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:
Apr. 21, 2015

Filed:

Aug. 05, 2010
Applicants:

Sergio Elorza Gomez, Munich, DE;

Rudolf Selmeier, Fahrenzhausen, DE;

Wilfried Schutte, Oberhaching, DE;

Peter Eibelshauser, Munich, DE;

Harald Passrucker, Salzburg, AT;

Manfred Dupslaff, Eichenau, DE;

Inventors:

Sergio Elorza Gomez, Munich, DE;

Rudolf Selmeier, Fahrenzhausen, DE;

Wilfried Schutte, Oberhaching, DE;

Peter Eibelshauser, Munich, DE;

Harald Passrucker, Salzburg, AT;

Manfred Dupslaff, Eichenau, DE;

Assignee:

MTU Aero Engines GmbH, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 17/16 (2006.01); F04D 29/68 (2006.01); F04D 29/56 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); F01D 5/145 (2013.01); F01D 17/162 (2013.01); F04D 29/681 (2013.01); F05D 2250/713 (2013.01); F05D 2250/711 (2013.01); F04D 29/563 (2013.01); F04D 29/544 (2013.01);
Abstract

The present invention relates to a blade of a turbomachine, in particular an adjustable guide blade or vane of a gas turbine, having at least one thickened area () on a pressure side (D) of the blade profile (P), wherein the thickened area () is disposed in a radially outer-lying, housing-side region of the blade (), wherein the thickened area () is designed at a distance from a front edge () and a rear edge () of the blade ().


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