FR923996A - Propulseur rotatif canalisé - Google Patents

Propulseur rotatif canalisé

Info

Publication number
FR923996A
FR923996A FR923996DA FR923996A FR 923996 A FR923996 A FR 923996A FR 923996D A FR923996D A FR 923996DA FR 923996 A FR923996 A FR 923996A
Authority
FR
France
Prior art keywords
channeled
rotary thruster
thruster
rotary
channeled rotary
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
Application number
Other languages
English (en)
Inventor
Louis Breguet
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 filed Critical
Application granted granted Critical
Publication of FR923996A publication Critical patent/FR923996A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001—Shrouded propellers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR923996D 1946-02-15 1946-02-15 Propulseur rotatif canalisé Expired FR923996A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR923996T 1946-02-15

Publications (1)

Publication Number Publication Date
FR923996A true FR923996A (fr) 1947-07-23

Family

ID=9439085

Family Applications (1)

Application Number Title Priority Date Filing Date
FR923996D Expired FR923996A (fr) 1946-02-15 1946-02-15 Propulseur rotatif canalisé

Country Status (1)

Country Link
FR (1) FR923996A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE963203C (de) * 1952-05-06 1957-05-02 Alfred Buechi Propellerturbinentriebwerk
US3528752A (en) * 1966-04-12 1970-09-15 Dowty Rotol Ltd Gas turbine engines
EP0244515A2 (fr) * 1986-04-16 1987-11-11 The Boeing Company Moteur d'avion à soufflante avec carénage tournant
FR2615906A1 (fr) * 1987-05-27 1988-12-02 Mtu Muenchen Gmbh Reacteur combine, commutable, pour l'entrainement d'avions et d'engins speciaux
EP2426342A3 (fr) * 2006-10-12 2012-05-09 United Technologies Corporation Turboréacteur à double flux doté d'une zone de sortie variable et procédé de fonctionnement

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE963203C (de) * 1952-05-06 1957-05-02 Alfred Buechi Propellerturbinentriebwerk
US3528752A (en) * 1966-04-12 1970-09-15 Dowty Rotol Ltd Gas turbine engines
EP0244515A2 (fr) * 1986-04-16 1987-11-11 The Boeing Company Moteur d'avion à soufflante avec carénage tournant
EP0244515A3 (fr) * 1986-04-16 1989-04-12 The Boeing Company Moteur d'avion à soufflante avec carénage tournant
FR2615906A1 (fr) * 1987-05-27 1988-12-02 Mtu Muenchen Gmbh Reacteur combine, commutable, pour l'entrainement d'avions et d'engins speciaux
EP2426342A3 (fr) * 2006-10-12 2012-05-09 United Technologies Corporation Turboréacteur à double flux doté d'une zone de sortie variable et procédé de fonctionnement
US8480350B2 (en) 2006-10-12 2013-07-09 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation

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