Patent · US Active

Stop pads for aircraft folding wing tips

US11077931B2 · kind B2 · utility

1Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateAug 1, 2018
Grant dateAug 3, 2021
Priority date
Expiry dateOct 23, 2039

Classification

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

Abstract

Stop pads for aircraft folding wing tips are described herein. An example aircraft wing includes a fixed wing portion and a wing tip moveably coupled to the fixed wing portion about a hinge axis. The wing tip is moveable between an extended position and a folded position. The aircraft wing also includes a first stop pad coupled to the fixed wing portion, the first stop pad having a first contact surface, and a second stop pad coupled to the wing tip, the second stop pad having a second contact surface. The first and second contact surfaces are to engage each other when the wing tip is in the extended position. A contact plane between the first and second contact surfaces is coplanar with the hinge axis.

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