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FR2958014B1 - COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN - Google Patents

COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN

Info

Publication number
FR2958014B1
FR2958014B1 FR1052106A FR1052106A FR2958014B1 FR 2958014 B1 FR2958014 B1 FR 2958014B1 FR 1052106 A FR1052106 A FR 1052106A FR 1052106 A FR1052106 A FR 1052106A FR 2958014 B1 FR2958014 B1 FR 2958014B1
Authority
FR
France
Prior art keywords
combustion chamber
injectors
same crown
shifting longitudinally
injection systems
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.)
Active
Application number
FR1052106A
Other languages
French (fr)
Other versions
FR2958014A1 (en
Inventor
Emilie Lachaud
Sebastien Roux
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1052106A priority Critical patent/FR2958014B1/en
Priority to PCT/FR2011/050605 priority patent/WO2011117533A2/en
Publication of FR2958014A1 publication Critical patent/FR2958014A1/en
Application granted granted Critical
Publication of FR2958014B1 publication Critical patent/FR2958014B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)

Abstract

The invention relates to an annular combustion chamber for a turbomachine, comprising an external wall (2), an internal wall (3) and a chamber base (4) on which identical injection systems (5) are mounted along at least one ring, said injection systems being intended to mix fuel from the injectors (6) with air from the compressor. The invention is characterised in that at least two injection systems (5) located on the same ring are offset longitudinally in the direction of the central axis of the combustion chamber.
FR1052106A 2010-03-23 2010-03-23 COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN Active FR2958014B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1052106A FR2958014B1 (en) 2010-03-23 2010-03-23 COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN
PCT/FR2011/050605 WO2011117533A2 (en) 2010-03-23 2011-03-22 Combustion chamber comprising injectors offset longitudinally on the same ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1052106A FR2958014B1 (en) 2010-03-23 2010-03-23 COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN

Publications (2)

Publication Number Publication Date
FR2958014A1 FR2958014A1 (en) 2011-09-30
FR2958014B1 true FR2958014B1 (en) 2013-12-13

Family

ID=43037849

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1052106A Active FR2958014B1 (en) 2010-03-23 2010-03-23 COMBUSTION CHAMBER WITH INJECTORS SHIFTING LONGITUDINALLY ON THE SAME CROWN

Country Status (2)

Country Link
FR (1) FR2958014B1 (en)
WO (1) WO2011117533A2 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10513984B2 (en) 2015-08-25 2019-12-24 General Electric Company System for suppressing acoustic noise within a gas turbine combustor
US10197275B2 (en) 2016-05-03 2019-02-05 General Electric Company High frequency acoustic damper for combustor liners
US10415480B2 (en) 2017-04-13 2019-09-17 General Electric Company Gas turbine engine fuel manifold damper and method of dynamics attenuation
US11149948B2 (en) 2017-08-21 2021-10-19 General Electric Company Fuel nozzle with angled main injection ports and radial main injection ports
US11156162B2 (en) 2018-05-23 2021-10-26 General Electric Company Fluid manifold damper for gas turbine engine
US11506125B2 (en) 2018-08-01 2022-11-22 General Electric Company Fluid manifold assembly for gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4336096B4 (en) * 1992-11-13 2004-07-08 Alstom Device for reducing vibrations in combustion chambers
FR2727193B1 (en) 1994-11-23 1996-12-20 Snecma TWO-HEAD COMBUSTION CHAMBER OPERATING AT FULL GAS SLOW MOTION
SE9802707L (en) * 1998-08-11 2000-02-12 Abb Ab Burner chamber device and method for reducing the influence of acoustic pressure fluctuations in a burner chamber device
EP1125087B1 (en) * 1998-08-31 2005-05-18 Siemens Aktiengesellschaft Burner assembly
FR2829228B1 (en) 2001-08-28 2005-07-15 Snecma Moteurs ANNULAR COMBUSTION CHAMBER WITH DOUBLE HEADED HEAD
EP1524469A1 (en) * 2003-10-13 2005-04-20 Siemens Aktiengesellschaft Premix burner for a gas turbine

Also Published As

Publication number Publication date
WO2011117533A2 (en) 2011-09-29
FR2958014A1 (en) 2011-09-30
WO2011117533A3 (en) 2012-05-31

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