Patent · US Active

Flap support for supporting a flap of a wing for an aircraft

US11685511B2 · kind B2 · utility

1Cited by
2References
14Claims
0Family size

Assignees

Inventors

Key dates

Filing dateAug 14, 2019
Grant dateJun 27, 2023
Priority date
Expiry dateAug 14, 2039

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C9/16
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A flap support for supporting a flap of a wing for an aircraft is disclosed and includes a load bearing fairing shell and a reinforcement structure at least partially received in the interior space of the fairing structure and mounted to the first and second side wall portions of the fairing shell. The fairing shell includes a front attachment device configured for attachment to a main wing, and the reinforcement structure includes an aft attachment device configured for attachment to the main wing. The flap support further includes a hinge device configured for forming an articulated connection to the flap.

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