Patent · US Active

Winglet

US8366056B2 · kind B2 · utility

33Cited by
20References
13Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJun 10, 2008
Grant dateFeb 5, 2013
Priority date
Expiry dateDec 22, 2028

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A winglet comprising a root connected to a distal end of a wing; an upwardly angled section; a tip; and a transition between the upwardly angled section and the tip at which an outboard cant angle of the winglet decreases relative to a reference plane of the wing. In one embodiment the winglet is continuously curved and includes a point of inflection at which the span-wise curvature of the winglet changes sign. In another embodiment the upwardly angled section is planar. The winglet generates a tip vortex when in flight. The tip vortex is displaced outboard from the winglet due to the decrease in outboard cant angle at the transition.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.