US4185462A
(en)
*
|
1978-04-05 |
1980-01-29 |
General Electric Company |
Fluid fitting for turbofan engines
|
GB2093584B
(en)
*
|
1981-02-21 |
1984-12-19 |
Rolls Royce |
Improvements in or relating to fuel burners and combustion equipment for use in gas turbine engines
|
FR2696502B1
(fr)
*
|
1992-10-07 |
1994-11-04 |
Snecma |
Dispositif de post-combustion pour turbo réacteur double flux.
|
US4765136A
(en)
*
|
1985-11-25 |
1988-08-23 |
United Technologies Corporation |
Gas turbine engine augmentor
|
US4817378A
(en)
*
|
1987-02-13 |
1989-04-04 |
General Electric Company |
Gas turbine engine with augmentor and variable area bypass injector
|
FR2610994B1
(fr)
*
|
1987-02-13 |
1993-06-11 |
Gen Electric |
Moteur a turbine a gaz avec dispositif de postcombustion et injecteur de dilution a section variable
|
US5076062A
(en)
*
|
1987-11-05 |
1991-12-31 |
General Electric Company |
Gas-cooled flameholder assembly
|
US4887425A
(en)
*
|
1988-03-18 |
1989-12-19 |
General Electric Company |
Fuel spraybar
|
US5088287A
(en)
*
|
1989-07-13 |
1992-02-18 |
Sundstrand Corporation |
Combustor for a turbine
|
EP0550126A1
(fr)
*
|
1992-01-02 |
1993-07-07 |
General Electric Company |
Bouclier thermique pour post-combusteur
|
FR2689567B1
(fr)
*
|
1992-04-01 |
1994-05-27 |
Snecma |
Injecteur de carburant pour chambre de post-combustion d'une turbomachine.
|
DE4309131A1
(de)
*
|
1993-03-22 |
1994-09-29 |
Abb Management Ag |
Verfahren und Vorrichtung zur Nachlaufbeeinflussung bei Brennkammereinbauten
|
FR2706588B1
(fr)
*
|
1993-06-16 |
1995-07-21 |
Snecma |
Système d'injection de carburant pour chambre de combustion.
|
US5402637A
(en)
*
|
1993-07-13 |
1995-04-04 |
Cooper Industries |
Igniter plug extender for a turbine engine combustor
|
US5617717A
(en)
*
|
1994-04-04 |
1997-04-08 |
Aero-Plasma, Inc. |
Flame stabilization system for aircraft jet engine augmentor using plasma plume ignitors
|
US5396761A
(en)
*
|
1994-04-25 |
1995-03-14 |
General Electric Company |
Gas turbine engine ignition flameholder with internal impingement cooling
|
US5396763A
(en)
*
|
1994-04-25 |
1995-03-14 |
General Electric Company |
Cooled spraybar and flameholder assembly including a perforated hollow inner air baffle for impingement cooling an outer heat shield
|
DE59409252D1
(de)
*
|
1994-09-21 |
2000-05-04 |
Abb Alstom Power Ch Ag |
Brennkammer einer Gasturbogruppe
|
GB2431984B
(en)
*
|
1996-11-07 |
2007-10-03 |
Rolls Royce Plc |
Afterburner igniter
|
US5813221A
(en)
*
|
1997-01-14 |
1998-09-29 |
General Electric Company |
Augmenter with integrated fueling and cooling
|
US6438940B1
(en)
*
|
1999-12-21 |
2002-08-27 |
General Electric Company |
Methods and apparatus for providing uniform ignition in an augmenter
|
US6415609B1
(en)
*
|
2001-03-15 |
2002-07-09 |
General Electric Company |
Replaceable afterburner heat shield
|
US6968694B2
(en)
*
|
2003-03-13 |
2005-11-29 |
United Technologies Corporation |
Augmentor
|
US7216488B2
(en)
*
|
2004-07-20 |
2007-05-15 |
General Electric Company |
Methods and apparatus for cooling turbine engine combustor ignition devices
|
US7481059B2
(en)
*
|
