FR963256A - - Google Patents

Info

Publication number
FR963256A
FR963256A FR963256DA FR963256A FR 963256 A FR963256 A FR 963256A FR 963256D A FR963256D A FR 963256DA FR 963256 A FR963256 A FR 963256A
Authority
FR
France
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
Application number
Other languages
French (fr)
Priority date (The priority date 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 date listed.)
Publication date
Application granted granted Critical
Publication of FR963256A publication Critical patent/FR963256A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
FR963256D 1947-03-14 Expired FR963256A (US07714131-20100511-C00038.png)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB268285X 1947-03-14

Publications (1)

Publication Number Publication Date
FR963256A true FR963256A (US07714131-20100511-C00038.png) 1950-07-05

Family

ID=10249898

Family Applications (1)

Application Number Title Priority Date Filing Date
FR963256D Expired FR963256A (US07714131-20100511-C00038.png) 1947-03-14

Country Status (5)

Country Link
US (1) US2594808A (US07714131-20100511-C00038.png)
BE (1) BE487768A (US07714131-20100511-C00038.png)
CH (1) CH268285A (US07714131-20100511-C00038.png)
FR (1) FR963256A (US07714131-20100511-C00038.png)
GB (1) GB622384A (US07714131-20100511-C00038.png)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
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 (US07714131-20100511-C00038.png) * 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
DE69523545T2 (de) * 1994-12-20 2002-05-29 Gen Electric Verstärkungrahmen für Gasturbinenbrennkammerendstück
WO1998016764A1 (en) * 1996-10-16 1998-04-23 Siemens Westinghouse Power Corporation Brush seal for gas turbine combustor-transition interface
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
WO2009103636A1 (de) * 2008-02-20 2009-08-27 Alstom Technology Ltd. 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)

* Cited by examiner, † Cited by third party
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 (US07714131-20100511-C00038.png) * 1946-03-25

Also Published As

Publication number Publication date
CH268285A (de) 1950-05-15
BE487768A (US07714131-20100511-C00038.png)
US2594808A (en) 1952-04-29
GB622384A (en) 1949-05-02

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