ES8204681A1 - Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiples - Google Patents

Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiples

Info

Publication number
ES8204681A1
ES8204681A1 ES500913A ES500913A ES8204681A1 ES 8204681 A1 ES8204681 A1 ES 8204681A1 ES 500913 A ES500913 A ES 500913A ES 500913 A ES500913 A ES 500913A ES 8204681 A1 ES8204681 A1 ES 8204681A1
Authority
ES
Spain
Prior art keywords
aircraft
force
stick
control
axis
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
ES500913A
Other languages
English (en)
Other versions
ES500913A0 (es
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 Technologies 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 Technologies Corp filed Critical United Technologies Corp
Publication of ES8204681A1 publication Critical patent/ES8204681A1/es
Publication of ES500913A0 publication Critical patent/ES500913A0/es
Granted legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/04Initiating means actuated personally
    • B64C13/042Initiating means actuated personally operated by hand
    • B64C13/0421Initiating means actuated personally operated by hand control sticks for primary flight controls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60NSEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/75Arm-rests
    • B60N2/79Adaptations for additional use of the arm-rests
    • B60N2/797Adaptations for additional use of the arm-rests for use as electrical control means, e.g. switches
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50Steerable undercarriages; Shimmy-damping
    • 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
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/22Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers
    • G01L5/223Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring the force applied to control members, e.g. control members of vehicles, triggers to joystick controls
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Transportation (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
  • Feedback Control In General (AREA)

Abstract

SISTEMA DE CONTROL DE AERONAVES. FORMADO POR EL CONTROLADOR DE BRAZO LATERAL (10) QUE COMPRENDE UNA PALANCA DE MANDO (12), MONTADA SOBRE UN CONJUNTO TRANSDUCTOR DE DETECCION ADECUADA (13) DISPUESTO SOBRE UN BRAZO (14) DEL ASIENTO (16). EL BRAZO (14) VA ARTICULADO (18) DE FORMA QUE SE DESPLAZA PARA PERMITIR EL ACCESO AL ASIENTO. EL CONTROLADOR (10) ES UN CONTROLADOR DE FUERZA, DE FORMA QUE NO PRECISA DE DESPLAZAMIENTOS PARA SU ACCIONAMIENTO. SE PRETENDE CON TODO ELLO MEJORAR LA VISIBILIDAD Y DISMINUIR LA FATIGA DEL PILOTO.
ES500913A 1980-04-01 1981-03-31 Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiples Granted ES500913A0 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13623380A 1980-04-01 1980-04-01

Publications (2)

Publication Number Publication Date
ES8204681A1 true ES8204681A1 (es) 1982-05-16
ES500913A0 ES500913A0 (es) 1982-05-16

Family

ID=22471948

Family Applications (1)

Application Number Title Priority Date Filing Date
ES500913A Granted ES500913A0 (es) 1980-04-01 1981-03-31 Perfeccionamientos en los dispositivos de control de vuelo de aeronaves de ejes multiples

Country Status (11)

Country Link
JP (2) JPS56167596A (es)
AU (1) AU538972B2 (es)
BR (1) BR8101648A (es)
CA (1) CA1158219A (es)
CH (1) CH652364A5 (es)
DE (1) DE3111604A1 (es)
ES (1) ES500913A0 (es)
FR (1) FR2479133A1 (es)
GB (1) GB2073114B (es)
IL (1) IL62270A (es)
IT (1) IT1137311B (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109592064A (zh) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 飞机与机械操纵***变形差异对机动操纵影响设计方法

