FR2580725B1 - Module propulsif pour un moteur a turbine a gaz aeronautique - Google Patents

Module propulsif pour un moteur a turbine a gaz aeronautique

Info

Publication number
FR2580725B1
FR2580725B1 FR868605191A FR8605191A FR2580725B1 FR 2580725 B1 FR2580725 B1 FR 2580725B1 FR 868605191 A FR868605191 A FR 868605191A FR 8605191 A FR8605191 A FR 8605191A FR 2580725 B1 FR2580725 B1 FR 2580725B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
aeronautical gas
propulsive
module
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
FR868605191A
Other languages
English (en)
Other versions
FR2580725A1 (fr
Inventor
William Butler Wright
Addison Charles Maguire
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2580725A1 publication Critical patent/FR2580725A1/fr
Application granted granted Critical
Publication of FR2580725B1 publication Critical patent/FR2580725B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
FR868605191A 1985-04-17 1986-04-11 Module propulsif pour un moteur a turbine a gaz aeronautique Expired - Fee Related FR2580725B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8509837A GB2173863B (en) 1985-04-17 1985-04-17 A propeller module for an aero gas turbine engine

Publications (2)

Publication Number Publication Date
FR2580725A1 FR2580725A1 (fr) 1986-10-24
FR2580725B1 true FR2580725B1 (fr) 1991-05-10

Family

ID=10577792

Family Applications (1)

Application Number Title Priority Date Filing Date
FR868605191A Expired - Fee Related FR2580725B1 (fr) 1985-04-17 1986-04-11 Module propulsif pour un moteur a turbine a gaz aeronautique

Country Status (5)

