GB201312667D0 - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB201312667D0
GB201312667D0 GB201312667A GB201312667A GB201312667D0 GB 201312667 D0 GB201312667 D0 GB 201312667D0 GB 201312667 A GB201312667 A GB 201312667A GB 201312667 A GB201312667 A GB 201312667A GB 201312667 D0 GB201312667 D0 GB 201312667D0
Authority
GB
United Kingdom
Prior art keywords
aircraft
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.)
Withdrawn
Application number
GB201312667A
Other versions
GB2516248A (en
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
Priority to GB1312667.7A priority Critical patent/GB2516248A/en
Publication of GB201312667D0 publication Critical patent/GB201312667D0/en
Priority to GB1320181.9A priority patent/GB2521814B/en
Priority to ES14177141T priority patent/ES2913951T3/en
Priority to EP14177141.0A priority patent/EP2826707B1/en
Priority to EP19184970.2A priority patent/EP3594111A1/en
Publication of GB2516248A publication Critical patent/GB2516248A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • 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
    • 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
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B64C13/46—Transmitting means with power amplification using fluid pressure 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
    • 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)
GB1312667.7A 2012-11-16 2013-07-16 Improvements in aircraft Withdrawn GB2516248A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB1312667.7A GB2516248A (en) 2012-11-16 2013-07-16 Improvements in aircraft
GB1320181.9A GB2521814B (en) 2012-11-16 2013-11-15 A 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
EP14177141.0A EP2826707B1 (en) 2013-07-16 2014-07-15 Feedback system for a flying control member of an aircraft
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 (2)

Publication Number Publication Date
GB201312667D0 true GB201312667D0 (en) 2013-08-28
GB2516248A GB2516248A (en) 2015-01-21

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 (1)

Application Number Title Priority Date Filing Date
GB201220653A Ceased GB201220653D0 (en) 2012-11-16 2012-11-16 Improvements in aircraft

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB1320181.9A Expired - Fee Related GB2521814B (en) 2012-11-16 2013-11-15 A feedback system for a flying control member of an aircraft

Country Status (1)

Country Link
GB (3) GB201220653D0 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110709709A (en) * 2017-09-01 2020-01-17 泰雷兹加拿大公司 Method and system for determining an estimate of a speed measurement parameter of an aircraft

Family Cites Families (18)

* 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
US4398242A (en) * 1980-02-25 1983-08-09 The Boeing Company Electronic controller
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
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
US8299905B2 (en) * 2005-02-10 2012-10-30 Quentin King System for applying tactile stimulation to the controller of unmanned vehicles
CA2637331A1 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation System and method for an integrated backup control system
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
US7701161B2 (en) * 2006-10-02 2010-04-20 Honeywell International Inc. Motor balanced active user interface assembly
US7759894B2 (en) * 2006-10-26 2010-07-20 Honeywell International Inc. Cogless motor driven active user interface haptic feedback system
US20080156939A1 (en) * 2007-01-03 2008-07-03 Honeywell International, Inc. Active pilot flight control stick system with passive electromagnetic feedback
CA2778058C (en) * 2009-10-19 2018-03-20 Bae Systems Plc Tactile cueing apparatus
US8374804B2 (en) * 2010-02-12 2013-02-12 Honeywell International Inc. Aircraft dynamic pressure estimation system and method
US8814103B2 (en) * 2010-07-28 2014-08-26 Woodward Mpc, Inc. Position control system for cross coupled operation of fly-by-wire control columns
US8729848B2 (en) * 2010-12-22 2014-05-20 Woodward Mpc Inc. Fail-passive variable gradient control stick drive system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110709709A (en) * 2017-09-01 2020-01-17 泰雷兹加拿大公司 Method and system for determining an estimate of a speed measurement parameter of an aircraft
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

Also Published As

Publication number Publication date
GB201220653D0 (en) 2013-01-02
GB201320181D0 (en) 2014-01-01
GB2521814A (en) 2015-07-08
GB2521814B (en) 2018-11-14
GB2516248A (en) 2015-01-21

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)