Patent · US Active

Three-dimensional extension linkage for aircraft

US11932400B2 · kind B2 · utility

0Cited by
7References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 31, 2022
Grant dateMar 19, 2024
Priority date
Expiry dateMar 31, 2042

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An extension linkage for a wing flap can include at least one arm that includes two elements connected by a joint. The linkage can include an actuation mechanism, additional arms and/or each arm can include more than two elements, tie rods and/or cross pieces connecting two or more arms, and any other suitable components. The linkage functions to translate and rotate a body attached to one end of the arm relative to a primary structure attached to a second end of the arm. The linkage resides entirely within a space defined by the upper skin and the lower skin of the wing rearward of the mounting when in a retracted configuration.

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