GB201220653D0 - Improvements in aircraft - Google Patents

Improvements in aircraft

Info

Publication number
GB201220653D0
GB201220653D0 GB201220653A GB201220653A GB201220653D0 GB 201220653 D0 GB201220653 D0 GB 201220653D0 GB 201220653 A GB201220653 A GB 201220653A GB 201220653 A GB201220653 A GB 201220653A GB 201220653 D0 GB201220653 D0 GB 201220653D0
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.)
Ceased
Application number
GB201220653A
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 GB201220653A priority Critical patent/GB201220653D0/en
Publication of GB201220653D0 publication Critical patent/GB201220653D0/en
Priority to GB1312667.7A priority patent/GB2516248A/en
Priority to GB1320181.9A priority patent/GB2521814B/en
Ceased legal-status Critical Current

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
    • 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

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)
GB201220653A 2012-11-16 2012-11-16 Improvements in aircraft Ceased GB201220653D0 (en)

Priority Applications (3)

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
GB1320181.9A GB2521814B (en) 2012-11-16 2013-11-15 A feedback system for a flying control member of an aircraft

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB201220653D0 true GB201220653D0 (en) 2013-01-02

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 After (2)

Application Number Title Priority Date Filing Date
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

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
EP3602078B1 (en) * 2017-09-01 2021-11-03 Thales Canada Inc. Method and system for determining an estimation of an anemometric parameter in 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

Also Published As

Publication number Publication date
GB201320181D0 (en) 2014-01-01
GB2521814A (en) 2015-07-08
GB2521814B (en) 2018-11-14
GB201312667D0 (en) 2013-08-28
GB2516248A (en) 2015-01-21

Similar Documents

Publication Publication Date Title
IL254716B (en) Zinc-lysine complex
IL236941A0 (en) Vertical-takeoff aircraft
ZA201503358B (en) Structure
EP2941539A4 (en) Propeller
IL227844A0 (en) Aircraft
ZA201402236B (en) Aircraft
IL213180A0 (en) Aircraft
EP3696093C0 (en) Runway arrangement
GB201319035D0 (en) Spolier structure
GB201217801D0 (en) An aircraft structure
SG11201503361SA (en) Composite
HUP1300640A2 (en) Belt-mounting structure
EP2871919A4 (en) Structure
EP2813390A4 (en) Armrest
SG11201505131UA (en) Sphingomyelin-containing supplement
GB201320181D0 (en) Improvements in aircraft
GB2508899B (en) Improvements in antennas
PL2932562T3 (en) Improvements in antennas
GB201216038D0 (en) Panel-wing airplane
GB201202593D0 (en) All in one
GB201203736D0 (en) Panelled airplane
GB201217715D0 (en) Improvements in swimfeeder devices
GB201210602D0 (en) Improvement in compsite materials
GB201212458D0 (en) Three in one icing bag
GB201220489D0 (en) Catapults

Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)