FR2285298A1 - Agencement de rotor de queue pour giravions - Google Patents

Agencement de rotor de queue pour giravions

Info

Publication number
FR2285298A1
FR2285298A1 FR7431664A FR7431664A FR2285298A1 FR 2285298 A1 FR2285298 A1 FR 2285298A1 FR 7431664 A FR7431664 A FR 7431664A FR 7431664 A FR7431664 A FR 7431664A FR 2285298 A1 FR2285298 A1 FR 2285298A1
Authority
FR
France
Prior art keywords
giravions
tail rotor
rotor arrangement
arrangement
tail
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
FR7431664A
Other languages
English (en)
Other versions
FR2285298B1 (fr
Inventor
Rene Louis Mouille
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 FR7431664A priority Critical patent/FR2285298A1/fr
Priority to GB34250/75A priority patent/GB1514828A/en
Priority to US05/608,215 priority patent/US4053258A/en
Priority to IT26721/75A priority patent/IT1042160B/it
Priority to DE2541637A priority patent/DE2541637C3/de
Priority to JP50112766A priority patent/JPS5166698A/ja
Publication of FR2285298A1 publication Critical patent/FR2285298A1/fr
Application granted granted Critical
Publication of FR2285298B1 publication Critical patent/FR2285298B1/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/33—Rotors having flexing arms
FR7431664A 1974-09-19 1974-09-19 Agencement de rotor de queue pour giravions Granted FR2285298A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR7431664A FR2285298A1 (fr) 1974-09-19 1974-09-19 Agencement de rotor de queue pour giravions
GB34250/75A GB1514828A (en) 1974-09-19 1975-08-18 Tail rotor arrangement for helicopters
US05/608,215 US4053258A (en) 1974-09-19 1975-08-27 Tail-rotor arrangement for rotor crafts
IT26721/75A IT1042160B (it) 1974-09-19 1975-08-29 Struttura di rotore di coda per aerogiri
DE2541637A DE2541637C3 (de) 1974-09-19 1975-09-18 Heckrotor fur Drehflügelflugzeuge
JP50112766A JPS5166698A (en) 1974-09-19 1975-09-19 2 maihanegatabibukaitenshi

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7431664A FR2285298A1 (fr) 1974-09-19 1974-09-19 Agencement de rotor de queue pour giravions

Publications (2)

Publication Number Publication Date
FR2285298A1 true FR2285298A1 (fr) 1976-04-16
FR2285298B1 FR2285298B1 (fr) 1976-12-31

Family

ID=9143245

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7431664A Granted FR2285298A1 (fr) 1974-09-19 1974-09-19 Agencement de rotor de queue pour giravions

Country Status (6)

Country Link
US (1) US4053258A (fr)
JP (1) JPS5166698A (fr)
DE (1) DE2541637C3 (fr)
FR (1) FR2285298A1 (fr)
GB (1) GB1514828A (fr)
IT (1) IT1042160B (fr)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2377324A1 (fr) * 1977-01-15 1978-08-11 Messerschmitt Boelkow Blohm Rotor pour appareil a voilure tournante
DE2829605A1 (de) * 1977-07-13 1979-02-08 Aerospatiale Rotornabe
DE2921421A1 (de) * 1978-06-05 1979-12-06 Aerospatiale Elastische montageanordnung fuer hubschrauberrotor mit durchgehendem streifen
FR2430885A1 (fr) * 1978-07-12 1980-02-08 United Technologies Corp Rotor d'helicoptere a sommier comportant un amortisseur aisement remplacable
FR2569243A1 (fr) * 1984-08-17 1986-02-21 Aubertin Edouard Rotor a helice a pas variable, en particulier pour moteur eolien
EP0706936A1 (fr) 1994-10-11 1996-04-17 Eurocopter France Perfectionnements aux dispositifs de commande de pas pour rotors sans articulation
EP0718188A1 (fr) 1994-12-22 1996-06-26 Eurocopter France Rotor sans articulation à anneaux intermédiaires de commande de pas
FR2855811A1 (fr) * 2003-06-05 2004-12-10 Eurocopter France Pale de rotor a pas variable, pour rotors carenes, notamment d'helicopteres
WO2009050547A2 (fr) * 2007-09-24 2009-04-23 Blue H Intellectual Properties Cyprus Limited Système de conversion d'énergie éolienne en mer adapté pour les eaux profondes

