FR2946317B1 - Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante - Google Patents

Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante

Info

Publication number
FR2946317B1
FR2946317B1 FR0902685A FR0902685A FR2946317B1 FR 2946317 B1 FR2946317 B1 FR 2946317B1 FR 0902685 A FR0902685 A FR 0902685A FR 0902685 A FR0902685 A FR 0902685A FR 2946317 B1 FR2946317 B1 FR 2946317B1
Authority
FR
France
Prior art keywords
guignol
flight control
aircraft flight
variable ratio
control chain
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.)
Active
Application number
FR0902685A
Other languages
English (en)
Other versions
FR2946317A1 (fr
Inventor
Bernard Gemmati
Romuald Biest
Carine Mirman
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 Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0902685A priority Critical patent/FR2946317B1/fr
Priority to US12/791,216 priority patent/US8196857B2/en
Publication of FR2946317A1 publication Critical patent/FR2946317A1/fr
Application granted granted Critical
Publication of FR2946317B1 publication Critical patent/FR2946317B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/22Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58Transmitting means, e.g. interrelated with initiating means or means acting on blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR0902685A 2009-06-04 2009-06-04 Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante Active FR2946317B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0902685A FR2946317B1 (fr) 2009-06-04 2009-06-04 Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante
US12/791,216 US8196857B2 (en) 2009-06-04 2010-06-01 Variable ratio crank for a manual flight control linkage of a rotary wing aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0902685A FR2946317B1 (fr) 2009-06-04 2009-06-04 Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante

Publications (2)

Publication Number Publication Date
FR2946317A1 FR2946317A1 (fr) 2010-12-10
FR2946317B1 true FR2946317B1 (fr) 2011-06-17

Family

ID=41566121

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0902685A Active FR2946317B1 (fr) 2009-06-04 2009-06-04 Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante

Country Status (2)

Country Link
US (1) US8196857B2 (fr)
FR (1) FR2946317B1 (fr)

Families Citing this family (21)

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CN105966616B (zh) 2009-06-05 2019-06-11 威罗门飞行公司 飞行器飞行机构和控制方法
WO2012112816A1 (fr) * 2011-02-16 2012-08-23 Aerovironment, Inc. Mécanisme de vol d'un véhicule aérien et procédé de commande pour un battement d'ailes non sinusoïdal
US9669925B2 (en) 2011-02-16 2017-06-06 Aerovironment, Inc. Air vehicle flight mechanism and control method for non-sinusoidal wing flapping
FR2972707B1 (fr) * 2011-03-18 2013-03-15 Eurocopter France Manette cyclique a transmission mecanique de commande d'un giravion, comprenant un bras de levier selectivement en cas d'urgence
EP2502825A1 (fr) 2011-03-25 2012-09-26 Eurocopter Pilotage de secours par vérin série pour chaine de commande de vol manuelle d'aéronef et Procédé
WO2012134460A1 (fr) * 2011-03-30 2012-10-04 Bell Helicopter Textron Inc. Lois de commande de vol pour virages à plat à vecteur constant
FR2973775B1 (fr) * 2011-04-06 2014-01-10 Eurocopter France Levier de commande d'une voilure tournante, systeme de commande mecanique muni dudit levier, et aeronef
RU2460671C1 (ru) * 2011-06-22 2012-09-10 Николай Евгеньевич Староверов Трехмоторный гелиплан
FR2977948B1 (fr) * 2011-07-12 2014-11-07 Eurocopter France Procede de pilotage automatique d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage automatique et aeronef
US10017248B2 (en) * 2014-04-28 2018-07-10 University Of Maryland, College Park Flapping wing aerial vehicles
US10676184B2 (en) * 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Pitch control system for an aircraft
WO2016043943A2 (fr) 2014-08-28 2016-03-24 Sikorsky Aircraft Corporation Système de commande de pas
WO2016054147A1 (fr) * 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Gestion de puissance entre un propulseur et un rotor coaxial d'un hélicoptère
FR3042474B1 (fr) 2015-10-15 2017-12-01 Airbus Helicopters Combinateur des commandes vol en lacet et de poussee pour un helicoptere hybride
US9715234B2 (en) * 2015-11-30 2017-07-25 Metal Industries Research & Development Centre Multiple rotors aircraft and control method
CN110935906B (zh) * 2019-12-16 2021-03-23 南京航空航天大学 一种基于混连式轨道制孔***的加工点定位、法向检测和调整方法
FR3108312B1 (fr) 2020-03-17 2022-12-23 Airbus Helicopters procédé de commande d’hélices d’un hélicoptère hybride et un hélicoptère hybride.
WO2021232273A1 (fr) * 2020-05-20 2021-11-25 深圳市大疆创新科技有限公司 Véhicule aérien sans pilote et procédé et appareil pour le commander, terminal de commande à distance et système de véhicule aérien sans pilote
FR3126693B1 (fr) 2021-09-09 2023-07-21 Airbus Helicopters combinateur à gain variable
CN115447762A (zh) * 2022-10-12 2022-12-09 中国航空工业集团公司西安飞机设计研究所 一种飞机无缝接入的应急操纵***
CN115447761A (zh) * 2022-10-12 2022-12-09 中国航空工业集团公司西安飞机设计研究所 一种变传动比飞机操纵***

