ATE438561T1 - Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells - Google Patents

Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells

Info

Publication number
ATE438561T1
ATE438561T1 AT06773970T AT06773970T ATE438561T1 AT E438561 T1 ATE438561 T1 AT E438561T1 AT 06773970 T AT06773970 T AT 06773970T AT 06773970 T AT06773970 T AT 06773970T AT E438561 T1 ATE438561 T1 AT E438561T1
Authority
AT
Austria
Prior art keywords
wing
increase
surface area
end portion
integrated
Prior art date
Application number
AT06773970T
Other languages
English (en)
Inventor
Victor Stuhr
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE438561T1 publication Critical patent/ATE438561T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069Influencing 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Looms (AREA)
AT06773970T 2005-07-21 2006-06-26 Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells ATE438561T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/187,443 US8544800B2 (en) 2005-07-21 2005-07-21 Integrated wingtip extensions for jet transport aircraft and other types of aircraft
PCT/US2006/024739 WO2007018785A1 (en) 2005-07-21 2006-06-26 Integrated wingtip extensions for jet transport aircraft and other types of aircraft

Publications (1)

Publication Number Publication Date
ATE438561T1 true ATE438561T1 (de) 2009-08-15

Family

ID=37069684

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06773970T ATE438561T1 (de) 2005-07-21 2006-06-26 Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells

Country Status (8)

Country Link
US (1) US8544800B2 (de)
EP (1) EP1934090B1 (de)
JP (1) JP5230413B2 (de)
CN (2) CN103661930B (de)
AT (1) ATE438561T1 (de)
CA (1) CA2613680C (de)
DE (1) DE602006008332D1 (de)
WO (1) WO2007018785A1 (de)

