GB622384A - Improvements relating to gas turbine engines - Google Patents
Improvements relating to gas turbine enginesInfo
- Publication number
- GB622384A GB622384A GB7219/47A GB721947A GB622384A GB 622384 A GB622384 A GB 622384A GB 7219/47 A GB7219/47 A GB 7219/47A GB 721947 A GB721947 A GB 721947A GB 622384 A GB622384 A GB 622384A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- flanges
- rings
- ring piece
- intermediate part
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB268285X | 1947-03-14 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB622384A true GB622384A (en) | 1949-05-02 |
Family
ID=10249898
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7219/47A Expired GB622384A (en) | 1947-03-14 | 1947-03-14 | Improvements relating to gas turbine engines |
Country Status (5)
Country | Link |
---|---|
US (1) | US2594808A (xx) |
BE (1) | BE487768A (xx) |
CH (1) | CH268285A (xx) |
FR (1) | FR963256A (xx) |
GB (1) | GB622384A (xx) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998016764A1 (en) * | 1996-10-16 | 1998-04-23 | Siemens Westinghouse Power Corporation | Brush seal for gas turbine combustor-transition interface |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2836959A (en) * | 1950-01-11 | 1958-06-03 | Gen Motors Corp | Gas turbine engine supporting frame |
US2702454A (en) * | 1951-06-07 | 1955-02-22 | United Aircraft Corp | Transition piece providing a connection between the combustion chambers and the turbine nozzle in gas turbine power plants |
NL267395A (xx) * | 1960-07-22 | |||
US3116604A (en) * | 1962-05-17 | 1964-01-07 | Gen Electric | Engine exhaust system |
US3750398A (en) * | 1971-05-17 | 1973-08-07 | Westinghouse Electric Corp | Static seal structure |
US4573315A (en) * | 1984-05-15 | 1986-03-04 | A/S Kongsberg Vapenfabrikk | Low pressure loss, convectively gas-cooled inlet manifold for high temperature radial turbine |
US5414999A (en) * | 1993-11-05 | 1995-05-16 | General Electric Company | Integral aft frame mount for a gas turbine combustor transition piece |
EP0718468B1 (en) * | 1994-12-20 | 2001-10-31 | General Electric Company | Transition piece frame support |
US6116013A (en) * | 1998-01-02 | 2000-09-12 | Siemens Westinghouse Power Corporation | Bolted gas turbine combustor transition coupling |
US6886343B2 (en) * | 2003-01-15 | 2005-05-03 | General Electric Company | Methods and apparatus for controlling engine clearance closures |
EP2245374B1 (de) * | 2008-02-20 | 2017-11-15 | General Electric Technology GmbH | Thermische maschine |
US8616007B2 (en) * | 2009-01-22 | 2013-12-31 | Siemens Energy, Inc. | Structural attachment system for transition duct outlet |
JP2012145098A (ja) * | 2010-12-21 | 2012-08-02 | Toshiba Corp | トランジションピースおよびガスタービン |
US8938976B2 (en) * | 2011-05-20 | 2015-01-27 | Siemens Energy, Inc. | Structural frame for gas turbine combustion cap assembly |
US9404421B2 (en) | 2014-01-23 | 2016-08-02 | Siemens Energy, Inc. | Structural support bracket for gas flow path |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2445114A (en) * | 1948-07-13 | Arrangement of jet propulsion | ||
US1794454A (en) * | 1928-09-08 | 1931-03-03 | Huron Ind Inc | Sealing ring for rotating machines or cylinders |
US1852279A (en) * | 1929-05-16 | 1932-04-05 | Superheater Co Ltd | Means for securing tubes to headers |
US2479573A (en) * | 1943-10-20 | 1949-08-23 | Gen Electric | Gas turbine power plant |
BE487120A (xx) * | 1946-03-25 |
-
0
- FR FR963256D patent/FR963256A/fr not_active Expired
- BE BE487768D patent/BE487768A/xx unknown
-
1947
- 1947-03-14 GB GB7219/47A patent/GB622384A/en not_active Expired
-
1948
- 1948-03-08 US US13689A patent/US2594808A/en not_active Expired - Lifetime
- 1948-03-12 CH CH268285D patent/CH268285A/de unknown
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1998016764A1 (en) * | 1996-10-16 | 1998-04-23 | Siemens Westinghouse Power Corporation | Brush seal for gas turbine combustor-transition interface |
Also Published As
Publication number | Publication date |
---|---|
FR963256A (xx) | 1950-07-05 |
CH268285A (de) | 1950-05-15 |
US2594808A (en) | 1952-04-29 |
BE487768A (xx) |
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