DE8915860U1 - - Google Patents

Info

Publication number
DE8915860U1
DE8915860U1 DE8915860U DE8915860U DE8915860U1 DE 8915860 U1 DE8915860 U1 DE 8915860U1 DE 8915860 U DE8915860 U DE 8915860U DE 8915860 U DE8915860 U DE 8915860U DE 8915860 U1 DE8915860 U1 DE 8915860U1
Authority
DE
Germany
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.)
Expired - Lifetime
Application number
DE8915860U
Other languages
German (de)
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
MTU Aero Engines GmbH
Original Assignee
Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
MTU Motoren und Turbinen Union Muenchen GmbH
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 Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR, MTU Motoren und Turbinen Union Muenchen GmbH filed Critical Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
Publication of DE8915860U1 publication Critical patent/DE8915860U1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
DE8915860U 1989-02-08 1989-02-08 Expired - Lifetime DE8915860U1 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3903713A DE3903713A1 (de) 1989-02-08 1989-02-08 Strahltriebwerk

Publications (1)

Publication Number Publication Date
DE8915860U1 true DE8915860U1 (ja) 1991-12-05

Family

ID=6373644

Family Applications (2)

Application Number Title Priority Date Filing Date
DE3903713A Withdrawn DE3903713A1 (de) 1989-02-08 1989-02-08 Strahltriebwerk
DE8915860U Expired - Lifetime DE8915860U1 (ja) 1989-02-08 1989-02-08

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE3903713A Withdrawn DE3903713A1 (de) 1989-02-08 1989-02-08 Strahltriebwerk

Country Status (3)

Country Link
DE (2) DE3903713A1 (ja)
FR (1) FR2642793A1 (ja)
GB (1) GB2231092A (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006019299B3 (de) * 2006-04-26 2007-11-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Ummanteltes Turbofan-Flugzeugtriebwerk

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5154052A (en) * 1990-05-07 1992-10-13 General Electric Company Exhaust assembly for a high speed civil transport aircraft engine
GB2259955A (en) * 1990-05-17 1993-03-31 Secr Defence Variable cycle gas turbine engine for supersonic aircraft
GB2244098A (en) * 1990-05-17 1991-11-20 Secr Defence Variable configuration gas turbine engine
US5157916A (en) * 1990-11-02 1992-10-27 United Technologies Corporation Apparatus and method for suppressing sound in a gas turbine engine powerplant
DE102004004076B4 (de) * 2004-01-27 2005-11-24 Universität Stuttgart Turboflugtriebwerk mit internem Mischer
DE102011008773A1 (de) 2011-01-18 2012-07-19 Mtu Aero Engines Gmbh Wärmetauscher und Strahltriebwerk mit solchem

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB777694A (en) * 1952-04-16 1957-06-26 Devendra Nath Sharma Improvements relating to internal combustion turbines in combination with ram-jet engines
US3463402A (en) * 1966-12-28 1969-08-26 United Aircraft Corp Jet sound suppressing means
GB1125658A (en) * 1967-06-30 1968-08-28 Rolls Royce Gas turbine by-pass engine
DE1923150A1 (de) * 1968-05-08 1970-01-15 Man Turbo Gmbh Zweistromturbinenstrahltriebwerk
BE755612A (fr) * 1969-06-18 1971-02-15 Gen Electric Tuyeres de propulsion a systeme suppresseur de bruit ameliore
US3625009A (en) * 1970-06-05 1971-12-07 Boeing Co Multi-tube noise suppressor providing thrust augmentation
GB1409887A (en) * 1972-12-18 1975-10-15 Secr Defence Aircraft gas turbine engine noise suppression
US4064692A (en) * 1975-06-02 1977-12-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable cycle gas turbine engines
US4175384A (en) * 1977-08-02 1979-11-27 General Electric Company Individual bypass injector valves for a double bypass variable cycle turbofan engine
US4134260A (en) * 1977-10-25 1979-01-16 General Motors Corporation Afterburner flow mixing means in turbofan jet engine
US4285194A (en) * 1979-04-23 1981-08-25 General Electric Company Apparatus and method for controlling fan duct flow in a gas turbine engine
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
DE3606286A1 (de) * 1985-03-04 1986-09-04 General Electric Co., Schenectady, N.Y. Verfahren und einrichtung zum steuern des kuehlmittelstroemungsflusses in einer nachbrennerauskleidung
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
FR2626044A1 (fr) * 1988-01-14 1989-07-21 Snecma Melangeur de flux a section variable avec stabilisateur de rechauffe integre pour turboreacteur double flux

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006019299B3 (de) * 2006-04-26 2007-11-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Ummanteltes Turbofan-Flugzeugtriebwerk

Also Published As

Publication number Publication date
GB2231092A (en) 1990-11-07
DE3903713A1 (de) 1990-08-09
FR2642793A1 (fr) 1990-08-10
GB9002858D0 (en) 1990-04-04

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