SE351608B - - Google Patents

Info

Publication number
SE351608B
SE351608B SE12133/68A SE1213368A SE351608B SE 351608 B SE351608 B SE 351608B SE 12133/68 A SE12133/68 A SE 12133/68A SE 1213368 A SE1213368 A SE 1213368A SE 351608 B SE351608 B SE 351608B
Authority
SE
Sweden
Application number
SE12133/68A
Inventor
H Ask
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.)
Filing date
Publication date
Application filed by United Aircraft Corp filed Critical United Aircraft Corp
Publication of SE351608B publication Critical patent/SE351608B/xx

Links

Classifications

    • 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
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0833Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control
    • 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
    • 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00Machine element or mechanism
    • Y10T74/20Control lever and linkage systems
    • Y10T74/20207Multiple controlling elements for single controlled element

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Security & Cryptography (AREA)
  • Mechanical Control Devices (AREA)
  • Hydraulic Clutches, Magnetic Clutches, Fluid Clutches, And Fluid Joints (AREA)
  • Regulating Braking Force (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
SE12133/68A 1967-09-11 1968-09-10 SE351608B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US66661967A 1967-09-11 1967-09-11

Publications (1)

Publication Number Publication Date
SE351608B true SE351608B (de) 1972-12-04

Family

ID=24674764

Family Applications (1)

Application Number Title Priority Date Filing Date
SE12133/68A SE351608B (de) 1967-09-11 1968-09-10

Country Status (6)

Country Link
US (1) US3421719A (de)
JP (1) JPS491438B1 (de)
DE (1) DE1781220C3 (de)
FR (1) FR1579955A (de)
GB (1) GB1207764A (de)
SE (1) SE351608B (de)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5158047U (de) * 1974-10-28 1976-05-07
JPS51136956U (de) * 1975-04-26 1976-11-05
JPS5444741U (de) * 1977-09-01 1979-03-28
JPS5462948U (de) * 1978-04-22 1979-05-02
JPS555727U (de) * 1978-06-29 1980-01-16
JPS558317U (de) * 1978-06-30 1980-01-19
DE3131646A1 (de) * 1981-08-11 1983-02-24 Viktor Lavrent'evič Božanov Einrichtung zur verhinderung einer ueberschreitung des zulaessigen anstellwinkels durch einen flugapparat
US6981409B2 (en) * 2003-08-01 2006-01-03 The Boeing Company Control surface controller force measurement system
US7331548B1 (en) * 2004-12-02 2008-02-19 Hawker Beechcraft Corporation Control linkage for T-tail aircraft elevator surfaces
US7624943B2 (en) 2006-03-22 2009-12-01 The Boeing Company Multi-mode unmanned and manned vehicle systems and methods
PT2341252E (pt) * 2009-12-30 2012-07-05 Agustawestland Spa Aeronave
US10065728B2 (en) * 2011-06-30 2018-09-04 Parker-Hannifin Corporation Horizontal stabilizer trim actuator failure detection system and method using position sensors
US10933978B2 (en) 2017-01-10 2021-03-02 Parker-Hannifin Corporation Moving end electronic detection of secondary load path engagement of aircraft flight control actuator
CN110775252A (zh) * 2019-10-24 2020-02-11 北京希姆咨询有限公司 一种飞机驾驶操纵结构及方法、飞机
CN114415706A (zh) * 2021-12-31 2022-04-29 中国航空工业集团公司西安飞机设计研究所 一种大型飞机俯仰角保持控制算法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2352334A (en) * 1942-06-09 1944-06-27 Macomber Thomas Wesson Aircraft control system
US2623717A (en) * 1946-05-06 1952-12-30 Sperry Corp Control system for controlled airfoils of aircraft
US2581250A (en) * 1950-08-28 1952-01-01 A V Roe Canada Ltd Power assisted control

Also Published As

Publication number Publication date
DE1781220A1 (de) 1970-10-08
US3421719A (en) 1969-01-14
DE1781220B2 (de) 1974-12-05
DE1781220C3 (de) 1975-07-17
JPS491438B1 (de) 1974-01-14
FR1579955A (de) 1969-08-29
GB1207764A (en) 1970-10-07

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