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GB613715A (en) 1946-06-27 1948-12-02 Fairey Aviat Co Ltd Improvements in or relating to rotary wing aircraft
FR1132452A (fr) 1954-06-03 1957-03-12 Hobson Ltd H M Système de commande de vol pour avions ou aérodynes
DE1186335B (de) * 1961-01-18 1965-01-28 Messerschmitt Ag Hebelsystem aus zwei Hebeln zur UEbertragung von Signalen, insbesondere fuer Flugzeugsteuerungen
DE1225502B (de) * 1962-09-14 1966-09-22 Dornier Werke Gmbh Steuerungseinrichtung fuer Flugzeuge mit Langsamflug- bzw. Schwebeflugeigenschaften, insbesondere senkrecht startende und landende Flugzeuge
GB1180311A (en) 1968-04-05 1970-02-04 Ver Flugtechnische Werke Variable Lever Mechanism for Actuating the Control Surfaces of Air- and Watercraft
US3589331A (en) * 1969-04-04 1971-06-29 Westinghouse Electric Corp Apparatus for coating metallic foil
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JPS5614519B1 (fr) * 1971-04-06 1981-04-04
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DE3006087C2 (de) 1980-02-19 1983-04-14 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Steuerungseinrichtung für Flugzeuge mit einer unterschiedlichen Charakteristik im Langsam- und Schnellflug
JPS63210454A (ja) 1987-02-25 1988-09-01 Matsushita Electric Ind Co Ltd 可変ストロ−クカムレバ−装置
US5163815A (en) * 1991-07-29 1992-11-17 Fetters Dennis L Rotor blade control mechanism
US5826822A (en) * 1996-04-19 1998-10-27 Rehm; Rehm N. System and method for providing cyclic and collective pitch control in a rotary wing aircraft
US5853145A (en) * 1997-01-09 1998-12-29 Cartercopters, Llc Rotor head for rotary wing aircraft
FR2837785B1 (fr) * 2002-03-29 2004-12-03 Eurocopter France Dispositif de commande du pas des pales d'un rotor d'aeronef convertible
US7677492B1 (en) * 2004-11-16 2010-03-16 Cartercopters, L.L.C. Automatic mechanical control of rotor blade collective pitch
US7585153B1 (en) * 2006-08-11 2009-09-08 Sikorsky Aircraft Corporation Upper rotor control system for a counter-rotating rotor system
US7658349B2 (en) 2006-10-26 2010-02-09 Honeywell International Inc. Pilot flight control stick haptic feedback system and method
US7674091B2 (en) * 2006-11-14 2010-03-09 The Boeing Company Rotor blade pitch control
FR2916419B1 (fr) 2007-05-22 2010-04-23 Eurocopter France Helicoptere hybride rapide a grande distance franchissable et rotor de sustentation optimise.
FR2916420B1 (fr) * 2007-05-22 2009-08-28 Eurocopter France Helicoptere hybride rapide a grande distance franchissable avec controle de l'assiette longitudinale.
FR2916418B1 (fr) 2007-05-22 2009-08-28 Eurocopter France Helicoptere hybride rapide a grande distance franchissable.

Also Published As

Publication number Publication date
US8196857B2 (en) 2012-06-12
FR2946317A1 (fr) 2010-12-10
US20100308178A1 (en) 2010-12-09

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