FR1073579A - Improvements to the combustion equipment of gas turbine engines - Google Patents

Improvements to the combustion equipment of gas turbine engines

Info

Publication number
FR1073579A
FR1073579A FR1073579DA FR1073579A FR 1073579 A FR1073579 A FR 1073579A FR 1073579D A FR1073579D A FR 1073579DA FR 1073579 A FR1073579 A FR 1073579A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
combustion equipment
combustion
equipment
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
Application number
Other languages
French (fr)
Inventor
George Oulianoff
Jeffrey Evans
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1073579A publication Critical patent/FR1073579A/en
Expired legal-status Critical Current

Links

Classifications

    • 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

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)
FR1073579D 1952-02-01 1953-01-27 Improvements to the combustion equipment of gas turbine engines Expired FR1073579A (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
FR1073579A true FR1073579A (en) 1954-09-27

Family

ID=9746016

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1073579D Expired FR1073579A (en) 1952-02-01 1953-01-27 Improvements to the combustion equipment of gas turbine engines

Country Status (4)

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

Families Citing this family (24)

* 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
US2852914A (en) * 1955-12-30 1958-09-23 United Aircraft Corp Combustion chamber support means
DE1096682B (en) * 1959-08-26 1961-01-05 Entwicklungsbau Pirna Veb Annular combustion chamber for gas turbines
US3049882A (en) * 1960-05-16 1962-08-21 Gen Electric Combustor construction with means for prevention of hot streaks
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
EP0363834B1 (en) * 1988-10-12 1994-04-13 Ruhrgas Aktiengesellschaft Burner, particularly a high-speed burner
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
US10260742B2 (en) * 2012-06-22 2019-04-16 Ferndale Investments Pty Ltd 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

Also Published As

Publication number Publication date
CH309297A (en) 1955-08-31
GB715909A (en) 1954-09-22
US2720080A (en) 1955-10-11

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