DE60130534D1 - Klappestellantriebssystem - Google Patents

Klappestellantriebssystem

Info

Publication number
DE60130534D1
DE60130534D1 DE60130534T DE60130534T DE60130534D1 DE 60130534 D1 DE60130534 D1 DE 60130534D1 DE 60130534 T DE60130534 T DE 60130534T DE 60130534 T DE60130534 T DE 60130534T DE 60130534 D1 DE60130534 D1 DE 60130534D1
Authority
DE
Germany
Prior art keywords
airfoil structure
flap
flap member
actuator system
point
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.)
Expired - Lifetime
Application number
DE60130534T
Other languages
English (en)
Other versions
DE60130534T2 (de
Inventor
David Allan Fink
Marcel Pierre Gaudreau
Stephen Mark Carson
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.)
Diversified Technologies Inc
Original Assignee
Diversified Technologies Inc
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 Diversified Technologies Inc filed Critical Diversified Technologies Inc
Publication of DE60130534D1 publication Critical patent/DE60130534D1/de
Application granted granted Critical
Publication of DE60130534T2 publication Critical patent/DE60130534T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/50—Varying camber by leading or trailing edge flaps
    • 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)
  • Power-Operated Mechanisms For Wings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
  • Seal Device For Vehicle (AREA)
  • Fluid-Driven Valves (AREA)
  • Actuator (AREA)
DE60130534T 2000-05-01 2001-04-27 Klappenstellantriebssystem Expired - Lifetime DE60130534T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US562155 2000-05-01
US09/562,155 US6508439B1 (en) 1999-05-18 2000-05-01 Flap actuator system
PCT/US2001/013696 WO2001083295A1 (en) 2000-05-01 2001-04-27 Flap actuator system

Publications (2)

Publication Number Publication Date
DE60130534D1 true DE60130534D1 (de) 2007-10-31
DE60130534T2 DE60130534T2 (de) 2008-06-26

Family

ID=24245019

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60130534T Expired - Lifetime DE60130534T2 (de) 2000-05-01 2001-04-27 Klappenstellantriebssystem

Country Status (5)

Country Link
US (1) US6508439B1 (de)
EP (1) EP1224116B1 (de)
AT (1) ATE373601T1 (de)
DE (1) DE60130534T2 (de)
WO (1) WO2001083295A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6513762B2 (en) * 1999-05-18 2003-02-04 Diversified Technologies, Inc. Flap actuator system
DE10035333B4 (de) * 2000-07-20 2008-08-14 Eads Deutschland Gmbh Rotorblatt mit Steuerklappen
US6672540B1 (en) 2002-12-03 2004-01-06 Rockwell Collins, Inc. Actuator for aircraft stabilizers with a failure responsive lock control mechanism
DE10356230A1 (de) * 2003-12-02 2005-07-07 Zf Friedrichshafen Ag Rotoreinheit an einem Drehflügler
US20060038058A1 (en) * 2004-08-23 2006-02-23 Routery Edward E Active control of airfoils
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
US7841559B1 (en) 2006-02-16 2010-11-30 Mbda Incorporated Aerial vehicle with variable aspect ratio deployable wings
WO2008063154A2 (en) * 2006-10-12 2008-05-29 United Technologies Corporation Fan variable area nozzle with adaptive structure
US7762770B2 (en) * 2006-12-14 2010-07-27 Sikorsky Aircraft Corporation Hybrid actuator for helicopter rotor blade control flaps
US8672627B2 (en) * 2006-12-14 2014-03-18 Sikorsky Aircraft Corporation On-blade actuator for helicopter rotor blade control flaps
GB2470345A (en) * 2009-03-17 2010-11-24 Vestas Wind Systems A S Rotary actuator hinge for connecting first and second wind turbine components.
GB2472759A (en) 2009-03-17 2011-02-23 Vestas Wind Sys As Retractable hinge apparatus for wind turbine control surface
DE102011018906A1 (de) * 2011-04-28 2012-10-31 Airbus Operations Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Beeinflussen der Hochauftriebseigenschaften eines Flugzeugs
EP2674359A1 (de) 2012-06-13 2013-12-18 Claverham Limited Trockengeschmierter Drehaktuator für interne Rotorblattsteuerung
WO2016076937A1 (en) 2014-10-28 2016-05-19 Sikorsky Aircraft Corporation Lubricant level sensing for an actuator
EP3584153A1 (de) * 2018-06-20 2019-12-25 Bombardier Inc. System mit variabler wölbung
US11738861B2 (en) * 2018-06-21 2023-08-29 Thomas Norman Hesse Propelling system with variable aerodynamic controls

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1449647A (fr) * 1965-04-08 1966-05-06 Marchetti Soc Charles Aérodyne à décollage vertical ou court et à vitesse de translation élevée
FR2125111B1 (de) * 1971-02-11 1974-02-15 Aerospatiale
DE4334680C2 (de) * 1993-10-12 1996-07-11 Daimler Benz Aerospace Airbus Vorrichtung zur Verstellung von Spalt-Steuerklappen
US5626312A (en) * 1994-07-06 1997-05-06 Mcdonnell Douglas Corporation Piezoelectric actuator
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
US5686907A (en) * 1995-05-15 1997-11-11 The Boeing Company Skew and loss detection system for individual high lift devices
US5661260A (en) * 1996-05-01 1997-08-26 The United States Of America As Represented By The Secretary Of The Navy Fin assembly for a vehicle
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

Also Published As

Publication number Publication date
ATE373601T1 (de) 2007-10-15
EP1224116B1 (de) 2007-09-19
EP1224116A1 (de) 2002-07-24
WO2001083295A1 (en) 2001-11-08
US6508439B1 (en) 2003-01-21
DE60130534T2 (de) 2008-06-26
EP1224116A4 (de) 2006-06-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition