FR2653496B1 - Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique. - Google Patents

Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique.

Info

Publication number
FR2653496B1
FR2653496B1 FR9012959A FR9012959A FR2653496B1 FR 2653496 B1 FR2653496 B1 FR 2653496B1 FR 9012959 A FR9012959 A FR 9012959A FR 9012959 A FR9012959 A FR 9012959A FR 2653496 B1 FR2653496 B1 FR 2653496B1
Authority
FR
France
Prior art keywords
statoreactor
aircraft
sub
hypersonic flight
integrated turbo
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
FR9012959A
Other languages
English (en)
Other versions
FR2653496A1 (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
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 FR2653496A1 publication Critical patent/FR2653496A1/fr
Application granted granted Critical
Publication of FR2653496B1 publication Critical patent/FR2653496B1/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
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines
    • 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)
FR9012959A 1989-10-24 1990-10-19 Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique. Expired - Fee Related FR2653496B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19893935313 DE3935313C1 (fr) 1989-10-24 1989-10-24

Publications (2)

Publication Number Publication Date
FR2653496A1 FR2653496A1 (fr) 1991-04-26
FR2653496B1 true FR2653496B1 (fr) 1993-08-13

Family

ID=6392043

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9012959A Expired - Fee Related FR2653496B1 (fr) 1989-10-24 1990-10-19 Turbo-statoreacteur integre, equipant des avions pour vol sub et/ou hypersonique.

Country Status (4)

Country Link
US (1) US5148673A (fr)
JP (1) JPH03210053A (fr)
DE (1) DE3935313C1 (fr)
FR (1) FR2653496B1 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2692939B1 (fr) * 1992-06-24 1994-09-02 Snecma Réacteur combiné en statoréacteur et turboréacteur.
FR2873751B1 (fr) * 2004-07-28 2006-09-29 Snecma Moteurs Sa Cone d'entree d'une turbomachine
US7730714B2 (en) * 2005-11-29 2010-06-08 General Electric Company Turbofan gas turbine engine with variable fan outlet guide vanes
US8429893B2 (en) 2009-08-11 2013-04-30 Northrop Grumman Corporation Airflow modulation for dual mode combined cycle propulsion systems
DE102010001059A1 (de) * 2010-01-20 2011-07-21 Rolls-Royce Deutschland Ltd & Co KG, 15827 Zwischengehäuse für ein Gasturbinentriebwerk
US9115593B2 (en) 2012-04-02 2015-08-25 United Technologies Corporation Turbomachine thermal management
US9062566B2 (en) 2012-04-02 2015-06-23 United Technologies Corporation Turbomachine thermal management
US9127566B2 (en) 2012-04-02 2015-09-08 United Technologies Corporation Turbomachine thermal management
FR3052493A1 (fr) * 2016-06-14 2017-12-15 Guillaume Thomas Pelcot Reacteur combine et les moyens de permutation entre ses deux modes de fonctionnement
CN108757221A (zh) * 2018-05-30 2018-11-06 南京理工大学 一种液体亚燃冲压发动机

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3296800A (en) * 1967-01-10 Gas turbine power plant
GB799504A (en) * 1955-03-11 1958-08-13 Power Jets Res & Dev Ltd An improved air intake duct for a jet propulsion plant
GB861101A (en) * 1957-09-03 1961-02-15 United Aircraft Corp Combination power plant for an aircraft
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
DE1144060B (de) * 1960-08-04 1963-02-21 Daimler Benz Ag Verbundtriebwerk fuer Flugzeuge
US3153904A (en) * 1961-12-29 1964-10-27 Stanley H Ellis Turbo-ramjet configuration
FR1408812A (fr) * 1964-07-06 1965-08-20 Nord Aviat Perfectionnement apporté aux chambres de combustion de propulseurs
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
DE3912330A1 (de) * 1989-04-14 1990-10-18 Mtu Muenchen Gmbh Integriertes turbo-staustrahltriebwerk
DE3912392A1 (de) * 1989-04-14 1990-10-25 Mtu Muenchen Gmbh Turbinen-staustrahltriebwerk

Also Published As

Publication number Publication date
FR2653496A1 (fr) 1991-04-26
US5148673A (en) 1992-09-22
DE3935313C1 (fr) 1991-06-06
JPH03210053A (ja) 1991-09-13

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Legal Events

Date Code Title Description
ST Notification of lapse