Patent · US Active

Manuel wing-fold mechanism

US10099770B2 · kind B2 · utility

4Cited by
7References
27Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 18, 2014
Grant dateOct 16, 2018
Priority date
Expiry dateFeb 29, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A manual wing-fold mechanism provides a means by which to reconfigure the wing of an aircraft between a flight configuration and one that can be easily stowed and transported. The folding mechanism includes an extension tube that enables the outboard portion of the wing to be extended away from the inboard section of the wing, rotated about the lateral axis of the aircraft and then pivoted rearward so that the wing is aligned with the longitudinal axis of the aircraft along side the fuselage. The wing-fold mechanism is independent of the structural components of the wing used to convey aerodynamic loads during flight and provides a means for the user to bring the outboard wing section into a near alignment position while the wing-fold mechanism thereafter assists to refine the alignment into its final flight configuration.

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