Families Citing this family (90)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7699261B2 (en) * 2007-03-05 2010-04-20 Lockheed Martin Corporation Small unmanned airborne vehicle airframe
US7900876B2 (en) * 2007-08-09 2011-03-08 The Boeing Company Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods
US20090084904A1 (en) * 2007-10-02 2009-04-02 The Boeing Company Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods
DE102007059455A1 (de) * 2007-12-10 2009-06-25 Airbus Deutschland Gmbh Flügelspitzenverlängerung zur Reduktion von Wirbelschleppen bei Flugzeugen
US8167569B2 (en) 2007-12-21 2012-05-01 General Electric Company Structure and method for self-aligning rotor blade joints
US20090172776A1 (en) * 2007-12-31 2009-07-02 Petr Makagon Method and System for Establishing and Managing Trust Metrics for Service Providers in a Federated Service Provider Network
US8128035B2 (en) * 2008-04-15 2012-03-06 The Boeing Company Winglets with recessed surfaces, and associated systems and methods
US7975965B2 (en) * 2008-05-13 2011-07-12 The Boeing Company Wing tip joint in airfoils
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
EP3663193A1 (de) 2008-06-20 2020-06-10 Aviation Partners, Inc. Gekrümmte flügelspitze
US8328516B2 (en) * 2009-09-29 2012-12-11 General Electric Company Systems and methods of assembling a rotor blade extension for use in a wind turbine
US9162755B2 (en) 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
US20110127383A1 (en) * 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
EP2558364B1 (de) 2010-04-12 2014-07-23 Airbus Operations GmbH Fixer flügel eines flugzeuges
GB201011843D0 (en) * 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
US8382041B1 (en) * 2010-08-04 2013-02-26 The United States Of America As Represented By The Secretary Of The Air Force Rakelet
DE102010040596A1 (de) * 2010-09-10 2012-03-15 Aloys Wobben Abnehmbare Rotorblattspitze
DE102010048266A1 (de) * 2010-10-12 2012-04-12 Airbus Operations Gmbh Flügel mit einem Strömungszaun und Flugzeug mit solchen Tragflügeln
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
CN102167154B (zh) * 2011-03-11 2014-04-16 中国商用飞机有限责任公司 飞机翼尖装置
EP2684797B1 (de) * 2011-03-11 2019-06-26 Commercial Aircraft Corporation Of China Ltd Flugzeugflügelspitzen-vorrichtung
CN102167153B (zh) * 2011-03-11 2014-04-16 中国商用飞机有限责任公司 后缘对齐的飞机翼尖装置
CN102167152B (zh) * 2011-03-11 2014-04-16 中国商用飞机有限责任公司 前缘对齐的飞机翼尖装置
GB201105104D0 (en) 2011-03-28 2011-05-11 Airbus Operations Ltd Joint
EP3650337B1 (de) * 2011-06-09 2020-11-25 Aviation Partners, Inc. Winglet in zwei teile
GB201110493D0 (en) 2011-06-21 2011-08-03 Airbus Operations Ltd Aircraft wing with wing tip device
WO2013070296A2 (en) * 2011-08-19 2013-05-16 Aerovironment, Inc. Aircraft system for reduced observer visibility
US8936219B2 (en) * 2012-03-30 2015-01-20 The Boeing Company Performance-enhancing winglet system and method
GB201209697D0 (en) * 2012-05-31 2012-07-18 Airbus Uk Ltd Method of coupling aerofoil surface structures and an aerofoil assembly
ES2799904T3 (es) 2012-10-03 2020-12-22 Airbus Operations Sl Carena de extremo de una superficie sustentadora horizontal
ES2960524T3 (es) 2013-02-05 2024-03-05 Tamarack Aerospace Group Inc Control de carga periódica de dispositivo controlable de modificación de flujo de aire
