ITMI20020600A1 - Metodo e dispositivo di regolazione per regolare un ipersostentatore supportato oscillante nella pala del rotore di un elicottero - Google Patents

Metodo e dispositivo di regolazione per regolare un ipersostentatore supportato oscillante nella pala del rotore di un elicottero

Info

Publication number
ITMI20020600A1
ITMI20020600A1 IT2002MI000600A ITMI20020600A ITMI20020600A1 IT MI20020600 A1 ITMI20020600 A1 IT MI20020600A1 IT 2002MI000600 A IT2002MI000600 A IT 2002MI000600A IT MI20020600 A ITMI20020600 A IT MI20020600A IT MI20020600 A1 ITMI20020600 A1 IT MI20020600A1
Authority
IT
Italy
Prior art keywords
positioner
hyper
oscillating
supported
adjusting
Prior art date
Application number
IT2002MI000600A
Other languages
English (en)
Inventor
Dieter Preibler
Original Assignee
Eurocopter Deutschland
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 Deutschland filed Critical Eurocopter Deutschland
Publication of ITMI20020600A0 publication Critical patent/ITMI20020600A0/it
Publication of ITMI20020600A1 publication Critical patent/ITMI20020600A1/it

Links

Classifications

    • 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
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/615—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including flaps mounted on blades
    • 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
    • B64C27/72—Means acting on blades
    • B64C2027/7205—Means acting on blades on each blade individually, e.g. individual blade control [IBC]
    • B64C2027/7261—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps
    • B64C2027/7266—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated by actuators
    • B64C2027/7283—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated by actuators of the piezoelectric type
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
IT2002MI000600A 2001-04-03 2002-03-22 Metodo e dispositivo di regolazione per regolare un ipersostentatore supportato oscillante nella pala del rotore di un elicottero ITMI20020600A1 (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE10116479A DE10116479C2 (de) 2001-04-03 2001-04-03 Verfahren und Regeleinrichtung zur Verstellung einer im Rotorblatt eines Hubschraubers schwenkbar gelagerten Klappe

Publications (2)

Publication Number Publication Date
ITMI20020600A0 ITMI20020600A0 (it) 2002-03-22
ITMI20020600A1 true ITMI20020600A1 (it) 2003-09-22

Family

ID=7680148

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2002MI000600A ITMI20020600A1 (it) 2001-04-03 2002-03-22 Metodo e dispositivo di regolazione per regolare un ipersostentatore supportato oscillante nella pala del rotore di un elicottero

Country Status (5)

Country Link
US (1) US6648599B2 (it)
JP (1) JP4148692B2 (it)
DE (1) DE10116479C2 (it)
FR (1) FR2827571B1 (it)
IT (1) ITMI20020600A1 (it)

