Patent · US Active

Active gurney flap

US8695926B2 · kind B2 · utility

3Cited by
17References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateApr 18, 2012
Grant dateApr 15, 2014
Priority date
Expiry dateJun 28, 2032

Classification

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

Abstract

A gurney flap assembly has an actuator, a flexible or hinged body, the body flexing from a retracted to a deployed position in reaction to motion of the actuator, and a first seal extending along a first edge of the flexible body that flexes from the stowed position. Linear motion of the actuator output is transposed to the gurney flap thereby moving it from a retracted position into the airstream. This trailing edge device will improve airfoil lift.

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