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2576281B1 (fr) * 1985-01-18 1992-04-30 Aerospatiale Poste de pilotage pourvu d'un manche a balai lateral actionnable par une seule main et siege pour un tel poste de pilotage
FR2604001B1 (fr) * 1986-09-15 1988-12-09 Aerospatiale Systeme de commande de vol electrique avec protection en incidence pour aeronef
US4696445A (en) * 1986-09-18 1987-09-29 United Technologies Corporation Collective control system for a helicopter
FI77334C (fi) * 1987-03-03 1989-02-10 Teopros Oy Styranordning.
GB2248947B (en) * 1988-02-22 1992-08-05 Honda Motor Co Ltd Synchronous operation control system for numerically controlled machine
JPH07107643B2 (ja) * 1988-02-22 1995-11-15 本田技研工業株式会社 Nc同期制御システム
FR2643331B1 (fr) * 1989-02-17 1995-01-13 Aerospatiale Dispositif de commande a manche basculant et systeme de commande de vol pour aeronef comportant au moins un tel dispositif de commande
FR2647922B1 (fr) * 1989-05-31 1993-12-31 Sextant Avionique Dispositif de commande electromecanique utilisable pour le pilotage d'un vehicule
US4947697A (en) * 1989-06-28 1990-08-14 Cae Electronics Ltd. System for measuring force versus position of a flight controller in an aircraft or flight simulator
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
JP2681428B2 (ja) * 1992-01-29 1997-11-26 日本航空電子工業株式会社 無人ヘリコプタ用飛行制御装置
JP2607205B2 (ja) * 1992-06-30 1997-05-07 川崎重工業株式会社 航空機用多軸サイドスティックコントローラ
FR2769283B1 (fr) * 1997-10-06 1999-12-03 Eurocopter France Procede et dispositif pour realiser le decouplage du comportement d'un aeronef, notamment un helicoptere
JP3091743B1 (ja) 1999-03-30 2000-09-25 株式会社コミュータヘリコプタ先進技術研究所 操縦装置
US6671588B2 (en) 2001-12-27 2003-12-30 Toyota Jidosha Kabushiki Kaisha System and method for controlling traveling direction of aircraft
DE10310717A1 (de) * 2003-03-10 2004-09-23 Wittenstein Ag Vorrichtung zum Steuern eines Fahrzeuges
FR2899562B1 (fr) * 2006-04-05 2009-01-09 Eurocopter France Dispositif de commandes de vol d'un giravion
FR2903660B1 (fr) * 2006-07-12 2009-06-12 Airbus France Sas Systeme de commandes de vol electriques pour aeronef et siege l'incorporant
FR2991295B1 (fr) * 2012-06-04 2015-02-27 Eurocopter France Aeronef a grande visibilite
US9033284B2 (en) 2012-11-20 2015-05-19 Sikorsky Aircraft Corporation Integrated seat mounted inceptor
FR3001439B1 (fr) 2013-01-29 2015-02-27 Eurocopter France Organe de commande muni d'un levier de pas collectif de pales et d'un moyen de commande en lacet, et aeronef
JP5698802B2 (ja) 2013-06-28 2015-04-08 ヤマハ発動機株式会社 遠隔操縦装置
EP3186146B1 (en) * 2014-08-28 2019-10-09 Sikorsky Aircraft Corporation Pitch control system
CN104502009B (zh) * 2014-11-28 2018-10-26 湖南三一智能控制设备有限公司 一种臂架防碰撞装置、方法及工程机械
FR3060528B1 (fr) * 2016-12-16 2018-12-07 Safran Electronics & Defense Dispositif de commande des surfaces mobiles et d'une roue directrice d'un aeronef
CN108407879B (zh) * 2018-05-15 2023-12-12 北京美佳靓丽日用品有限公司 一种三维方向控制装置
WO2021248116A1 (en) * 2020-06-05 2021-12-09 Joby Aero, Inc. Aircraft control system and method
GB2602953A (en) * 2020-08-21 2022-07-27 Hill Group Tech Limited Helicopter collective control apparatus
FR3119601A1 (fr) 2021-02-10 2022-08-12 Airbus Helicopters Système de commande d’un aéronef et aéronef associé

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3447766A (en) * 1967-02-14 1969-06-03 Bendix Corp Control stick with solid state sensors
US3584814A (en) * 1967-07-18 1971-06-15 Bell Aerospace Corp Stability and control augmentation system
GB1240866A (en) * 1968-08-22 1971-07-28 Amf Inc Control device
US3771037A (en) * 1973-03-15 1973-11-06 Nasa Solid state controller three-axes controller
JPS5366600U (es) * 1976-11-05 1978-06-05

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109592064A (zh) * 2018-11-02 2019-04-09 中国航空工业集团公司西安飞机设计研究所 飞机与机械操纵***变形差异对机动操纵影响设计方法

Also Published As

Publication number Publication date
FR2479133B1 (es) 1984-03-30
IL62270A (en) 1985-03-31
BR8101648A (pt) 1981-10-06
GB2073114B (en) 1983-10-12
CA1158219A (en) 1983-12-06
FR2479133A1 (fr) 1981-10-02
JPH0358959B2 (es) 1991-09-09
GB2073114A (en) 1981-10-14
AU6886481A (en) 1981-10-08
AU538972B2 (en) 1984-09-06
CH652364A5 (de) 1985-11-15
DE3111604C2 (es) 1993-07-29
JPH01289798A (ja) 1989-11-21
ES500913A0 (es) 1982-05-16
IT8120794A0 (it) 1981-03-30
JPS56167596A (en) 1981-12-23
JPH0725355B2 (ja) 1995-03-22
DE3111604A1 (de) 1982-04-22
IT1137311B (it) 1986-09-10

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20010402