PL3359880T3 - Pierścieniowa komora spalania do maszyny wirowej - Google Patents

Pierścieniowa komora spalania do maszyny wirowej

Info

Publication number
PL3359880T3
PL3359880T3 PL16787502T PL16787502T PL3359880T3 PL 3359880 T3 PL3359880 T3 PL 3359880T3 PL 16787502 T PL16787502 T PL 16787502T PL 16787502 T PL16787502 T PL 16787502T PL 3359880 T3 PL3359880 T3 PL 3359880T3
Authority
PL
Poland
Prior art keywords
ring
combustion chamber
turbine engine
shaped combustion
shaped
Prior art date
Application number
PL16787502T
Other languages
English (en)
Inventor
Stéphane PASCAUD
Guillaume TALIERCIO
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3359880T3 publication Critical patent/PL3359880T3/pl

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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/35—Combustors or associated equipment

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)
  • Turbine Rotor Nozzle Sealing (AREA)
PL16787502T 2015-10-06 2016-10-04 Pierścieniowa komora spalania do maszyny wirowej PL3359880T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1559491A FR3042023B1 (fr) 2015-10-06 2015-10-06 Chambre de combustion annulaire pour turbomachine
PCT/FR2016/052539 WO2017060605A1 (fr) 2015-10-06 2016-10-04 Chambre de combustion annulaire pour turbomachine
EP16787502.0A EP3359880B1 (fr) 2015-10-06 2016-10-04 Chambre de combustion annulaire pour turbomachine

Publications (1)

Publication Number Publication Date
PL3359880T3 true PL3359880T3 (pl) 2019-12-31

Family

ID=54979773

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16787502T PL3359880T3 (pl) 2015-10-06 2016-10-04 Pierścieniowa komora spalania do maszyny wirowej

Country Status (10)

Country Link
US (1) US10895383B2 (pl)
EP (1) EP3359880B1 (pl)
JP (1) JP2018534518A (pl)
KR (1) KR20180063120A (pl)
CN (1) CN108139077B (pl)
CA (1) CA3000922A1 (pl)
FR (1) FR3042023B1 (pl)
PL (1) PL3359880T3 (pl)
RU (1) RU2718375C2 (pl)
WO (1) WO2017060605A1 (pl)

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3671171A (en) 1970-11-27 1972-06-20 Avco Corp Annular combustors
CA2076102C (en) 1991-09-23 2001-12-18 Stephen John Howell Aero-slinger combustor
FR2690977B1 (fr) 1992-05-06 1995-09-01 Snecma Chambre de combustion comportant des passages reglables d'admission de comburant primaire.
EP0700498B1 (en) * 1993-06-01 1998-10-21 Pratt & Whitney Canada, Inc. Radially mounted air blast fuel injector
FR2751054B1 (fr) * 1996-07-11 1998-09-18 Snecma Chambre de combustion anti-nox a injection de carburant de type annulaire
US6155056A (en) * 1998-06-04 2000-12-05 Pratt & Whitney Canada Corp. Cooling louver for annular gas turbine engine combustion chamber
US6367262B1 (en) * 2000-09-29 2002-04-09 General Electric Company Multiple annular swirler
FR2856467B1 (fr) * 2003-06-18 2005-09-02 Snecma Moteurs Chambre de combustion annulaire de turbomachine
US7509809B2 (en) * 2005-06-10 2009-03-31 Pratt & Whitney Canada Corp. Gas turbine engine combustor with improved cooling
FR2903169B1 (fr) * 2006-06-29 2011-11-11 Snecma Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
FR2911667B1 (fr) * 2007-01-23 2009-10-02 Snecma Sa Systeme d'injection de carburant a double injecteur.
US8171634B2 (en) * 2007-07-09 2012-05-08 Pratt & Whitney Canada Corp. Method of producing effusion holes
FR2919380B1 (fr) * 2007-07-26 2013-10-25 Snecma Chambre de combustion d'une turbomachine.
US8616004B2 (en) * 2007-11-29 2013-12-31 Honeywell International Inc. Quench jet arrangement for annular rich-quench-lean gas turbine combustors
FR2941287B1 (fr) * 2009-01-19 2011-03-25 Snecma Paroi de chambre de combustion de turbomachine a une seule rangee annulaire d'orifices d'entree d'air primaire et de dilution
US8171740B2 (en) * 2009-02-27 2012-05-08 Honeywell International Inc. Annular rich-quench-lean gas turbine combustors with plunged holes
FR2948988B1 (fr) 2009-08-04 2011-12-09 Snecma Chambre de combustion de turbomachine comprenant des orifices d'entree d'air ameliores
US9080770B2 (en) * 2011-06-06 2015-07-14 Honeywell International Inc. Reverse-flow annular combustor for reduced emissions
CN204460285U (zh) * 2014-12-03 2015-07-08 中国航空工业集团公司金城南京机电液压工程研究中心 一种环形回流燃烧室火焰筒

Also Published As

Publication number Publication date
WO2017060605A1 (fr) 2017-04-13
EP3359880B1 (fr) 2019-08-21
CA3000922A1 (fr) 2017-04-13
CN108139077A (zh) 2018-06-08
FR3042023B1 (fr) 2020-06-05
US20180299127A1 (en) 2018-10-18
RU2018116261A3 (pl) 2020-01-21
KR20180063120A (ko) 2018-06-11
FR3042023A1 (fr) 2017-04-07
CN108139077B (zh) 2020-09-15
JP2018534518A (ja) 2018-11-22
RU2718375C2 (ru) 2020-04-02
RU2018116261A (ru) 2019-11-07
EP3359880A1 (fr) 2018-08-15
US10895383B2 (en) 2021-01-19

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