JPS5181216A - - Google Patents

Info

Publication number
JPS5181216A
JPS5181216A JP50138791A JP13879175A JPS5181216A JP S5181216 A JPS5181216 A JP S5181216A JP 50138791 A JP50138791 A JP 50138791A JP 13879175 A JP13879175 A JP 13879175A JP S5181216 A JPS5181216 A JP S5181216A
Authority
JP
Japan
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
JP50138791A
Other versions
JPS5916170B2 (ja
Inventor
Uiriamu Budoiatsuku Jon
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JPS5181216A publication Critical patent/JPS5181216A/ja
Publication of JPS5916170B2 publication Critical patent/JPS5916170B2/ja
Expired 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP50138791A 1975-01-08 1975-11-20 アフタバ−ナホエンソウチ Expired JPS5916170B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/539,315 US3931707A (en) 1975-01-08 1975-01-08 Augmentor flameholding apparatus

Publications (2)

Publication Number Publication Date
JPS5181216A true JPS5181216A (ja) 1976-07-16
JPS5916170B2 JPS5916170B2 (ja) 1984-04-13

Family

ID=24150705

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50138791A Expired JPS5916170B2 (ja) 1975-01-08 1975-11-20 アフタバ−ナホエンソウチ

Country Status (8)

Country Link
US (1) US3931707A (ja)
JP (1) JPS5916170B2 (ja)
BE (1) BE837339A (ja)
CA (1) CA1050286A (ja)
DE (1) DE2551005A1 (ja)
FR (1) FR2297327A1 (ja)
GB (1) GB1522826A (ja)
IT (1) IT1049017B (ja)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4064691A (en) * 1975-11-04 1977-12-27 General Electric Company Cooling of fastener means for a removable flameholder
FR2351258A1 (fr) * 1976-05-13 1977-12-09 Snecma Dispositif d'allumage de carburant injecte dans un milieu gazeux en ecoulement rapide
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
US4203285A (en) * 1978-02-06 1980-05-20 The United States Of America As Represented By The Secretary Of The Air Force Partial swirl augmentor for a turbofan engine
US4185458A (en) * 1978-05-11 1980-01-29 The United States Of America As Represented By The Secretary Of The Air Force Turbofan augmentor flameholder
FR2429326A1 (fr) * 1978-06-22 1980-01-18 Snecma Perfectionnements aux dispositifs accroche-flammes pour chambres de combustion, notamment pour canaux de post-combustion de turboreacteurs
FR2551500B1 (fr) * 1983-09-07 1985-11-08 Snecma Anneau-bruleur pour postcombustion de moteur a reaction
JPS61218198A (ja) * 1985-03-25 1986-09-27 株式会社日立製作所 表示装置付制御基板
FR2594939B1 (fr) * 1986-02-27 1989-11-03 Snecma Structure d'accroche-flamme pour systeme de rechauffe de turboreacteur
US5076062A (en) * 1987-11-05 1991-12-31 General Electric Company Gas-cooled flameholder assembly
US4893468A (en) * 1987-11-30 1990-01-16 General Electric Company Emissions control for gas turbine engine
US4901527A (en) * 1988-02-18 1990-02-20 General Electric Company Low turbulence flame holder mount
IL93630A0 (en) * 1989-03-27 1990-12-23 Gen Electric Flameholder for gas turbine engine afterburner
US5142858A (en) * 1990-11-21 1992-09-01 General Electric Company Compact flameholder type combustor which is staged to reduce emissions
US5491974A (en) * 1993-04-15 1996-02-20 General Electric Company Removable afterburner flameholder
US5685142A (en) * 1996-04-10 1997-11-11 United Technologies Corporation Gas turbine engine afterburner
FR2873168B1 (fr) * 2004-07-16 2008-10-31 Snecma Moteurs Sa Turboreacteur comprenant une chambre de post-combustion a allumage securise
US7647775B2 (en) * 2005-06-30 2010-01-19 United Technologies Corporation Augmentor spray bars
US7565804B1 (en) * 2006-06-29 2009-07-28 General Electric Company Flameholder fuel shield
US7581398B2 (en) * 2006-06-29 2009-09-01 General Electric Company Purged flameholder fuel shield
US7568346B2 (en) * 2006-10-31 2009-08-04 General Electric Company Method and apparatus for assembling a flameholder for an augmenter
US8209987B2 (en) * 2008-11-26 2012-07-03 United Technologies Corporation Augmentor pilot
US9879862B2 (en) 2013-03-08 2018-01-30 Rolls-Royce North American Technologies, Inc. Gas turbine engine afterburner
US9366184B2 (en) * 2013-06-18 2016-06-14 General Electric Company Gas turbine engine and method of operating thereof
GB2524782B (en) * 2014-04-02 2016-04-20 Verderg Ltd Turbine assembly
JP6229590B2 (ja) * 2014-04-30 2017-11-15 株式会社Ihi アフタバーナ及び航空機エンジン
JP6245057B2 (ja) * 2014-04-30 2017-12-13 株式会社Ihi アフタバーナ及び航空機エンジン
FR3039220B1 (fr) * 2015-07-24 2017-08-11 Snecma Dipositif de postcombustion pour turboreacteur
RU2666835C1 (ru) * 2017-06-20 2018-09-12 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Способ работы форсажного комплекса турбореактивного двигателя (ТРД) и форсажный комплекс, работающий этим способом (варианты), способ работы ТРД и ТРД, работающий этим способом
RU2656525C1 (ru) * 2017-06-20 2018-06-05 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Способ работы форсажного комплекса турбореактивного двигателя (ТРД) и форсажный комплекс, работающий этим способом, способ работы насоса форсажного и насос форсажный, работающий этим способом, способ работы ТРД и ТРД, работающий этим способом
RU2682220C1 (ru) * 2018-03-01 2019-03-15 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Форсажная камера сгорания турбореактивного двухконтурного двигателя
JP6792728B2 (ja) * 2018-12-11 2020-11-25 株式会社エイチアンドエフ レーザーブランキング装置
CN115183274B (zh) * 2022-07-21 2023-08-04 中国航发沈阳发动机研究所 一种内涵点火加力燃烧室

