FR2430354A1 - Helice multipale a pas variable d'un type simplifie - Google Patents

Helice multipale a pas variable d'un type simplifie

Info

Publication number
FR2430354A1
FR2430354A1 FR7820258A FR7820258A FR2430354A1 FR 2430354 A1 FR2430354 A1 FR 2430354A1 FR 7820258 A FR7820258 A FR 7820258A FR 7820258 A FR7820258 A FR 7820258A FR 2430354 A1 FR2430354 A1 FR 2430354A1
Authority
FR
France
Prior art keywords
blade
propeller
multipale
variable step
simplified type
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
FR7820258A
Other languages
English (en)
Other versions
FR2430354B1 (fr
Inventor
Maurice Louis Duret
Bernard Leon Joseph Lamarche
Marc Declercq
Robert Denis Martin
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7820258A priority Critical patent/FR2430354A1/fr
Priority to DE19792954465 priority patent/DE2954465A1/de
Priority to DE2926180A priority patent/DE2926180C2/de
Priority to DE2954466A priority patent/DE2954466C2/de
Priority to GB8132063A priority patent/GB2082964B/en
Priority to GB7923067A priority patent/GB2026416B/en
Priority to US06/055,096 priority patent/US4281966A/en
Priority to JP54085820A priority patent/JPS591636B2/ja
Priority to IT24159/79A priority patent/IT1122047B/it
Publication of FR2430354A1 publication Critical patent/FR2430354A1/fr
Application granted granted Critical
Publication of FR2430354B1 publication Critical patent/FR2430354B1/fr
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/20Constructional features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/37Rotors having articulated joints
    • B64C27/45Rotors having articulated joints with a feathering hinge only
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/82Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8254Shrouded tail rotors, e.g. "Fenestron" fans

Abstract

L'invention concerne une hélice multipale à pas variable. Cette hélice comprend au moins une paire de pales opposées, 3al et 3a2, portées par une même lame allongée la, en fibres à haute résistance, qu'un axe 5 traverse par une ouverture médiane 4a, de la lame la; chaque pale comprend une coquille 3a1 fixée à la partie correspondante de la lame 1a, par une masse de matiere synthétique adhésive, 10a1. Le pied de chaque pale 3a1 est muni d'un manchon 11a1, par un bras latéral, 13a1, duquel on peut tordre la lame 1a, pour communiquer un pas approprié à ladite pale. L'invention est applicable en particulier à la réalisation d'un rotor arrière de giravion.
FR7820258A 1978-07-07 1978-07-07 Helice multipale a pas variable d'un type simplifie Granted FR2430354A1 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
FR7820258A FR2430354A1 (fr) 1978-07-07 1978-07-07 Helice multipale a pas variable d'un type simplifie
DE2926180A DE2926180C2 (de) 1978-07-07 1979-06-28 Verstellrotor
DE2954466A DE2954466C2 (fr) 1978-07-07 1979-06-28
DE19792954465 DE2954465A1 (fr) 1978-07-07 1979-06-28
GB8132063A GB2082964B (en) 1978-07-07 1979-07-03 Making a propeller blade
GB7923067A GB2026416B (en) 1978-07-07 1979-07-03 Multi-blade propellers and method of making same
US06/055,096 US4281966A (en) 1978-07-07 1979-07-05 Multi-blade propellers
JP54085820A JPS591636B2 (ja) 1978-07-07 1979-07-06 多翼プロペラおよび多翼プロペラの製造方法
IT24159/79A IT1122047B (it) 1978-07-07 1979-07-06 Elica multipale a passo variabile di tipo semplificato

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7820258A FR2430354A1 (fr) 1978-07-07 1978-07-07 Helice multipale a pas variable d'un type simplifie

Publications (2)

Publication Number Publication Date
FR2430354A1 true FR2430354A1 (fr) 1980-02-01
FR2430354B1 FR2430354B1 (fr) 1983-01-07

Family

ID=9210436

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7820258A Granted FR2430354A1 (fr) 1978-07-07 1978-07-07 Helice multipale a pas variable d'un type simplifie

Country Status (6)

Country Link
US (1) US4281966A (fr)
JP (1) JPS591636B2 (fr)
DE (3) DE2954465A1 (fr)
FR (1) FR2430354A1 (fr)
GB (2) GB2026416B (fr)
IT (1) IT1122047B (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0121462A1 (fr) * 1983-03-18 1984-10-10 AEROSPATIALE Société Nationale Industrielle Hélice multipale à pas variable à pales en matériaux composites démontables individuellement
FR2776263A1 (fr) * 1998-03-20 1999-09-24 Eurocopter France Blindage de bord d'attaque de pale de rotor, et pale le comportant
FR2855811A1 (fr) * 2003-06-05 2004-12-10 Eurocopter France Pale de rotor a pas variable, pour rotors carenes, notamment d'helicopteres

