DE60142830D1 - Multimodales schwenkrotorgondel-steuerungssystem - Google Patents

Multimodales schwenkrotorgondel-steuerungssystem

Info

Publication number
DE60142830D1
DE60142830D1 DE60142830T DE60142830T DE60142830D1 DE 60142830 D1 DE60142830 D1 DE 60142830D1 DE 60142830 T DE60142830 T DE 60142830T DE 60142830 T DE60142830 T DE 60142830T DE 60142830 D1 DE60142830 D1 DE 60142830D1
Authority
DE
Germany
Prior art keywords
multimodal
control system
tape control
swivel rotor
rotor tape
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 - Lifetime
Application number
DE60142830T
Other languages
English (en)
Inventor
David W King
Peter M Shultz
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.)
Bell Helicopter Textron Inc
Original Assignee
Bell Helicopter Textron Inc
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 Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Application granted granted Critical
Publication of DE60142830D1 publication Critical patent/DE60142830D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] 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
    • B64C13/503—Fly-by-Wire
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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)
  • Mechanical Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Wind Motors (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Control Of Turbines (AREA)
  • Mechanical Control Devices (AREA)
DE60142830T 2000-05-16 2001-05-16 Multimodales schwenkrotorgondel-steuerungssystem Expired - Lifetime DE60142830D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US20449900P 2000-05-16 2000-05-16
PCT/US2001/015719 WO2001087706A1 (en) 2000-05-16 2001-05-16 Multi-mode tiltrotor nacelle control system with integrated envelope protection

Publications (1)

Publication Number Publication Date
DE60142830D1 true DE60142830D1 (de) 2010-09-30

Family

ID=22758157

Family Applications (2)

Application Number Title Priority Date Filing Date
DE60142830T Expired - Lifetime DE60142830D1 (de) 2000-05-16 2001-05-16 Multimodales schwenkrotorgondel-steuerungssystem
DE1282555T Pending DE1282555T1 (de) 2000-05-16 2001-05-16 Multimodales schwenkrotorgondel-steuerungssystem mit integriertem flugbereichsschutz

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE1282555T Pending DE1282555T1 (de) 2000-05-16 2001-05-16 Multimodales schwenkrotorgondel-steuerungssystem mit integriertem flugbereichsschutz

Country Status (7)

