Patent · US Active

Fuselage structure and method for manufacturing a fuselage structure

US10486789B2 · kind B2 · utility

0Cited by
10References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 7, 2016
Grant dateNov 26, 2019
Priority date
Expiry dateOct 1, 2037

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C1/064
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A fuselage structure includes a pressure bulkhead and a frame being arranged behind the pressure bulkhead. The fuselage structure includes a first beam element with a first cantilever and a second cantilever, while the first beam element extends in a vertical direction of the fuselage structure. The first cantilever and the second cantilever protrude from the first beam element in a first direction toward the frame. The first direction of both cantilevers is inclined at a first angle with respect to a longitudinal direction of the fuselage structure. An aircraft with a fuselage structure and a method for manufacturing a fuselage structure are also described.

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