FR2603657A1 - Mecanisme pour faire varier le pas des pales d'une helice d'un moteur a turbine a gaz - Google Patents

Mecanisme pour faire varier le pas des pales d'une helice d'un moteur a turbine a gaz

Info

Publication number
FR2603657A1
FR2603657A1 FR8712140A FR8712140A FR2603657A1 FR 2603657 A1 FR2603657 A1 FR 2603657A1 FR 8712140 A FR8712140 A FR 8712140A FR 8712140 A FR8712140 A FR 8712140A FR 2603657 A1 FR2603657 A1 FR 2603657A1
Authority
FR
France
Prior art keywords
rotating structure
blades
pinion
gas turbine
gas
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.)
Granted
Application number
FR8712140A
Other languages
English (en)
Other versions
FR2603657B1 (fr
Inventor
Lawrence Butler
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2603657A1 publication Critical patent/FR2603657A1/fr
Application granted granted Critical
Publication of FR2603657B1 publication Critical patent/FR2603657B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • B64C11/32—Blade pitch-changing mechanisms mechanical
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Wind Motors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Retarders (AREA)

Abstract

LE MOTEUR A TURBINE A GAZ COMPORTE UNE STRUCTURE TOURNANTE, UN TRAJET ANNULAIRE DE CIRCULAIRE DES GAZ AYANT LE MEME AXE QUE LA STRUCTURE TOURNANTE, UNE MULTITUDE D'AUBES DE ROTOR ACCOUPLEES A LA STRUCTURE TOURNANTE ET S'ETENDANT JUSQUE DANS LE TRAJET DE CIRCULATION DES GAZ DE SORTE QUE LE COURANT GAZEUX SUIVANT CE TRAJET PROVOQUE LA ROTATION DE LA STRUCTURE TOURNANTE PAR RAPPORT A L'ELEMENT FIXE, ET UNE MULTITUDE DE PALES D'HELICE A PAS VARIABLE QUI SONT ACCOUPLEES A LA STRUCTURE TOURNANTE EN ETANT DISPOSEES RADIALEMENT A L'EXTERIEUR DE CELLE-CI. LE PAS DES PALES EST MODIFIE PAR UN PIGNON 60 ACCOUPLE COAXIALEMENT A L'UNE DES PALES ET UN ENGRENAGE INTERNE DISPOSE RADIALEMENT AUTOUR DU PIGNON POUR ENTRAINER CE DERNIER. LE DEPLACEMENT ANNULAIRE DU PIGNON PROVOQUE UN DEPLACEMENT ANGULAIRE DE LA PALE PAR RAPPORT A LA STRUCTURE TOURNANTE. L'ENGRENAGE INTERNE 64 EST ANIME D'UN MOUVEMENT DE ROTATION AUTOUR DU PIGNON, D'OU IL RESULTE QUE LE PIGNON EST DEPLACE ANGULAIREMENT PAR RAPPORT A LA STRUCTURE TOURNANTE. APPLICATION AUX HELICES DES MOTEURS A TURBINE A GAZ.
FR878712140A 1986-09-09 1987-09-01 Mecanisme pour faire varier le pas des pales d'une helice d'un moteur a turbine a gaz Expired - Fee Related FR2603657B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/905,207 US4738591A (en) 1986-09-09 1986-09-09 Blade pitch varying mechanism

Publications (2)

Publication Number Publication Date
FR2603657A1 true FR2603657A1 (fr) 1988-03-11
FR2603657B1 FR2603657B1 (fr) 1990-08-03

Family

ID=25420424

Family Applications (1)

Application Number Title Priority Date Filing Date
FR878712140A Expired - Fee Related FR2603657B1 (fr) 1986-09-09 1987-09-01 Mecanisme pour faire varier le pas des pales d'une helice d'un moteur a turbine a gaz

Country Status (7)

