DE602006004817D1 - Rotorblatt versehen mit einer schwenbaren Klappe und mit einer Befestigungslasche - Google Patents

Rotorblatt versehen mit einer schwenbaren Klappe und mit einer Befestigungslasche

Info

Publication number
DE602006004817D1
DE602006004817D1 DE602006004817T DE602006004817T DE602006004817D1 DE 602006004817 D1 DE602006004817 D1 DE 602006004817D1 DE 602006004817 T DE602006004817 T DE 602006004817T DE 602006004817 T DE602006004817 T DE 602006004817T DE 602006004817 D1 DE602006004817 D1 DE 602006004817D1
Authority
DE
Germany
Prior art keywords
rotor blade
fastening tab
blade provided
hinged flap
flap
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
DE602006004817T
Other languages
English (en)
Inventor
De La Grandmaison Francois Lorin
Michel Morant
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 DE602006004817D1 publication Critical patent/DE602006004817D1/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
    • 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
    • B64C2027/7272—Means acting on blades on each blade individually, e.g. individual blade control [IBC] with flaps actuated by actuators of the electro-hydraulic 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
DE602006004817T 2005-10-26 2006-10-18 Rotorblatt versehen mit einer schwenbaren Klappe und mit einer Befestigungslasche Active DE602006004817D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0510917A FR2892383B1 (fr) 2005-10-26 2005-10-26 Pale de giravion munie d'un volet orientable et d'une languette de fixation.

Publications (1)

Publication Number Publication Date
DE602006004817D1 true DE602006004817D1 (de) 2009-03-05

Family

ID=36933558

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006004817T Active DE602006004817D1 (de) 2005-10-26 2006-10-18 Rotorblatt versehen mit einer schwenbaren Klappe und mit einer Befestigungslasche

Country Status (4)

Country Link
US (1) US7594796B2 (de)
EP (1) EP1780121B1 (de)
DE (1) DE602006004817D1 (de)
FR (1) FR2892383B1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9278755B2 (en) * 2011-02-11 2016-03-08 Sikorsky Aircraft Corporation Modular integrated device for rotor blade control
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method
US9850720B2 (en) 2014-06-30 2017-12-26 Halliburton Energy Services, Inc. Helical control line connector for connecting to a downhole completion receptacle
US10113371B2 (en) 2014-06-30 2018-10-30 Halliburton Energy Services, Inc. Downhole control line connector
US9915104B2 (en) 2014-06-30 2018-03-13 Halliburton Energy Services, Inc. Downhole expandable control line connector
WO2016003392A1 (en) 2014-06-30 2016-01-07 Halliburton Energy Services, Inc. Helical dry mate control line connector
US10060196B2 (en) 2014-06-30 2018-08-28 Halliburton Energy Services, Inc. Methods of coupling a downhole control line connector
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
GB2537630B (en) 2015-04-21 2020-11-04 Agustawestland Ltd An aerofoil
JP7096698B2 (ja) * 2018-04-23 2022-07-06 株式会社Subaru 翼構造体、翼構造体の制御方法及び航空機
CN111366043A (zh) * 2020-03-23 2020-07-03 上海机电工程研究所 适用于释放热应力的弹翼连接结构
CN113834627B (zh) * 2021-10-25 2024-04-09 中航通飞华南飞机工业有限公司 一种基于大尺寸舵面铰链力矩的气动试验装置

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2776718A (en) * 1952-09-20 1957-01-08 Daniel R Zuck Helicopter rotor
FR2770826B1 (fr) 1997-11-07 2000-01-07 Eurocopter France Pale de rotor a volet orientable
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

Also Published As

Publication number Publication date
US7594796B2 (en) 2009-09-29
FR2892383A1 (fr) 2007-04-27
EP1780121A1 (de) 2007-05-02
EP1780121B1 (de) 2009-01-14
FR2892383B1 (fr) 2007-12-07
US20070098554A1 (en) 2007-05-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition