DE3803992A1 - Gasturbinentriebwerk mit nachbrenner und verstellbarem bypass-injektor - Google Patents

Gasturbinentriebwerk mit nachbrenner und verstellbarem bypass-injektor

Info

Publication number
DE3803992A1
DE3803992A1 DE19883803992 DE3803992A DE3803992A1 DE 3803992 A1 DE3803992 A1 DE 3803992A1 DE 19883803992 DE19883803992 DE 19883803992 DE 3803992 A DE3803992 A DE 3803992A DE 3803992 A1 DE3803992 A1 DE 3803992A1
Authority
DE
Germany
Prior art keywords
hollow
bypass
core
gas
gases
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.)
Withdrawn
Application number
DE19883803992
Other languages
German (de)
English (en)
Inventor
Iii Rollin George Giffin
Ivan Elmer Woltmann
Donald Patric Machugh
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 DE3803992A1 publication Critical patent/DE3803992A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • 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

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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Combustion Of Fluid Fuel (AREA)
DE19883803992 1987-02-13 1988-02-10 Gasturbinentriebwerk mit nachbrenner und verstellbarem bypass-injektor Withdrawn DE3803992A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1456287A 1987-02-13 1987-02-13

Publications (1)

Publication Number Publication Date
DE3803992A1 true DE3803992A1 (de) 1988-08-25

Family

ID=21766218

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19883803992 Withdrawn DE3803992A1 (de) 1987-02-13 1988-02-10 Gasturbinentriebwerk mit nachbrenner und verstellbarem bypass-injektor

Country Status (5)

Country Link
JP (1) JPS63227930A (ja)
DE (1) DE3803992A1 (ja)
FR (1) FR2610994B1 (ja)
GB (1) GB2202589B (ja)
SE (1) SE466559B (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1865260A3 (en) * 2006-06-05 2015-06-03 General Electric Company Secondary fuel injection from stage one turbine nozzle

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3903713A1 (de) * 1989-02-08 1990-08-09 Mtu Muenchen Gmbh Strahltriebwerk
US5261229A (en) * 1992-08-03 1993-11-16 General Electric Company Noise-suppressed exhaust nozzles for jet engines
FR2712962B1 (fr) * 1993-11-24 1995-12-29 Snecma Dispositif de postcombustion comprenant un dispositif accroche-flammes perfectionné.
FR2763648B1 (fr) * 1997-05-22 1999-07-02 Snecma Systeme de rechauffe dichotomique reduisant les pertes en sec
US7596950B2 (en) * 2005-09-16 2009-10-06 General Electric Company Augmentor radial fuel spray bar with counterswirling heat shield
JP5625585B2 (ja) * 2010-07-27 2014-11-19 株式会社Ihi アフタバーナ及び航空機エンジン
JP6229590B2 (ja) * 2014-04-30 2017-11-15 株式会社Ihi アフタバーナ及び航空機エンジン

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
GB928475A (en) * 1961-12-27 1963-06-12 Rolls Royce Improvements in or relating to by-pass gas turbine engines
GB1029900A (en) * 1964-11-27 1966-05-18 Rolls Royce By-pass gas turbine jet engine
DE1923150A1 (de) * 1968-05-08 1970-01-15 Man Turbo Gmbh Zweistromturbinenstrahltriebwerk
US4335573A (en) * 1970-09-02 1982-06-22 General Electric Company Gas turbine engine mixer
US3698186A (en) * 1970-12-24 1972-10-17 United Aircraft Corp Afterburner combustion apparatus
BE795529A (fr) * 1972-02-17 1973-06-18 Gen Electric Allumeur monte sur un dispositif d'augmentation de la poussee de turboreacteurs et refroidi a l'air
US4072008A (en) * 1976-05-04 1978-02-07 General Electric Company Variable area bypass injector system
JPS5641815A (en) * 1979-09-12 1981-04-18 Mitsui Toatsu Chem Inc Purifying method for wet process phosphoric acid solution
US4461146A (en) * 1982-10-22 1984-07-24 The United States Of America As Represented By The Secretary Of The Navy Mixed flow swirl augmentor for turbofan engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1865260A3 (en) * 2006-06-05 2015-06-03 General Electric Company Secondary fuel injection from stage one turbine nozzle

Also Published As

Publication number Publication date
JPS63227930A (ja) 1988-09-22
SE8800465L (sv) 1988-08-14
SE466559B (sv) 1992-03-02
SE8800465D0 (sv) 1988-02-11
GB8803121D0 (en) 1988-03-09
GB2202589A (en) 1988-09-28
FR2610994B1 (fr) 1993-06-11
FR2610994A1 (fr) 1988-08-19
GB2202589B (en) 1991-10-02
JPH0587652B2 (ja) 1993-12-17

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Legal Events

Date Code Title Description
8128 New person/name/address of the agent

Representative=s name: VOIGT, R., DIPL.-ING., PAT.-ANW., 6232 BAD SODEN

8139 Disposal/non-payment of the annual fee