FR2996289B1 - COMBUSTION CHAMBER COMPRISING A FIXED FLAME TUBE USING THREE CENTERING ELEMENTS. - Google Patents

COMBUSTION CHAMBER COMPRISING A FIXED FLAME TUBE USING THREE CENTERING ELEMENTS.

Info

Publication number
FR2996289B1
FR2996289B1 FR1259290A FR1259290A FR2996289B1 FR 2996289 B1 FR2996289 B1 FR 2996289B1 FR 1259290 A FR1259290 A FR 1259290A FR 1259290 A FR1259290 A FR 1259290A FR 2996289 B1 FR2996289 B1 FR 2996289B1
Authority
FR
France
Prior art keywords
combustion chamber
flame tube
centering elements
fixed flame
fixed
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
FR1259290A
Other languages
French (fr)
Other versions
FR2996289A1 (en
Inventor
Bernard Carrere
Philippe Olharan
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 Helicopter Engines SAS
Original Assignee
Turbomeca SA
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 Turbomeca SA filed Critical Turbomeca SA
Priority to FR1259290A priority Critical patent/FR2996289B1/en
Priority to PCT/FR2013/052203 priority patent/WO2014053728A1/en
Publication of FR2996289A1 publication Critical patent/FR2996289A1/en
Application granted granted Critical
Publication of FR2996289B1 publication Critical patent/FR2996289B1/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00017—Assembling combustion chamber liners or subparts

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1259290A 2012-10-01 2012-10-01 COMBUSTION CHAMBER COMPRISING A FIXED FLAME TUBE USING THREE CENTERING ELEMENTS. Active FR2996289B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1259290A FR2996289B1 (en) 2012-10-01 2012-10-01 COMBUSTION CHAMBER COMPRISING A FIXED FLAME TUBE USING THREE CENTERING ELEMENTS.
PCT/FR2013/052203 WO2014053728A1 (en) 2012-10-01 2013-09-23 Combustion chamber comprising a flame tube fixed by means of three centring members

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1259290A FR2996289B1 (en) 2012-10-01 2012-10-01 COMBUSTION CHAMBER COMPRISING A FIXED FLAME TUBE USING THREE CENTERING ELEMENTS.

Publications (2)

Publication Number Publication Date
FR2996289A1 FR2996289A1 (en) 2014-04-04
FR2996289B1 true FR2996289B1 (en) 2018-10-12

Family

ID=47356137

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1259290A Active FR2996289B1 (en) 2012-10-01 2012-10-01 COMBUSTION CHAMBER COMPRISING A FIXED FLAME TUBE USING THREE CENTERING ELEMENTS.

Country Status (2)

Country Link
FR (1) FR2996289B1 (en)
WO (1) WO2014053728A1 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3022613B1 (en) * 2014-06-24 2019-04-19 Safran Helicopter Engines BOSSAGE FOR COMBUSTION CHAMBER.
FR3095499B1 (en) 2019-04-23 2021-06-11 Safran Helicopter Engines INJECTOR OF A MIXTURE OF AIR AND FUEL FOR A TURBOMACHINE COMBUSTION CHAMBER
WO2020245537A1 (en) 2019-06-07 2020-12-10 Safran Helicopter Engines Method for manufacturing a flame tube for a turbomachine
FR3097028B1 (en) 2019-06-07 2021-05-14 Safran Helicopter Engines Method of manufacturing a flame tube for a turbomachine
FR3097029B1 (en) 2019-06-07 2021-05-21 Safran Helicopter Engines Method of manufacturing a flame tube for a turbomachine
FR3097299B1 (en) 2019-06-13 2021-07-23 Safran SET FOR A GAS TURBINE
FR3107106B1 (en) 2020-02-11 2022-07-08 Safran Aircraft Engines Assembly COMPRISING a crankcase and a combustion chamber, and turbomachine so equipped
FR3107108B1 (en) 2020-02-11 2022-07-08 Safran Aircraft Engines Assembly COMPRISING a crankcase and a combustion chamber, and turbomachine so equipped
CN113137639B (en) * 2021-04-25 2022-07-15 中国航发湖南动力机械研究所 Turboprop engine backflow combustion chamber and turboprop engine
CN114543120B (en) * 2021-11-30 2023-07-18 中国航发湖南动力机械研究所 Flame tube fixing structure based on ceramic matrix composite

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2723546A1 (en) 1977-05-25 1978-11-30 Motoren Turbinen Union COMBUSTION CHAMBER, IN PARTICULAR REVERSAL COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
EP1135578B1 (en) * 1998-08-12 2004-06-16 ETN Präzisionstechnik GmbH Support devices for the vanes of power units
JP2004524479A (en) * 2001-04-27 2004-08-12 シーメンス　アクチエンゲゼルシヤフト Especially for gas turbine combustion chambers
EP1312865A1 (en) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Gas turbine annular combustion chamber
US7523616B2 (en) * 2005-11-30 2009-04-28 General Electric Company Methods and apparatuses for assembling a gas turbine engine
FR2971039B1 (en) * 2011-02-02 2013-01-11 Turbomeca GAS TURBINE FUEL COMBUSTION CHAMBER INJECTOR WITH DOUBLE FUEL CIRCUIT AND COMBUSTION CHAMBER EQUIPPED WITH AT LEAST ONE SUCH INJECTOR

Also Published As

Publication number Publication date
FR2996289A1 (en) 2014-04-04
WO2014053728A1 (en) 2014-04-10

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