CH309674A - Installation de turbine à gaz. - Google Patents

Installation de turbine à gaz.

Info

Publication number
CH309674A
CH309674A CH309674DA CH309674A CH 309674 A CH309674 A CH 309674A CH 309674D A CH309674D A CH 309674DA CH 309674 A CH309674 A CH 309674A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine installation
installation
gas
turbine
Prior art date
Application number
Other languages
English (en)
Inventor
Boyd Winnett
Thompson Purvis Joseph
Original Assignee
Canadian Patents Dev
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.)
Filing date
Publication date
Application filed by Canadian Patents Dev filed Critical Canadian Patents Dev
Publication of CH309674A publication Critical patent/CH309674A/fr

Links

Classifications

    • 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
    • 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
    • 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
CH309674D 1949-12-24 1950-12-22 Installation de turbine à gaz. CH309674A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US134894A US2608057A (en) 1949-12-24 1949-12-24 Gas turbine nozzle box

Publications (1)

Publication Number Publication Date
CH309674A true CH309674A (fr) 1955-09-15

Family

ID=22465495

Family Applications (1)

Application Number Title Priority Date Filing Date
CH309674D CH309674A (fr) 1949-12-24 1950-12-22 Installation de turbine à gaz.

Country Status (5)

Country Link
US (1) US2608057A (fr)
CH (1) CH309674A (fr)
DE (1) DE874680C (fr)
FR (1) FR1030068A (fr)
GB (1) GB682128A (fr)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2743579A (en) * 1950-11-02 1956-05-01 Gen Motors Corp Gas turbine engine with turbine nozzle cooled by combustion chamber jacket air
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
US2848191A (en) * 1951-11-03 1958-08-19 A V Roe Canada Ltd Nozzle box
US2710503A (en) * 1952-04-08 1955-06-14 A V Roe Canada Ltd Nozzle box attachment
US3018624A (en) * 1954-03-02 1962-01-30 Bristol Siddeley Engines Ltd Flame tubes for use in combustion systems of gas turbine engines
DE1055884B (de) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flammrohr fuer eine Brennkammer eines Gasturbinenmotors
US3152443A (en) * 1959-07-17 1964-10-13 United Aircraft Canada Gas turbine powerplant
GB1086432A (en) * 1965-09-21 1967-10-11 Bristol Siddeley Engines Ltd Gas turbine engines
US3657882A (en) * 1970-11-13 1972-04-25 Westinghouse Electric Corp Combustion apparatus
US4109864A (en) * 1976-12-23 1978-08-29 General Electric Company Coolant flow metering device
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
DE69306025T2 (de) * 1992-03-30 1997-05-28 Gen Electric Konstruktion eines Brennkammerdomes
DE4304989A1 (de) * 1993-02-18 1994-08-25 Abb Management Ag Verfahren zur Kühlung einer Gasturbinenanlage
US5414999A (en) * 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
GB2293232B (en) * 1994-09-15 1998-05-20 Rolls Royce Plc A combustion chamber assembly
EP0718468B1 (fr) * 1994-12-20 2001-10-31 General Electric Company Cadre de renforcement pour un élément de transition d'une chambre de combustion
GB2300909B (en) * 1995-05-18 1998-09-30 Europ Gas Turbines Ltd A gas turbine gas duct arrangement
US6116013A (en) * 1998-01-02 2000-09-12 Siemens Westinghouse Power Corporation Bolted gas turbine combustor transition coupling
DE10032454A1 (de) * 2000-07-04 2002-01-17 Man Turbomasch Ag Ghh Borsig Vorrichtung zum Kühlen eines ungleichmäßig stark temperaturbelasteten Bauteiles
JP2002243154A (ja) 2001-02-16 2002-08-28 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器
US20100050640A1 (en) * 2008-08-29 2010-03-04 General Electric Company Thermally compliant combustion cap device and system
US8381526B2 (en) * 2010-02-15 2013-02-26 General Electric Company Systems and methods of providing high pressure air to a head end of a combustor
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
WO2013157976A1 (fr) * 2012-04-19 2013-10-24 General Electric Company Butée de chemise de chambre de combustion
US9322335B2 (en) 2013-03-15 2016-04-26 Siemens Energy, Inc. Gas turbine combustor exit piece with hinged connections
US9470422B2 (en) 2013-10-22 2016-10-18 Siemens Energy, Inc. Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier
US10024180B2 (en) * 2014-11-20 2018-07-17 Siemens Energy, Inc. Transition duct arrangement in a gas turbine engine
US10125634B2 (en) * 2015-12-10 2018-11-13 General Electric Company Combustor assembly alignment and securement systems

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR742787A (fr) * 1931-09-14 1933-03-15
US2414551A (en) * 1941-07-21 1947-01-21 Northrop Aircraft Inc Compressor
GB589541A (en) * 1941-09-22 1947-06-24 Hayne Constant Improvements in axial flow turbines, compressors and the like
US2479573A (en) * 1943-10-20 1949-08-23 Gen Electric Gas turbine power plant
GB615915A (en) * 1946-03-25 1949-01-13 George Oulianoff Improvements in or relating to jet-propulsion and gas-turbine power-units
BE487120A (fr) * 1946-03-25
FR962862A (fr) * 1946-10-26 1950-06-22
US2564218A (en) * 1947-03-04 1951-08-14 Power Jets Res & Dev Ltd Combustion chamber and diffusion nozzle arrangement for reducing over-all length of jet engines
US2548886A (en) * 1947-10-25 1951-04-17 Gen Electric Gas turbine power plant with axial flow compressor
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
US2565843A (en) * 1949-06-02 1951-08-28 Elliott Co Multiple tubular combustion chamber

Also Published As

Publication number Publication date
GB682128A (en) 1952-11-05
US2608057A (en) 1952-08-26
FR1030068A (fr) 1953-06-09
DE874680C (de) 1953-04-27

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