Patent · US Expired

Flap/spoiler combination

US4720066A · kind A · utility

38Cited by
2References
4Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 26, 1986
Grant dateJan 19, 1988
Priority date
Expiry dateAug 26, 2006

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C13/26
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A flap arrangement for an aircraft wing having along its trailing edge independently actuated high lift flap and spoiler. During cruising the flap is used for camber line curvature control while the spoiler is controlled in a follow up configuration such that a gap between the spoiler and the high lift flap does not form.

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