Country Link
US (1) US4738591A (fr)
JP (1) JPS63129131A (fr)
DE (1) DE3729805A1 (fr)
FR (1) FR2603657B1 (fr)
GB (1) GB2194990B (fr)
IT (1) IT1222621B (fr)
SE (1) SE464714B (fr)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3905282C1 (en) * 1987-10-13 1990-05-31 Karl Dipl.-Ing. 2742 Gnarrenburg De Kastens Propeller fan
US4976102A (en) * 1988-05-09 1990-12-11 General Electric Company Unducted, counterrotating gearless front fan engine
DE3818466C1 (fr) * 1988-05-31 1989-12-21 Mtu Muenchen Gmbh
US5022824A (en) * 1988-10-07 1991-06-11 United Technologies Corporation Pinned airfoil propeller blade
US5022825A (en) * 1988-10-07 1991-06-11 United Technologies Corporation Pitch retention member
US5102300A (en) * 1988-10-07 1992-04-07 United Technologies Corporation Pinned airfoil propeller assembly
US4927329A (en) * 1988-10-21 1990-05-22 General Electric Company Aircraft engine unducted fan blade pitch control system
US5263898A (en) * 1988-12-14 1993-11-23 General Electric Company Propeller blade retention system
US4951461A (en) * 1989-03-20 1990-08-28 General Electric Company Power turbine support arrangement
US5112191A (en) * 1989-04-11 1992-05-12 General Electric Company Rotating cowling
US5039278A (en) * 1989-04-11 1991-08-13 General Electric Company Power turbine ventilation system
US4934901A (en) * 1989-04-21 1990-06-19 Duchesneau Jerome G Pitch change actuation system
US5156648A (en) * 1990-07-09 1992-10-20 General Electric Company Prop-fan pitch-change mechanism
US5154580A (en) * 1990-07-23 1992-10-13 General Electric Company Propeller pitch change mechanism
US5152668A (en) * 1990-07-23 1992-10-06 General Electric Company Pitch change mechanism for prop fans
US5174716A (en) * 1990-07-23 1992-12-29 General Electric Company Pitch change mechanism
US5242265A (en) * 1990-07-23 1993-09-07 General Electric Company Aircraft pitch change mechanism
US5154372A (en) * 1990-07-23 1992-10-13 General Electric Company Torque multiplier for aircraft propeller
US5415602A (en) * 1993-03-11 1995-05-16 Benesch; Lloyd Transmission device
US6341419B1 (en) * 2000-02-29 2002-01-29 General Electric Company Loop stacked rotor assembly
US6592328B1 (en) 2001-04-17 2003-07-15 Emerson Electric Co. Method and apparatus for adjusting the pitch of a fan blade
US7976279B2 (en) * 2007-06-11 2011-07-12 Hamilton Sundstrand Corporation Blade pitch actuation mechanism
CN102066768A (zh) * 2008-05-13 2011-05-18 旋转合成技术有限责任公司 风扇叶片保持和可变桨距系统
DE102009007013A1 (de) * 2009-01-31 2010-08-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerk, insbesondere CROR-Antrieb, für ein Flugzeug
FR2945268B1 (fr) * 2009-05-05 2013-05-17 Airbus France Generateur electrique sur une partie tournante de turbopropulseur
FR2946010B1 (fr) * 2009-05-29 2011-06-24 Snecma Dispositif a verin fixe pour la commande des pales de soufflante d'un turbopropulseur
US8689538B2 (en) 2009-09-09 2014-04-08 The Boeing Company Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan
FR2958621B1 (fr) * 2010-04-09 2012-03-23 Snecma Helice non carenee pour turbomachine.
US8371105B2 (en) 2010-09-30 2013-02-12 General Electric Company Hydraulic system for fan pitch change actuation of counter-rotating propellers
US8336290B2 (en) 2010-09-30 2012-12-25 General Electric Company Pitch change apparatus for counter-rotating propellers
FR2980770B1 (fr) * 2011-10-03 2014-06-27 Snecma Turbomachine a helice(s) pour aeronef avec systeme pour changer le pas de l'helice.
FR3017667B1 (fr) * 2014-02-14 2019-05-03 Safran Aircraft Engines Dispositif pour une helice non carenee a pales a calage variable d'une turbomachine
US10221706B2 (en) 2015-11-17 2019-03-05 General Electric Company Variable pitch fan actuator
US10107130B2 (en) * 2016-03-24 2018-10-23 United Technologies Corporation Concentric shafts for remote independent variable vane actuation
US11571807B2 (en) 2016-10-05 2023-02-07 Robert Darby Drive unit for robotic manipulators
FR3075257B1 (fr) * 2017-12-14 2021-02-19 Safran Aircraft Engines Dispositif de reglage du calage d'une helice