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
GB674641A (en) * 1949-11-30 1952-06-25 Armstrong Siddeley Motors Ltd Fuel-burning means for a gaseous-fluid propulsion jet
GB723830A (en) * 1952-09-13 1955-02-09 Armstrong Siddeley Motors Ltd Flame stabilising device
US2918794A (en) * 1955-09-21 1959-12-29 United Aircraft Corp Flameholder
FR1165618A (fr) * 1956-12-12 1958-10-28 Continental Aviat & Eng Corp Perfectionnements aux stato-réacteurs
US2964907A (en) * 1957-11-15 1960-12-20 Rolls Royce Combustion stabilising device for combustion equipment
FR1207017A (fr) * 1958-05-29 1960-02-12 Gen Electric Dispositif d'allumage pour système de postcombustion de turboréacteur
FR1210398A (fr) * 1958-09-24 1960-03-08 Snecma Perfectionnements aux dispositifs de combustion
FR1217698A (fr) * 1958-11-05 1960-05-05 United Aircraft Corp Guide-flamme
FR1408812A (fr) * 1964-07-06 1965-08-20 Nord Aviat Perfectionnement apporté aux chambres de combustion de propulseurs
FR1525092A (fr) * 1967-01-23 1968-05-17 Snecma Turbo-réacteur à flux de gaz chaud et à flux d'air froid
US3788065A (en) * 1970-10-26 1974-01-29 United Aircraft Corp Annular combustion chamber for dissimilar fluids in swirling flow relationship
FR2124141B1 (ja) * 1971-02-09 1975-02-21 Snecma
US3800527A (en) * 1971-03-18 1974-04-02 United Aircraft Corp Piloted flameholder construction
FR2188060B1 (ja) * 1972-06-01 1976-06-11 Snecma
US3765178A (en) * 1972-09-08 1973-10-16 Gen Electric Afterburner flameholder

Also Published As

Publication number Publication date
US3931707A (en) 1976-01-13
DE2551005A1 (de) 1976-07-15
IT1049017B (it) 1981-01-20
GB1522826A (en) 1978-08-31
BE837339A (fr) 1976-05-03
CA1050286A (en) 1979-03-13
JPS5916170B2 (ja) 1984-04-13
FR2297327A1 (fr) 1976-08-06

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