Aircraft wing modification and related methods

Details Aircraft wing modification and related methods Aircraft wing modification and related methods

B - Operations, Transporting

64

C

B64C 3/28 (2006.01)

Patent

CA 2617137

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 maybe 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.

Cette invention porte sur un bord d'attaque modifié transférable pour une aile qui est monté de façon détachable à une aile parente. L'aile parente peut utiliser une surface portante NACA de série 23 000. Un bout d'aile modifié peut être utilisé conjointement avec le bord d'attaque modifié. Le bord d'attaque modifié peut être monté sur une aile parente d'une manière qui n'endommage pas l'aile parente. Le bord d'attaque et le bout d'aile modifiés peuvent fournir une sustentation accrue.

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