The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 11, 2013

Filed:

Mar. 28, 2008
Applicants:

Anders Sjunnesson, Trollhättan, SE;

Niklas Jansson, Mölndal, SE;

Robert Reimers, Uddevalla, SE;

Rickard Samuelsson, Trollhättan, SE;

Inventors:

Anders Sjunnesson, Trollhättan, SE;

Niklas Jansson, Mölndal, SE;

Robert Reimers, Uddevalla, SE;

Rickard Samuelsson, Trollhättan, SE;

Assignee:

Volvo Aero Corporation, Trollhättan, SE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01);
U.S. Cl.
CPC ...
Abstract

A gas turbine engine component is provided including at least one ring element, and a plurality of circumferentially spaced load carrying vanes extending in a radial direction of the ring element. The load carrying vanes have an internal structure with an anisotropic load carrying property, and the internal structure is configured so that a main load carrying direction is in parallel with the extension direction of the load carrying vane. The component includes a stiffening structure bridging the distance between at least two adjacent load carrying vanes in the circumferential direction of the ring element, and the at least two adjacent load carrying vanes are attached to the stiffening structure.


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