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. 24, 2018

Filed:

Jun. 26, 2014
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Krzysztof Skura, Majdan Krolewski, PL;

Marcin Kozdras, Krosno, PL;

Lukasz Sosnowka, Rzeszow, PL;

Manfred Feldmann, Eichenau, DE;

Manfred Schill, Munich, DE;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/08 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3007 (2013.01); F05D 2250/292 (2013.01); F05D 2250/38 (2013.01); F05D 2250/712 (2013.01);
Abstract

A rotor blade for a turbomachine, including an airfoil () for flow deflection, a blade root () for attachment to a rotor of the turbomachine, an inner platform () between the airfoil and the blade root, and at least one pocket () defined by two axially spaced walls () extending from the side of the platform opposite the airfoil toward the blade root. A first () of these walls has an outer side (A,A) that faces away from the pocket and, in at least one cross section perpendicular to a radial longitudinal axis of the rotor blade, slopes outwardly.


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