FR2694799B1 - Conventional annular combustion chamber with several injectors. - Google Patents

Conventional annular combustion chamber with several injectors.

Info

Publication number
FR2694799B1
FR2694799B1 FR9209933A FR9209933A FR2694799B1 FR 2694799 B1 FR2694799 B1 FR 2694799B1 FR 9209933 A FR9209933 A FR 9209933A FR 9209933 A FR9209933 A FR 9209933A FR 2694799 B1 FR2694799 B1 FR 2694799B1
Authority
FR
France
Prior art keywords
combustion chamber
annular combustion
conventional annular
several injectors
injectors
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 - Fee Related
Application number
FR9209933A
Other languages
French (fr)
Other versions
FR2694799A1 (en
Inventor
Denis Ansart
Yves Bouchie
Patrice Commaret
Serge Meunier
Michel Desaulty
Denis Sandelis
Pierre Schroer
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 FR9209933A priority Critical patent/FR2694799B1/en
Publication of FR2694799A1 publication Critical patent/FR2694799A1/en
Application granted granted Critical
Publication of FR2694799B1 publication Critical patent/FR2694799B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/34—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)
FR9209933A 1992-08-12 1992-08-12 Conventional annular combustion chamber with several injectors. Expired - Fee Related FR2694799B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9209933A FR2694799B1 (en) 1992-08-12 1992-08-12 Conventional annular combustion chamber with several injectors.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9209933A FR2694799B1 (en) 1992-08-12 1992-08-12 Conventional annular combustion chamber with several injectors.

Publications (2)

Publication Number Publication Date
FR2694799A1 FR2694799A1 (en) 1994-02-18
FR2694799B1 true FR2694799B1 (en) 1994-09-23

Family

ID=9432793

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9209933A Expired - Fee Related FR2694799B1 (en) 1992-08-12 1992-08-12 Conventional annular combustion chamber with several injectors.

Country Status (1)

Country Link
FR (1) FR2694799B1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10108560A1 (en) 2001-02-22 2002-09-05 Alstom Switzerland Ltd Method for operating an annular combustion chamber and an associated annular combustion chamber
US6968699B2 (en) 2003-05-08 2005-11-29 General Electric Company Sector staging combustor
US8028528B2 (en) 2005-10-17 2011-10-04 United Technologies Corporation Annular gas turbine combustor
US7954325B2 (en) 2005-12-06 2011-06-07 United Technologies Corporation Gas turbine combustor
US9068748B2 (en) 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
US9958162B2 (en) 2011-01-24 2018-05-01 United Technologies Corporation Combustor assembly for a turbine engine
US8479521B2 (en) 2011-01-24 2013-07-09 United Technologies Corporation Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies
US9541292B2 (en) 2013-03-12 2017-01-10 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9958161B2 (en) 2013-03-12 2018-05-01 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9228747B2 (en) 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9127843B2 (en) 2013-03-12 2015-09-08 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9366187B2 (en) 2013-03-12 2016-06-14 Pratt & Whitney Canada Corp. Slinger combustor
GB2554384A (en) 2016-09-23 2018-04-04 Hieta Tech Limited Combustion chamber and heat exchanger

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR944310A (en) * 1946-01-09 1949-04-01 Bendix Aviat Corp Burners
GB662764A (en) * 1949-01-12 1951-12-12 Lucas Ltd Joseph Improvements relating to combustion chambers for jet-engines or gas turbines
US4819438A (en) * 1982-12-23 1989-04-11 United States Of America Steam cooled rich-burn combustor liner
EP0481111B1 (en) * 1990-10-17 1995-06-28 Asea Brown Boveri Ag Gas-turbine combustion chamber

Also Published As

Publication number Publication date
FR2694799A1 (en) 1994-02-18

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse

Effective date: 20060428