WO2009153236A3 - Taumelscheibenbetätigungsvorrichtung für einen helikopter - Google Patents

Taumelscheibenbetätigungsvorrichtung für einen helikopter Download PDF

Info

Publication number
WO2009153236A3
WO2009153236A3 PCT/EP2009/057345 EP2009057345W WO2009153236A3 WO 2009153236 A3 WO2009153236 A3 WO 2009153236A3 EP 2009057345 W EP2009057345 W EP 2009057345W WO 2009153236 A3 WO2009153236 A3 WO 2009153236A3
Authority
WO
WIPO (PCT)
Prior art keywords
helicopter
swash plate
actuating device
plate actuating
actuators
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.)
Ceased
Application number
PCT/EP2009/057345
Other languages
English (en)
French (fr)
Other versions
WO2009153236A2 (de
Inventor
Markus Christmann
Boris Grohmann
Peter JÄNKER
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.)
Airbus Defence and Space GmbH
Original Assignee
EADS Deutschland GmbH
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 EADS Deutschland GmbH filed Critical EADS Deutschland GmbH
Publication of WO2009153236A2 publication Critical patent/WO2009153236A2/de
Publication of WO2009153236A3 publication Critical patent/WO2009153236A3/de
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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
    • B64C27/605—Transmitting 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)
  • Transmission Devices (AREA)
  • Toys (AREA)

Abstract

Helikopterrotor mit wenigstens vier elektromechanisehen Aktuatoren (31-36) zum Betätigen einer Taumelscheibe (5), wobei die Zuverlässigkeit der Helikoptersteuerung durch redundante Aktuatoren erhöht wird.
PCT/EP2009/057345 2008-06-19 2009-06-15 Taumelscheibenbetätigungsvorrichtung für einen helikopter Ceased WO2009153236A2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE200810028866 DE102008028866B4 (de) 2008-06-19 2008-06-19 Taumelscheibenbetätigungsvorrichtung für einen Helikopter
DE102008028866.7 2008-06-19

Publications (2)

Publication Number Publication Date
WO2009153236A2 WO2009153236A2 (de) 2009-12-23
WO2009153236A3 true WO2009153236A3 (de) 2010-04-15

Family

ID=41319532

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2009/057345 Ceased WO2009153236A2 (de) 2008-06-19 2009-06-15 Taumelscheibenbetätigungsvorrichtung für einen helikopter

Country Status (2)

Country Link
DE (1) DE102008028866B4 (de)
WO (1) WO2009153236A2 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010021026A1 (de) 2010-05-19 2011-11-24 Eads Deutschland Gmbh Hybrides Antriebs- und Energiesystem für Fluggeräte
DE102010021025B4 (de) 2010-05-19 2014-05-08 Eads Deutschland Gmbh Hubschrauber mit Hybridantrieb
DE102010021024B4 (de) 2010-05-19 2014-07-03 Eads Deutschland Gmbh Hauptrotorantrieb für Hubschrauber
US9365288B2 (en) * 2012-11-15 2016-06-14 Textron Innovations Inc. Blade-pitch control system with indexing swashplate
US10753444B2 (en) 2016-01-13 2020-08-25 Moog Inc. Summing and fault tolerant rotary actuator assembly
DE102016115485A1 (de) * 2016-08-22 2018-02-22 Valerian Design Gmbh Innovativer Helikopter
FR3055312B1 (fr) * 2016-08-31 2019-04-19 Airbus Helicopters Aeronef muni d'un ensemble de plateaux cyclique et d'au moins une servocommande inclinee
US11427315B2 (en) * 2019-06-26 2022-08-30 Textron Innovations Inc. Rotor blade control system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2941258A1 (de) * 1978-10-11 1980-04-30 Textron Inc Taumelscheiben-steuerung fuer einen hubschrauberrotor
US4362085A (en) * 1979-06-11 1982-12-07 The United States Of America As Represented By The Secretary Of The Army Flight control system
GB2108917A (en) * 1981-11-06 1983-05-25 Draper Lab Charles S Helicopter swashplate controller
DE69205810T2 (de) * 1991-12-11 1996-06-13 Aerospatiale Vorrichtung mit verminderter Störanfälligkeit zur Steuerung eines Hubschrauberrotors durch eine Taumelscheibe.

