Patent · US Active

Wing for an aircraft

US12428133B2 · kind B2 · utility

0Cited by
13References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 24, 2023
Grant dateSep 30, 2025
Priority date
Expiry dateFeb 24, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C13/0425
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A wing for an aircraft. The wing includes a main wing and a trailing edge high lift assembly movably arranged at a trailing edge of the main wing. The trailing edge high lift assembly includes a flap and a connection assembly movably mounting the flap to the main wing, such that the flap is movable between a retracted position and at least one extended position, wherein the connection assembly is configured such that the flap is movable relative to the main wing in a linear and/or rotational manner. The connection assembly is configured such that the flap is movable relative to the main wing in a decoupled linear and rotational manner.

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