a Partnership of Jim Langley and Courtney Hunter

Canada

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B64C 3/14 - Aerofoil profile 1
B64C 3/16 - Frontal aspect 1
B64C 3/28 - Leading or trailing edges attached to primary structures, e.g. forming fixed slots 1
B64C 3/40 - Varying angle of sweep 1
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1.

AIRCRAFT WING MODIFICATION AND RELATED METHODS

      
Application Number CA2007000701
Publication Number 2008/022428
Status In Force
Filing Date 2007-04-25
Publication Date 2008-02-28
Owner A PARTNERSHIP OF JIM LANGLEY AND COURTNEY HUNTER (Canada)
Inventor Hunter, Courtney Heath

Abstract

A transferable modified leading edge for a wing is detachably mountable to a parent wing. The parent wing may use a NACA 23000-series airfoil. A modified wing tip may be used in conjunction with the modified leading edge. The modified leading edge can be mounted to a parent wing in a way that does not damage the parent wing. The modified leading edge and wing tip can provide increased lift.

IPC Classes  ?

  • B64C 3/28 - Leading or trailing edges attached to primary structures, e.g. forming fixed slots
  • B64C 3/14 - Aerofoil profile
  • B64C 3/16 - Frontal aspect
  • B64C 3/40 - Varying angle of sweep