GB201307066D0 (en) 2013-04-18 2013-05-29 Airbus Operations Ltd Winglet and braided composite spar
US9452825B2 (en) * 2013-04-19 2016-09-27 The Boeing Company Winglet attach fitting for attaching a split winglet to a wing
US20150014482A1 (en) * 2013-07-15 2015-01-15 Design Intelligence Incorporated, LLC Unmanned aerial vehicle (uav) with inter-connecting wing sections
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
US9738375B2 (en) * 2013-12-05 2017-08-22 The Boeing Company One-piece composite bifurcated winglet
US9511850B2 (en) 2014-04-12 2016-12-06 The Boeing Company Wing tip device for an aircraft wing
US20150369211A1 (en) * 2014-06-19 2015-12-24 General Electric Company Wind blade tip joint
EP3130534B1 (de) * 2014-09-30 2020-03-18 Commercial Aircraft Corporation Of China Ltd Flugzeugflügelanordnung
GB2532238A (en) * 2014-11-12 2016-05-18 Airbus Operations Ltd An aircraft with a wing tip comprising a fuel pod
GB2536447A (en) * 2015-03-17 2016-09-21 Airbus Operations Ltd Load transfer apparatus for transferring loads in an aircraft structure
GB2536448A (en) * 2015-03-17 2016-09-21 Airbus Operations Ltd A connector between two aircraft components, such as a wing and wing tip device
JP6114337B2 (ja) * 2015-05-27 2017-04-12 エアバス オペレーションズ ゲーエムベーハーAirbus Operations GmbH 航空機の翼を構成する方法、航空機の翼の構成および翼の構成を備えている航空機
GB2551311A (en) * 2016-05-24 2017-12-20 Airbus Operations Ltd Winglet
GB2547957A (en) * 2016-05-24 2017-09-06 Airbus Operations Ltd Winglet
GB2551708A (en) * 2016-06-23 2018-01-03 Airbus Operations Ltd Winglet
EP3263446B1 (de) * 2016-06-29 2019-06-05 Goodrich Actuation Systems Limited Klappflügel
EP3269635A1 (de) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Flugzeugflügel
CN106005369B (zh) * 2016-07-24 2018-07-03 尹鸿俊 一种无人机
US10710702B2 (en) * 2016-08-12 2020-07-14 Aviation Partners, Inc. Shape adaptive airfoil
US10495058B2 (en) * 2017-02-21 2019-12-03 General Electric Company Joint assembly for rotor blade segments of a wind turbine
US10830214B2 (en) * 2017-03-22 2020-11-10 General Electric Company Method for securing a lightning receptor cable within a segmented rotor blade
US10647406B2 (en) * 2017-06-01 2020-05-12 The Boeing Company Closed-angle composite airfoil spar and method of fabricating the same
US11046434B2 (en) * 2017-09-19 2021-06-29 The Boeing Company Methods and apparatus to align and secure aircraft
CN108513557A (zh) * 2017-09-27 2018-09-07 深圳市大疆创新科技有限公司 机翼组件及无人飞行器
GB2568229B (en) 2017-10-19 2020-01-29 Airbus Operations Ltd An aircraft assembly including a wingtip device
GB201719806D0 (en) * 2017-11-29 2018-01-10 Airbus Operations Ltd Retrofit flight control surface
EP3492374A3 (de) 2017-11-29 2019-09-04 Airbus Operations Limited Nachrüsten der flugsteuerungsfläche
ES2905192T3 (es) * 2018-01-15 2022-04-07 The Aircraft Performance Company Gmbh Ala de avión
EP3774527A1 (de) 2018-04-02 2021-02-17 Aero Design Labs, Inc. Elliptische flügelspitze und verfahren zur herstellung davon
CN108454822A (zh) * 2018-04-28 2018-08-28 成都航空职业技术学院 一种可拆换小翼装置及其拆换方法
CN110550187A (zh) * 2018-06-01 2019-12-10 空中客车德国运营有限责任公司 用于飞行器的机翼装置和飞行器
US10830207B2 (en) 2018-08-28 2020-11-10 General Electric Company Spar configuration for jointed wind turbine rotor blades
GB2576929A (en) * 2018-09-07 2020-03-11 Airbus Operations Ltd A wing tip device
WO2020086080A1 (en) 2018-10-25 2020-04-30 General Electric Company Spar cap configuration for a jointed wind turbine blade
US11162476B2 (en) * 2018-10-30 2021-11-02 General Electric Company Wind turbine rotor blade pre-staged for retrofitting with a replacement blade tip segment
MA54072A (fr) 2018-10-31 2022-02-09 Gen Electric Pale de rotor d'éolienne articulée ayant des combinaisons de matériaux variables le long de son envergure pour renforcement de broche
CN113286696A (zh) 2018-11-01 2021-08-20 通用电气公司 用于减小梁结构与分节段式转子叶片的叶片壳之间的结合间隙的间隔物材料
WO2020091784A1 (en) 2018-11-01 2020-05-07 General Electric Company Wind turbine jointed rotor blade having a hollow chord-wise extending pin
CA3117312A1 (en) 2018-11-01 2020-05-07 General Electric Company Method for installing and retaining a bushing in a bearing block of a rotor blade joint
CN112955646A (zh) 2018-11-01 2021-06-11 通用电气公司 用于风力涡轮转子叶片的嵌接连接部
CA3117311A1 (en) 2018-11-01 2020-05-07 General Electric Company Compliant structures for jointed rotor blades
EP3874141A1 (de) 2018-11-01 2021-09-08 General Electric Company Spannweitenweiser spreizstift zum verbinden von rotorblattsegmenten
MX2021006487A (es) 2018-12-11 2021-11-25 Gen Electric Metodo para fabricar una estructura compuesta hueca, particularmente una viga para un aspa de rotor de turbina eolica y un mandril asociado.
CN113165283A (zh) 2018-12-11 2021-07-23 通用电气公司 用于制造用于风力涡轮转子叶片的叶片构件的方法
WO2020122865A1 (en) 2018-12-11 2020-06-18 General Electric Company Method for manufacturing a structural component of a blade segment for a rotor blade of a wind turbine
WO2020122866A1 (en) 2018-12-11 2020-06-18 General Electric Company Beam structure for a segmented rotor blade having a transitioning shape
CN113165288B (zh) 2018-12-11 2023-06-20 通用电气公司 用于制造用于风力涡轮的转子叶片的叶片节段的结构构件的方法
WO2020122909A1 (en) 2018-12-13 2020-06-18 General Electric Company Jointed rotor blade having a chord-wise extending pin supported via one or more structural members
EP3899246B1 (de) 2018-12-19 2024-02-14 LM Wind Power A/S Segmentiertes rotorblatt mit innerer trägerstruktur mit unterschiedlicher faserorientierung zur zapfenverstärkung.
CN113167214A (zh) 2018-12-20 2021-07-23 通用电气公司 具有沿其翼展由不同形式的材料构成的翼梁帽的接头式风力涡轮转子叶片
DK3899243T3 (da) 2018-12-20 2024-06-17 Lm Wind Power As Rotorvingesegmenter, der er fastgjort via indvendige støttestrukturer, der definerer et variabelt størrelsesmellemrum derimellem
US20220178346A1 (en) * 2019-03-01 2022-06-09 General Electric Company Jointed wind turbine rotor blade with chord-wise extending pin bushings designed to minimize chord-wise gap
GB2583465A (en) * 2019-04-18 2020-11-04 Airbus Operations Ltd Wingtip device attachment
CN112373673B (zh) * 2020-09-25 2023-09-26 哈尔滨工业大学 改善双凸起翼段性能的前缘双凸起结构的流动控制方法
GB2616252A (en) * 2022-01-31 2023-09-06 Airbus Operations Ltd Aircraft with movable wing tip device
GB2615311A (en) * 2022-01-31 2023-08-09 Airbus Operations Ltd Aircraft wing with movable wing tip device
GB2619276A (en) * 2022-05-25 2023-12-06 Airbus Operations Ltd Wing structures for supporting wing tip devices
US20240199200A1 (en) * 2022-12-16 2024-06-20 The Boeing Company Removable winglet for an aircraft
US11891171B1 (en) * 2023-06-12 2024-02-06 Faruk Dizdarevic Aircraft wing with tiplet

