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FR2656377B1 - Installation pour liberer ou fermer l'entree d'air aspire ou la sortie des gaz d'echappement d'une turbine. - Google Patents

Installation pour liberer ou fermer l'entree d'air aspire ou la sortie des gaz d'echappement d'une turbine.

Info

Publication number
FR2656377B1
FR2656377B1 FR9016118A FR9016118A FR2656377B1 FR 2656377 B1 FR2656377 B1 FR 2656377B1 FR 9016118 A FR9016118 A FR 9016118A FR 9016118 A FR9016118 A FR 9016118A FR 2656377 B1 FR2656377 B1 FR 2656377B1
Authority
FR
France
Prior art keywords
turbine
releasing
closing
installation
air inlet
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.)
Expired - Fee Related
Application number
FR9016118A
Other languages
English (en)
Other versions
FR2656377A1 (fr
Inventor
Claus Herzog
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.)
MTU Aero Engines AG
Original Assignee
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2656377A1 publication Critical patent/FR2656377A1/fr
Application granted granted Critical
Publication of FR2656377B1 publication Critical patent/FR2656377B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
FR9016118A 1989-12-21 1990-12-21 Installation pour liberer ou fermer l'entree d'air aspire ou la sortie des gaz d'echappement d'une turbine. Expired - Fee Related FR2656377B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3942323A DE3942323C2 (de) 1989-12-21 1989-12-21 Einlaufkonfiguration für ein kombiniertes Turbo-Staustrahltriebwerk

Publications (2)

Publication Number Publication Date
FR2656377A1 FR2656377A1 (fr) 1991-06-28
FR2656377B1 true FR2656377B1 (fr) 1993-08-20

Family

ID=6396043

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9016118A Expired - Fee Related FR2656377B1 (fr) 1989-12-21 1990-12-21 Installation pour liberer ou fermer l'entree d'air aspire ou la sortie des gaz d'echappement d'une turbine.

Country Status (4)

Country Link
US (1) US5150571A (fr)
DE (1) DE3942323C2 (fr)
FR (1) FR2656377B1 (fr)
GB (1) GB2240814B (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2763098B1 (fr) * 1997-05-07 1999-06-11 Snecma Systeme d'admission d'air dans une veine de turbomachine
US8371124B2 (en) * 2008-04-15 2013-02-12 Aerion Corporation Jet nozzle plug with varying, non-circular cross sections
US8429893B2 (en) 2009-08-11 2013-04-30 Northrop Grumman Corporation Airflow modulation for dual mode combined cycle propulsion systems
US9291101B2 (en) * 2013-02-28 2016-03-22 United Technologies Corporation Gas turbine engine inlet wall design
US20160102609A1 (en) * 2014-10-09 2016-04-14 United Technologies Corporation Pulse detonation combustor
US10822100B2 (en) * 2017-06-26 2020-11-03 General Electric Company Hybrid electric propulsion system for an aircraft
CN114837811A (zh) * 2022-04-19 2022-08-02 南京航空航天大学 一种延伸外机匣的组合动力模态转换方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2570629A (en) * 1945-10-05 1951-10-09 Anxionnaz Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles
US2955414A (en) * 1957-09-03 1960-10-11 United Aircraft Corp Combined power plant
US2970431A (en) * 1959-01-02 1961-02-07 Curtiss Wright Corp Rotating inlet for jet engines
US3242671A (en) * 1964-04-08 1966-03-29 Boeing Co Fixed spike inlet with variable throat and capture area
US3495605A (en) * 1965-09-29 1970-02-17 Boeing Co Annular internal compression supersonic air inlet
FR1496091A (fr) * 1966-04-20 1967-09-29 Snecma Tuyère d'éjection pour propulseurs à plusieurs flux moteurs, notamment à deux flux moteurs
US3659422A (en) * 1966-11-04 1972-05-02 North American Rockwell Method and apparatus for aircraft propulsion
GB1190774A (en) * 1967-04-05 1970-05-06 Rolls Royce Improvements relating to the Silencing of Gas Turbine Engines
US3841091A (en) * 1973-05-21 1974-10-15 Gen Electric Multi-mission tandem propulsion system
DE3236487C2 (de) * 1982-10-01 1984-07-19 Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt e.V., 5000 Köln Rotationssymmetrischer Überschall-Lufteinlauf für Strahltriebwerke
DE3738703A1 (de) * 1987-05-27 1988-12-08 Mtu Muenchen Gmbh Kombiniertes, umschaltbares strahltriebwerk zum antrieb von flugzeugen und raumfahrzeugen
DE3836912A1 (de) * 1988-09-01 1990-03-15 Mtu Muenchen Gmbh Verfahren zur brennstoffzufuehrung

Also Published As

Publication number Publication date
US5150571A (en) 1992-09-29
GB2240814B (en) 1994-06-01
GB2240814A (en) 1991-08-14
GB9027941D0 (en) 1991-02-13
DE3942323C2 (de) 1993-11-25
DE3942323A1 (de) 1991-06-27
FR2656377A1 (fr) 1991-06-28

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Legal Events

Date Code Title Description
ST Notification of lapse