ATE510768T1 - Schneller weitbereichs-hybridhelikopter mit längshaltungssteuerung - Google Patents

Schneller weitbereichs-hybridhelikopter mit längshaltungssteuerung

Info

Publication number
ATE510768T1
ATE510768T1 AT08787886T AT08787886T ATE510768T1 AT E510768 T1 ATE510768 T1 AT E510768T1 AT 08787886 T AT08787886 T AT 08787886T AT 08787886 T AT08787886 T AT 08787886T AT E510768 T1 ATE510768 T1 AT E510768T1
Authority
AT
Austria
Prior art keywords
hybrid helicopter
rotor
blades
pitch
attitude control
Prior art date
Application number
AT08787886T
Other languages
English (en)
Inventor
Philippe Roesch
Original Assignee
Eurocopter France
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 Eurocopter France filed Critical Eurocopter France
Application granted granted Critical
Publication of ATE510768T1 publication Critical patent/ATE510768T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
    • B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8263—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like
    • B64C2027/8281—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft comprising in addition rudders, tails, fins, or the like comprising horizontal tail planes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Inorganic Insulating Materials (AREA)
  • Catching Or Destruction (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
AT08787886T 2007-05-22 2008-03-31 Schneller weitbereichs-hybridhelikopter mit längshaltungssteuerung ATE510768T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0703615A FR2916420B1 (fr) 2007-05-22 2007-05-22 Helicoptere hybride rapide a grande distance franchissable avec controle de l'assiette longitudinale.
PCT/FR2008/000447 WO2008142256A1 (fr) 2007-05-22 2008-03-31 Hélicoptère hybride rapide à grande distance franchissable et avec contrôle de l'assiette longitudinale

Publications (1)

Publication Number Publication Date
ATE510768T1 true ATE510768T1 (de) 2011-06-15

Family

ID=38858947

Family Applications (1)

Application Number Title Priority Date Filing Date
AT08787886T ATE510768T1 (de) 2007-05-22 2008-03-31 Schneller weitbereichs-hybridhelikopter mit längshaltungssteuerung

Country Status (6)

Country Link
US (1) US8052094B2 (de)
EP (1) EP2148814B1 (de)
AT (1) ATE510768T1 (de)
FR (1) FR2916420B1 (de)
PL (1) PL2148814T3 (de)
WO (1) WO2008142256A1 (de)

Families Citing this family (44)

