CH309297A - Combustion device in gas turbine plants. - Google Patents

Combustion device in gas turbine plants.

Info

Publication number
CH309297A
CH309297A CH309297DA CH309297A CH 309297 A CH309297 A CH 309297A CH 309297D A CH309297D A CH 309297DA CH 309297 A CH309297 A CH 309297A
Authority
CH
Switzerland
Prior art keywords
gas turbine
combustion device
turbine plants
plants
combustion
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH309297A publication Critical patent/CH309297A/en

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH309297D 1952-02-01 1953-01-30 Combustion device in gas turbine plants. CH309297A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2793/52A GB715909A (en) 1952-02-01 1952-02-01 Improvements in or relating to combustion equipment of gas-turbine engines

Publications (1)

Publication Number Publication Date
CH309297A true CH309297A (en) 1955-08-31

Family

ID=9746016

Family Applications (1)

Application Number Title Priority Date Filing Date
CH309297D CH309297A (en) 1952-02-01 1953-01-30 Combustion device in gas turbine plants.

Country Status (4)

Country Link
US (1) US2720080A (en)
CH (1) CH309297A (en)
FR (1) FR1073579A (en)
GB (1) GB715909A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1062985B (en) * 1955-12-30 1959-08-06 United Aircraft Corp Combustion chamber for turbo-jet engines
DE1177415B (en) * 1960-05-16 1964-09-03 Gen Electric Gas turbine combustion chamber with a flow channel which is formed by an outer wall and an inner wall that is coaxial with it

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB736823A (en) * 1953-01-19 1955-09-14 Lucas Industries Ltd Engine combustion chambers
DE1096682B (en) * 1959-08-26 1961-01-05 Entwicklungsbau Pirna Veb Annular combustion chamber for gas turbines
GB1021588A (en) * 1963-12-04 1966-03-02 Rolls Royce Combustion equipment for a gas turbine engine
US3512359A (en) * 1968-05-24 1970-05-19 Gen Electric Dummy swirl cup combustion chamber
US3670497A (en) * 1970-09-02 1972-06-20 United Aircraft Corp Combustion chamber support
US3978664A (en) * 1974-12-20 1976-09-07 United Technologies Corporation Gas turbine engine diffuser
US4098074A (en) * 1976-06-01 1978-07-04 United Technologies Corporation Combustor diffuser for turbine type power plant and construction thereof
GB2097112B (en) * 1981-04-16 1984-12-12 Rolls Royce Fuel burners and combustion equipment for use in gas turbine engines
GB2134243A (en) * 1983-01-27 1984-08-08 Rolls Royce Combustion equipment for a gas turbine engine
GB2135440B (en) * 1983-02-19 1986-06-25 Rolls Royce Mounting combustion chambers
US4628694A (en) * 1983-12-19 1986-12-16 General Electric Company Fabricated liner article and method
US4785623A (en) * 1987-12-09 1988-11-22 United Technologies Corporation Combustor seal and support
DE58907451D1 (en) * 1988-10-12 1994-05-19 Ruhrgas Ag Burners, especially high speed burners.
FR2686683B1 (en) * 1992-01-28 1994-04-01 Snecma TURBOMACHINE WITH REMOVABLE COMBUSTION CHAMBER.
FR2706534B1 (en) * 1993-06-10 1995-07-21 Snecma Multiflux diffuser-separator with integrated rectifier for turbojet.
US8800290B2 (en) * 2007-12-18 2014-08-12 United Technologies Corporation Combustor
US8448444B2 (en) * 2011-02-18 2013-05-28 General Electric Company Method and apparatus for mounting transition piece in combustor
EP2864702B1 (en) * 2012-06-22 2017-02-22 Ferndale Investments Pty Ltd A heating torch
US9273868B2 (en) * 2013-08-06 2016-03-01 General Electric Company System for supporting bundled tube segments within a combustor
GB201408690D0 (en) * 2014-05-16 2014-07-02 Rolls Royce Plc A combustion chamber arrangement
US20160223196A1 (en) * 2015-02-02 2016-08-04 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Crude Oil Spray Combustor
GB201505502D0 (en) 2015-03-31 2015-05-13 Rolls Royce Plc Combustion equipment

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB620270A (en) * 1945-11-20 1949-03-22 Westinghouse Electric Int Co Improvements in or relating to turbine apparatus
US2552851A (en) * 1949-10-25 1951-05-15 Westinghouse Electric Corp Combustion chamber with retrorse baffles for preheating the fuelair mixture

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1062985B (en) * 1955-12-30 1959-08-06 United Aircraft Corp Combustion chamber for turbo-jet engines
DE1177415B (en) * 1960-05-16 1964-09-03 Gen Electric Gas turbine combustion chamber with a flow channel which is formed by an outer wall and an inner wall that is coaxial with it

Also Published As

Publication number Publication date
US2720080A (en) 1955-10-11
GB715909A (en) 1954-09-22
FR1073579A (en) 1954-09-27

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