Patent · US Active

Structural element of an aircraft fuselage

US8905349B2 · kind B2 · utility

2Cited by

4References

14Claims

0Family size

Assignee

AIRBUS OPERATIONS LIMITED · DE

Inventors

Claus-Peter Gross · Hamburg, DE
Cord Haack · Augsburg, DE
Dirk Humfeldt · Hamburg, DE
Oliver Thomaschewski · Hamburg, DE

Key dates

Filing date	Apr 25, 2008
Grant date	Dec 9, 2014
Priority date	—
Expiry date	Sep 26, 2030

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02T50/40
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

The structural element of an aircraft fuselage, with stringers running in the longitudinal direction of the aircraft fuselage and ribs running transversely to the stringers in the circumferential direction of the fuselage. According to the invention, at least one of the stringers running in the longitudinal direction of the aircraft fuselage is designed as a fastening rail for elements to be installed in the aircraft fuselage.

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