GB2521814B - A feedback system for a flying control member of an aircraft - Google Patents

A feedback system for a flying control member of an aircraft

Info

Publication number
GB2521814B
GB2521814B GB1320181.9A GB201320181A GB2521814B GB 2521814 B GB2521814 B GB 2521814B GB 201320181 A GB201320181 A GB 201320181A GB 2521814 B GB2521814 B GB 2521814B
Authority
GB
United Kingdom
Prior art keywords
aircraft
control member
feedback system
flying control
flying
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 - Fee Related
Application number
GB1320181.9A
Other versions
GB2521814A (en
GB201320181D0 (en
Inventor
L Mcculloch Norman
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB201320181D0 publication Critical patent/GB201320181D0/en
Priority to EP14177141.0A priority Critical patent/EP2826707B1/en
Priority to ES14177141T priority patent/ES2913951T3/en
Priority to EP19184970.2A priority patent/EP3594111A1/en
Publication of GB2521814A publication Critical patent/GB2521814A/en
Application granted granted Critical
Publication of GB2521814B publication Critical patent/GB2521814B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/507—Transmitting means with power amplification using electrical energy with artificial feel
    • 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
    • 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
    • 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
    • B64C13/24—Transmitting means
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/345—Transmitting means without power amplification or where power amplification is irrelevant mechanical with artificial feel
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
GB1320181.9A 2012-11-16 2013-11-15 A feedback system for a flying control member of an aircraft Expired - Fee Related GB2521814B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP14177141.0A EP2826707B1 (en) 2013-07-16 2014-07-15 Feedback system for a flying control member of an aircraft
ES14177141T ES2913951T3 (en) 2013-07-16 2014-07-15 Feedback system for an aircraft flight control member
EP19184970.2A EP3594111A1 (en) 2013-07-16 2014-07-15 Feedback system for a flying control member

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB201220653A GB201220653D0 (en) 2012-11-16 2012-11-16 Improvements in aircraft
GB1312667.7A GB2516248A (en) 2012-11-16 2013-07-16 Improvements in aircraft

Publications (3)

Publication Number Publication Date
GB201320181D0 GB201320181D0 (en) 2014-01-01
GB2521814A GB2521814A (en) 2015-07-08
GB2521814B true GB2521814B (en) 2018-11-14

Family

ID=47521287

Family Applications (3)

Application Number Title Priority Date Filing Date
GB201220653A Ceased GB201220653D0 (en) 2012-11-16 2012-11-16 Improvements in aircraft
GB1312667.7A Withdrawn GB2516248A (en) 2012-11-16 2013-07-16 Improvements in aircraft
GB1320181.9A Expired - Fee Related GB2521814B (en) 2012-11-16 2013-11-15 A feedback system for a flying control member of an aircraft

Family Applications Before (2)

Application Number Title Priority Date Filing Date
GB201220653A Ceased GB201220653D0 (en) 2012-11-16 2012-11-16 Improvements in aircraft
GB1312667.7A Withdrawn GB2516248A (en) 2012-11-16 2013-07-16 Improvements in aircraft

Country Status (1)

Country Link
GB (3) GB201220653D0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110709709B (en) * 2017-09-01 2022-02-25 泰雷兹加拿大公司 Method and system for determining an estimate of a speed measurement parameter of an aircraft

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB619988A (en) * 1946-10-16 1949-03-17 Saunders Roe Ltd Improvements in flying controls for aircraft
US3094300A (en) * 1960-06-23 1963-06-18 Sperry Rand Corp Flight path control system
US3747876A (en) * 1971-06-01 1973-07-24 Mc Donnell Douglas Corp Variable load feel
EP0034873A2 (en) * 1980-02-25 1981-09-02 The Boeing Company Aircraft rudder ratio servo loop system
US5911390A (en) * 1997-07-09 1999-06-15 Mcdonnell Douglas Corporation Bobweight assembly for establishing a force feedback on a manually movable control element
US5979835A (en) * 1995-05-15 1999-11-09 The Boeing Company Aircraft pitch-axis stability and command augmentation system
DE19960288A1 (en) * 1999-12-14 2001-07-05 Gabor Csapo Device to support control stick operation for vehicle; has force-applying element in working train of control stick and mechanically connected to aileron to apply additional force
US20070164168A1 (en) * 2006-01-17 2007-07-19 Hirvonen Jukka M System and method for an integrated backup control system
EP1908685A2 (en) * 2006-10-02 2008-04-09 Honeywell International Inc. Motor balanced active user interface assembly
US20080142642A1 (en) * 2006-10-26 2008-06-19 Honeywell International, Inc. Cogless motor driven active user interface haptic feedback system
WO2011048399A1 (en) * 2009-10-19 2011-04-28 Bae Systems Plc Tactile cueing apparatus
GB2482407A (en) * 2010-07-28 2012-02-01 Woodward Mpc Inc Position control system for cross coupled operation of fly-by-wire control columns

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8299905B2 (en) * 2005-02-10 2012-10-30 Quentin King System for applying tactile stimulation to the controller of unmanned vehicles
US8401716B2 (en) * 2006-05-17 2013-03-19 Textron Innovations Inc. Flight control systems
US7805226B2 (en) * 2006-09-29 2010-09-28 Honeywell International Inc. Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback
US8374804B2 (en) * 2010-02-12 2013-02-12 Honeywell International Inc. Aircraft dynamic pressure estimation system and method
US8729848B2 (en) * 2010-12-22 2014-05-20 Woodward Mpc Inc. Fail-passive variable gradient control stick drive system

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB619988A (en) * 1946-10-16 1949-03-17 Saunders Roe Ltd Improvements in flying controls for aircraft
US3094300A (en) * 1960-06-23 1963-06-18 Sperry Rand Corp Flight path control system
US3747876A (en) * 1971-06-01 1973-07-24 Mc Donnell Douglas Corp Variable load feel
EP0034873A2 (en) * 1980-02-25 1981-09-02 The Boeing Company Aircraft rudder ratio servo loop system
US5979835A (en) * 1995-05-15 1999-11-09 The Boeing Company Aircraft pitch-axis stability and command augmentation system
US5911390A (en) * 1997-07-09 1999-06-15 Mcdonnell Douglas Corporation Bobweight assembly for establishing a force feedback on a manually movable control element
DE19960288A1 (en) * 1999-12-14 2001-07-05 Gabor Csapo Device to support control stick operation for vehicle; has force-applying element in working train of control stick and mechanically connected to aileron to apply additional force
US20070164168A1 (en) * 2006-01-17 2007-07-19 Hirvonen Jukka M System and method for an integrated backup control system
EP1908685A2 (en) * 2006-10-02 2008-04-09 Honeywell International Inc. Motor balanced active user interface assembly
US20080142642A1 (en) * 2006-10-26 2008-06-19 Honeywell International, Inc. Cogless motor driven active user interface haptic feedback system
WO2011048399A1 (en) * 2009-10-19 2011-04-28 Bae Systems Plc Tactile cueing apparatus
GB2482407A (en) * 2010-07-28 2012-02-01 Woodward Mpc Inc Position control system for cross coupled operation of fly-by-wire control columns

Also Published As

Publication number Publication date
GB201312667D0 (en) 2013-08-28
GB2521814A (en) 2015-07-08
GB201320181D0 (en) 2014-01-01
GB201220653D0 (en) 2013-01-02
GB2516248A (en) 2015-01-21

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)

Free format text: REGISTERED BETWEEN 20210513 AND 20210519

PCNP Patent ceased through non-payment of renewal fee

Effective date: 20211115