JP2015531448A5 - - Google Patents

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Publication number
JP2015531448A5
JP2015531448A5 JP2015533668A JP2015533668A JP2015531448A5 JP 2015531448 A5 JP2015531448 A5 JP 2015531448A5 JP 2015533668 A JP2015533668 A JP 2015533668A JP 2015533668 A JP2015533668 A JP 2015533668A JP 2015531448 A5 JP2015531448 A5 JP 2015531448A5
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JP
Japan
Prior art keywords
fuel
combustion
combustion chamber
turbine engine
wall
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.)
Granted
Application number
JP2015533668A
Other languages
English (en)
Japanese (ja)
Other versions
JP6170562B2 (ja
JP2015531448A (ja
Filing date
Publication date
Priority claimed from FR1259287A external-priority patent/FR2996288B1/fr
Application filed filed Critical
Publication of JP2015531448A publication Critical patent/JP2015531448A/ja
Publication of JP2015531448A5 publication Critical patent/JP2015531448A5/ja
Application granted granted Critical
Publication of JP6170562B2 publication Critical patent/JP6170562B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015533668A 2012-10-01 2013-09-23 タービンエンジンの燃焼室のための2つの回路の噴射器 Expired - Fee Related JP6170562B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1259287 2012-10-01
FR1259287A FR2996288B1 (fr) 2012-10-01 2012-10-01 Injecteur a double circuit de chambre de combustion de turbomachine.
PCT/FR2013/052205 WO2014053730A2 (fr) 2012-10-01 2013-09-23 Injecteur a double circuit de chambre de combustion de turbomachine

Publications (3)

Publication Number Publication Date
JP2015531448A JP2015531448A (ja) 2015-11-02
JP2015531448A5 true JP2015531448A5 (https=) 2016-10-20
JP6170562B2 JP6170562B2 (ja) 2017-07-26

Family

ID=47425067

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015533668A Expired - Fee Related JP6170562B2 (ja) 2012-10-01 2013-09-23 タービンエンジンの燃焼室のための2つの回路の噴射器

Country Status (10)

Country Link
US (1) US9927125B2 (https=)
EP (1) EP2904329B1 (https=)
JP (1) JP6170562B2 (https=)
KR (1) KR102093955B1 (https=)
CA (1) CA2886564C (https=)
FR (1) FR2996288B1 (https=)
IN (1) IN2015DN02445A (https=)
PL (1) PL2904329T3 (https=)
RU (1) RU2632358C2 (https=)
WO (1) WO2014053730A2 (https=)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2996285B1 (fr) * 2012-10-01 2014-09-12 Turbomeca Ensemble de combustion de turbomachine a variation d'alimentation d'air.
FR3021073B1 (fr) * 2014-05-19 2019-06-07 Safran Helicopter Engines Architecture d'injection de carburant amelioree.
FR3028011A1 (fr) * 2014-10-30 2016-05-06 Turbomeca Architecture de combustion de carburant adaptee pour le ralenti et le demarrage rapide
KR102268593B1 (ko) * 2016-07-01 2021-06-23 한화에어로스페이스 주식회사 슬링거 연소기 및 이를 구비한 가스 터빈 엔진 시스템
US11519334B2 (en) 2017-07-31 2022-12-06 General Electric Company Torch igniter for a combustor
US11391212B2 (en) 2018-09-12 2022-07-19 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11286861B2 (en) 2018-09-12 2022-03-29 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11391213B2 (en) 2018-09-12 2022-07-19 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11255271B2 (en) 2018-09-12 2022-02-22 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11408351B2 (en) 2018-09-12 2022-08-09 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11401867B2 (en) 2018-09-12 2022-08-02 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11415060B2 (en) 2018-09-12 2022-08-16 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US10865761B2 (en) * 2018-09-12 2020-12-15 Pratt & Whitney Canada Corp Igniter for gas turbine engine
US11268447B2 (en) 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11268486B2 (en) 2018-09-12 2022-03-08 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11454173B2 (en) 2018-09-12 2022-09-27 Pratt & Whitney Canada Corp. Igniter for gas turbine engine
US11608783B2 (en) 2020-11-04 2023-03-21 Delavan, Inc. Surface igniter cooling system
US11692488B2 (en) * 2020-11-04 2023-07-04 Delavan Inc. Torch igniter cooling system
US11473505B2 (en) 2020-11-04 2022-10-18 Delavan Inc. Torch igniter cooling system
US11635027B2 (en) 2020-11-18 2023-04-25 Collins Engine Nozzles, Inc. Fuel systems for torch ignition devices
US11421602B2 (en) 2020-12-16 2022-08-23 Delavan Inc. Continuous ignition device exhaust manifold
US11754289B2 (en) 2020-12-17 2023-09-12 Delavan, Inc. Axially oriented internally mounted continuous ignition device: removable nozzle
US11486309B2 (en) 2020-12-17 2022-11-01 Delavan Inc. Axially oriented internally mounted continuous ignition device: removable hot surface igniter
US11635210B2 (en) 2020-12-17 2023-04-25 Collins Engine Nozzles, Inc. Conformal and flexible woven heat shields for gas turbine engine components
US12092333B2 (en) 2020-12-17 2024-09-17 Collins Engine Nozzles, Inc. Radially oriented internally mounted continuous ignition device
US11209164B1 (en) * 2020-12-18 2021-12-28 Delavan Inc. Fuel injector systems for torch igniters
US11680528B2 (en) * 2020-12-18 2023-06-20 Delavan Inc. Internally-mounted torch igniters with removable igniter heads
KR102584126B1 (ko) * 2021-11-01 2023-09-27 한국항공우주연구원 가스터빈용 슬링거 연소기

