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

Dispositif de commande du rotor d'un hélicoptère

Info

Publication number: FR1505127A
Authority: FR; France
Prior art keywords: control device; helicopter rotor; rotor control; helicopter; rotor
Prior art date: 1965-12-20
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.)

Raytheon Technologies 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.)

1965-12-20

Filing date

1966-12-16

Publication date

1967-12-08

1966-12-16 Application filed by United Aircraft Corp filed Critical United Aircraft Corp

1967-12-08 Application granted granted Critical

1967-12-08 Publication of FR1505127A publication Critical patent/FR1505127A/fr

Status 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
US10752347B2 (en) *	2014-08-20	2020-08-25	Sikorsky Aircraft Corporation	Rotor blade pitch horn assembly
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

1965
- 1965-12-20 US US514847A patent/US3308888A/en not_active Expired - Lifetime
1966
- 1966-12-09 GB GB55349/66A patent/GB1145887A/en not_active Expired
- 1966-12-16 FR FR5028A patent/FR1505127A/fr not_active Expired
- 1966-12-19 DE DE19661481673 patent/DE1481673B1/de active Pending

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

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