FR2658248B1 - Ensemble moteur a turbine a gaz-statoreacteur comportant une entree d'air variable. - Google Patents

Ensemble moteur a turbine a gaz-statoreacteur comportant une entree d'air variable.

Info

Publication number
FR2658248B1
FR2658248B1 FR919100983A FR9100983A FR2658248B1 FR 2658248 B1 FR2658248 B1 FR 2658248B1 FR 919100983 A FR919100983 A FR 919100983A FR 9100983 A FR9100983 A FR 9100983A FR 2658248 B1 FR2658248 B1 FR 2658248B1
Authority
FR
France
Prior art keywords
statoreactor
gas
air intake
turbine engine
engine assembly
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
FR919100983A
Other languages
English (en)
Other versions
FR2658248A1 (fr
Inventor
Heinrich Enderle
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 GmbH
Rolls Royce Solutions GmbH
Original Assignee
MTU Motoren und Turbinen Union Friedrichshafen GmbH
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 Friedrichshafen GmbH, MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Friedrichshafen GmbH
Publication of FR2658248A1 publication Critical patent/FR2658248A1/fr
Application granted granted Critical
Publication of FR2658248B1 publication Critical patent/FR2658248B1/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
    • 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
    • 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
    • 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)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR919100983A 1990-02-13 1991-01-29 Ensemble moteur a turbine a gaz-statoreacteur comportant une entree d'air variable. Expired - Fee Related FR2658248B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4004416A DE4004416C2 (de) 1990-02-13 1990-02-13 Turbo-Staustrahltriebwerk mit Absperreinrichtung für variablen Umschaltbetrieb

Publications (2)

Publication Number Publication Date
FR2658248A1 FR2658248A1 (fr) 1991-08-16
FR2658248B1 true FR2658248B1 (fr) 1993-08-13

Family

ID=6400053

Family Applications (1)

Application Number Title Priority Date Filing Date
FR919100983A Expired - Fee Related FR2658248B1 (fr) 1990-02-13 1991-01-29 Ensemble moteur a turbine a gaz-statoreacteur comportant une entree d'air variable.

Country Status (5)

Country Link
US (1) US5165228A (fr)
JP (1) JPH04219421A (fr)
DE (1) DE4004416C2 (fr)
FR (1) FR2658248B1 (fr)
GB (1) GB2241745B (fr)

Families Citing this family (14)

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US6584764B2 (en) 2000-01-12 2003-07-01 Allison Advanced Development Company Propulsion module
DE10033653A1 (de) * 2000-06-16 2002-03-07 Sandor Nagy Kombinationsantrieb
DE10126632A1 (de) * 2000-08-08 2002-09-12 Sandor Nagy Kombinationsantrieb
CN101014495A (zh) * 2004-10-29 2007-08-08 菲利克斯·桑切斯·桑切斯 空气喷射推进器
US7540142B2 (en) * 2006-02-21 2009-06-02 Honeywell International Inc. Multiple auxiliary power unit system inlet ducts controlled by a single actuator
CN100458189C (zh) * 2007-03-13 2009-02-04 南京航空航天大学 激波形状控制器
DE102008026117A1 (de) * 2008-05-30 2009-12-10 Airbus Deutschland Gmbh Frischlufteinlass für ein Flugzeug
US8678310B2 (en) * 2011-08-22 2014-03-25 Honeywell International Inc. Ducted ram air generator assembly
US9957060B2 (en) 2012-03-21 2018-05-01 Hamilton Sundstrand Corporation Deployable inlet scoop for an inboard ram air turbine
JP6183836B2 (ja) * 2013-08-12 2017-08-23 株式会社Ｉｈｉエアロスペース ポートカバー開口装置
US9862482B2 (en) * 2015-09-04 2018-01-09 The Boeing Company Variable geometry flush boundary diverter
CN109667670B (zh) * 2019-01-24 2021-03-09 南京航空航天大学 一种辅助超/高超声速二元进气道起动的涡控可调活门装置
US11258333B2 (en) * 2019-07-29 2022-02-22 Aurora Flight Sciences Corporation Propulsor system with integrated passive cooling
CN116773274B (zh) * 2023-08-28 2023-10-24 成都成高阀门股份有限公司 一种基于球阀的取样装置及取样方法

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE1131467B (de) * 1959-04-30 1962-06-14 Daimler Benz Ag Verbundtriebwerk zum Antrieb von Flugzeugen
FR1271544A (fr) * 1960-07-11 1961-09-15 Nord Aviation Combiné turboréacteur-statoréacteur
US3153904A (en) * 1961-12-29 1964-10-27 Stanley H Ellis Turbo-ramjet configuration
GB971222A (en) * 1962-12-17 1964-09-30 Rolls Royce Gas turbine power plant
US3242671A (en) * 1964-04-08 1966-03-29 Boeing Co Fixed spike inlet with variable throat and capture area
US3490472A (en) * 1968-01-19 1970-01-20 Rolls Royce Air intake duct for a gas turbine engine
US3568694A (en) * 1968-05-08 1971-03-09 Lockheed Aircraft Corp Jet engine installation for noise control
FR1586188A (fr) * 1968-09-06 1970-02-13
US4085583A (en) * 1975-03-31 1978-04-25 The Boeing Company Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine
US4068471A (en) * 1975-06-16 1978-01-17 General Electric Company Variable cycle engine with split fan section
IL59497A (en) * 1979-04-23 1984-08-31 Gen Electric Valve actuation system for use on a gas turbine engine
DE3217741A1 (de) * 1982-05-12 1983-11-17 General Electric Co., Schenectady, N.Y. Betaetigungsvorrichtung
US4477039A (en) * 1982-06-30 1984-10-16 Mcdonnell Douglas Corporation Vented cowl variable geometry inlet for aircraft
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
DE3811614C1 (fr) * 1988-04-07 1989-05-18 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
DE3836912A1 (de) * 1988-09-01 1990-03-15 Mtu Muenchen Gmbh Verfahren zur brennstoffzufuehrung
DE3912330A1 (de) * 1989-04-14 1990-10-18 Mtu Muenchen Gmbh Integriertes turbo-staustrahltriebwerk

Also Published As

Publication number Publication date
DE4004416C2 (de) 1993-10-14
GB9102970D0 (en) 1991-03-27
DE4004416A1 (de) 1991-08-14
FR2658248A1 (fr) 1991-08-16
JPH04219421A (ja) 1992-08-10
US5165228A (en) 1992-11-24
GB2241745A (en) 1991-09-11
GB2241745B (en) 1994-03-30

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Legal Events

Date Code Title Description
ST Notification of lapse