GB1273017A - Improvements in or relating to burners for reheat combustion chambers - Google Patents

Improvements in or relating to burners for reheat combustion chambers

Info

Publication number
GB1273017A
GB1273017A GB48289/69A GB4828969A GB1273017A GB 1273017 A GB1273017 A GB 1273017A GB 48289/69 A GB48289/69 A GB 48289/69A GB 4828969 A GB4828969 A GB 4828969A GB 1273017 A GB1273017 A GB 1273017A
Authority
GB
United Kingdom
Prior art keywords
fuel
air
pipes
annular
pipe
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
GB48289/69A
Other languages
English (en)
Inventor
Louis Jules Bauger
Armand Jean-Baptiste Lacroix
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of GB1273017A publication Critical patent/GB1273017A/en
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Sampling And Sample Adjustment (AREA)
GB48289/69A 1968-10-02 1969-10-01 Improvements in or relating to burners for reheat combustion chambers Expired GB1273017A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR168514 1968-10-02

Publications (1)

Publication Number Publication Date
GB1273017A true GB1273017A (en) 1972-05-03

Family

ID=8655220

Family Applications (1)

Application Number Title Priority Date Filing Date
GB48289/69A Expired GB1273017A (en) 1968-10-02 1969-10-01 Improvements in or relating to burners for reheat combustion chambers

Country Status (3)

Country Link
US (1) US3633361A (enrdf_load_stackoverflow)
FR (1) FR1588974A (enrdf_load_stackoverflow)
GB (1) GB1273017A (enrdf_load_stackoverflow)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2327187A1 (de) * 1972-06-01 1973-12-20 Snecma Nachverbrennungsvorrichtung fuer einen gasturbinenmotor
DE3247169A1 (de) * 1981-12-24 1983-07-14 Rolls-Royce Ltd., London Brennstoffverdampfer fuer gasturbinenbrennkammern
US4561257A (en) * 1981-05-20 1985-12-31 Rolls-Royce Limited Gas turbine engine combustion apparatus
GB2233714A (en) * 1989-04-26 1991-01-16 Gen Electric Thrust augmented bypass gas turbine engine
RU2209992C1 (ru) * 2002-03-06 2003-08-10 Государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" - дочернее предприятие Федерального государственного унитарного предприятия "Российской самолётостроительной корпорации "МиГ" Форсажная камера двухконтурного турбореактивного двигателя
GB2425574A (en) * 2005-04-29 2006-11-01 Gen Electric Fuel control in a supersonic jet engine.
US7448199B2 (en) 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
US7475545B2 (en) 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
US7509797B2 (en) 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
EP3636906A1 (en) * 2018-10-12 2020-04-15 Rolls-Royce plc Afterburner system

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1392739A (en) * 1971-07-16 1975-04-30 Snecma Devices for pre-vaporising liquid fuel
US3977186A (en) * 1975-07-24 1976-08-31 General Motors Corporation Impinging air jet combustion apparatus
US4389185A (en) * 1980-10-31 1983-06-21 Alpkvist Jan A Combustor for burning a volatile fuel with air
US4549402A (en) * 1982-05-26 1985-10-29 Pratt & Whitney Aircraft Of Canada Limited Combustor for a gas turbine engine
US4896501A (en) * 1987-10-22 1990-01-30 Faulkner Robie L Turbojet engine with sonic injection afterburner
EP0703413B1 (de) * 1994-09-21 2000-03-29 ABB Alstom Power (Schweiz) AG Brennkammer einer Gasturbogruppe
US6250066B1 (en) 1996-11-26 2001-06-26 Honeywell International Inc. Combustor with dilution bypass system and venturi jet deflector
FR2856744B1 (fr) * 2003-06-25 2007-05-25 Snecma Moteurs Canaux de ventilation sur tole de confluence d'une chambre de post-combustion
RU2335651C1 (ru) * 2007-02-01 2008-10-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "Салют" Форсажная камера газотурбинного двигателя
AU2009352302A1 (en) * 2009-09-13 2012-04-12 Lean Flame, Inc. Vortex premixer for combustion apparatus
CN105716120B (zh) * 2016-02-22 2018-02-16 中国科学院工程热物理研究所 一种燃油冷却式蒸发管结构
CN107044636B (zh) * 2017-04-27 2018-11-06 中国科学院工程热物理研究所 一种蒸发管燃烧室用燃油喷射装置
FR3101696B1 (fr) * 2019-10-08 2021-10-29 Safran Helicopter Engines Canne de prevaporisation pour une chambre de combustion de turbomachine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2672727A (en) * 1951-05-31 1954-03-23 Westinghouse Electric Corp Fuel vaporizer system for combustion chambers
US2931174A (en) * 1952-12-20 1960-04-05 Armstrong Siddeley Motors Ltd Vaporizer for liquid fuel
US2979899A (en) * 1953-06-27 1961-04-18 Snecma Flame spreading device for combustion equipments
US2978868A (en) * 1959-12-21 1961-04-11 Gen Electric Concentric combustion system with cooled dividing partition
GB938553A (en) * 1961-05-09 1963-10-02 Rolls Royce Reheat combustion apparatus for a gas turbine engine
US3236048A (en) * 1963-09-25 1966-02-22 Gen Motors Corp Vaporizing manifold and flameholder for afterburners
US3330117A (en) * 1964-11-27 1967-07-11 Rolls Royce By-pass gas turbine jet engine

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2327187A1 (de) * 1972-06-01 1973-12-20 Snecma Nachverbrennungsvorrichtung fuer einen gasturbinenmotor
US4561257A (en) * 1981-05-20 1985-12-31 Rolls-Royce Limited Gas turbine engine combustion apparatus
DE3247169A1 (de) * 1981-12-24 1983-07-14 Rolls-Royce Ltd., London Brennstoffverdampfer fuer gasturbinenbrennkammern
US4742684A (en) * 1981-12-24 1988-05-10 Rolls-Royce Plc Fuel vaporizers for a gas turbine engine combustion engine
GB2233714A (en) * 1989-04-26 1991-01-16 Gen Electric Thrust augmented bypass gas turbine engine
US5070690A (en) * 1989-04-26 1991-12-10 General Electric Company Means and method for reducing differential pressure loading in an augmented gas turbine engine
GB2233714B (en) * 1989-04-26 1993-11-17 Gen Electric Augmented gas turbine engine
RU2209992C1 (ru) * 2002-03-06 2003-08-10 Государственное унитарное предприятие Тушинское машиностроительное конструкторское бюро "Союз" - дочернее предприятие Федерального государственного унитарного предприятия "Российской самолётостроительной корпорации "МиГ" Форсажная камера двухконтурного турбореактивного двигателя
GB2425574A (en) * 2005-04-29 2006-11-01 Gen Electric Fuel control in a supersonic jet engine.
US7424805B2 (en) 2005-04-29 2008-09-16 General Electric Company Supersonic missile turbojet engine
US7448199B2 (en) 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
US7475545B2 (en) 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
US7509797B2 (en) 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
GB2425574B (en) * 2005-04-29 2010-06-16 Gen Electric Supersonic missile turbojet engine
EP3636906A1 (en) * 2018-10-12 2020-04-15 Rolls-Royce plc Afterburner system
US11008976B2 (en) 2018-10-12 2021-05-18 Rolls-Royce Plc Afterburner system for turbofan engine

Also Published As

Publication number Publication date
US3633361A (en) 1972-01-11
FR1588974A (enrdf_load_stackoverflow) 1970-03-16

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee