• Inventors:
  • Assignees:
  • Publication Date: December 31, 1969
  • Publication Number:

Patent Citations (0)

    Publication numberPublication dateAssigneeTitle

NO-Patent Citations (0)

    Title

Cited By (84)

    Publication numberPublication dateAssigneeTitle
    US-8944373-B2February 03, 2015Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
    US-2013105652-A1May 02, 2013United Technologies CorporationBlind retention mount
    US-7275722-B2October 02, 2007Airbus Uk LimitedWing tip device
    US-8469315-B2June 25, 2013The Boeing CompanyDeployable flap edge fence
    US-2007018049-A1January 25, 2007Stuhr Victor KIntegrated wingtip extensions for jet transport aircraft and other types of aircraft
    US-6827314-B2December 07, 2004Airbus FranceAircraft with active control of the warping of its wings
    US-2011186689-A1August 04, 2011Tamarack Aerospace Group, Inc.Active winglet
    US-7900877-B1March 08, 2011Tamarack Aerospace Group, Inc.Active winglet
    US-7015829-B2March 21, 2006Airbus France S.A.S.Method for displaying flight information
    US-9540101-B2January 10, 2017Aurora Flight Sciences CorporationSystem, apparatus and method for long endurance vertical takeoff and landing vehicle
    US-2015336663-A1November 26, 2015Aurora Flight Sciences CorporationSystem, apparatus and method for long endurance vertical takeoff and landing vehicle
    US-4545552-AOctober 08, 1985Welles Stanley WAirframe design
    US-9463871-B2October 11, 2016The Boeing CompanyWinglet system having upper and lower winglet
    US-7316371-B2January 08, 2008Airbus Deutschland GmbhMethod and device for steepening a landing approach of an aircraft
    US-2012246874-A1October 04, 2012Beuth Hochschule Fur Technik BerlinComponents designed to be load-adaptive
    EP-1375342-A1January 02, 2004Airbus FranceAirplane with active control of the twist of its wings
    US-D732657-SJune 23, 2015Delta T CorporationWinglet
    US-2008191099-A1August 14, 2008Vitalij Werthmann, Michael KordtConcept of a Variable Winglet for Lateral Load Reduction for Combined Lateral and Vertical Load Reduction, and for Improving the Performance of Means of Locomotion
    US-9346537-B2May 24, 2016The Boeing CompanyWinglet system
    US-2014306067-A1October 16, 2014Tamarack Aerospace Group, Inc.Controllable airflow modification device periodic load control
    US-8382041-B1February 26, 2013The United States Of America As Represented By The Secretary Of The Air ForceRakelet
    US-2016068258-A1March 10, 2016Airbus Defence and Space GmbHAircraft with C-Shaped Carrier Surfaces and Movable Top Surfaces
    US-2015360773-A1December 17, 2015Dann M AllenHelicopter rotor with a mechanical means for configuring rotor tips to control brown outs
    US-9567066-B2February 14, 2017Tamarack Aerospace Group, Inc.Controllable airflow modification device periodic load control
    US-8128035-B2March 06, 2012The Boeing CompanyWinglets with recessed surfaces, and associated systems and methods
    US-6547181-B1April 15, 2003The Boeing CompanyGround effect wing having a variable sweep winglet
    US-9682774-B2June 20, 2017Aurora Flight Sciences CorporationSystem, apparatus and method for long endurance vertical takeoff and landing vehicle
    US-7900876-B2March 08, 2011The Boeing CompanyWingtip feathers, including forward swept feathers, and associated aircraft systems and methods
    US-9340301-B2May 17, 2016Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
    US-2012112005-A1May 10, 2012Airbus Operations LimitedWing tip device attachment apparatus and method
    US-9499255-B2November 22, 2016Airbus Operations LimitedWing tip device attachment apparatus and method
    US-2009039204-A1February 12, 2009The Boeing CompanyWingtip Feathers, Including Forward Swept Feathers, and Associated Aircraft Systems and Methods
    US-9290260-B2March 22, 2016The Boeing CompanyWing fold controller
    US-9469392-B2October 18, 2016The Boeing CompanyWing fold system rotating latch
    US-2016009378-A1January 14, 2016Tamarack Aerospace Group, Inc.Adjustable lift modification wingtip
    US-8936219-B2January 20, 2015The Boeing CompanyPerformance-enhancing winglet system and method
    US-8136766-B2March 20, 2012Insitu, Inc.Frangible fasteners for aircraft components and associated systems and methods
    US-9296469-B2March 29, 2016The Boeing CompanyHorizontal folding wingtip
    US-2015360765-A1December 17, 2015Airbus Operations LimitedDownwardly extending wing tip device
    WO-2006122826-A1November 23, 2006Airbus Deutschland GmbhConcept of a variable winglet for lateral load reduction for combined lateral and vertical load reduction, and for improving the performance of means of locomotion
    US-5738331-AApril 14, 1998Woolley; Paul A.Aircraft crosswind control apparatus
    US-2013001367-A1January 03, 2013Michael Frederick Boer, Anthony Charles HoffeMethod for reducing in fligt wake vortices and an aircraft wingtip arrangement used in such method
    US-2004000619-A1January 01, 2004Bernard BarrietyAircraft with active control of the warping of its wings
    US-9216817-B1December 22, 2015The Boeing CompanyWinglet system and method
    US-2004155798-A1August 12, 2004Eric Godard, David Chabe, Jacques EspinasseMethod for displaying flight information
    US-8757555-B2June 24, 2014Airbus Operations GmbhConcept of a variable winglet for lateral load reduction for combined lateral and vertical load reduction, and for improving the performance of means of locomotion
    US-9637226-B2May 02, 2017The Boeing CompanySplit winglet system
    US-2005133672-A1June 23, 2005Jan Irving, Robert DaviesWing tip device
    US-9452825-B2September 27, 2016The Boeing CompanyWinglet attach fitting for attaching a split winglet to a wing
    US-2004155146-A1August 12, 2004Susanne Wyrembek, Peter May, Klaus MuthreichMethod of controlling a landing guide path of an aircraft
    US-9856036-B2January 02, 2018Insitu, Inc.Line capture devices for unmanned aircraft, and associated systems and methods
    WO-2011076202-A1June 30, 2011Beuth Hochschule Für Technik BerlinBelastungsadaptiv ausgebildete bauteile
    US-2015203190-A1July 23, 2015The Boeing CompanyWinglet attach fitting and method for attaching a split winglet to a wing
    US-2004155157-A1August 12, 2004Bray Robert MWinglet
    US-8894018-B2November 25, 2014University Of The WitwatersrandMethod for reducing in flight wake vortices and an aircraft wingtip arrangement used in such method
    US-2003106961-A1June 12, 2003Susanne Wyrembek, Peter May, Klaus MuthreichMethod and device for steepening a landing approach of an aircraft
    US-2009256029-A1October 15, 2009The Boeing CompanyWinglets with Recessed Surfaces, and Associated Systems and Methods
    FR-2862044-A1May 13, 2005Deutsch Zentr Luft & RaumfahrtProcede pour miminiser la resistance d'un avion en vol
    US-8544800-B2October 01, 2013The Boeing CompanyIntegrated wingtip extensions for jet transport aircraft and other types of aircraft
    US-9415857-B2August 16, 2016The Boeing CompanyWing fold system
    US-9714080-B2July 25, 2017Airbus Operations LimitedWing tip device having configurations for flight and ground-based operations
    US-6980128-B2December 27, 2005Airbus France S.A.S.Display system for an aircraft
    US-2010219288-A1September 02, 2010The Boeing CompanyDeployable Flap Edge Fence
    US-6937166-B2August 30, 2005Airbus FranceProcess and device for aiding the piloting of an aircraft
    US-2009084904-A1April 02, 2009The Boeing CompanyWingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods
    US-8967570-B2March 03, 2015United Technologies CorporationBlind retention mount
    US-7070148-B2July 04, 2006Airbus Deutschland GmbhAerodynamic component for controlling a landing guide path of an aircraft
    US-9511850-B2December 06, 2016The Boeing CompanyWing tip device for an aircraft wing
    WO-03000547-A1January 03, 2003Bae Systems PlcAilette de bout d'aile
    DE-102010017509-A1May 12, 2011Thomas FischerWinglet für eine Auftriebsfläche
    US-9499252-B2November 22, 2016The Boeing CompanyWing fold controller
    US-2003137434-A1July 24, 2003Eric Godard, David Chabe, Jacques EspinasseProcess and device for aiding the piloting of an aircraft
    US-5582364-ADecember 10, 1996Hughes Missile Systems CompanyFlyable folding fin
    US-2004155799-A1August 12, 2004Eric Godard, David Chabe, Jacques EspinasseDisplay system for an aircraft
    US-9162755-B2October 20, 2015Tamarack Aerospace Group, Inc.Multiple controllable airflow modification devices
    US-2004169110-A1September 02, 2004Susanne Wyrembek, Peter May, Klaus MuthreichAerodynamic component for controlling a landing guide path of an aircraft
    EP-1531126-A1May 18, 2005Airbus UK LimitedWing tip device
    US-2014117151-A1May 01, 2014The Boeing CompanyWing fold system
    US-8684315-B2April 01, 2014Tamarack Aerospace Group, Inc.Active winglet
    US-7597285-B2October 06, 2009Airbus Deutschland GmbhFluid dynamically effective surface for minimizing induced resistance
    US-9211946-B2December 15, 2015The Boeing CompanyWing fold system with latch pins through multiple mating lugs
    FR-2841532-A1January 02, 2004Airbus FranceAvion a controle actif du vrillage de ses ailes
    US-9764825-B2September 19, 2017Tamarack Aerospace Group, Inc.Active winglet