PL4004442T3 - Wtryskiwacz paliwa z obwodem przedmuchowym do turbiny samolotu - Google Patents

Wtryskiwacz paliwa z obwodem przedmuchowym do turbiny samolotu

Info

Publication number
PL4004442T3
PL4004442T3 PL20751616.2T PL20751616T PL4004442T3 PL 4004442 T3 PL4004442 T3 PL 4004442T3 PL 20751616 T PL20751616 T PL 20751616T PL 4004442 T3 PL4004442 T3 PL 4004442T3
Authority
PL
Poland
Prior art keywords
turbine engine
fuel injector
aircraft turbine
purge circuit
purge
Prior art date
Application number
PL20751616.2T
Other languages
English (en)
Inventor
Thomas Jean Olivier LEDERLIN
Denis Luc Alain Chanteloup
Simon Arthur Meilleurat
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 PL4004442T3 publication Critical patent/PL4004442T3/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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
PL20751616.2T 2019-07-24 2020-07-16 Wtryskiwacz paliwa z obwodem przedmuchowym do turbiny samolotu PL4004442T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1908419A FR3099231B1 (fr) 2019-07-24 2019-07-24 Injecteur de carburant a circuit de purge pour une turbomachine d’aeronef
PCT/FR2020/051274 WO2021014074A1 (fr) 2019-07-24 2020-07-16 Injecteur de carburant a circuit de purge pour une turbomachine d'aeronef

Publications (1)

Publication Number Publication Date
PL4004442T3 true PL4004442T3 (pl) 2025-05-26

Family

ID=68987816

Family Applications (1)

Application Number Title Priority Date Filing Date
PL20751616.2T PL4004442T3 (pl) 2019-07-24 2020-07-16 Wtryskiwacz paliwa z obwodem przedmuchowym do turbiny samolotu

Country Status (7)

Country Link
US (1) US11892166B2 (pl)
EP (1) EP4004442B1 (pl)
CN (1) CN114222889B (pl)
CA (1) CA3144907A1 (pl)
FR (1) FR3099231B1 (pl)
PL (1) PL4004442T3 (pl)
WO (1) WO2021014074A1 (pl)

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE200106C (pl)
JP2003247425A (ja) * 2002-02-25 2003-09-05 Mitsubishi Heavy Ind Ltd 燃料ノズル、燃焼器およびガスタービン
FR2875584B1 (fr) * 2004-09-23 2009-10-30 Snecma Moteurs Sa Injecteur a effervescence pour systeme aeromecanique d'injection air/carburant dans une chambre de combustion de turbomachine
US8015815B2 (en) * 2007-04-18 2011-09-13 Parker-Hannifin Corporation Fuel injector nozzles, with labyrinth grooves, for gas turbine engines
US8286433B2 (en) * 2007-10-26 2012-10-16 Solar Turbines Inc. Gas turbine fuel injector with removable pilot liquid tube
US8256226B2 (en) * 2009-04-23 2012-09-04 General Electric Company Radial lean direct injection burner
US9151227B2 (en) * 2010-11-10 2015-10-06 Solar Turbines Incorporated End-fed liquid fuel gallery for a gas turbine fuel injector
FR2971039B1 (fr) 2011-02-02 2013-01-11 Turbomeca Injecteur de chambre de combustion de turbine a gaz a double circuit de carburant et chambre de combustion equipee d'au moins un tel injecteur
RU2618801C2 (ru) * 2013-01-10 2017-05-11 Дженерал Электрик Компани Топливная форсунка, концевой узел топливной форсунки и газовая турбина
DE102013208069A1 (de) * 2013-05-02 2014-11-06 Siemens Aktiengesellschaft Brennerlanze für einen Brenner einer Gasturbine
FR3013805B1 (fr) 2013-11-26 2018-01-26 Safran Helicopter Engines Ensemble de combustion a acces facilite des cannes de prevaporisation.
US9528705B2 (en) * 2014-04-08 2016-12-27 General Electric Company Trapped vortex fuel injector and method for manufacture
US20170328568A1 (en) * 2014-11-26 2017-11-16 Siemens Aktiengesellschaft Fuel lance with means for interacting with a flow of air and improve breakage of an ejected liquid jet of fuel
JP6100295B2 (ja) * 2015-03-02 2017-03-22 三菱日立パワーシステムズ株式会社 燃料ノズル、これを備えた燃焼器及びガスタービン
FR3059047B1 (fr) * 2016-11-21 2020-08-28 Safran Helicopter Engines Injecteur de chambre de combustion pour une turbomachine et son procede de fabrication
DE102017200106A1 (de) * 2017-01-05 2018-07-05 Siemens Aktiengesellschaft Brennerspitze mit einem Luftkanalsystem und einem Brennstoffkanalsystem für einen Brenner und Verfahren zu deren Herstellung
FR3067792B1 (fr) 2017-06-16 2021-05-21 Safran Helicopter Engines Injecteur de carburant a jet plat pour une turbomachine d'aeronef et son procede de fabrication

Also Published As

Publication number Publication date
US11892166B2 (en) 2024-02-06
US20220282869A1 (en) 2022-09-08
EP4004442B1 (fr) 2025-04-02
CN114222889B (zh) 2024-08-23
CA3144907A1 (en) 2021-01-28
FR3099231A1 (fr) 2021-01-29
WO2021014074A1 (fr) 2021-01-28
FR3099231B1 (fr) 2022-08-12
EP4004442A1 (fr) 2022-06-01
CN114222889A (zh) 2022-03-22

Similar Documents

Publication Publication Date Title
GB2573853B (en) Fuel injector assembly for gas turbine engine
GB2619684B (en) Modulating fuel for a turbine engine
GB2571813B (en) Jet swirl air blast fuel injector for gas turbine engine
GB201516977D0 (en) A Fuel Injector For A Gas Turbine Engine Combustion Chamber
PL2671028T3 (pl) Wtryskiwacz komory spalania turbiny gazowej z podwójnym obwodem paliwa i komora spalania wyposażona w co najmniej jeden taki wtryskiwacz
GB2581244B (en) Fuel injector assembly for a heat engine
GB201811512D0 (en) Fuel nozzle for a gas turbine engine
GB2581417B (en) Combustion section and fuel injector assembly for a heat engine
GB2600814B (en) Fuel injector assembly for a turbine engine
GB2570035B (en) A Lean Burn Fuel Injector for a Gas Turbine Engine Combustion Chamber
PL3607190T3 (pl) Sposób sprawdzania maksymalnej dostępnej mocy maszyny wirowej statku powietrznego wyposażonego w dwie maszyny wirowe
GB201808512D0 (en) A Gas Turbine Engine Combustion Arrangement and a Gas Turbine Engine
EP3244056B8 (en) A fuel rail assembly for an internal combustion engine
GB201802251D0 (en) An air swirler arrangement for a fuel injector of a combustion chamber
GB2607118B (en) Fuel injector assembly for a turbine engine
GB202018264D0 (en) Gas turbine engine with improved vigv shielding
WO2014197072A3 (en) Fuel nozzle for a gas turbine engine
GB201912446D0 (en) A gas turbine engine for an aircraft comprising an air intake
GB201603329D0 (en) Fuel injector for a combustion engine
PL4004442T3 (pl) Wtryskiwacz paliwa z obwodem przedmuchowym do turbiny samolotu
GB2582445B (en) Turbine unit for aircraft turbine engine with improved disc-cooling circuit
GB201917415D0 (en) Nacelle for a gas turbine engine
GB201906167D0 (en) Gas turbine engine with core mount
GB201912443D0 (en) A gas turbine engine for an aircraft comprising an air intake
GB201912445D0 (en) A gas turbine engine for an aircraft comprising an air intake