Patent · US Active

Aircraft wing

US8231084B2 · kind B2 · utility

5Cited by
2References
34Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMay 13, 2009
Grant dateJul 31, 2012
Priority date
Expiry dateFeb 27, 2030

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/30
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft wing comprising a leading element and a trailing element moveably coupled together, said elements being positionable relative to each other so that air can flow from the underside of the leading element over the top of the trailing element through a gap between the leading element and the trailing element, wherein a trailing edge of the leading element proximate to the trailing element is configured to disrupt air flow as it flows over said trailing edge and through the gap.

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