BR8101648A - Sistema de controle de voo de aeronaves autocompensado por manche de forca de eixos multiplos - Google Patents

Sistema de controle de voo de aeronaves autocompensado por manche de forca de eixos multiplos

Info

Publication number
BR8101648A
BR8101648A BR8101648A BR8101648A BR8101648A BR 8101648 A BR8101648 A BR 8101648A BR 8101648 A BR8101648 A BR 8101648A BR 8101648 A BR8101648 A BR 8101648A BR 8101648 A BR8101648 A BR 8101648A
Authority
BR
Brazil
Prior art keywords
stain
compensated
control system
flight control
aircraft flight
Prior art date
Application number
BR8101648A
Other languages
English (en)
Portuguese (pt)
Inventor
E Diamond
L Kingston
J Maciolek
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 BR8101648A publication Critical patent/BR8101648A/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/75—Arm-rests
    • B60N2/79—Adaptations for additional use of the arm-rests
    • B60N2/797—Adaptations for additional use of the arm-rests for use as electrical control means, e.g. switches
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50—Steerable undercarriages; Shimmy-damping
    • 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
    • B64C27/56—Mechanisms 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00—Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/22—Apparatus 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
    • G01L5/223—Apparatus 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
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Transportation (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
  • Toys (AREA)
BR8101648A 1980-04-01 1981-03-19 Sistema de controle de voo de aeronaves autocompensado por manche de forca de eixos multiplos BR8101648A (pt)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BR8101648A true BR8101648A (pt) 1981-10-06

Family

ID=22471948

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8101648A BR8101648A (pt) 1980-04-01 1981-03-19 Sistema de controle de voo de aeronaves autocompensado por manche de forca de eixos multiplos

Country Status (11)

Country Link
JP (2) JPS56167596A (enExample)
AU (1) AU538972B2 (enExample)
BR (1) BR8101648A (enExample)
CA (1) CA1158219A (enExample)
CH (1) CH652364A5 (enExample)
DE (1) DE3111604A1 (enExample)
ES (1) ES8204681A1 (enExample)
FR (1) FR2479133A1 (enExample)
GB (1) GB2073114B (enExample)
IL (1) IL62270A (enExample)
IT (1) IT1137311B (enExample)

Families Citing this family (31)

* 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.
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
GB2248947B (en) * 1988-02-22 1992-08-05 Honda Motor Co Ltd Synchronous operation control system for numerically controlled machine
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
US10676185B2 (en) 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Rotary wing aircraft 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
MA51273A (fr) * 2017-12-21 2021-05-12 Bae Systems Plc Systèmes de commande d'aéronef
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
CN109592064B (zh) * 2018-11-02 2022-04-19 中国航空工业集团公司西安飞机设计研究所 飞机与机械操纵系统变形差异对机动操纵影响设计方法
EP4162473A4 (en) 2020-06-05 2024-07-03 Joby Aero, Inc. Aircraft control system and method
GB2602953B (en) * 2020-08-21 2024-08-14 Hill Group Tech Limited Helicopter collective control apparatus
FR3119601B1 (fr) 2021-02-10 2025-05-02 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 (enExample) * 1976-11-05 1978-06-05

Also Published As

Publication number Publication date
ES500913A0 (es) 1982-05-16
CH652364A5 (de) 1985-11-15
JPS56167596A (en) 1981-12-23
DE3111604C2 (enExample) 1993-07-29
JPH0725355B2 (ja) 1995-03-22
JPH0358959B2 (enExample) 1991-09-09
FR2479133B1 (enExample) 1984-03-30
IL62270A (en) 1985-03-31
ES8204681A1 (es) 1982-05-16
CA1158219A (en) 1983-12-06
FR2479133A1 (fr) 1981-10-02
DE3111604A1 (de) 1982-04-22
IT1137311B (it) 1986-09-10
AU6886481A (en) 1981-10-08
JPH01289798A (ja) 1989-11-21
IT8120794A0 (it) 1981-03-30
AU538972B2 (en) 1984-09-06
GB2073114B (en) 1983-10-12
GB2073114A (en) 1981-10-14

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