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FR2825680B1 (fr) * 2001-06-07 2003-09-26 Sagem Actionneur de commande de vol primaire a moteur a vibration
DE10141098A1 (de) * 2001-08-22 2003-03-06 Gen Electric Windkraftanlage
CA2426711C (en) * 2002-05-02 2009-11-17 General Electric Company Wind power plant, control arrangement for a wind power plant, and method for operating a wind power plant
DE10301978A1 (de) * 2003-01-20 2004-08-05 Eurocopter Deutschland Gmbh Vorrichtung und Verfahren zum Übertragen und Bereitstellen der Energie kapazitiver Aktuatoren
BRPI0407491A (pt) 2003-02-15 2006-02-14 Gulfstream Aerospace Corp métodos para redução da probabilidade de formação de trombose da veia profunda, para elevação de concentração de oxigênio atmosférico, e de concentração de nitrogênio, para monitoração de pressão parcial de oxigênio, para controle do grau de deslocamento de oxigênio/nitrogênio de ar de chegada em resposta à pressão parcial de oxigênio, para remisturar a atmosfera nas áreas ocupadas e não ocupadas da aeronave, para abaixamento da pressão parcial de oxigênio para abaixo do nìvel natural, e para ajuste de concentrações de nitrogênio e oxigênio no interior de regiões de uma aeronave
US7410133B2 (en) * 2005-05-31 2008-08-12 The Board Of Trustees Of The Leland Stanford Junior University Miniature trailing edge effector for aerodynamic control
US20070131820A1 (en) * 2005-12-09 2007-06-14 Sikorsky Aircraft Corporation Rotorcraft control system and method of using
US8915710B2 (en) 2005-12-09 2014-12-23 Sikorsky Aircraft Corporation Brushless direct current (BLDC) motor based linear or rotary actuator for helicopter rotor control
DE102005061751B4 (de) * 2005-12-21 2013-09-19 Eurocopter Deutschland Gmbh Rotorblatt für ein Drehflügelflugzeug
CA2637226A1 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation Apparatus and method for backup control in a distributed flight control system
CA2637331A1 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation System and method for an integrated backup control system
EP1961657A1 (en) * 2007-02-22 2008-08-27 Steadicopter Ltd. Improved stabilization for flight platforms
DE102007012167B4 (de) 2007-03-12 2013-05-29 Eurocopter Deutschland Gmbh Drillelastisches und biegesteifes Stabelement zum Lagern und Führen einer beweglichen Klappe gegenüber einem Flügel eines Luftfahrzeugs
DE102007012984B4 (de) 2007-03-14 2018-10-11 Airbus Helicopters Deutschland GmbH Verbindungselement zur Kraftübertragung zwischen einem Klappenantrieb und einer an einem Flügel eines Luftfahrzeugs schwenkbeweglich gelagerten Klappe
DE102007013289B4 (de) 2007-03-16 2010-02-04 Eurocopter Deutschland Gmbh Profilverformung am Beispiel Rotorblatt
DE102007030095B4 (de) 2007-06-28 2012-12-20 Eurocopter Deutschland Gmbh Rotorblatt für ein Drehflügelflugzeug
DK2222955T3 (en) * 2007-10-29 2017-02-27 Vestas Wind Sys As Wind turbine blade and method for controlling the load on a blade
DE102008025414B4 (de) 2008-05-27 2014-09-04 Eurocopter Deutschland Gmbh Aerodynamisches Profil mit reversibel verformbarer Kontur für Luftfahrzeuge, insbesondere für Drehflügelflugzeuge
GB201009087D0 (en) * 2010-05-28 2010-07-14 Microtecnica Actuation Technol Actuator assembly for use in a rotor blade
ITTO20110981A1 (it) 2011-10-28 2012-01-27 Torino Politecnico Profilo aerodinamico a svergolamento variabile.
US8616846B2 (en) 2011-12-13 2013-12-31 General Electric Company Aperture control system for use with a flow control system
EP2743179B1 (en) * 2012-12-17 2016-06-01 Airbus Defence and Space GmbH Actuator arrangement and control surface arrangement, especially for an aircraft
EP2769915B1 (en) * 2013-02-20 2015-08-12 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotor blade with control flap
EP3485161A4 (en) * 2016-07-15 2020-04-08 Sikorsky Aircraft Corporation SENSOR SYSTEM FOR ROTOR BLADE DEFLECTION
DE102016213720A1 (de) * 2016-07-26 2018-02-01 Zf Friedrichshafen Ag System zur Datenübermittlung und -verarbeitung zur Regelung eines Rotorblattaktuators
KR102338845B1 (ko) 2020-05-22 2021-12-13 서울대학교산학협력단 플랩 구동 장치 및 회전익기의 블레이드
CN112182932B (zh) * 2020-09-25 2022-11-25 中国直升机设计研究所 一种旋转状态模型旋翼后缘襟翼偏转角度预估方法

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DE29804349U1 (de) * 1998-03-11 1998-05-20 Univ Magdeburg Tech Schaltungsanordnung zur Strom- und Ladungsregelung von kapazitiven Lasten
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FR2781174B1 (fr) * 1998-07-20 2000-10-06 Essilor Int Outil de finissage, notamment pour lentille ophtalmique, et equipements propres a sa mise en oeuvre
US6135713A (en) * 1999-01-19 2000-10-24 The Mcdonnell Douglas Helicopter Company Helicopter rotor blade flap actuator government interest
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JP3053620B1 (ja) * 1999-02-25 2000-06-19 株式会社コミュータヘリコプタ先進技術研究所 ロ―タブレ―ドのフラップ駆動装置
JP3004644B1 (ja) * 1999-03-03 2000-01-31 株式会社コミュータヘリコプタ先進技術研究所 ロ―タブレ―ドのフラップ駆動装置
US6295006B1 (en) * 1999-04-16 2001-09-25 Sikorsky Aircraft Corporation Flap angle measurement system for an active rotor control system
US6231013B1 (en) * 1999-06-16 2001-05-15 Daimlerchrysler Ag Airfoil member with a piezoelectrically actuated servo-flap
GB9918289D0 (en) * 1999-08-03 2000-05-24 British Aerospace Actuator system for aerospace controls and functions
US6354536B1 (en) * 2000-08-08 2002-03-12 Sikorsky Aircraft Corporation Rotor hub mounted actuator for controlling a blade on a rotorcraft

Also Published As

Publication number Publication date
DE10116479C2 (de) 2003-12-11
FR2827571A1 (fr) 2003-01-24
ITMI20020600A0 (it) 2002-03-22
DE10116479A1 (de) 2002-10-17
JP2002308194A (ja) 2002-10-23
US20020141867A1 (en) 2002-10-03
JP4148692B2 (ja) 2008-09-10
FR2827571B1 (fr) 2005-02-18
US6648599B2 (en) 2003-11-18

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