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FR2946318B1 (fr) 2009-06-04 2012-11-16 Eurocopter France Dispositif mecanique pour combiner un premier et un deuxieme ordres de commande,et aeronef muni d'un tel dispositif.
FR2946316A1 (fr) * 2009-06-04 2010-12-10 Eurocopter France Procede de controle en lacet d'un helicoptere hybride,et helicoptere hybride muni d'un dispositif de commande en lacet apte a mettre en oeuvre ledit procede
FR2946317B1 (fr) * 2009-06-04 2011-06-17 Eurocopter France Guignol a rapport variable pour chaine de commande de vol manuelle d'aeronef a voiture tournante
FR2948629B1 (fr) * 2009-07-28 2011-08-19 Eurocopter France Amortissement variable de restitution haptique pour chaine cinematique de changement d'attitude de vol d'un aeronef
FR2952612B1 (fr) 2009-11-17 2012-01-13 Eurocopter France Aeronef a grande distance franchissable et a vitesse d'avancement elevee en vol de croisiere
FR2959205B1 (fr) * 2010-04-27 2012-04-13 Eurocopter France Procede de commande et de regulation de l'angle de braquage d'un empennage d'helicoptere hybride
FR2962404B1 (fr) 2010-07-08 2012-07-20 Eurocopter France Architecture electrique pour aeronef a voilure tournante a motorisation hybride
FR2973428B1 (fr) 2011-03-31 2019-03-15 Airbus Helicopters Encadrement etanche pour largage securise de panneau amovible
FR2977948B1 (fr) * 2011-07-12 2014-11-07 Eurocopter France Procede de pilotage automatique d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage automatique et aeronef
FR2980771B1 (fr) 2011-09-29 2014-10-31 Eurocopter France Aeronef hybride a voilure tournante
US8662442B2 (en) * 2011-11-01 2014-03-04 Textron Innovations Inc. Active prop rotor stability system
FR2990685B1 (fr) * 2012-05-21 2014-11-21 Eurocopter France Procede de commande des volets d'ailes et de l'empennage horizontal d'un helicoptere hybride
FR2990684B1 (fr) 2012-05-21 2014-11-21 Eurocopter France Procede de commande des volets d'ailes et de l'empennage horizontal d'un helicoptere hybride
FR2993243B1 (fr) 2012-07-12 2014-07-11 Eurocopter France Architecture d'alimentation hybride en puissance mecanique d'un rotor, geree a partir du reseau de bord d'un giravion
RU2521090C1 (ru) * 2013-06-13 2014-06-27 Дмитрий Сергеевич Дуров Скоростной турбоэлектрический вертолет
WO2016053408A1 (en) 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Acoustic signature variation of aircraft utilizing a clutch
WO2016054209A1 (en) 2014-10-01 2016-04-07 Sikorsky Aircraft Corporation Dual rotor, rotary wing aircraft
FR3035979B1 (fr) 2015-05-05 2018-08-17 Airbus Helicopters Loi de commande avancee pour empennage braquable
FR3037924B1 (fr) * 2015-06-23 2018-05-04 Airbus Helicopters Procede de regulation d'une installation motrice trimoteur pour un aeronef a voilure tournante
US9944388B2 (en) * 2015-08-27 2018-04-17 Sikorsky Aircraft Corporation Rotorcraft state control
US9828095B1 (en) * 2015-12-11 2017-11-28 Amazon Technologies, Inc. Motor deflection monitoring for unmanned aerial vehicles
FR3055883B1 (fr) * 2016-09-09 2019-03-29 Airbus Helicopters Systeme mecanique de transmission d'un mouvement et aeronef equipe d'un systeme correspondant
US11453480B2 (en) * 2016-10-13 2022-09-27 Alexander I. Poltorak Apparatus and method for balancing aircraft with robotic arms
CN106741903B (zh) * 2017-01-24 2023-12-15 天津凤凰智能科技有限公司 一种混合动力无人机
US10562618B2 (en) * 2017-04-03 2020-02-18 Bell Helicopter Textron Inc. Helicopter with wing augmented lift
US11092136B2 (en) * 2018-05-04 2021-08-17 Raytheon Technologies Corporation Systems and methods for optimal speed protection for power turbine governing
CN109131838A (zh) * 2018-09-21 2019-01-04 湖南湘晨飞机工业有限公司 一种旋翼机旋翼盘配平机构
CN109543271B (zh) * 2018-11-14 2022-04-26 中国直升机设计研究所 一种应用于共轴带推力桨高速直升机的配平操纵设计方法
CN109896026B (zh) * 2019-03-21 2020-08-07 南京航空航天大学 变旋翼转速直升机-涡轴发动机综合控制方法及装置
US11220852B2 (en) * 2019-05-02 2022-01-11 Textron Innovations Inc. Aircraft having versatile door systems
FR3108094B1 (fr) 2020-03-12 2022-05-13 Airbus Helicopters procédé de commande d’au moins un organe aérodynamique de dérive d’un hélicoptère hybride et un hélicoptère hybride.
FR3108093B1 (fr) 2020-03-16 2022-02-18 Airbus Helicopters Procédé d’ajustement automatique d’une portance d’un giravion hybride et un giravion hybride associé
FR3108312B1 (fr) 2020-03-17 2022-12-23 Airbus Helicopters procédé de commande d’hélices d’un hélicoptère hybride et un hélicoptère hybride.
FR3108311B1 (fr) 2020-03-17 2022-02-18 Airbus Helicopters procédé de protection d’une marge de contrôle de l’attitude en lacet d’un hélicoptère hybride et un hélicoptère hybride.
FR3108313B1 (fr) 2020-03-17 2023-05-26 Airbus Helicopters procédé de commande d’au moins une hélice d’un hélicoptère hybride et un hélicoptère hybride.
FR3108310B1 (fr) 2020-03-18 2022-11-25 Airbus Helicopters procédé de protection en couple et/ou en poussée d’hélices d’un hélicoptère hybride et hélicoptère hybride.
EP3901034A1 (de) * 2020-04-20 2021-10-27 Air Taxi Science and Technology Company Limited Verbundrotorflugzeug
FR3110545B1 (fr) 2020-05-20 2022-04-29 Airbus Helicopters Procédé d’optimisation d’une consommation d’énergie d’un hélicoptère hybride en vol en palier
CN112389636B (zh) * 2020-11-10 2022-12-09 成都云尘科技有限责任公司 一种内置整体式桨毂及控制方法
FR3117447B1 (fr) 2020-12-10 2022-11-04 Airbus Helicopters Procédé de pilotage d’un hélicoptère hybride ayant une cellule maintenue à incidence constante par régulation d’une position d’au moins un plan mobile d’empennage
FR3121124B1 (fr) 2021-03-26 2024-03-29 Airbus Helicopters Système de commande pour commander au moins une hélice d’un giravion hybride, giravion hybride et procédé de commande associé.
US12384551B2 (en) 2023-03-31 2025-08-12 Beta Air Llc System for controlling a propulsor assembly of an electric aircraft
US12312066B2 (en) 2023-03-31 2025-05-27 Beta Air Llc Propulsor assembly of an electric aircraft
CN116086756B (zh) * 2023-04-10 2023-06-13 中国空气动力研究与发展中心低速空气动力研究所 一种前飞状态下直升机全机配平的地面模拟试验方法

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US3075727A (en) * 1960-12-06 1963-01-29 Kaman Aircraft Corp Velocity sensitive stabilizer
US3698666A (en) * 1969-01-24 1972-10-17 Siai Marchetti Spa High-speed helicopter characterized by a lifting wing and by two engines fitted thereon
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CA2348217A1 (en) * 2000-05-22 2001-11-22 Jay W. Carter, Jr. Hovering gyro aircraft
US6830214B2 (en) * 2002-07-12 2004-12-14 Franklin D. Carson Rotary-wing aircraft
FR2864025B1 (fr) * 2003-12-23 2007-01-12 Eurocopter France Procede et dispositif pour reduire par un empennage orientable les vibrations engendrees sur le fuselage d'un helicoptere
US7438259B1 (en) * 2006-08-16 2008-10-21 Piasecki Aircraft Corporation Compound aircraft control system and method
US7970498B2 (en) * 2007-06-01 2011-06-28 Sikorsky Aircraft Corporation Model based sensor system for loads aware control laws

Also Published As

Publication number Publication date
US20100224720A1 (en) 2010-09-09
EP2148814A1 (de) 2010-02-03
FR2916420A1 (fr) 2008-11-28
WO2008142256A1 (fr) 2008-11-27
US8052094B2 (en) 2011-11-08
EP2148814B1 (de) 2011-05-25
FR2916420B1 (fr) 2009-08-28
PL2148814T3 (pl) 2011-10-31

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