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2430354A1 (fr) * 1978-07-07 1980-02-01 Aerospatiale Helice multipale a pas variable d'un type simplifie
DE2919684C3 (de) * 1979-05-16 1981-12-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schlag-, schwenk-und blattverstellgelenkloser Rotor
DE3367371D1 (en) * 1982-03-18 1986-12-11 Westland Plc Helicopter rotors
AU568381B2 (en) * 1983-07-01 1987-12-24 Ladney, M. Jr. Rear air-foil
DE3412592A1 (de) * 1984-04-04 1985-10-17 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Rotor mit zu blattpaaren zusammengefassten rotorblaettern
GB2167500B (en) * 1984-11-20 1988-05-18 Rolls Royce Rotor aerofoil blade containment
DE3544814A1 (de) * 1985-12-18 1987-06-19 Gutehoffnungshuette Man Mehrblattrotor fuer eine windkraftanlage
DK155848C (da) * 1987-04-10 1989-10-02 Novenco As Aksialventilatorhjul
FR2616409B1 (fr) * 1987-06-09 1989-09-15 Aerospatiale Pale en materiaux composites et son procede de fabrication
FR2628062B1 (fr) * 1988-03-07 1990-08-10 Aerospatiale Pale pour helice carenee a hautes performances, helice carenee multipale pourvue de telles pales et agencement de rotor de queue a helice carenee pour aeronef a voilure tournante
JPH03104799A (ja) * 1989-09-20 1991-05-01 Fuji Heavy Ind Ltd 複合材ブレードの製造方法
IT1240178B (it) * 1990-04-06 1993-11-27 Agusta Spa Rotore principale per elicotteri
IT1240177B (it) * 1990-04-06 1993-11-27 Agusta Spa Rotore principale per elicotteri
DE4015207C1 (en) * 1990-05-11 1991-10-17 Mtu Muenchen Gmbh Bearing for aircraft engine rotor blade - incorporates torsional tie rod in compact design
JP2768826B2 (ja) * 1991-08-02 1998-06-25 ザ、ボーイング、カンパニー 回転翼型航空機の尾部回転翼のダクトファンおよびピッチ制御装置
WO1993002918A1 (fr) * 1991-08-02 1993-02-18 The Boeing Company Fenestron pour aerodyne a voilure tournante a commande de compensation de couple et d'attitude de lacet
US5297934A (en) * 1991-08-02 1994-03-29 The Boeing Company Compensation for kinematic foreshortening effect in pitch control system for rotary wing aircraft
FR2682663B1 (fr) * 1991-10-16 1994-01-07 Aerospatiale Ste Nationale Indle Rotor multipale, notamment pour helice arriere anticouple d'helicoptere et procede pour sa realisation.
FR2684351B1 (fr) * 1991-12-02 1994-02-04 Aerospatiale Ste Nationale Indle Rotor multipale a pas variable, notamment pour systeme arriere anticouple d'aeronef a voilure tournante.
JP2662838B2 (ja) * 1992-03-24 1997-10-15 川崎重工業株式会社 回転翼航空機の尾部回転翼
US5273401A (en) * 1992-07-01 1993-12-28 The United States Of America As Represented By The Secretary Of The Air Force Wrapped paired blade rotor
FR2699497B1 (fr) * 1992-12-23 1995-03-10 Eurocopter France Dispositif de liaison pale-moyeu à attache feuilletée, pale de rotor munie d'une telle attache, et rotor équipé de telles pales.
US5620305A (en) * 1995-03-20 1997-04-15 The Boeing Company Hub for rotary wing aircraft
FR2740380B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere
FR2740378B1 (fr) * 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale a pas variable en materiau composite pour rotor d'helicoptere, et pale a pas variable pouvant etre obtenue par un tel procede
FR2745589B1 (fr) * 1996-02-29 1998-04-30 Snecma Piece hybride a haut rapport resistance-masse et procede de realisation
DE19622834A1 (de) * 1996-06-07 1997-12-11 Tardy Tuch Georg Von Cand Aer Luft- oder Schiffsschraube
US6024325A (en) * 1997-01-09 2000-02-15 Cartercopters, Llc Rotor for rotary wing aircraft
US6155784A (en) * 1997-01-09 2000-12-05 Cartercopters, Llc. Variable pitch aircraft propeller
DE19717208C1 (de) * 1997-04-24 1998-06-10 Eurocopter Deutschland Rotorkopfverkleidung
CA2348677A1 (fr) * 2000-05-24 2001-11-24 Cartercopters, Llc Rotor pour giravion
US6527515B2 (en) 2000-05-24 2003-03-04 Cartercopter, L.L.C. Rotor for rotary wing aircraft
US6986642B2 (en) * 2002-08-30 2006-01-17 Cartercopters, L.L.C. Extreme mu rotor
GB2412410B (en) * 2004-03-16 2008-01-02 Christopher Flint Variable pitch propeller mechanism
US7926759B2 (en) * 2007-11-28 2011-04-19 The Boeing Company Tail rotor hub
US8182222B2 (en) * 2009-02-12 2012-05-22 Hamilton Sundstrand Corporation Thermal protection of rotor blades
EP2246259B1 (fr) * 2009-04-29 2012-12-12 Eurocopter Deutschland GmbH Aile de rotor avec élément integral de transmission de tension et de couple et son procédé de fabrication
US8262358B1 (en) * 2009-05-26 2012-09-11 The Boeing Company Ultra-light weight self-lubricating propeller hub
WO2011026009A1 (fr) 2009-08-28 2011-03-03 Polystrand, Inc Pale de rotor en matière thermoplastique
KR101267072B1 (ko) 2010-10-11 2013-05-24 유로캅터 도이칠란트 게엠베하 일체형 응력-토크-전달 요소를 구비한 회전자 날개 및 이의 제조방법
US10059438B2 (en) 2011-12-26 2018-08-28 Textron Innovations Inc. Hub assembly with grease lubricated roller bearing and tension-torsion strap
EP2669192B8 (fr) * 2012-05-29 2017-03-01 Ratier-Figeac SAS Pale d'hélice
WO2015183658A1 (fr) * 2014-05-30 2015-12-03 Sikorsky Aircraft Corporation Enveloppe de tige structurellement efficace
US10703466B2 (en) 2015-05-19 2020-07-07 Sikorsky Aircraft Corporation Propulsor hub weight element and balancing method
CN106741974A (zh) * 2016-12-12 2017-05-31 惠阳航空螺旋桨有限责任公司 一种螺旋桨用复合材料整流罩
EP3366584B1 (fr) * 2017-02-27 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Dispositif de commande de pas pour un fenestron d'un giravion

