FR1505127A - Dispositif de commande du rotor d'un hélicoptère - Google Patents

Dispositif de commande du rotor d'un hélicoptère

Info

Publication number
FR1505127A
FR1505127A FR5028A FR38005028A FR1505127A FR 1505127 A FR1505127 A FR 1505127A FR 5028 A FR5028 A FR 5028A FR 38005028 A FR38005028 A FR 38005028A FR 1505127 A FR1505127 A FR 1505127A
Authority
FR
France
Prior art keywords
control device
helicopter rotor
rotor control
helicopter
rotor
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
FR5028A
Other languages
English (en)
Inventor
Peter Joseph Arcidiacono
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.)
RTX Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of FR1505127A publication Critical patent/FR1505127A/fr
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
FR5028A 1965-12-20 1966-12-16 Dispositif de commande du rotor d'un hélicoptère Expired FR1505127A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US514847A US3308888A (en) 1965-12-20 1965-12-20 Compound helicopter rotor control system

Publications (1)

Publication Number Publication Date
FR1505127A true FR1505127A (fr) 1967-12-08

Family

ID=24048921

Family Applications (1)

Application Number Title Priority Date Filing Date
FR5028A Expired FR1505127A (fr) 1965-12-20 1966-12-16 Dispositif de commande du rotor d'un hélicoptère

Country Status (4)

Country Link
US (1) US3308888A (fr)
DE (1) DE1481673B1 (fr)
FR (1) FR1505127A (fr)
GB (1) GB1145887A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0706938A1 (fr) * 1994-10-13 1996-04-17 Eurocopter France Dispositif de commande de pas des pales d'un rotor de giravion
EP1232943A3 (fr) * 2001-02-16 2003-03-12 Bell Helicopter Textron Inc. Système de rotor du type couplé pour aéronef

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3729272A (en) * 1968-01-25 1973-04-24 Fairchild Industries Reverse velocity rotor and rotorcraft
US3924965A (en) * 1973-01-22 1975-12-09 Fairchild Industries Reverse velocity rotor and rotorcraft
US3841586A (en) * 1973-04-26 1974-10-15 Boeing Co Rotor swashplate assembly
US4195966A (en) * 1978-07-03 1980-04-01 Cornelius George W Pitch control system for helicopter rotor blades
DE3036093C1 (de) * 1980-09-25 1982-07-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Rotor insbesondere fuer ein Drehfluegelflugzeug
US8357023B2 (en) * 2006-01-19 2013-01-22 Silverlit Limited Helicopter
DE102006030089B3 (de) * 2006-06-28 2008-01-03 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauber-Rotorsteuereinrichtung
US8979495B2 (en) * 2009-12-21 2015-03-17 Sikorsky Aircraft Corporation Control system and method for rotor assembly
GB2491129B (en) * 2011-05-23 2014-04-23 Blue Bear Systems Res Ltd Air vehicle
WO2016028762A1 (fr) * 2014-08-20 2016-02-25 Sikorsky Aircraft Corporation Ensemble guignol de pas de pale de rotor
US10994840B1 (en) 2017-08-16 2021-05-04 United States Of America As Represented By The Secretary Of The Air Force Thrust vectoring control of a cyclorotor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA555690A (en) * 1958-04-08 Henrich C.J. Focke Means for stabilizing a helicopter flying machine
US1992015A (en) * 1933-04-25 1935-02-19 Rutherford Walton Victor Arey Rotative wing aircraft
US2256635A (en) * 1939-08-19 1941-09-23 Arthur M Young Aircraft and means for stabilizing the same
US2428200A (en) * 1942-08-07 1947-09-30 Autogiro Co Of America Pitch control for aircraft sustaining rotors
GB811211A (en) * 1954-04-15 1959-04-02 Charles Walter Mccutchen Improvements in or relating to cyclic pitch controls for helicopters

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0706938A1 (fr) * 1994-10-13 1996-04-17 Eurocopter France Dispositif de commande de pas des pales d'un rotor de giravion
FR2725690A1 (fr) * 1994-10-13 1996-04-19 Eurocopter France Dispositif de commande de pas des pales d'un rotor de giravion
US5599167A (en) * 1994-10-13 1997-02-04 Eurocopter France Device for controlling the pitch of the blades of a rotorcraft rotor
EP1232943A3 (fr) * 2001-02-16 2003-03-12 Bell Helicopter Textron Inc. Système de rotor du type couplé pour aéronef
US6616095B2 (en) 2001-02-16 2003-09-09 Bell Helicopter Textron Inc. Coupled aircraft rotor system

Also Published As

Publication number Publication date
DE1481673B1 (de) 1970-01-02
GB1145887A (en) 1969-03-19
US3308888A (en) 1967-03-14

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