Family Cites Families (64)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE634884C (de) 1936-09-05 Hamburger Flugzeugbau G M B H Aus etwa halbkreisfoermigen Schalen bestehender Tragholm fuer Flugzeuge
US1354677A (en) * 1918-04-08 1920-10-05 Melville W Mix Knockdown airplane-fuselage and process therefor
US1466554A (en) * 1919-05-13 1923-08-28 Hurm Horace Sound-arm coupling for talking machines
US1888418A (en) * 1921-04-14 1932-11-22 Adams Herbert Luther Flying machine
US2370801A (en) * 1941-05-14 1945-03-06 Cons Vultee Aireraft Corp Airplane wing structure
US2576981A (en) * 1949-02-08 1951-12-04 Vogt Richard Twisted wing tip fin for airplanes
US2743888A (en) * 1951-10-20 1956-05-01 Collins Radio Co Variable wing
US2750134A (en) * 1952-04-17 1956-06-12 Lockheed Aircraft Corp Multiple wheel main landing gear
US2749061A (en) * 1954-06-18 1956-06-05 Wesley A Franz Airplane wing stress compensating structure assembly
US3018985A (en) * 1956-12-31 1962-01-30 Martin Marietta Corp Swept wing with unswept spar
US3027118A (en) * 1959-01-28 1962-03-27 English Electric Co Ltd Ram jet propelled aircraft
US3270988A (en) * 1962-12-26 1966-09-06 Jr Clarence D Cone Minimum induced drag airfoil body
US3273833A (en) * 1965-01-21 1966-09-20 Dow Chemical Co Airfoil structure
US3712564A (en) * 1970-11-13 1973-01-23 S Rethorst Slotted diffuser system for reducing aircraft induced drag
US3840199A (en) * 1972-05-09 1974-10-08 R Tibbs Aircraft
US4045336A (en) * 1974-08-23 1977-08-30 Pauli Henrik Isteri Method and device for oxygenating water with vibrations and under pressure strokes
US4046336A (en) * 1975-05-13 1977-09-06 Textron, Inc. Vortex diffusion and dissipation
US4172574A (en) * 1976-06-16 1979-10-30 National Research Development Corporation Fluid stream deflecting members for aircraft bodies or the like
US4190219A (en) * 1977-05-17 1980-02-26 Lockheed Corporation Vortex diffuser
US4205810A (en) * 1977-12-19 1980-06-03 The Boeing Company Minimum drag wing configuration for aircraft operating at transonic speeds
US4700911A (en) * 1982-02-09 1987-10-20 Dornier Gmbh Transverse driving bodies, particularly airplane wings
FR2521520A1 (fr) * 1982-02-15 1983-08-19 Daude Martine Ailettes marginales a angles d'attaque variables
EP0094064A1 (de) 1982-05-11 1983-11-16 George Stanmore Rasmussen An der Tragflügelspitze befestigte Vorrichtung zur Erhöhung des Vorschubs
US4455004A (en) * 1982-09-07 1984-06-19 Lockheed Corporation Flight control device for airplanes
DE3242584A1 (de) * 1982-11-18 1984-05-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung von zusatzflaechen an den spitzen eines tragfluegels
GB8310224D0 (en) * 1983-04-15 1983-05-18 British Aerospace Wing tip arrangement
US4545552A (en) * 1983-06-20 1985-10-08 Welles Stanley W Airframe design
US4674709A (en) * 1983-06-20 1987-06-23 Welles Stanley W Airframe design
US4671473A (en) * 1984-11-08 1987-06-09 Goodson Kenneth W Airfoil
FR2614264B1 (fr) * 1987-04-24 1989-07-21 Aerospatiale Systeme de roulement pour aeronef.
US4776542A (en) * 1987-05-27 1988-10-11 Vigyan Research Associates, Inc. Aircraft stall-spin entry deterrent system
US5039032A (en) * 1988-11-07 1991-08-13 The Boeing Company High taper wing tip extension
US5082204A (en) * 1990-06-29 1992-01-21 Croston Leon J All wing aircraft
IL101069A (en) * 1991-02-25 1996-09-12 Valsan Partners Purchase N Y A system for increasing the fuel efficiency of an aircraft and a kit for changing aircraft wings
US5102068A (en) * 1991-02-25 1992-04-07 Gratzer Louis B Spiroid-tipped wing
US5275358A (en) * 1991-08-02 1994-01-04 The Boeing Company Wing/winglet configurations and methods for aircraft
US5348253A (en) * 1993-02-01 1994-09-20 Gratzer Louis B Blended winglet
JPH06255587A (ja) * 1993-03-09 1994-09-13 Honda Motor Co Ltd 航空機
US5634613A (en) * 1994-07-18 1997-06-03 Mccarthy; Peter T. Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect
JP2622670B2 (ja) * 1994-10-05 1997-06-18 川崎重工業株式会社 超音速航空機の主翼
CN1061005C (zh) * 1995-03-15 2001-01-24 乐正伟 一种飞机翼梢引射器
US5788191A (en) * 1995-08-18 1998-08-04 Sikorsky Aircraft Corporation Half-plow vortex generators for rotor blades for reducing blade-vortex interaction noise
US5897078A (en) * 1995-12-15 1999-04-27 The Boeing Company Multi-service common airframe-based aircraft
GB9600123D0 (en) * 1996-01-04 1996-03-06 Westland Helicopters Aerofoil
US5692703A (en) * 1996-05-10 1997-12-02 Mcdonnell Douglas Corporation Multiple application wheel well design
US6161797A (en) * 1996-11-25 2000-12-19 Dugan Air Technologies, Inc. Method and apparatus for reducing airplane noise
CA2291275C (en) * 1997-06-13 2007-11-06 The Boeing Company Blunt-leading-edge raked wingtips
US5909858A (en) * 1997-06-19 1999-06-08 Mcdonnell Douglas Corporation Spanwise transition section for blended wing-body aircraft
JP2000006893A (ja) * 1998-06-23 2000-01-11 Fuji Heavy Ind Ltd 複合材翼構造
US5975464A (en) * 1998-09-22 1999-11-02 Scaled Composites, Inc. Aircraft with removable structural payload module
DE19926832B4 (de) * 1999-06-12 2005-09-15 Airbus Deutschland Gmbh Unterschallflugzeug vorzugsweise mit gepfeilten Tragflügeln
US6484968B2 (en) * 2000-12-11 2002-11-26 Fort F. Felker Aircraft with elliptical winglets
US6575406B2 (en) * 2001-01-19 2003-06-10 The Boeing Company Integrated and/or modular high-speed aircraft
US6578798B1 (en) * 2002-04-08 2003-06-17 Faruk Dizdarevic Airlifting surface division
US6547181B1 (en) * 2002-05-29 2003-04-15 The Boeing Company Ground effect wing having a variable sweep winglet
US6726149B2 (en) * 2002-05-31 2004-04-27 The Boeing Company Derivative aircraft and methods for their manufacture
US20040135032A1 (en) * 2002-06-20 2004-07-15 Gregg Robert D Spanwise tailoring of a trailing edge wedge to a wing
FR2841532B1 (fr) * 2002-06-27 2004-12-17 Airbus France Avion a controle actif du vrillage de ses ailes
US7048228B2 (en) * 2002-10-09 2006-05-23 The Boeing Company Slotted aircraft wing
US6886778B2 (en) * 2003-06-30 2005-05-03 The Boeing Company Efficient wing tip devices and methods for incorporating such devices into existing wing designs
GB0326228D0 (en) * 2003-11-10 2003-12-17 Airbus Uk Ltd Wing tip device
US7246998B2 (en) * 2004-11-18 2007-07-24 Sikorsky Aircraft Corporation Mission replaceable rotor blade tip section
CN201296357Y (zh) * 2008-09-09 2009-08-26 中国船舶重工集团公司第七○二研究所 一种地效翼船船体
US20110127383A1 (en) * 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet

Also Published As

Publication number Publication date
CN103661930A (zh) 2014-03-26
US8544800B2 (en) 2013-10-01
JP2009501678A (ja) 2009-01-22
EP1934090B1 (de) 2009-08-05
WO2007018785A1 (en) 2007-02-15
CA2613680C (en) 2010-11-02
JP5230413B2 (ja) 2013-07-10
CA2613680A1 (en) 2007-02-15
US20070018049A1 (en) 2007-01-25
CN103661930B (zh) 2018-01-02
DE602006008332D1 (de) 2009-09-17
CN101228067A (zh) 2008-07-23
EP1934090A1 (de) 2008-06-25

Similar Documents

Publication Publication Date Title
ATE438561T1 (de) Integrierte flügelspitzenverlängerungen und verfahren zum vergrössern der flügeloberfläche eines flugzeuggrundmodells
WO2011087475A3 (en) Laminar flow wing optimized for supersonic and high subsonic cruise aircraft
ATE546358T1 (de) Flügelspitzenform für einen flügel, insbesondere einen flugzeugflügel
WO2009133217A8 (es) Conjunto soporte-maqueta de mínima interferencia aerodinámica para ensayos en régimen transónico en túnel de viento
ATE512049T1 (de) Flugzeug mit ringförmigem heck
DE502005003965D1 (de) Flugzeugflügel, Verfahren zum Herstellen eines Flugzeugflügels und Verwendung eines Schweissverfahrens zum Verschweissen eines Flügelholms
JP2016175631A5 (de)
WO2009029796A3 (en) Oblique blended wing body aircraft
ATE427883T1 (de) Flugelspitzenvorrichtung
EP2607231A3 (de) Tragflächen mit Spitzenprofil zur Geräuschreduktion und Verfahren zur Herstellung davon
ATE434560T1 (de) Flügelspitzenvorrichtungen
DE502004008095D1 (de) It veränderbarem profil
RU2010146134A (ru) Концевые крылышки, содержащие поверхности с углублением и соответствующие системы и способы
ATE545580T1 (de) Nicht planare flügelspitzenvorrichtung für flugzeugflügel und flügel mit einer solchen flügelspitzenvorrichtung
JP2009501678A5 (de)
DE602006009252D1 (de) Systeme zur nutzlastverkleidung bei luftfahrzeugen und entsprechende verfahren
EP2441670A3 (de) Nach vorne geneigter Winglet
AR109035A1 (es) Ala para aeronave y aeronave
DE602006014219D1 (de) Verfahren zur reparatur eines beschädigten aussenhautbereichs an einem flugzeug
WO2009045694A3 (en) Wingtip feathers, including paired, fixed feathers, and associated systems and methods
ATE535340T1 (de) Verfahren und system zur erstellung der flugbahn eines luftfahrzeugs
WO2008154066A3 (en) Methods and apparatus for aircraft
WO2009032384A3 (en) Airfoil system for cruising flight
FR2982845B1 (fr) Carenage aerodynamique arriere de mat de moteur d'aeronef
BRPI0911484A2 (pt) asa de sustentação para uma aeronave

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties