Patent · US Active

Assemblies and methods for deploying a trailing edge flap of an aircraft

US11964766B2 · kind B2 · utility

0Cited by
30References
8Claims
0Family size

Assignee

Inventors

Key dates

Filing dateFeb 25, 2022
Grant dateApr 23, 2024
Priority date—
Expiry dateMay 20, 2042

Classification

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

Abstract

Trailing edge assemblies, couplers and methods for deploying a trailing edge flap of an aircraft wing are disclosed. An exemplary method disclosed herein comprises guiding an aft portion of the trailing edge flap along an elongated track member as the trailing edge flap moves toward the deployed position; guiding a forward portion of the trailing edge flap along the elongated track member as the trailing edge flap moves toward the deployed position; and accommodating transverse movement of the forward portion of the trailing edge flap relative to the elongated track member.

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