Patent · US Active

Circumferential stiffener for an aircraft fuselage

US8640990B2 · kind B2 · utility

0Cited by

4References

9Claims

0Family size

Assignee

AIRBUS OPERATIONS LIMITED · DE

Inventor

Torsten Noebel · Hamburg, DE

Key dates

Filing date	Apr 29, 2011
Grant date	Feb 4, 2014
Priority date	—
Expiry date	Jan 16, 2032

Classification

Technology area (CPC B)Performing Operations; Transporting
CPC primaryB64C1/061
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

A circumferential stiffener configured for a fuselage of an aircraft includes a web disposed at an angle to a normal axis of the circumferential stiffener, at least one inner flange, at least one outer flange and an integral angle profile configured for connection to a skin section of the fuselage.

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