FR2691235B1 - Chambre de combustion comprenant un ensemble separateur des gaz. - Google Patents

Chambre de combustion comprenant un ensemble separateur des gaz.

Info

Publication number
FR2691235B1
FR2691235B1 FR9205771A FR9205771A FR2691235B1 FR 2691235 B1 FR2691235 B1 FR 2691235B1 FR 9205771 A FR9205771 A FR 9205771A FR 9205771 A FR9205771 A FR 9205771A FR 2691235 B1 FR2691235 B1 FR 2691235B1
Authority
FR
France
Prior art keywords
combustion chamber
gas separator
separator assembly
assembly
gas
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
FR9205771A
Other languages
English (en)
Other versions
FR2691235A1 (fr
Inventor
Ansart Denis
Sandelis Denis
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 FR9205771A priority Critical patent/FR2691235B1/fr
Priority to US08/059,752 priority patent/US5311743A/en
Publication of FR2691235A1 publication Critical patent/FR2691235A1/fr
Application granted granted Critical
Publication of FR2691235B1 publication Critical patent/FR2691235B1/fr
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
FR9205771A 1992-05-13 1992-05-13 Chambre de combustion comprenant un ensemble separateur des gaz. Expired - Fee Related FR2691235B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR9205771A FR2691235B1 (fr) 1992-05-13 1992-05-13 Chambre de combustion comprenant un ensemble separateur des gaz.
US08/059,752 US5311743A (en) 1992-05-13 1993-05-12 Gas separator for a combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9205771A FR2691235B1 (fr) 1992-05-13 1992-05-13 Chambre de combustion comprenant un ensemble separateur des gaz.

Publications (2)

Publication Number Publication Date
FR2691235A1 FR2691235A1 (fr) 1993-11-19
FR2691235B1 true FR2691235B1 (fr) 1995-07-07

Family

ID=9429729

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9205771A Expired - Fee Related FR2691235B1 (fr) 1992-05-13 1992-05-13 Chambre de combustion comprenant un ensemble separateur des gaz.

Country Status (2)

Country Link
US (1) US5311743A (fr)
FR (1) FR2691235B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706534B1 (fr) * 1993-06-10 1995-07-21 Snecma Diffuseur-séparateur multiflux avec redresseur intégré pour turboréacteur.
FR2712379B1 (fr) * 1993-11-10 1995-12-29 Snecma Chambre de combustion pour turbomachine munie d'un séparateur des gaz.
FR2730555B1 (fr) * 1995-02-15 1997-03-14 Snecma Ensemble d'injection de carburant pour chambre de combustion de turbines a gaz
FR2770283B1 (fr) * 1997-10-29 1999-11-19 Snecma Chambre de combustion pour turbomachine
US6564555B2 (en) * 2001-05-24 2003-05-20 Allison Advanced Development Company Apparatus for forming a combustion mixture in a gas turbine engine
FR2920525B1 (fr) * 2007-08-31 2014-06-13 Snecma Separateur pour alimentation de l'air de refroidissement d'une turbine
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH260957A (de) * 1945-11-20 1949-04-15 Westinghouse Electric Corp Verbrennungseinrichtung für Gasturbinenanlage.
GB874644A (en) * 1959-03-11 1961-08-10 Rolls Royce Combustion chamber
GB948128A (en) * 1959-03-26 1964-01-29 Lucas Industries Ltd Combustion apparatus for jet-propulsion engines, gas turbines, or other prime movers
FR76734E (fr) * 1959-12-14 1961-11-24 Bristol Aero Engines Ltd Perfectionnements aux chambres de combustion
FR1286562A (fr) * 1961-04-22 1962-03-02 Rolls Royce Chambre de combustion de turbo-moteur à gaz
FR2221621B1 (fr) * 1973-03-13 1976-09-10 Snecma
FR2402068A1 (fr) * 1977-09-02 1979-03-30 Snecma Chambre de combustion anti-pollution
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
GB2013788B (en) * 1978-01-28 1982-06-03 Rolls Royce Gas turbine engine

Also Published As

Publication number Publication date
US5311743A (en) 1994-05-17
FR2691235A1 (fr) 1993-11-19

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Legal Events

Date Code Title Description
CL Concession to grant licences
CD Change of name or company name
TP Transmission of property
ST Notification of lapse

Effective date: 20060131