PL3262348T3 - Komora spalania maszyny wirowej zawierająca część wchodzącą z otworem - Google Patents

Komora spalania maszyny wirowej zawierająca część wchodzącą z otworem

Info

Publication number
PL3262348T3
PL3262348T3 PL16713957T PL16713957T PL3262348T3 PL 3262348 T3 PL3262348 T3 PL 3262348T3 PL 16713957 T PL16713957 T PL 16713957T PL 16713957 T PL16713957 T PL 16713957T PL 3262348 T3 PL3262348 T3 PL 3262348T3
Authority
PL
Poland
Prior art keywords
opening
combustion chamber
turbine engine
turbine
engine
Prior art date
Application number
PL16713957T
Other languages
English (en)
Inventor
Olivier LAMAISON
Nicolas SAVARY
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 PL3262348T3 publication Critical patent/PL3262348T3/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/52—Toroidal 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • 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
    • F05D2260/00—Function
    • F05D2260/60—Fluid transfer
    • F05D2260/606—Bypassing the fluid
    • 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
    • F23R2900/03042—Film cooled combustion chamber walls or domes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Portable Nailing Machines And Staplers (AREA)
PL16713957T 2015-02-25 2016-02-23 Komora spalania maszyny wirowej zawierająca część wchodzącą z otworem PL3262348T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1551600A FR3033028B1 (fr) 2015-02-25 2015-02-25 Chambre de combustion de turbomachine comportant une piece penetrante avec ouverture
EP16713957.5A EP3262348B1 (fr) 2015-02-25 2016-02-23 Chambre de combustion de turbomachine comportant une pièce pénétrante avec ouverture
PCT/FR2016/050411 WO2016135409A1 (fr) 2015-02-25 2016-02-23 Chambre de combustion de turbomachine comportant une pièce pénétrante avec ouverture

Publications (1)

Publication Number Publication Date
PL3262348T3 true PL3262348T3 (pl) 2020-08-10

Family

ID=53794290

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16713957T PL3262348T3 (pl) 2015-02-25 2016-02-23 Komora spalania maszyny wirowej zawierająca część wchodzącą z otworem

Country Status (10)

Country Link
US (1) US20180045413A1 (pl)
EP (1) EP3262348B1 (pl)
JP (1) JP6764871B2 (pl)
KR (1) KR20170119708A (pl)
CN (1) CN107257904B (pl)
CA (1) CA2977004A1 (pl)
FR (1) FR3033028B1 (pl)
PL (1) PL3262348T3 (pl)
RU (1) RU2704440C2 (pl)
WO (1) WO2016135409A1 (pl)

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB665155A (en) * 1949-03-30 1952-01-16 Lucas Ltd Joseph Improvements relating to combustion chambers for prime movers
SU1454021A1 (ru) * 1987-03-19 1995-07-20 А.С. Косой Жаровая труба камеры сгорания газотурбинного двигателя
RU2066424C1 (ru) * 1994-04-28 1996-09-10 Акционерное общество "Авиадвигатель" Камера сгорания газотурбинного двигателя
GB9623195D0 (en) * 1996-11-07 1997-01-08 Rolls Royce Plc Gas turbine engine combustor
FR2826202B1 (fr) * 2001-06-18 2003-12-19 Cit Alcatel Procede et dispositif d'equilibrage de supercapacite
FR2826102B1 (fr) * 2001-06-19 2004-01-02 Snecma Moteurs Perfectionnements apportes aux chambres de combustion de turbine a gaz
FR2856466B1 (fr) * 2003-06-20 2005-08-26 Snecma Moteurs Dispositif d'etancheite de bougie non soude sur la paroi de chambre
US7546739B2 (en) * 2005-07-05 2009-06-16 General Electric Company Igniter tube and method of assembling same
US7546737B2 (en) * 2006-01-24 2009-06-16 Honeywell International Inc. Segmented effusion cooled gas turbine engine combustor
FR2927367B1 (fr) * 2008-02-11 2010-05-28 Snecma Dispositif de montage d'une bougie d'allumage dans une chambre de combustion de moteur a turbine a gaz
US9897320B2 (en) * 2009-07-30 2018-02-20 Honeywell International Inc. Effusion cooled dual wall gas turbine combustors
CN202813440U (zh) * 2012-06-15 2013-03-20 北京中陆航星机械动力科技有限公司 小型涡轮喷气发动机燃烧室
FR3009747B1 (fr) * 2013-08-19 2018-06-15 Snecma Chambre de combustion de turbomachine pourvue d'un passage d'entree d'air ameliore en aval d'un orifice de passage de bougie
US20160003150A1 (en) * 2014-07-03 2016-01-07 General Electric Company Igniter tip with cooling passage

Also Published As

Publication number Publication date
FR3033028B1 (fr) 2019-12-27
RU2017133015A (ru) 2019-03-25
KR20170119708A (ko) 2017-10-27
EP3262348A1 (fr) 2018-01-03
JP6764871B2 (ja) 2020-10-07
CN107257904B (zh) 2020-05-26
US20180045413A1 (en) 2018-02-15
CN107257904A (zh) 2017-10-17
WO2016135409A1 (fr) 2016-09-01
EP3262348B1 (fr) 2020-04-01
CA2977004A1 (fr) 2016-09-01
JP2018510285A (ja) 2018-04-12
FR3033028A1 (fr) 2016-08-26
RU2704440C2 (ru) 2019-10-29
RU2017133015A3 (pl) 2019-07-25

Similar Documents

Publication Publication Date Title
GB201610878D0 (en) Gas turbine engine
GB2528356B (en) An annular combustion chamber in a turbine engine
GB2551551B (en) Gas Turbine Engine
GB201600180D0 (en) Gas turbine engine
GB2569449B (en) A gas turbine engine combustion chamber arrangement
GB201610879D0 (en) Gas turbine engine
GB2544735B (en) Vanes of a gas turbine engine
GB2545538B (en) A gas turbine engine having sequential combustion
GB201402930D0 (en) Method of operating an internal combustion engine
PL3114409T3 (pl) Pierścieniowa komora spalania maszyny wirowej
GB201616108D0 (en) Gas turbine engine
GB201619960D0 (en) Gas turbine engine
GB2538606B (en) Internal combustion engine
EP3140527A4 (en) Combustion chamber for an internal combustion engine and an internal combustion engine
GB201603254D0 (en) Gas turbine engine
PL3443266T3 (pl) Ulepszone wtryskiwacze do komory spalania turbiny gazowej
GB2550201B (en) Gas turbine engine
GB201609702D0 (en) Gas turbine engine
DE112015003456A5 (de) Brennkammergestaltung eines VCR-Motors
PL3320269T3 (pl) Zagięta komora spalania maszyny wirowej
GB201618454D0 (en) Gas turbine engine
GB201616197D0 (en) Gas turbine engine
GB201614888D0 (en) Gas turbine engine
GB201614889D0 (en) Gas turbine engine
GB201514401D0 (en) A method of operating an internal combustion engine