Country Link
US (1) US6644588B2 (de)
EP (1) EP1282555B1 (de)
JP (1) JP2003533404A (de)
KR (1) KR100748567B1 (de)
CA (1) CA2392734C (de)
DE (2) DE60142830D1 (de)
WO (1) WO2001087706A1 (de)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2300602T3 (es) * 2002-05-14 2008-06-16 Alfred Wilhelm Turbina eolica con envoltura.
US6719244B1 (en) * 2003-02-03 2004-04-13 Gary Robert Gress VTOL aircraft control using opposed tilting of its dual propellers or fans
US6880782B2 (en) * 2003-05-06 2005-04-19 Bell Helicopter Textron Inc. Control system for rotorcraft for preventing the vortex ring state
FR2871438B1 (fr) * 2004-06-10 2006-08-04 Eurocopter France Procede pour regler au moins un rotor deficient d'un giravion
US7878457B2 (en) * 2005-06-30 2011-02-01 Bell Helicopter Textron, Inc. Retractable vortex generator
US7571879B2 (en) * 2006-09-22 2009-08-11 Bell Helicopter Textron Inc. Automatic conversion system for tiltrotor aircraft
KR100856688B1 (ko) * 2007-04-11 2008-09-04 한국항공우주연구원 엔빌로프 보호 제어기 및 이를 구비한 틸트로터 항공기
EP2119626B1 (de) * 2008-05-15 2011-08-03 Stichting Nationaal Lucht- en Ruimtevaart Laboratorium Steuerhebelanordnung für ein Kipprotorflugzeug
KR20100026130A (ko) * 2008-08-29 2010-03-10 임채호 가변형 회전익을 이용한 수직이착륙기
WO2010038922A1 (en) * 2008-10-04 2010-04-08 Chaeho Lim Taking off and landing airplane using variable rotary wings
KR101023754B1 (ko) * 2008-10-20 2011-03-21 정수철 지상주행이 가능한 비행체 시스템
FR2941754B1 (fr) * 2009-01-30 2011-01-14 Eurocopter France Couplage a rattrapage de jeu, rotor et aeronef a voilure tournante
CN101837195B (zh) * 2010-01-21 2012-02-08 罗之洪 一种垂直起降的模型飞机
US9162748B2 (en) 2011-07-22 2015-10-20 Textron Innovations Inc. Aft-loading aircraft with twin T-tail assembly
IL222053A (en) * 2012-09-23 2016-11-30 Israel Aerospace Ind Ltd A device, method, and computerized product for aircraft management
US10518595B2 (en) 2013-03-15 2019-12-31 Terrafugia, Inc. Combined flying/driving vehicle with vertical takeoff and fixed-wing cruise capabilities
US9377784B2 (en) 2014-07-25 2016-06-28 The Boeing Company Adaptable automatic nacelle conversion for tilt rotor aircraft
US9126677B1 (en) 2014-10-16 2015-09-08 Sydney Robert Curtis Universal multi-role aircraft protocol
CN104590557B (zh) * 2015-02-05 2016-10-26 中电科（德阳广汉）特种飞机系统工程有限公司 一种多旋翼和固定翼复合飞行器的飞行控制方法及装置
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
CN105480416A (zh) * 2016-01-18 2016-04-13 南京信息工程大学 一种倾转旋翼无人机
US11067164B2 (en) 2016-04-15 2021-07-20 Terrafugia, Inc. Electronic gear shifter assembly for a dual-mode flying and driving vehicle
US11383851B2 (en) 2016-10-06 2022-07-12 Textron Innovations Inc. Tiltrotor control
US11731772B2 (en) 2017-03-02 2023-08-22 Textron Innovations Inc. Hybrid propulsion drive train system for tiltrotor aircraft
US10974827B2 (en) 2018-05-10 2021-04-13 Joby Aero, Inc. Electric tiltrotor aircraft
US10710741B2 (en) 2018-07-02 2020-07-14 Joby Aero, Inc. System and method for airspeed determination
EP3853736A4 (de) 2018-09-17 2022-11-16 Joby Aero, Inc. Flugzeugsteuerungssystem
US10983534B2 (en) * 2018-12-07 2021-04-20 Joby Aero, Inc. Aircraft control system and method
US20200331602A1 (en) 2018-12-07 2020-10-22 Joby Aero, Inc. Rotary airfoil and design method therefor
US10845823B2 (en) 2018-12-19 2020-11-24 Joby Aero, Inc. Vehicle navigation system
CN116646641A (zh) 2019-04-23 2023-08-25 杰欧比飞行有限公司 电池热管理系统及方法
US11230384B2 (en) 2019-04-23 2022-01-25 Joby Aero, Inc. Vehicle cabin thermal management system and method
US11554855B2 (en) * 2019-12-31 2023-01-17 Textron Innovations Inc. System and method for protection against vortex ring state
JP7418738B2 (ja) * 2020-01-17 2024-01-22 国立研究開発法人宇宙航空研究開発機構 形態遷移制御装置、垂直離着陸機、形態遷移制御方法及びプログラム
US11673649B2 (en) 2020-06-05 2023-06-13 Joby Aero, Inc. Aircraft control system and method
US11560225B2 (en) 2020-07-15 2023-01-24 Beta Air, Llc Hover and thrust control assembly for dual-mode aircraft
US11518497B2 (en) 2020-07-15 2022-12-06 Beta Air, Llc Hover and thrust control assembly for dual-mode aircraft

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3404852A (en) 1966-08-24 1968-10-08 Bell Aerospace Corp Trailing rotor convertiplane
GB1322169A (en) * 1969-07-23 1973-07-04 Kisovec A V Convertiplanes
US4500398A (en) * 1984-06-20 1985-02-19 The United States Of America As Represented By The Secretary Of The Interior Production of lead from sulfides
US4979698A (en) * 1988-07-07 1990-12-25 Paul Lederman Rotor system for winged aircraft
US5000398A (en) * 1988-10-25 1991-03-19 Rashev Michael S Flying multi-purpose aircraft carrier and method of V/STOL assisted flight
US5054716A (en) * 1989-10-16 1991-10-08 Bell Helicopter Textron Inc. Drive system for tiltrotor aircraft
US5823468A (en) * 1995-10-24 1998-10-20 Bothe; Hans-Jurgen Hybrid aircraft

Also Published As

Publication number Publication date
EP1282555A4 (de) 2008-02-27
KR100748567B1 (ko) 2007-08-13
US20020153452A1 (en) 2002-10-24
EP1282555B1 (de) 2010-08-18
CA2392734C (en) 2009-01-20
EP1282555A1 (de) 2003-02-12
DE1282555T1 (de) 2003-09-18
KR20030004310A (ko) 2003-01-14
CA2392734A1 (en) 2001-11-22
WO2001087706A1 (en) 2001-11-22
US6644588B2 (en) 2003-11-11
JP2003533404A (ja) 2003-11-11

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