Patent · US Active

Serrated fitting

US12286998B1 · kind B1 · utility

0Cited by
1References
20Claims
0Family size

Assignee

Inventor

Key dates

Filing dateOct 6, 2023
Grant dateApr 29, 2025
Priority date
Expiry dateOct 6, 2043

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16B5/0225
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A serrated fitting and method for installing fixed length roller tray segments spanning an aircraft fuselage integration zone. The serrated fitting includes a first surface for attachment to a fixed length roller tray segment. The serrated fitting also includes a serrated surface for engagement with a serrated plate attached to a floor beam of an aircraft. A fastener connects the serrated surface to the serrated plate and the floor beam through a pre-drilled hole in the floor beam. The pre-drilled hole is larger than the diameter of the fastener to accommodate accumulated tolerance between joined fuselage sections at a fuselage integration zone.

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