Patent · US Active

Structural component of an aircraft or spacecraft and a fuselage component arrangement of an aircraft or spacecraft

US8770519B2 · kind B2 · utility

0Cited by

5References

6Claims

0Family size

Assignee

AIRBUS OPERATIONS LIMITED · DE

Inventor

Claus-Peter Gross · Hamburg, DE

Key dates

Filing date	May 23, 2011
Grant date	Jul 8, 2014
Priority date	—
Expiry date	Aug 8, 2031

Classification

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

Abstract

In the case of a structural component of an aircraft or spacecraft comprising a fuselage portion connection region for connecting to an associated fuselage portion and having a thermal expansion coefficient which is approximately matched to the associated fuselage portion; an inner connection region for connecting to an associated installation element and having a thermal expansion coefficient which is approximately matched to the associated installation element; and a separation region for connecting the fuselage portion connection region and the inner connection region, at least one of the regions has a high heat conduction resistance.

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