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FR2415723A1 - Perfectionnements aux turbomachines - Google Patents

Perfectionnements aux turbomachines

Info

Publication number
FR2415723A1
FR2415723A1 FR7902017A FR7902017A FR2415723A1 FR 2415723 A1 FR2415723 A1 FR 2415723A1 FR 7902017 A FR7902017 A FR 7902017A FR 7902017 A FR7902017 A FR 7902017A FR 2415723 A1 FR2415723 A1 FR 2415723A1
Authority
FR
France
Prior art keywords
annular
walls
forming
chamber
turbomachine
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.)
Granted
Application number
FR7902017A
Other languages
English (en)
Other versions
FR2415723B1 (fr
Inventor
Arthur Sotheran
David Harding Parnell
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
Publication of FR2415723A1 publication Critical patent/FR2415723A1/fr
Application granted granted Critical
Publication of FR2415723B1 publication Critical patent/FR2415723B1/fr
Granted legal-status Critical Current

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)

Abstract

L'invention concerne une turbomachine comportant une chambre de combustion annulaire. Cette chambre comprend des parois annulaires 15, 16 s'étendant dans la direction de l'axe 13A de la chambre et formant un conduit annulaire de pré-mélange 33 ayant à une de ses extrémités axiales une entrée d'air annulaire 30 et ayant à son autre extrémité axiale une rangés annulaire de sorties 35, des parois 14A, 17A formant la zone principale de la chambre disposées en série avec le conduit et des parois formant deux zones pilotes annulaires situées respectivement radialement à l'intérieur et à l'extérieur dudit conduit.
FR7902017A 1978-01-28 1979-01-26 Perfectionnements aux turbomachines Granted FR2415723A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB354878 1978-01-28

Publications (2)

Publication Number Publication Date
FR2415723A1 true FR2415723A1 (fr) 1979-08-24
FR2415723B1 FR2415723B1 (fr) 1982-10-15

Family

ID=9760413

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7902017A Granted FR2415723A1 (fr) 1978-01-28 1979-01-26 Perfectionnements aux turbomachines

Country Status (5)

Country Link
US (1) US4249373A (fr)
JP (1) JPS5826499B2 (fr)
DE (1) DE2902707C2 (fr)
FR (1) FR2415723A1 (fr)
IT (1) IT1109876B (fr)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2043868B (en) * 1979-03-08 1982-12-15 Rolls Royce Gas turbine
US4474014A (en) * 1981-09-17 1984-10-02 United Technologies Corporation Partially unshrouded swirler for combustion chambers
CH672366A5 (fr) * 1986-12-09 1989-11-15 Bbc Brown Boveri & Cie
JPH0684817B2 (ja) * 1988-08-08 1994-10-26 株式会社日立製作所 ガスタービン燃焼器及びその運転方法
JPH0772616B2 (ja) * 1989-05-24 1995-08-02 株式会社日立製作所 燃焼器及びその運転方法
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor
US5220795A (en) * 1991-04-16 1993-06-22 General Electric Company Method and apparatus for injecting dilution air
US5421158A (en) * 1994-10-21 1995-06-06 General Electric Company Segmented centerbody for a double annular combustor
US5970716A (en) 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits
US7861532B2 (en) * 2007-06-26 2011-01-04 General Electric Company System and methods for heat recovery steam generators hot purging
US9121613B2 (en) * 2012-06-05 2015-09-01 General Electric Company Combustor with brief quench zone with slots
US10767865B2 (en) * 2016-06-13 2020-09-08 Rolls-Royce North American Technologies Inc. Swirl stabilized vaporizer combustor

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1094619A (fr) * 1955-05-23
US3228451A (en) * 1957-06-25 1966-01-11 Urquhart S 1926 Ltd Method of burning fuels
FR2295235A1 (fr) * 1974-12-18 1976-07-16 United Technologies Corp Chambre de combustion

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB650608A (en) * 1948-11-26 1951-02-28 Lucas Ltd Joseph Improvements relating to internal combustion engine systems
DE959694C (de) * 1952-12-20 1957-03-07 Armstrong Siddeley Motors Ltd Verdampfer und Brenner fuer fluessige Brennstoffe, insbesondere fuer Gasturbinen und Strahltriebwerke
US2931174A (en) * 1952-12-20 1960-04-05 Armstrong Siddeley Motors Ltd Vaporizer for liquid fuel
DE1097213B (de) * 1958-05-22 1961-01-12 Rolls Royce Verbrennungsanlage fuer Gasturbinentriebwerke
GB1136543A (en) * 1966-02-21 1968-12-11 Rolls Royce Liquid fuel combustion apparatus for gas turbine engines

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1094619A (fr) * 1955-05-23
US3228451A (en) * 1957-06-25 1966-01-11 Urquhart S 1926 Ltd Method of burning fuels
FR2295235A1 (fr) * 1974-12-18 1976-07-16 United Technologies Corp Chambre de combustion

Also Published As

Publication number Publication date
IT7919648A0 (it) 1979-01-26
JPS5826499B2 (ja) 1983-06-03
FR2415723B1 (fr) 1982-10-15
DE2902707A1 (de) 1979-08-02
JPS54111007A (en) 1979-08-31
DE2902707C2 (de) 1982-10-21
IT1109876B (it) 1985-12-23
US4249373A (en) 1981-02-10

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Legal Events

Date Code Title Description
ST Notification of lapse