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2397327A1 (fr) * 1977-07-13 1979-02-09 Aerospatiale Rotor a pas variable, en particulier pour un giravion
FR2397326A2 (fr) * 1977-07-13 1979-02-09 Aerospatiale Rotor sans articulations, en particulier pour un giravion
DE2810334A1 (de) * 1978-03-10 1979-09-13 Messerschmitt Boelkow Blohm Rotorblatt, insbesondere fuer drehfluegelflugzeuge
US4299538A (en) * 1978-12-06 1981-11-10 United Technologies Corporation Cross beam rotor
DE2903524C2 (de) * 1979-01-31 1982-02-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schlag- und schwenkgelenkloser Anschluß von Rotorblättern eines Drehflügelflugzeuges
DE2929906C3 (de) * 1979-07-24 1982-01-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor für einen Hubschrauber mit zumindest einem Paar einander gegenüberliegender Rotorblätter
US4381902A (en) * 1979-12-20 1983-05-03 Hughes Helicopters, Inc. Helicopter tail rotor of the elastomerically-mounted composite flexbeam type
IT1129070B (it) * 1980-04-03 1986-06-04 Agusta Aeronaut Costr Rotore a giunti elastomerici per elicotteri
IT1143359B (it) * 1981-02-05 1986-10-22 Agusta Aeronaut Costr Rotore anticoppia per elicotteri
US4695227A (en) * 1985-02-27 1987-09-22 Hughes Helicopters Inc. All composite, constant speed universal joint for use in a shaft driven tiltable main rotor for a helicopter
DE3526470C1 (de) * 1985-07-24 1987-01-02 Messerschmitt Boelkow Blohm Rotor,insbesondere eines Drehfluegelflugzeugs
US4729753A (en) * 1985-11-04 1988-03-08 Bell Helicopter Textron Inc. Constant velocity elastomeric bearing joint
GB8922338D0 (en) * 1989-10-04 1989-11-22 Westland Helicopters Helicopter rotors
FR2778165B1 (fr) * 1998-04-29 2000-07-13 Eurocopter France Rotor sans articulation avec demi-paliers precomprimes d'appui des manchettes de pied de pale sur des lames torsibles d'emplanture des pales
US7489045B1 (en) 2005-05-11 2009-02-10 Watson Borman Acme Corporation Energy generating expansion joint
US7621480B2 (en) * 2005-05-26 2009-11-24 Sikorsky Aircraft Corporation De-rotation system for a counter-rotating, coaxial rotor hub shaft fairing
US7607607B2 (en) * 2005-05-26 2009-10-27 Sikorsky Aircraft Corporation De-rotation system suitable for use with a shaft fairing system
US7229251B2 (en) * 2005-05-31 2007-06-12 Sikorsky Aircraft Corporation Rotor hub fairing system for a counter-rotating, coaxial rotor system
EP2227641B1 (fr) * 2007-12-03 2016-07-20 Sikorsky Aircraft Corporation Système de dérotation magnétique pour un système de carénage d'arbre
EP2238018A2 (fr) * 2008-01-02 2010-10-13 Sikorsky Aircraft Corporation Systeme de de-rotation planetaire pour un systeme de carenage d'arbre
US9884680B2 (en) * 2008-12-11 2018-02-06 Sikorsky Aircraft Corporation Elastomeric bearing system motion limiter
US9073636B2 (en) * 2009-06-02 2015-07-07 Saab Ab Rotor damper and tail rotor with such a rotor damper
US11718391B2 (en) * 2021-03-23 2023-08-08 Avx Aircraft Company Rotary aircraft hybrid rotor mast

