IT1137311B - FLIGHT CONTROL SYSTEM OF A SELF-BALANCED AIRCRAFT WITH MULTIPLE AXLE STRENGTH - Google Patents

FLIGHT CONTROL SYSTEM OF A SELF-BALANCED AIRCRAFT WITH MULTIPLE AXLE STRENGTH

Info

Publication number
IT1137311B
IT1137311B IT20794/81A IT2079481A IT1137311B IT 1137311 B IT1137311 B IT 1137311B IT 20794/81 A IT20794/81 A IT 20794/81A IT 2079481 A IT2079481 A IT 2079481A IT 1137311 B IT1137311 B IT 1137311B
Authority
IT
Italy
Prior art keywords
self
control system
flight control
multiple axle
axle strength
Prior art date
Application number
IT20794/81A
Other languages
Italian (it)
Other versions
IT8120794A0 (en
Inventor
Edmond Daniel Diamond
Joseph Richard Maciolek
Leo Kingston
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 IT8120794A0 publication Critical patent/IT8120794A0/en
Application granted granted Critical
Publication of IT1137311B publication Critical patent/IT1137311B/en

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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control 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
    • 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)
  • 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)
  • Feedback Control In General (AREA)
  • Toys (AREA)
IT20794/81A 1980-04-01 1981-03-30 FLIGHT CONTROL SYSTEM OF A SELF-BALANCED AIRCRAFT WITH MULTIPLE AXLE STRENGTH IT1137311B (en)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
IT8120794A0 IT8120794A0 (en) 1981-03-30
IT1137311B true IT1137311B (en) 1986-09-10

Family

ID=22471948

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20794/81A IT1137311B (en) 1980-04-01 1981-03-30 FLIGHT CONTROL SYSTEM OF A SELF-BALANCED AIRCRAFT WITH MULTIPLE AXLE STRENGTH

Country Status (11)

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

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2576281B1 (en) * 1985-01-18 1992-04-30 Aerospatiale STEERING STATION PROVIDED WITH A SIDE BROOM HANDLE ACTUABLE BY ONE HAND AND SEAT FOR SUCH A STEERING STATION
FR2604001B1 (en) * 1986-09-15 1988-12-09 Aerospatiale ELECTRIC FLIGHT CONTROL SYSTEM WITH INCIDENT PROTECTION FOR AIRCRAFT
US4696445A (en) * 1986-09-18 1987-09-29 United Technologies Corporation Collective control system for a helicopter
FI77334C (en) * 1987-03-03 1989-02-10 Teopros Oy The control device.
JPH07107643B2 (en) * 1988-02-22 1995-11-15 本田技研工業株式会社 NC synchronous control system
GB2248947B (en) * 1988-02-22 1992-08-05 Honda Motor Co Ltd Synchronous operation control system for numerically controlled machine
FR2643331B1 (en) * 1989-02-17 1995-01-13 Aerospatiale TILTING SLEEVE CONTROL DEVICE AND AIRCRAFT FLIGHT CONTROL SYSTEM COMPRISING AT LEAST ONE SUCH CONTROL DEVICE
FR2647922B1 (en) * 1989-05-31 1993-12-31 Sextant Avionique ELECTROMECHANICAL CONTROL DEVICE FOR USE IN DRIVING A VEHICLE
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 (en) * 1990-11-06 1993-01-22 Aerospatiale SYSTEM FOR INTEGRATED DEPTH AND PUSH CONTROL OF AN AIRCRAFT.
JP2681428B2 (en) * 1992-01-29 1997-11-26 日本航空電子工業株式会社 Flight controller for unmanned helicopter
JP2607205B2 (en) * 1992-06-30 1997-05-07 川崎重工業株式会社 Multi-axis side stick controller for aircraft
FR2769283B1 (en) * 1997-10-06 1999-12-03 Eurocopter France METHOD AND DEVICE FOR PERFORMING DECOUPLING OF THE BEHAVIOR OF AN AIRCRAFT, IN PARTICULAR A HELICOPTER
JP3091743B1 (en) 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 Pilot device
US6671588B2 (en) 2001-12-27 2003-12-30 Toyota Jidosha Kabushiki Kaisha System and method for controlling traveling direction of aircraft
DE10310717A1 (en) * 2003-03-10 2004-09-23 Wittenstein Ag Helicopter or simulator control device, has a control assembly that has a linear movement mechanism that is activated using a handgrip to control rotational movement of a drive element
FR2899562B1 (en) 2006-04-05 2009-01-09 Eurocopter France DEVICE FOR CONTROLLING FLIGHT OF A GIRAVION
FR2903660B1 (en) * 2006-07-12 2009-06-12 Airbus France Sas ELECTRICAL FLIGHT CONTROL SYSTEM FOR AIRCRAFT AND SEAT INCORPORATING THE SAME
FR2991295B1 (en) * 2012-06-04 2015-02-27 Eurocopter France AIRCRAFT WITH GREAT VISIBILITY
US9033284B2 (en) * 2012-11-20 2015-05-19 Sikorsky Aircraft Corporation Integrated seat mounted inceptor
FR3001439B1 (en) 2013-01-29 2015-02-27 Eurocopter France CONTROL MEMBER HAVING A COLLECTIVE LEVER OF PALESTS AND A LACET CONTROL MEANS, AND AIRCRAFT
JP5698802B2 (en) 2013-06-28 2015-04-08 ヤマハ発動機株式会社 Remote control device
US10676185B2 (en) 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Rotary wing aircraft pitch control system
CN104502009B (en) * 2014-11-28 2018-10-26 湖南三一智能控制设备有限公司 A kind of arm support collision prevention device, method and engineering machinery
FR3060528B1 (en) * 2016-12-16 2018-12-07 Safran Electronics & Defense DEVICE FOR CONTROLLING MOBILE SURFACES AND A WHEEL DIRECTOR OF AN AIRCRAFT
CN108407879B (en) * 2018-05-15 2023-12-12 北京美佳靓丽日用品有限公司 Three-dimensional direction control device
CN109592064B (en) * 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 Method for designing influence of deformation difference of airplane and mechanical control system on maneuvering control
GB2602953A (en) * 2020-08-21 2022-07-27 Hill Group Tech Limited Helicopter collective control apparatus
FR3119601A1 (en) 2021-02-10 2022-08-12 Airbus Helicopters Aircraft control system and associated aircraft

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 (en) * 1976-11-05 1978-06-05

Also Published As

Publication number Publication date
IT8120794A0 (en) 1981-03-30
JPS56167596A (en) 1981-12-23
FR2479133B1 (en) 1984-03-30
FR2479133A1 (en) 1981-10-02
ES500913A0 (en) 1982-05-16
DE3111604C2 (en) 1993-07-29
AU6886481A (en) 1981-10-08
JPH01289798A (en) 1989-11-21
JPH0358959B2 (en) 1991-09-09
AU538972B2 (en) 1984-09-06
JPH0725355B2 (en) 1995-03-22
DE3111604A1 (en) 1982-04-22
CA1158219A (en) 1983-12-06
CH652364A5 (en) 1985-11-15
IL62270A (en) 1985-03-31
ES8204681A1 (en) 1982-05-16
BR8101648A (en) 1981-10-06
GB2073114B (en) 1983-10-12
GB2073114A (en) 1981-10-14

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970228