DE602006001047D1 - Rotorblatt mit einer verstellbaren Klappe, die mittels eines Hauptkugelgelenkes montiert ist, wobei eine erste Achse mit der Klappe fest verbunden ist. - Google Patents

Rotorblatt mit einer verstellbaren Klappe, die mittels eines Hauptkugelgelenkes montiert ist, wobei eine erste Achse mit der Klappe fest verbunden ist.

Info

Publication number
DE602006001047D1
DE602006001047D1 DE602006001047T DE602006001047T DE602006001047D1 DE 602006001047 D1 DE602006001047 D1 DE 602006001047D1 DE 602006001047 T DE602006001047 T DE 602006001047T DE 602006001047 T DE602006001047 T DE 602006001047T DE 602006001047 D1 DE602006001047 D1 DE 602006001047D1
Authority
DE
Germany
Prior art keywords
flap
axis
fixedly connected
rotor blade
ball joint
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.)
Active
Application number
DE602006001047T
Other languages
English (en)
Other versions
DE602006001047T2 (de
Inventor
De La Grandmaison Franco Lorin
Michel Morant
Olivier Ardesi
Jacques Gaffiero
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 Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 SA, Eurocopter SA filed Critical Eurocopter France SA
Publication of DE602006001047D1 publication Critical patent/DE602006001047D1/de
Application granted granted Critical
Publication of DE602006001047T2 publication Critical patent/DE602006001047T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
DE602006001047T 2005-10-26 2006-10-18 Rotorblatt mit einer verstellbaren Klappe, die mittels eines Hauptkugelgelenkes montiert ist, wobei eine erste Achse mit der Klappe fest verbunden ist. Active DE602006001047T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0510916 2005-10-26
FR0510916A FR2892384B1 (fr) 2005-10-26 2005-10-26 Pale de giravion munie d'un volet orientable a l'aide d'au moins une rotule principale dont le premier arbre est solidaire dudit volet.

Publications (2)

Publication Number Publication Date
DE602006001047D1 true DE602006001047D1 (de) 2008-06-12
DE602006001047T2 DE602006001047T2 (de) 2009-07-02

Family

ID=36658862

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006001047T Active DE602006001047T2 (de) 2005-10-26 2006-10-18 Rotorblatt mit einer verstellbaren Klappe, die mittels eines Hauptkugelgelenkes montiert ist, wobei eine erste Achse mit der Klappe fest verbunden ist.

Country Status (4)

Country Link
US (1) US7585151B2 (de)
EP (1) EP1783049B1 (de)
DE (1) DE602006001047T2 (de)
FR (1) FR2892384B1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007030095B4 (de) * 2007-06-28 2012-12-20 Eurocopter Deutschland Gmbh Rotorblatt für ein Drehflügelflugzeug
US9278755B2 (en) * 2011-02-11 2016-03-08 Sikorsky Aircraft Corporation Modular integrated device for rotor blade control
EP2769915B1 (de) * 2013-02-20 2015-08-12 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Rotorschaufel mit Stellklappe
US10562619B2 (en) * 2015-01-07 2020-02-18 Sikorsky Aircraft Corporation Main rotor trim tab retention system, an aircraft employing same and a method of replacing a trim tab assembly from blade housing
GB2550889A (en) * 2016-05-27 2017-12-06 Teignbridge Propellers International Ltd Adjustable pitch propeller

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3129769A (en) * 1962-09-21 1964-04-21 Kaman Aircraft Corp Fail safe device for servo flap controlled rotor blades
US5344103A (en) * 1992-01-24 1994-09-06 Alliedsignal, Inc. Actuating system for aircraft wing slat and flap panels
JP2617281B2 (ja) * 1995-03-27 1997-06-04 株式会社コミュータヘリコプタ先進技術研究所 フラップ付きヘリコプタロータ
FR2770826B1 (fr) * 1997-11-07 2000-01-07 Eurocopter France Pale de rotor a volet orientable
FR2770827B1 (fr) * 1997-11-13 2000-01-14 Eurocopter France Dispositif a plateaux cycliques de commande du pas des pales d'un rotor avec plateau non-tournant articule par clavettes sur une rotule centrale
DE19808196C2 (de) * 1998-02-27 2003-06-05 Eurocopter Deutschland Rotorblatt für einen Hubschrauber
JP3498838B2 (ja) * 1999-11-01 2004-02-23 川崎重工業株式会社 フラップ支持機構およびフラップ付ロータブレード
DE10026018C2 (de) * 2000-05-25 2002-11-21 Daimler Chrysler Ag Kipp- bzw. Drehpositionierungsmittel
DE20320625U1 (de) * 2003-10-02 2004-11-11 Eurocopter Deutschland Gmbh Rotorblatt sowie Drehflügelflugzeug mit einem solchen Rotorblatt

Also Published As

Publication number Publication date
FR2892384B1 (fr) 2007-12-07
DE602006001047T2 (de) 2009-07-02
US7585151B2 (en) 2009-09-08
EP1783049A1 (de) 2007-05-09
EP1783049B1 (de) 2008-04-30
FR2892384A1 (fr) 2007-04-27
US20070098553A1 (en) 2007-05-03

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Legal Events

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8364 No opposition during term of opposition