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2132864A1 (fr) * 1971-04-08 1972-11-24 United Aircraft Corp
US3874820A (en) * 1974-04-08 1975-04-01 United Aircraft Corp Hingeless in-plane rotor blade design
FR2315432A1 (fr) * 1975-06-26 1977-01-21 United Technologies Corp Rotor d'helicoptere
FR2376791A1 (fr) * 1977-01-07 1978-08-04 United Technologies Corp Rotor d'helicoptere a sommier perfectionne

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DE1264266B (de) * 1963-03-29 1968-03-21 Boelkow Gmbh Verfahren zum Herstellen von Rotorblaettern aus glasfaserverstaerktem Kunststoff
DE1531355B1 (de) * 1967-07-01 1970-07-23 Bolkow Gmbh schlag-und schwenkgelenklose aufhangung der roterblatter eines drehflugelflgzeuges am roterkopf.
US3484174A (en) * 1968-04-08 1969-12-16 Kaman Corp Rotary wing system
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JPS584679B2 (ja) * 1976-06-26 1983-01-27 川崎重工業株式会社 複合材料翼の製造方法
FR2430354A1 (fr) * 1978-07-07 1980-02-01 Aerospatiale Helice multipale a pas variable d'un type simplifie

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2132864A1 (fr) * 1971-04-08 1972-11-24 United Aircraft Corp
US3874820A (en) * 1974-04-08 1975-04-01 United Aircraft Corp Hingeless in-plane rotor blade design
FR2315432A1 (fr) * 1975-06-26 1977-01-21 United Technologies Corp Rotor d'helicoptere
FR2376791A1 (fr) * 1977-01-07 1978-08-04 United Technologies Corp Rotor d'helicoptere a sommier perfectionne

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0121462A1 (fr) * 1983-03-18 1984-10-10 AEROSPATIALE Société Nationale Industrielle Hélice multipale à pas variable à pales en matériaux composites démontables individuellement
US4639284A (en) * 1983-03-18 1987-01-27 Societe Nationale Industrielle Aerospatiale Process for manufacturing a variable pitch multi-blade propeller by molding resin-impregnated fails around a preform
EP0212724A2 (fr) * 1983-03-18 1987-03-04 AEROSPATIALE Société Nationale Industrielle Pale en matériaux composites, notamment pour hélice multipale à pas variable et à pales démontables individuellement, et son procédé de fabrication
EP0212724A3 (en) * 1983-03-18 1987-05-13 Aerospatiale Societe Nationale Industrielle Composite blade, in particular for a multiblade propeller with variable pitch and individually removable blades, and manufacturing process
FR2776263A1 (fr) * 1998-03-20 1999-09-24 Eurocopter France Blindage de bord d'attaque de pale de rotor, et pale le comportant
FR2855811A1 (fr) * 2003-06-05 2004-12-10 Eurocopter France Pale de rotor a pas variable, pour rotors carenes, notamment d'helicopteres
US7040863B2 (en) 2003-06-05 2006-05-09 Eurocopter Variable pitch rotor blade for shrouded rotors, in particular helicopter rotors

Also Published As

Publication number Publication date
FR2430354B1 (fr) 1983-01-07
DE2954466A1 (fr) 1985-07-18
IT7924159A0 (it) 1979-07-06
US4281966A (en) 1981-08-04
DE2926180C2 (de) 1986-10-30
GB2082964B (en) 1983-03-09
DE2954465A1 (fr) 1985-07-11
GB2026416A (en) 1980-02-06
GB2026416B (en) 1982-12-22
GB2082964A (en) 1982-03-17
JPS591636B2 (ja) 1984-01-13
IT1122047B (it) 1986-04-23
DE2954466C2 (fr) 1989-06-01
JPS5511986A (en) 1980-01-28
DE2926180A1 (de) 1980-01-24

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ST Notification of lapse