Country Link
US (1) US4688995A (fr)
JP (1) JPS61268598A (fr)
DE (1) DE3611792C2 (fr)
FR (1) FR2580725B1 (fr)
GB (1) GB2173863B (fr)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2182397B (en) * 1985-11-02 1989-10-04 Rolls Royce Plc Propeller module for an aero gas turbine engine
GB2209575A (en) * 1987-09-05 1989-05-17 Rolls Royce Plc A gearbox arrangement for driving contra-rotating multi-bladed rotors
DE3905282C1 (en) * 1987-10-13 1990-05-31 Karl Dipl.-Ing. 2742 Gnarrenburg De Kastens Propeller fan
DE3812027A1 (de) * 1988-04-11 1989-10-26 Mtu Muenchen Gmbh Propfan-turbotriebwerk
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
US4936746A (en) * 1988-10-18 1990-06-26 United Technologies Corporation Counter-rotation pitch change system
DE3837994A1 (de) * 1988-11-09 1990-05-10 Mtu Muenchen Gmbh Vorrichtung zur verstellung der rotorschaufeln eines propfan/turboproptriebwerkes
US5010729A (en) * 1989-01-03 1991-04-30 General Electric Company Geared counterrotating turbine/fan propulsion system
US4968217A (en) * 1989-09-06 1990-11-06 Rolls-Royce Plc Variable pitch arrangement for a gas turbine engine
DE3933776A1 (de) * 1989-10-10 1991-04-18 Mtu Muenchen Gmbh Propfan-turbotriebwerk
US5070413A (en) * 1989-10-10 1991-12-03 Eastman Kodak Company Color digital halftoning with vector error diffusion
US5954479A (en) * 1996-12-16 1999-09-21 Smith; Ronald A. Twin engine, coaxial, dual-propeller propulsion system
KR100432490B1 (ko) 2001-09-17 2004-05-22 (주)니트 젠 광학식 지문취득 장치
US7144349B2 (en) * 2004-04-06 2006-12-05 Pratt & Whitney Canada Corp. Gas turbine gearbox
DE102005043615B4 (de) * 2005-09-09 2009-11-19 König, Christian Propellerantriebseinheit
US7685808B2 (en) * 2005-10-19 2010-03-30 General Electric Company Gas turbine engine assembly and methods of assembling same
US7493753B2 (en) * 2005-10-19 2009-02-24 General Electric Company Gas turbine engine assembly and methods of assembling same
US7526913B2 (en) * 2005-10-19 2009-05-05 General Electric Company Gas turbine engine assembly and methods of assembling same
US7513103B2 (en) * 2005-10-19 2009-04-07 General Electric Company Gas turbine engine assembly and methods of assembling same
US7726113B2 (en) * 2005-10-19 2010-06-01 General Electric Company Gas turbine engine assembly and methods of assembling same
US7490461B2 (en) * 2005-10-19 2009-02-17 General Electric Company Gas turbine engine assembly and methods of assembling same
US8210798B2 (en) 2008-02-13 2012-07-03 United Technologies Corporation Cooled pusher propeller system
FR2928977B1 (fr) * 2008-03-21 2010-04-09 Snecma Systeme d'helices contrarotatives disposant d'un dispositif de mise en drapeau des pales d'helices
FR2931797B1 (fr) * 2008-05-29 2010-07-30 Snecma Systeme simplifie de commande de calage de pale d'une helice d'un turbomoteur pour aeronef
US8186951B2 (en) * 2008-07-14 2012-05-29 Hamilton Sundstrand Corporation Mounting assembly for a propeller system component
FR2942203B1 (fr) * 2009-02-13 2011-04-22 Snecma Systeme d'helices contrarotatives a encombrement reduit
DE102009010524A1 (de) * 2009-02-25 2010-09-02 Rolls-Royce Deutschland Ltd & Co Kg Turbopropantrieb mit Druckpropeller
FR2945512B1 (fr) * 2009-05-15 2012-08-24 Snecma Helice non carenee a pales a calage variable pour une turbomachine
FR2956378B1 (fr) * 2010-02-15 2012-05-11 Snecma Turbopropulseur muni d'un dispositif d'orientation de pales
US8701381B2 (en) 2010-11-24 2014-04-22 Rolls-Royce Corporation Remote shaft driven open rotor propulsion system with electrical power generation
EP2971517B1 (fr) * 2013-03-15 2021-08-18 Raytheon Technologies Corporation Dégivrage par production de chaleur électrique intégrée
US9701395B2 (en) 2014-01-06 2017-07-11 United Technologies Corporation Contra-rotating open rotor distributed propulsion system
FR3050431B1 (fr) 2016-04-20 2018-04-27 Safran Aircraft Engines Systeme d'actionnement simplifie de pas pour une helice de turbomachine
US10737801B2 (en) * 2016-10-31 2020-08-11 Rolls-Royce Corporation Fan module with rotatable vane ring power system
US10618667B2 (en) 2016-10-31 2020-04-14 Rolls-Royce Corporation Fan module with adjustable pitch blades and power system
FR3087849B1 (fr) * 2018-10-26 2020-11-20 Safran Aircraft Engines Turbomachine a double helices non carenees