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR928354A (fr) * 1946-05-21 1947-11-26 Jacottet Paul Ets Dispositif de commande à distance
FR2122019A5 (fr) * 1971-01-14 1972-08-25 Durand Engrenages
FR2135670A1 (fr) * 1971-05-05 1972-12-22 Parsons John
FR2218241A1 (fr) * 1973-02-21 1974-09-13 United Aircraft Corp
DE2731486A1 (de) * 1977-07-12 1979-01-18 Polysius Ag Getriebe
GB2129502A (en) * 1982-11-01 1984-05-16 Gen Electric Counter rotation power turbine
US4657484A (en) * 1984-09-04 1987-04-14 General Electric Company Blade pitch varying means

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR579067A (fr) * 1923-11-21 1924-10-09 Mécanisme de commande
US2906143A (en) * 1955-03-21 1959-09-29 United Shoe Machinery Corp Strain wave gearing
GB1196588A (en) * 1966-11-09 1970-07-01 British Aircraft Corp Ltd Form Improvements relating to Turbo-fan Aircraft Engines
US3467198A (en) * 1966-12-05 1969-09-16 Rolls Royce Gear transmission
FR1553936A (fr) * 1966-12-05 1969-01-17
GB1375988A (en) * 1971-12-11 1974-12-04 Rolls Royce Pitch varying mechanism for variable pitch fan
GB1445107A (en) * 1973-01-12 1976-08-04 Rolls Royce Pitch varying mechanisms for a variable pitch fan
US3964839A (en) * 1974-10-21 1976-06-22 United Technologies Corporation Pitch change mechanism
PT65597B (de) * 1975-10-11 1978-03-28 Balcke Duerr Ag Planetengetriebe
GB2117054B (en) * 1982-02-17 1985-01-30 Rolls Royce Aircraft propulsion engine having a rear mounted propfan
DE3233078C1 (de) * 1982-09-06 1984-03-29 Balcke-Dürr AG, 4030 Ratingen Stroemungsmaschine
US4621978A (en) * 1984-12-03 1986-11-11 General Electric Company Counterrotating power turbine

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR928354A (fr) * 1946-05-21 1947-11-26 Jacottet Paul Ets Dispositif de commande à distance
FR2122019A5 (fr) * 1971-01-14 1972-08-25 Durand Engrenages
FR2135670A1 (fr) * 1971-05-05 1972-12-22 Parsons John
FR2218241A1 (fr) * 1973-02-21 1974-09-13 United Aircraft Corp
DE2731486A1 (de) * 1977-07-12 1979-01-18 Polysius Ag Getriebe
GB2129502A (en) * 1982-11-01 1984-05-16 Gen Electric Counter rotation power turbine
US4657484A (en) * 1984-09-04 1987-04-14 General Electric Company Blade pitch varying means

Also Published As

Publication number Publication date
SE8703463D0 (sv) 1987-09-07
DE3729805A1 (de) 1988-03-17
SE464714B (sv) 1991-06-03
IT8721845A0 (it) 1987-09-09
JPH0520571B2 (fr) 1993-03-19
SE8703463L (sv) 1988-03-10
GB2194990B (en) 1991-01-23
GB8713927D0 (en) 1987-07-22
GB2194990A (en) 1988-03-23
IT1222621B (it) 1990-09-05
US4738591A (en) 1988-04-19
JPS63129131A (ja) 1988-06-01
FR2603657B1 (fr) 1990-08-03

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