ATE553425T1 - Präzisionsarretierungen für einen hubschrauber - Google Patents

Präzisionsarretierungen für einen hubschrauber

Info

Publication number
ATE553425T1
ATE553425T1 AT09251109T AT09251109T ATE553425T1 AT E553425 T1 ATE553425 T1 AT E553425T1 AT 09251109 T AT09251109 T AT 09251109T AT 09251109 T AT09251109 T AT 09251109T AT E553425 T1 ATE553425 T1 AT E553425T1
Authority
AT
Austria
Prior art keywords
helicopter
detent
flight
inceptor
control computer
Prior art date
Application number
AT09251109T
Other languages
English (en)
Inventor
David George Miller
Robert Paul Gradle
James E Taylor
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE553425T1 publication Critical patent/ATE553425T1/de

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
    • B64C13/26—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
    • 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
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

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)
  • Mechanical Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AT09251109T 2008-04-25 2009-04-16 Präzisionsarretierungen für einen hubschrauber ATE553425T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/109,696 US8025256B2 (en) 2008-04-25 2008-04-25 Precision adjust split detent for a vehicle

Publications (1)

Publication Number Publication Date
ATE553425T1 true ATE553425T1 (de) 2012-04-15

Family

ID=41110500

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09251109T ATE553425T1 (de) 2008-04-25 2009-04-16 Präzisionsarretierungen für einen hubschrauber

Country Status (3)

Country Link
US (1) US8025256B2 (de)
EP (1) EP2133768B1 (de)
AT (1) ATE553425T1 (de)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9156546B2 (en) * 2008-03-11 2015-10-13 The Boeing Company Active-inceptor tactile-cueing hands-off rate-limit
AU2010309603B2 (en) 2009-10-19 2014-04-17 Bae Systems Plc Tactile cueing apparatus
CN103314336B (zh) * 2011-01-14 2016-08-10 贝尔直升机泰克斯特龙公司 用于控制竖直飞行航迹的飞行控制系统和方法
EP3101505B1 (de) 2011-07-15 2018-07-11 Bell Helicopter Textron Inc. Flugsteuerungsfunktionen fuer einen helikopter
US9102400B2 (en) * 2011-10-21 2015-08-11 Sikorsky Aircraft Corporation Methods and systems for providing constant-feel, multi-axis tactile cues
US8967552B2 (en) * 2012-10-19 2015-03-03 Bell Helicopter Textron Inc. Direct-drive control of aircraft stability augmentation
US9658639B2 (en) * 2012-12-20 2017-05-23 Bae Systems Plc Inceptor apparatus
US9856017B2 (en) * 2013-06-11 2018-01-02 Bell Helicopter Textron Inc. Torque based method of limiting vertical axis augmentation
CN103600836B (zh) * 2013-11-08 2015-08-05 中航飞机股份有限公司西安飞机分公司 一种飞机突风锁防误操作结构
US9121487B2 (en) * 2013-11-13 2015-09-01 Honeywell International Inc. Pilot interface for aircraft electric taxi system
FR3016488B1 (fr) * 2014-01-14 2016-02-12 Ratier Figeac Soc Procede et dispositif de commande d'un levier de manœuvre d'un vehicule
WO2015122876A1 (en) * 2014-02-11 2015-08-20 Sikorsky Aircraft Corporation Magnetic positive detent for helicopter pilot input
US9734726B2 (en) 2014-02-17 2017-08-15 The Boeing Company Systems and methods for providing landing exceedance warnings and avoidance
US20150307203A1 (en) * 2014-04-23 2015-10-29 Sikorsky Aircraft Corporation Vertical axis soft landing control
US9868522B2 (en) * 2014-08-21 2018-01-16 Bell Helicopter Textron Inc. Rotorcraft autopilot control
US10676185B2 (en) * 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Rotary wing aircraft pitch control system
US10676184B2 (en) 2014-08-28 2020-06-09 Sikorsky Aircraft Corporation Pitch control system for an aircraft
US9437056B2 (en) 2014-10-09 2016-09-06 The Boeing Company Methods and apparatus for operating flight control systems of aircrafts
EP3069990B1 (de) * 2015-03-20 2017-01-11 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Vorrichtung zur erzeugung von künstlicher krafterfassung für ein fahrzeugsteuerungssystem eines fahrzeugs, insbesondere eines flugzeugs
FR3034750B1 (fr) * 2015-04-13 2017-12-08 Airbus Helicopters Systeme de commande d'un rotor de giravion, giravion equipe d'un tel systeme et methode de commande associee
FR3042885B1 (fr) 2015-10-23 2018-07-27 Airbus Helicopters Systeme de commande d'un rotor de giravion, giravion equipe d'un tel systeme et methide de commande associee
RU2624760C1 (ru) * 2016-03-03 2017-07-06 Сергей Николаевич Низов Летательный аппарат
US10359785B2 (en) * 2016-03-31 2019-07-23 Sikorsky Aircraft Corporation Touchdown orientation control system for a rotary wing aircraft and method
US10802482B2 (en) * 2017-02-27 2020-10-13 Textron Innovations Inc. Reverse tactile cue for rotorcraft rotor overspeed protection
US10261517B2 (en) * 2017-04-11 2019-04-16 Bell Helicopter Textron Inc. Default in-detent vertical speed/altitude hold
US10474237B2 (en) * 2017-07-25 2019-11-12 Rolls-Royce Corporation Haptic feedback for rotary wing aircraft
US10926871B2 (en) * 2017-11-27 2021-02-23 Textron Innovations Inc. System and method for pilot-in-control sensing in a rotorcraft
US11117653B2 (en) * 2017-11-28 2021-09-14 Textron Innovations Inc. System and method for tactile cueing through rotorcraft pilot controls using variable friction and force gradient
US10908560B2 (en) * 2019-03-11 2021-02-02 The Boeing Company Variable rate damping based control system for backdriven control input devices
US11059568B2 (en) 2019-03-11 2021-07-13 The Boeing Company Variable operator interface for backdriving control input devices
US11745856B2 (en) * 2019-12-30 2023-09-05 Bombardier Inc. Systems and methods for controlling a resistive force of an inceptor of an aircraft
US11623740B2 (en) 2021-02-19 2023-04-11 The Boeing Company Split-reference system and method for rapid re-trimming rate command of force trim release
US12384550B2 (en) 2021-12-23 2025-08-12 Electra Aero, Inc. System and method for controlling flight path of a blown lift aircraft
WO2023122111A1 (en) * 2021-12-23 2023-06-29 Electra Aero, Inc. System and method for controlling flight path of a blown lift aircraft
US12312067B2 (en) 2022-01-24 2025-05-27 Lockheed Martin Corporation Deadband control for an aircraft

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5853152A (en) * 1997-04-29 1998-12-29 Sikorsky Aircraft Corporation Collective detent system for vertical takeoff flight operations
US7098811B2 (en) * 2002-03-21 2006-08-29 Bell Helicopter Textron Inc. Method and apparatus for tactile cueing of aircraft controls
US6679458B2 (en) * 2002-06-10 2004-01-20 The Boeing Company Split detent tactile cueing vehicle control system
US7930074B2 (en) * 2007-03-19 2011-04-19 Sikorsky Aircraft Corporation Vertical speed and flight path command module for displacement collective utilizing tactile cueing and tactile feedback

Also Published As

Publication number Publication date
EP2133768A2 (de) 2009-12-16
EP2133768B1 (de) 2012-04-11
US20090266940A1 (en) 2009-10-29
EP2133768A3 (de) 2010-09-29
US8025256B2 (en) 2011-09-27

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