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR776789A (fr) * 1933-08-25 1935-02-04 Perfectionnements aux hélicoptères ou autogyres
US3484174A (en) * 1968-04-08 1969-12-16 Kaman Corp Rotary wing system

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR752142A (fr) * 1933-03-08 1933-09-16 Hélice à pas variable et constant
US2369048A (en) * 1943-07-14 1945-02-06 Russell R Hays Helicopter
US2830669A (en) * 1955-06-03 1958-04-15 Herman R Klockner Blade-pitch-regulating means for the rotors of sustaining-rotor-equipped aircraft
US3002569A (en) * 1959-05-28 1961-10-03 Mcdonnell Aircraft Corp Locking device for floating hub helicopter rotors
GB880590A (en) * 1959-11-06 1961-10-25 Hugo Torben Grut Propeller with adjustable blade twist
US3231222A (en) * 1964-05-20 1966-01-25 Scheutzow Helicopter Corp Rotary wing aircraft
US3193019A (en) * 1964-06-05 1965-07-06 Bell Aerospace Corp Rotor system
US3261407A (en) * 1964-08-05 1966-07-19 Lockheed Aircraft Corp Helicopter rotor system
FR2041747A1 (fr) * 1969-05-20 1971-02-05 Sud Aviation
US3880551A (en) * 1973-11-15 1975-04-29 Boeing Co Rotary head assembly for rotary wing aircraft
US3874815A (en) * 1973-11-15 1975-04-01 Boeing Co Rotary head assembly for rotary wing aircraft

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR776789A (fr) * 1933-08-25 1935-02-04 Perfectionnements aux hélicoptères ou autogyres
US3484174A (en) * 1968-04-08 1969-12-16 Kaman Corp Rotary wing system

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2377324A1 (fr) * 1977-01-15 1978-08-11 Messerschmitt Boelkow Blohm Rotor pour appareil a voilure tournante
DE2829605A1 (de) * 1977-07-13 1979-02-08 Aerospatiale Rotornabe
DE2921421A1 (de) * 1978-06-05 1979-12-06 Aerospatiale Elastische montageanordnung fuer hubschrauberrotor mit durchgehendem streifen
FR2430885A1 (fr) * 1978-07-12 1980-02-08 United Technologies Corp Rotor d'helicoptere a sommier comportant un amortisseur aisement remplacable
FR2569243A1 (fr) * 1984-08-17 1986-02-21 Aubertin Edouard Rotor a helice a pas variable, en particulier pour moteur eolien
US5562415A (en) * 1994-10-11 1996-10-08 Eurocopter France Pitch-control devices for hingeless rotors
EP0706936A1 (fr) 1994-10-11 1996-04-17 Eurocopter France Perfectionnements aux dispositifs de commande de pas pour rotors sans articulation
EP0718188A1 (fr) 1994-12-22 1996-06-26 Eurocopter France Rotor sans articulation à anneaux intermédiaires de commande de pas
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
WO2009050547A2 (fr) * 2007-09-24 2009-04-23 Blue H Intellectual Properties Cyprus Limited Système de conversion d'énergie éolienne en mer adapté pour les eaux profondes
WO2009050547A3 (fr) * 2007-09-24 2010-08-26 Blue H Intellectual Properties Cyprus Limited Système de conversion d'énergie éolienne en mer adapté pour les eaux profondes
CN101981306A (zh) * 2007-09-24 2011-02-23 布鲁H知识产权塞浦路斯有限公司 用于深水中的离岸风能转换系统

Also Published As

Publication number Publication date
FR2285298B1 (fr) 1976-12-31
DE2541637B2 (de) 1979-09-27
DE2541637C3 (de) 1980-06-12
DE2541637A1 (de) 1976-04-01
JPS5734160B2 (fr) 1982-07-21
IT1042160B (it) 1980-01-30
JPS5166698A (en) 1976-06-09
GB1514828A (en) 1978-06-21
US4053258A (en) 1977-10-11

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Legal Events

Date Code Title Description
ST Notification of lapse