Patent · US Active

Aircraft fuselage frame

US10124876B2 · kind B2 · utility

0Cited by
9References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 25, 2015
Grant dateNov 13, 2018
Priority date
Expiry dateJul 2, 2036

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C3/32
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An aircraft fuselage frame including a central element adapted to be located within the perimeter of the fuselage, and two lateral extensions projecting outside the perimeter of the fuselage from both sides of the central element that are a portion of a longitudinal structure of a lifting surface. The central element and the two lateral extensions are configured as an integrated piece.

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