2004-08-12 |
2009-01-27 |
Volvo Aero Corporation |
Method and apparatus for providing an afterburner fuel-feed arrangement
|
US8044319B2
(en)
*
|
2005-02-07 |
2011-10-25 |
Pratt & Whitney Canada Corp. |
Variable arc gap plasma igniter
|
JP2006250374A
(ja)
*
|
2005-03-08 |
2006-09-21 |
Miura Co Ltd |
燃焼装置
|
US20080196414A1
(en)
*
|
2005-03-22 |
2008-08-21 |
Andreadis Dean E |
Strut cavity pilot and fuel injector assembly
|
US7571598B2
(en)
*
|
2005-05-19 |
2009-08-11 |
Virginia Tech Intellectual Properties, Inc. |
Plasma torch for ignition, flameholding and enhancement of combustion in high speed flows
|
US7647775B2
(en)
*
|
2005-06-30 |
2010-01-19 |
United Technologies Corporation |
Augmentor spray bars
|
US7596950B2
(en)
*
|
2005-09-16 |
2009-10-06 |
General Electric Company |
Augmentor radial fuel spray bar with counterswirling heat shield
|
US7637094B2
(en)
*
|
2005-12-16 |
2009-12-29 |
General Electric Company |
Cooling apparatus for a gas turbine engine igniter lead
|
EP2074318B1
(fr)
*
|
2006-10-12 |
2016-03-09 |
United Technologies Corporation |
Turboréacteur à double flux et procédé de réglage de la section de sortie
|
US8434292B2
(en)
*
|
2006-12-15 |
2013-05-07 |
State Of Franklin Innovations, Llc |
Ceramic-encased hot surface igniter system for jet engines
|
US8479490B2
(en)
*
|
2007-03-30 |
2013-07-09 |
Honeywell International Inc. |
Combustors with impingement cooled igniters and igniter tubes for improved cooling of igniters
|
JP5333044B2
(ja)
*
|
2009-08-21 |
2013-11-06 |
株式会社Ihi |
アフタバーナ及び航空機エンジン
|
US8893502B2
(en)
*
|
2011-10-14 |
2014-11-25 |
United Technologies Corporation |
Augmentor spray bar with tip support bushing
|
US9267687B2
(en)
*
|
2011-11-04 |
2016-02-23 |
General Electric Company |
Combustion system having a venturi for reducing wakes in an airflow
|
US8534071B1
(en)
*
|
2012-04-06 |
2013-09-17 |
United Technologies Corporation |
Engine hot section vane with tapered flame holder surface
|
US8997453B2
(en)
|
2012-06-29 |
2015-04-07 |
United Technologies Corporation |
Igniter for a turbomachine and mounting assembly therefor
|
US20140026590A1
(en)
*
|
2012-07-25 |
2014-01-30 |
Hannes A. Alholm |
Flexible combustor bracket
|
KR101265883B1
(ko)
*
|
2012-11-22 |
2013-05-20 |
에스티엑스중공업 주식회사 |
점화기 결합구조를 구비하는 마이크로 가스터빈 및 그 조립방법
|
US10156189B2
(en)
*
|
2014-01-28 |
2018-12-18 |
Pratt & Whitney Canada Corp. |
Combustor igniter assembly
|
US10145559B2
(en)
|
2015-12-15 |
2018-12-04 |
General Electric Company |
Gas turbine engine with igniter stack or borescope mount having noncollinear cooling passages
|
FR3097298B1
(fr)
*
|
2019-06-12 |
2021-06-04 |
Safran Aircraft Engines |
Bougie intégrée au bras accroche-flamme
|
US11408610B1
(en)
*
|
2021-02-03 |
2022-08-09 |
General Electric Company |
Systems and methods for spraying fuel in an augmented gas turbine engine
|
CN113669161A
(zh)
*
|
2021-08-24 |
2021-11-19 |
中国航发贵阳发动机设计研究所 |
一种带补氧结构的点火器
|
US11795879B2
(en)
*
|
2021-12-20 |
2023-10-24 |
General Electric Company |
Combustor with an igniter provided within at least one of a fuel injector or a compressed air passage
|