HK1206694A1 - 多重可控制氣流改良裝置 - Google Patents

多重可控制氣流改良裝置

Info

Publication number
HK1206694A1
HK1206694A1 HK15107484.1A HK15107484A HK1206694A1 HK 1206694 A1 HK1206694 A1 HK 1206694A1 HK 15107484 A HK15107484 A HK 15107484A HK 1206694 A1 HK1206694 A1 HK 1206694A1
Authority
HK
Hong Kong
Prior art keywords
modification devices
multiple controllable
airflow modification
controllable airflow
devices
Prior art date
Application number
HK15107484.1A
Other languages
English (en)
Inventor
Nicholas R Guida
Original Assignee
Tamarack Aerospace Group 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
Priority claimed from US13/438,614 external-priority patent/US9162755B2/en
Application filed by Tamarack Aerospace Group Inc filed Critical Tamarack Aerospace Group Inc
Publication of HK1206694A1 publication Critical patent/HK1206694A1/zh

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
    • B64C3/54—Varying in area
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B64C23/076—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices comprising one or more separate moveable members thereon affecting the vortices, e.g. flaps
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/16—Stabilising surfaces adjustable about spanwise axes
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)
  • User Interface Of Digital Computer (AREA)
  • Traffic Control Systems (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
HK15107484.1A 2012-04-03 2015-08-04 多重可控制氣流改良裝置 HK1206694A1 (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/438,614 US9162755B2 (en) 2009-12-01 2012-04-03 Multiple controllable airflow modification devices
PCT/US2013/033577 WO2013151810A1 (en) 2012-04-03 2013-03-22 Multiple controllable airflow modification devices

Publications (1)

Publication Number Publication Date
HK1206694A1 true HK1206694A1 (zh) 2016-01-15

Family

ID=49300949

Family Applications (1)

Application Number Title Priority Date Filing Date
HK15107484.1A HK1206694A1 (zh) 2012-04-03 2015-08-04 多重可控制氣流改良裝置

Country Status (6)

Country Link
EP (1) EP2834146B1 (zh)
JP (1) JP6272823B2 (zh)
AU (1) AU2013243818B2 (zh)
ES (1) ES2964283T3 (zh)
HK (1) HK1206694A1 (zh)
WO (1) WO2013151810A1 (zh)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110127383A1 (en) 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
US9162755B2 (en) 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
EP3594115B1 (en) 2013-02-05 2023-08-23 Tamarack Aerospace Group, Inc. Controllable airflow modification device periodic load control
DE202014104042U1 (de) * 2014-08-28 2015-09-01 Centerline Design Gmbh Winglet für angeströmte Flächen
GB2532228A (en) * 2014-11-12 2016-05-18 Airbus Operations Ltd An aircraft wing
FR3053955A1 (fr) * 2016-07-13 2018-01-19 Jean-Pierre Martinez Aeronef polyvalent a helice propulsive dote de trois surfaces portantes et de dispositifs permettant d’accueillir differentes rallonges d’ailes.
GB2559968A (en) * 2017-02-22 2018-08-29 Airbus Operations Ltd A winglet and method of designing a winglet
US11254412B2 (en) * 2019-03-29 2022-02-22 The Boeing Company Foldable raked wing tips having aerodynamic devices

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2149956C3 (de) * 1971-10-07 1974-03-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochauftriebsflügel
US4725020A (en) * 1980-12-09 1988-02-16 The Boeing Company Control system incorporating structural feedback
DE3242584A1 (de) * 1982-11-18 1984-05-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung von zusatzflaechen an den spitzen eines tragfluegels
US4671473A (en) * 1984-11-08 1987-06-09 Goodson Kenneth W Airfoil
JPH01254491A (ja) * 1988-04-04 1989-10-11 Mitsubishi Heavy Ind Ltd 前縁フラップ装置
JPH06502364A (ja) * 1990-07-25 1994-03-17 サドレアー・ヴィートール・エアクラフト・カンパニー・プロプライエタリー・リミテッド Ｖｔｏｌ航空機のための推進ユニット
US5156358A (en) * 1991-04-11 1992-10-20 Northrop Corporation Aircraft outboard control
DE10302514B4 (de) * 2003-01-23 2008-12-18 Eads Deutschland Gmbh Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts
DE10313290B4 (de) * 2003-03-25 2005-12-29 Johannes Schweiger Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche oder Ruderfläche eines Fluggeräts
EP2064116B1 (de) * 2006-09-15 2014-07-23 Airbus Operations GmbH Aerodynamischer körper sowie tragflügel mit aerodynamischem körper zur beeinflussung von nachlaufwirbeln
US7744038B2 (en) * 2007-06-15 2010-06-29 The Boeing Company Controllable winglets
US20110127383A1 (en) 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet

Also Published As

Publication number Publication date
JP6272823B2 (ja) 2018-01-31
EP2834146A1 (en) 2015-02-11
ES2964283T3 (es) 2024-04-05
JP2015516329A (ja) 2015-06-11
WO2013151810A1 (en) 2013-10-10
EP2834146A4 (en) 2015-12-09
AU2013243818A1 (en) 2014-10-23
EP2834146B1 (en) 2023-10-11
AU2013243818B2 (en) 2017-06-29

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