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB544948A (en) * 1938-10-13 1942-05-05 Daimler Benz Ag Improvements in and connected with variable pitch airscrews
GB531756A (en) * 1939-06-14 1941-01-10 John Stafford Northcote Device employing epicyclic or bevel gears or a combination of both for controlling the pitch of variable pitch airscrews
US2394299A (en) * 1940-02-05 1946-02-05 Friedrich Albert Drive for oppositely rotating propellers
DE880103C (de) * 1940-02-06 1953-06-18 Daimler Benz Ag Antrieb fuer gegenlaeufige Luftschrauben
FR865942A (fr) * 1940-02-16 1941-06-09 Dispositif de liaison entre un arbre moteur et deux hélices co-axiales et mécanisme de commande des changements de pas de ces hélices
GB575765A (en) * 1941-04-15 1946-03-05 Haviland Aircraft Company Ltd Improvements in variable pitch propellers
FR887543A (fr) * 1941-11-06 1943-11-16 Bmw Flugmotorenbau Gmbh Hélices à pas variable, tournant en sens inverse
BE468782A (fr) * 1942-01-12
FR977459A (fr) * 1942-07-08 1951-04-02 Perfectionnements aux mécanismes d'accouplement et de commande des variations de pas des hélices co-axiales
FR897057A (fr) * 1942-10-01 1945-03-12 Ettore Ambrosetti Off Moyeu d'hélice pour aéronefs
FR900664A (fr) * 1943-08-24 1945-07-05 équipement de piolets
CH259296A (de) * 1945-10-13 1949-01-15 Svenska Turbinfab Ab Propeller-Antriebseinrichtung an Fahrzeugen.
FR1005590A (fr) * 1947-08-14 1952-04-11 Cie Gen Equip Aeronautique Perfectionnements à la commande de changement de pas des pales d'hélices coaxiales
FR1005734A (fr) * 1947-09-15 1952-04-15 Snecma Machine aéronautique à hélice
US2679907A (en) * 1950-05-18 1954-06-01 United Aircraft Corp Dual rotation coaxial propeller mechanism
US3900274A (en) * 1974-06-25 1975-08-19 Gen Electric Remote controlled actuation system for the rotor of a gas turbine engine
US4486146A (en) * 1980-08-08 1984-12-04 British Aerospace Public Limited Company Aircraft propulsion means
SE445107B (sv) * 1983-06-22 1986-06-02 Volvo Penta Ab Rotoranordning
GB2145777B (en) * 1983-08-29 1987-07-22 Gen Electric Aircraft propeller system
US4563129A (en) * 1983-12-08 1986-01-07 United Technologies Corporation Integrated reduction gear and counterrotation propeller
US4591313A (en) * 1983-12-30 1986-05-27 The Boeing Company Propeller pitch control system and apparatus
GB2182397B (en) * 1985-11-02 1989-10-04 Rolls Royce Plc Propeller module for an aero gas turbine engine
GB2186918B (en) * 1986-02-25 1989-11-15 Rolls Royce Propeller module for an aero gas turbine engine

Also Published As

Publication number Publication date
FR2580725A1 (fr) 1986-10-24
DE3611792A1 (de) 1986-11-06
GB2173863A (en) 1986-10-22
JPS61268598A (ja) 1986-11-28
GB2173863B (en) 1989-07-19
DE3611792C2 (de) 1994-02-17
US4688995A (en) 1987-08-25
JPH0533200B2 (fr) 1993-05-18

Similar Documents

Publication Publication Date Title
FR2580725B1 (fr) Module propulsif pour un moteur a turbine a gaz aeronautique
FR2594886B1 (fr) Module propulsif pour un moteur aeronautique a turbine a gaz
FR2589427B1 (fr) Module d'helice pour un moteur a turbine a gaz aeronautique
FR2586453B1 (fr) Carburateur pour moteur a turbine a gaz
FR2557212B1 (fr) Structure de stator pour un moteur a turbine a gaz
GB2165964B (en) Combustion system for a gas turbine engine
DE3665627D1 (en) Combustion liner for a gas turbine engine
FR2575221B1 (fr) Stator refroidissable pour un moteur a turbine a gaz
FR2617907B1 (fr) Moteur a turbine a gaz
DE3663847D1 (en) Combustor for gas turbine engine
GB2121613B (en) A gas turbine engine for an aircraft
FR2592092B1 (fr) Turbine a aubes refroidies notamment pour moteur a turbine a gaz
FR2533620B1 (fr) Assemblage de rotor pour un moteur a turbine a gaz
GB2110762B (en) Gas turbine engine for a v/stol aircraft
GB2150277B (en) Combustion apparatus for a gas turbine engine
GB2138075B (en) Driving a turbine by ic engine exhaust gases
FR2586755B1 (fr) Systeme de carburant pour un moteur a turbine a gaz
FR2583459B1 (fr) Dispositif de regulation de carburant pour un moteur a turbine a gaz.
FR2527268B1 (fr) Prediffuseur pour un moteur a turbine a gaz
IT1185058B (it) Dispositivo di modulazione di spinta per turbomotore a gas
GB2105027B (en) Starting means for a gas turbine engine
DE3474191D1 (en) Fuel control system for a gas turbine engine
IT8620223A1 (it) Struttura trasmettitrice di potenza per turbomotori a gas
GB2176274B (en) Combustor for gas turbine engine
GB2198518B (en) Combustion apparatus for a gas turbine engine

Legal Events

Date Code Title Description
ST Notification of lapse