
(en)
*
|
1978-07-17 |
1980-10-28 |
General Electric Company |
Rotor/shroud clearance control system
|
US4247248A
(en)
*
|
1978-12-20 |
1981-01-27 |
United Technologies Corporation |
Outer air seal support structure for gas turbine engine
|
DE2907748A1
(de)
*
|
1979-02-28 |
1980-09-04 |
Motoren Turbinen Union |
Einrichtung zur minimierung und konstanthaltung der bei axialturbinen vorhandenen schaufelspitzenspiele, insbesondere fuer gasturbinentriebwerke
|
US4307993A
(en)
*
|
1980-02-25 |
1981-12-29 |
Avco Corporation |
Air-cooled cylinder with piston ring labyrinth
|
GB2119452A
(en)
*
|
1982-04-27 |
1983-11-16 |
Rolls Royce |
Shroud assemblies for axial flow turbomachine rotors
|
FR2540939A1
(fr)
*
|
1983-02-10 |
1984-08-17 |
Snecma |
Anneau d'etancheite pour un rotor de turbine d'une turbomachine et installation de turbomachine munie de tels anneaux
|
US4573866A
(en)
*
|
1983-05-02 |
1986-03-04 |
United Technologies Corporation |
Sealed shroud for rotating body
|
DE3333436C1
(de)
*
|
1983-09-16 |
1985-02-14 |
MTU Motoren- und Turbinen-Union München GmbH, 8000 München |
Einrichtung zur Axial- und Umfangssicherung von statischen Gehaeusebauteilen fuer Stroemungsmaschinen
|
US4643638A
(en)
*
|
1983-12-21 |
1987-02-17 |
United Technologies Corporation |
Stator structure for supporting an outer air seal in a gas turbine engine
|
US4650394A
(en)
*
|
1984-11-13 |
1987-03-17 |
United Technologies Corporation |
Coolable seal assembly for a gas turbine engine
|
US4642024A
(en)
*
|
1984-12-05 |
1987-02-10 |
United Technologies Corporation |
Coolable stator assembly for a rotary machine
|
US4650395A
(en)
*
|
1984-12-21 |
1987-03-17 |
United Technologies Corporation |
Coolable seal segment for a rotary machine
|
US4668164A
(en)
*
|
1984-12-21 |
1987-05-26 |
United Technologies Corporation |
Coolable stator assembly for a gas turbine engine
|
US5601402A
(en)
*
|
1986-06-06 |
1997-02-11 |
The United States Of America As Represented By The Secretary Of The Air Force |
Turbo machine shroud-to-rotor blade dynamic clearance control
|
US4767260A
(en)
*
|
1986-11-07 |
1988-08-30 |
United Technologies Corporation |
Stator vane platform cooling means
|
US5188506A
(en)
*
|
1991-08-28 |
1993-02-23 |
General Electric Company |
Apparatus and method for preventing leakage of cooling air in a shroud assembly of a gas turbine engine
|
US5219268A
(en)
*
|
1992-03-06 |
1993-06-15 |
General Electric Company |
Gas turbine engine case thermal control flange
|
US6877952B2
(en)
*
|
2002-09-09 |
2005-04-12 |
Florida Turbine Technologies, Inc |
Passive clearance control
|
DE102005013796A1
(de)
*
|
2005-03-24 |
2006-09-28 |
Alstom Technology Ltd. |
Wärmestausegment
|
DE102005013797A1
(de)
*
|
2005-03-24 |
2006-09-28 |
Alstom Technology Ltd. |
Wärmestausegment
|
FR2891300A1
(fr)
*
|
2005-09-23 |
2007-03-30 |
Snecma Sa |
Dispositif de controle de jeu dans une turbine a gaz
|
US8826668B2
(en)
*
|
2011-08-02 |
2014-09-09 |
Siemens Energy, Inc. |
Two stage serial impingement cooling for isogrid structures
|
US11761343B2
(en)
*
|
2019-03-13 |
2023-09-19 |
Rtx Corporation |
BOAS carrier with dovetail attachments
|
CN115070662B
(zh)
*
|
2021-03-15 |
2024-01-12 |
中国航发商用航空发动机有限责任公司 |
涡轮盘组件的叶片挡环安装工具
|