DE602005001723D1 - Schubverstärker für Gasturbinenantriebe - Google Patents

Schubverstärker für Gasturbinenantriebe

Info

Publication number
DE602005001723D1
DE602005001723D1 DE602005001723T DE602005001723T DE602005001723D1 DE 602005001723 D1 DE602005001723 D1 DE 602005001723D1 DE 602005001723 T DE602005001723 T DE 602005001723T DE 602005001723 T DE602005001723 T DE 602005001723T DE 602005001723 D1 DE602005001723 D1 DE 602005001723D1
Authority
DE
Germany
Prior art keywords
amplifiers
thrust
gas turbine
turbine drives
drives
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.)
Active
Application number
DE602005001723T
Other languages
English (en)
Other versions
DE602005001723T2 (de
Inventor
John Michael Koshoffer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE602005001723D1 publication Critical patent/DE602005001723D1/de
Application granted granted Critical
Publication of DE602005001723T2 publication Critical patent/DE602005001723T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners

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)
DE602005001723T 2004-05-28 2005-05-18 Schubverstärker für Gasturbinenantriebe Active DE602005001723T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US856902 1997-05-15
US10/856,902 US6983601B2 (en) 2004-05-28 2004-05-28 Method and apparatus for gas turbine engines

Publications (2)

Publication Number Publication Date
DE602005001723D1 true DE602005001723D1 (de) 2007-09-06
DE602005001723T2 DE602005001723T2 (de) 2008-04-10

Family

ID=34941365

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005001723T Active DE602005001723T2 (de) 2004-05-28 2005-05-18 Schubverstärker für Gasturbinenantriebe

Country Status (3)

Country Link
US (1) US6983601B2 (de)
EP (1) EP1605207B1 (de)
DE (1) DE602005001723T2 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6895756B2 (en) * 2002-09-13 2005-05-24 The Boeing Company Compact swirl augmented afterburners for gas turbine engines
US7481059B2 (en) * 2004-08-12 2009-01-27 Volvo Aero Corporation Method and apparatus for providing an afterburner fuel-feed arrangement
US7188467B2 (en) * 2004-09-30 2007-03-13 General Electric Company Methods and apparatus for assembling a gas turbine engine
US7140174B2 (en) * 2004-09-30 2006-11-28 General Electric Company Methods and apparatus for assembling a gas turbine engine
US7627939B2 (en) * 2004-12-21 2009-12-08 Endress + Hauser Flowtec Ag In-line measuring device with measuring tube and method for manufacture thereof
US7225623B2 (en) * 2005-08-23 2007-06-05 General Electric Company Trapped vortex cavity afterburner
US20070134087A1 (en) * 2005-12-08 2007-06-14 General Electric Company Methods and apparatus for assembling turbine engines
US7467518B1 (en) * 2006-01-12 2008-12-23 General Electric Company Externally fueled trapped vortex cavity augmentor
US8011188B2 (en) * 2007-08-31 2011-09-06 General Electric Company Augmentor with trapped vortex cavity pilot
US8713909B2 (en) 2009-03-04 2014-05-06 United Technologies Corporation Elimination of unfavorable outflow margin
US8763400B2 (en) * 2009-08-04 2014-07-01 General Electric Company Aerodynamic pylon fuel injector system for combustors
US8984859B2 (en) * 2010-12-28 2015-03-24 Rolls-Royce North American Technologies, Inc. Gas turbine engine and reheat system
US8826667B2 (en) 2011-05-24 2014-09-09 General Electric Company System and method for flow control in gas turbine engine
US20140026590A1 (en) * 2012-07-25 2014-01-30 Hannes A. Alholm Flexible combustor bracket
US9416682B2 (en) * 2012-12-11 2016-08-16 United Technologies Corporation Turbine engine alignment assembly
US9879862B2 (en) 2013-03-08 2018-01-30 Rolls-Royce North American Technologies, Inc. Gas turbine engine afterburner
US10330011B2 (en) * 2013-03-11 2019-06-25 United Technologies Corporation Bench aft sub-assembly for turbine exhaust case fairing
CN104048325B (zh) * 2014-07-03 2016-01-06 中国科学院工程热物理研究所 一种双凹腔无焰燃烧器
WO2016203540A1 (ja) * 2015-06-16 2016-12-22 株式会社Ihi エンジン後部構造
RU2614029C1 (ru) * 2016-03-22 2017-03-22 Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") Опора вала ротора компрессора низкого давления газотурбинного двигателя (варианты), корпус задней опоры вала ротора, элемент вала ротора, полифункциональный внешний стяжной элемент вала ротора, соединительный элемент вала ротора, корпус подшипника задней опоры вала ротора
US10941938B2 (en) * 2018-02-22 2021-03-09 Delavan Inc. Fuel injectors including gas fuel injection
CN112031879A (zh) * 2020-09-18 2020-12-04 中国航发四川燃气涡轮研究院 涡轮后支板叶片及其航空发动机
MX2023004252A (es) * 2020-10-13 2023-04-25 House Of Metals Company Ltd Metodo para reciclar aleaciones de aluminio utilizando estimados de concentracion de contaminantes para control de calidad.
US11408610B1 (en) * 2021-02-03 2022-08-09 General Electric Company Systems and methods for spraying fuel in an augmented gas turbine engine