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3767323A (en) * 1972-06-21 1973-10-23 Messerschmitt Boelkow Blohm Control means primarily for rotary-wing aircraft
DE2447877A1 (de) * 1974-10-08 1976-04-22 Fritz W Heller Hubschrauber- oder drehflueglerrotorblattsteuerung
US5678786A (en) * 1995-12-06 1997-10-21 Mcdonnell Douglas Helicopter Co. Reconfigurable helicopter flight control system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2941258A1 (de) * 1978-10-11 1980-04-30 Textron Inc Taumelscheiben-steuerung fuer einen hubschrauberrotor
US4362085A (en) * 1979-06-11 1982-12-07 The United States Of America As Represented By The Secretary Of The Army Flight control system
GB2108917A (en) * 1981-11-06 1983-05-25 Draper Lab Charles S Helicopter swashplate controller
DE69205810T2 (de) * 1991-12-11 1996-06-13 Aerospatiale Vorrichtung mit verminderter Störanfälligkeit zur Steuerung eines Hubschrauberrotors durch eine Taumelscheibe.

Also Published As

Publication number Publication date
DE102008028866A1 (de) 2009-12-31
DE102008028866B4 (de) 2011-04-07
WO2009153236A2 (de) 2009-12-23

Similar Documents

Publication Publication Date Title
WO2012110569A3 (en) Door system having an actuator
WO2011011800A3 (de) Stellantrieb für ein bewegbares möbelteil
SG155150A1 (en) Detachable electrical actuator
WO2008033884A3 (en) Dual higher harmonic control (hhc) for a counter-rotating, coaxial rotor system
EP2121438A4 (de) Aktor auf dem blatt für helikopterrotorblatt-steuerklappen
EP1985536A3 (de) Steuerungseinrichtung eines Hubschrauber-Hauptrotors
EP2097316A4 (de) Hbridantrieb für rotorblattregelklappen eines hubschraubers
WO2010037732A3 (en) Projection exposure apparatus for microlithography for the production of semiconductor components
WO2009118547A3 (en) Slat deployment mechanism
EP2264562A3 (de) Verfahren und Vorrichtung zur Erzeugung einer haptischen Rückmeldung und haptische Schnittstelle
WO2009150251A3 (de) Aufzugsanlage und verfahren zur wartung einer solchen aufzugsanlage
EP2094562A4 (de) Selbstschmierender aktuator für rotorsteuerung auf der laufschaufel
MY155498A (en) Actuator having an override apparatus
EP1828621A4 (de) Drucksteuerungsventil mit intrinsischem mechanischem rückkopplungssystem
WO2007096624A3 (en) Control surface failsafe drop link
WO2012065123A3 (en) Remote operation of cementing head
GB2494603A (en) Electromechanical switch device and method of operating the same
GB2479089B (en) Rotary encoder with built-in-self-test
WO2008104370A3 (en) Multilayer film structure
WO2011159253A3 (en) A module for controlling a force required to actuate an electromechanical actuator
WO2009115662A8 (fr) Systeme d'actionnement et de controle d'un capot mobile de nacelle de turboreacteur
EP1997767A4 (de) Notstopp-vorrichtung für aufzug
WO2011000850A3 (de) Elektromechanische linearstelleinheit
PL2201674T3 (pl) Sposób analizy działania napędu elektromechanicznego do zmechanizowanego manewrowania osłoną oraz napęd do jego realizacji
WO2010004200A3 (fr) Système d'ouverture et de fermeture de trappe pour case de train d'atterrissage d'un aéronef

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 09765816

Country of ref document: EP

Kind code of ref document: A2

122 Ep: pct application non-entry in european phase

Ref document number: 09765816

Country of ref document: EP

Kind code of ref document: A2