Patent · US Active

Annular torsional rigid static component for an aircraft engine

US7905448B2 · kind B2 · utility

8Cited by

16References

18Claims

0Family size

Assignee

Volvo Aero Corporation · SE

Inventors

Anders Sjunnesson · carrer de Sertori, SE
Henrik Karlsson · Värnamo, SE
Mathias Andersson · Österbymo, SE

Key dates

Filing date	Dec 19, 2005
Grant date	Mar 15, 2011
Priority date	—
Expiry date	Jun 23, 2027

Classification

Technology area (CPC Y)Emerging Cross-Sectional Technologies
CPC primaryY02T50/60
WIPO fieldEngines, pumps, turbines
WIPO sectorMechanical engineering

Abstract

In an annular torsional rigid static component for an aircraft engine, the component includes at least one arrangement for mounting the engine to an aircraft. The mounting arrangement comprises a body formed in a composite material.

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