Family Cites Families (18)

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Publication number Priority date Publication date Assignee Title
CH288548A (fr) * 1948-12-24 1953-01-31 Canadian Patents Dev Chambre de combustion pour turbine à gaz.
US2693082A (en) * 1951-04-04 1954-11-02 Gen Motors Corp Gas turbine fuel igniter
BE525083A (https=) * 1952-12-20
US2972231A (en) * 1954-09-23 1961-02-21 Ii James W Mullen Rod-igniters for ramjet burners
US2949012A (en) * 1957-03-01 1960-08-16 Snecma Vaporisation burner device
FR1217843A (fr) * 1958-12-10 1960-05-05 Snecma Brûleur de combustion ou de post-combustion pour combustible chaud
US4121419A (en) * 1977-01-26 1978-10-24 Kuznetsov Vladimir Grigorievic Start flame igniter of the combustion chamber of a gas-turbine engine
DE3728712A1 (de) * 1987-08-28 1989-03-09 Webasto Ag Fahrzeugtechnik Brenner fuer schwer-zuendliche gemische
US5167122A (en) * 1991-04-30 1992-12-01 Sundstrand Corporation Fuel system for a turbo machine
RU2083858C1 (ru) * 1993-03-02 1997-07-10 Омское моторостроительное конструкторское бюро Воспламенитель камеры сгорания газотурбинного двигателя
EP0992661B1 (de) * 1998-10-05 2003-12-03 ALSTOM (Switzerland) Ltd Zündbrenner für eine Brennkammer
DE10112864A1 (de) * 2001-03-16 2002-09-19 Alstom Switzerland Ltd Verfahren zum Zünden einer thermischen Turbomaschine
DE10211141A1 (de) * 2002-03-14 2003-09-25 Alstom Switzerland Ltd Verfahren zum Zünden der Brennkammer einer Gasturbinenanlage sowie Zündvorrichtung zur Durchführung des Verfahrens
JP3990678B2 (ja) * 2004-03-17 2007-10-17 川崎重工業株式会社 ガスタービン燃焼器
GB2444737B (en) * 2006-12-13 2009-03-04 Siemens Ag Improvements in or relating to burners for a gas turbine engine
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
EP2743588A1 (en) * 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Recessed fuel injector positioning
US9080772B2 (en) * 2013-06-13 2015-07-14 Delavan Inc Continuous ignition

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