Family Cites Families (32)

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Publication number Priority date Publication date Assignee Title
US2603945A (en) * 1949-06-14 1952-07-22 Charles R Brown Jet engine with afterburner
US2674845A (en) * 1951-05-02 1954-04-13 Walter D Pouchot Diffuser apparatus with boundary layer control
US2862359A (en) * 1952-10-28 1958-12-02 Gen Motors Corp Fuel manifold and flameholder in combustion apparatus for jet engines
DE1139330B (de) * 1957-12-20 1962-11-08 Snecma Brennervorrichtung fuer im Gleichstrom arbeitende Strahltriebwerke
US3667680A (en) * 1970-04-24 1972-06-06 Boeing Co Jet engine exhaust nozzle system
US4686826A (en) * 1980-05-14 1987-08-18 The United States Of America As Represented By The Secretary Of The Air Force Mixed flow augmentor incorporating a fuel/air tube
FR2696502B1 (fr) * 1992-10-07 1994-11-04 Snecma Dispositif de post-combustion pour turbo réacteur double flux.
US5001898A (en) * 1986-08-29 1991-03-26 United Technologies Corporation Fuel distributor/flameholder for a duct burner
US4798048A (en) * 1987-12-21 1989-01-17 United Technologies Corporation Augmentor pilot
US4901527A (en) * 1988-02-18 1990-02-20 General Electric Company Low turbulence flame holder mount
US4920742A (en) * 1988-05-31 1990-05-01 General Electric Company Heat shield for gas turbine engine frame
DE3836912A1 (de) * 1988-09-01 1990-03-15 Mtu Muenchen Gmbh Verfahren zur brennstoffzufuehrung
FR2672641B1 (fr) * 1991-02-13 1995-01-13 Snecma Dispositif de post-combustion a volets pivotants.
EP0550126A1 (de) 1992-01-02 1993-07-07 General Electric Company Hitzeschild für Nachbrenner
FR2689567B1 (fr) * 1992-04-01 1994-05-27 Snecma Injecteur de carburant pour chambre de post-combustion d'une turbomachine.
FR2699227B1 (fr) * 1992-12-16 1995-01-13 Snecma Ensemble monobloc de post-combustion d'une turbine à gaz.
US5385015A (en) * 1993-07-02 1995-01-31 United Technologies Corporation Augmentor burner
US5617717A (en) * 1994-04-04 1997-04-08 Aero-Plasma, Inc. Flame stabilization system for aircraft jet engine augmentor using plasma plume ignitors
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
US5396761A (en) * 1994-04-25 1995-03-14 General Electric Company Gas turbine engine ignition flameholder with internal impingement cooling
US5685140A (en) * 1995-06-21 1997-11-11 United Technologies Corporation Method for distributing fuel within an augmentor
US5867980A (en) * 1996-12-17 1999-02-09 General Electric Company Turbofan engine with a low pressure turbine driven supercharger in a bypass duct operated by a fuel rich combustor and an afterburner
US5813221A (en) * 1997-01-14 1998-09-29 General Electric Company Augmenter with integrated fueling and cooling
FR2763648B1 (fr) * 1997-05-22 1999-07-02 Snecma Systeme de rechauffe dichotomique reduisant les pertes en sec
US6038852A (en) * 1997-12-05 2000-03-21 United Technologies Corporation Wear resistant augmentor fuel manifold clamp
US6125627A (en) * 1998-08-11 2000-10-03 Allison Advanced Development Company Method and apparatus for spraying fuel within a gas turbine engine
US6442930B1 (en) * 2000-03-31 2002-09-03 General Electric Company Combined cycle pulse detonation turbine engine
US6463739B1 (en) * 2001-02-05 2002-10-15 General Electric Company Afterburner heat shield
US6415609B1 (en) * 2001-03-15 2002-07-09 General Electric Company Replaceable afterburner heat shield
US6715983B2 (en) 2001-09-27 2004-04-06 General Electric Company Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
US7093442B2 (en) * 2003-04-30 2006-08-22 United Technologies Corporation Augmentor
US6971239B2 (en) * 2003-05-13 2005-12-06 United Technologies Corporation Augmentor pilot nozzle

Also Published As

Publication number Publication date
EP1605207A1 (de) 2005-12-14
EP1605207B1 (de) 2007-07-25
DE602005001723T2 (de) 2008-04-10
US6983601B2 (en) 2006-01-10
US20050262847A1 (en) 2005-12-01

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Legal Events

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