PL2096031T3 - Śmigłowiec wyposażony w wiele elementów nośnych do sterowania kątem natarcia jego łopat - Google Patents

Śmigłowiec wyposażony w wiele elementów nośnych do sterowania kątem natarcia jego łopat

Info

Publication number
PL2096031T3
PL2096031T3 PL09002430T PL09002430T PL2096031T3 PL 2096031 T3 PL2096031 T3 PL 2096031T3 PL 09002430 T PL09002430 T PL 09002430T PL 09002430 T PL09002430 T PL 09002430T PL 2096031 T3 PL2096031 T3 PL 2096031T3
Authority
PL
Poland
Prior art keywords
attack
blades
controlling
angle
lifting elements
Prior art date
Application number
PL09002430T
Other languages
English (en)
Inventor
Pierre Berthie
Original Assignee
Airbus Helicopters
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 Airbus Helicopters filed Critical Airbus Helicopters
Publication of PL2096031T3 publication Critical patent/PL2096031T3/pl

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/54Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/605Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
PL09002430T 2008-02-27 2009-02-20 Śmigłowiec wyposażony w wiele elementów nośnych do sterowania kątem natarcia jego łopat PL2096031T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0801079A FR2927881B1 (fr) 2008-02-27 2008-02-27 Helicoptere muni d'une pluralite d'elements sustentateurs pour commander l'incidence de ses pales
EP09002430A EP2096031B1 (fr) 2008-02-27 2009-02-20 Hélicoptère muni d' une pluralité d' éléments sustentateurs pour commander l' incidence de ses pales

Publications (1)

Publication Number Publication Date
PL2096031T3 true PL2096031T3 (pl) 2012-09-28

Family

ID=39816840

Family Applications (1)

Application Number Title Priority Date Filing Date
PL09002430T PL2096031T3 (pl) 2008-02-27 2009-02-20 Śmigłowiec wyposażony w wiele elementów nośnych do sterowania kątem natarcia jego łopat

Country Status (6)

Country Link
US (1) US8177508B2 (pl)
EP (1) EP2096031B1 (pl)
CN (1) CN101519123B (pl)
CA (1) CA2655894C (pl)
FR (1) FR2927881B1 (pl)
PL (1) PL2096031T3 (pl)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO330820B1 (no) * 2009-12-24 2011-07-25 Prox Dynamics As Rotormekanisme for helikoptere
CN102081353B (zh) * 2010-06-28 2012-10-31 南京航空航天大学 电控旋翼桨距自适应控制方法
CN101927831B (zh) * 2010-07-28 2012-12-19 北京航空航天大学 一种基于变桨矩发动机配置的无人机遥控链路中断处理方法
CN102069907A (zh) * 2010-09-16 2011-05-25 孙为红 旋翼机旋翼角度固定装置
CN102285450A (zh) * 2011-06-08 2011-12-21 中北大学 变桨距三轴飞行器
CN102390527B (zh) * 2011-09-06 2015-02-04 陈仁多 一种直升机旋翼活动系统改进设计
FR2982584B1 (fr) 2011-11-10 2014-03-21 Eurocopter France Dispositif de variation de pas des pales d'un rotor de sustentation
EP2818407B1 (en) * 2013-06-24 2016-12-21 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotor system of a helicopter
CN103407571B (zh) * 2013-07-15 2015-09-09 南京航空航天大学 一种可主动摆振的直升机旋翼系统
US9315265B2 (en) * 2013-07-29 2016-04-19 Sikorsky Aircraft Corporation Adjustable scissor control link
US9796469B2 (en) * 2014-04-04 2017-10-24 The Boeing Company Modular rotor craft rotor hub system
US20160090178A1 (en) * 2014-09-29 2016-03-31 Blair John Paynton Leverage Pitch Link
US9957041B2 (en) * 2015-05-21 2018-05-01 Merlin Technology, Inc. Advanced emergency collective actuator with friction pull-off and method for a helicopter
CN105292465B (zh) * 2015-11-04 2017-05-03 中航维拓(北京)科技有限责任公司 一种直升机的刚性旋翼系统
EP3225543B1 (en) * 2016-04-01 2018-11-14 AIRBUS HELICOPTERS DEUTSCHLAND GmbH A propeller assembly with at least two propeller blades
US10994840B1 (en) 2017-08-16 2021-05-04 United States Of America As Represented By The Secretary Of The Air Force Thrust vectoring control of a cyclorotor
CN112623211B (zh) * 2020-12-28 2022-09-06 桂林航天工业学院 一种测绘航拍用的无人机

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457429A (en) * 1945-05-09 1948-12-28 Bell Aircraft Corp Rotary wing aircraft
US2481750A (en) * 1947-06-03 1949-09-13 United Helicopters Inc Helicopter
US2534353A (en) * 1949-01-24 1950-12-19 United Helicopters Inc Rotary wing aircraft
GB735571A (en) * 1951-06-25 1955-08-24 Hiller Helicopters Rotor head for rotary wing aircraft
US2818123A (en) * 1955-06-23 1957-12-31 Hiller Helicopters Rotary wing aircraft
DE2409227A1 (de) * 1974-02-27 1975-09-04 Schlueter Dieter Hauptrotor fuer einen hubschrauber
CN1472113A (zh) * 2002-08-02 2004-02-04 洪 章 新型旋翼飞行器
CN2776504Y (zh) * 2005-01-31 2006-05-03 杨克伟 一种直升机螺旋桨操纵装置
CN100415602C (zh) * 2005-06-29 2008-09-03 上海大学 非对称桨叶变距装置

Also Published As

Publication number Publication date
CA2655894C (fr) 2012-05-15
CA2655894A1 (fr) 2009-08-27
CN101519123A (zh) 2009-09-02
CN101519123B (zh) 2011-11-16
EP2096031A1 (fr) 2009-09-02
FR2927881B1 (fr) 2010-10-29
US20090214340A1 (en) 2009-08-27
EP2096031B1 (fr) 2012-04-18
FR2927881A1 (fr) 2009-08-28
US8177508B2 (en) 2012-05-15

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