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.

Patent No.:

US 10544687 B1

PDF
Full Text
Expired
Date of Patent:
Jan. 28, 2020

Filed:

Jul. 10, 2017
Applicant:

Mtu Aero Engines Ag, Munich, DE;

Inventors:

Krzysztof Skura, Majdan Krolewski, PL;

Piotr Lebiedowicz, Hrubieszow, PL;

Marek Szponar, Ksiezpol, PL;

Assignee:

MTU Aero Engines AG, Munich, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/22 (2006.01); F01D 11/00 (2006.01); F01D 5/16 (2006.01);
U.S. Cl.
CPC ...
F01D 5/225 (2013.01); F01D 11/003 (2013.01); F01D 5/16 (2013.01); F05D 2250/13 (2013.01); F05D 2270/114 (2013.01); Y02T 50/671 (2013.01);
Abstract

The present invention relates to an improved cast-to-size gas turbine blade comprising a blade tip shroud with a stiffening rib extending outwardly from the section of the outer side of the shroud platform located between the upstream sealing fin and the upstream edge. The stiffening rib having substantially planar top surface in form of a trapezium, and two sloping sidewalls extending between the upstream sealing fin and the upstream edge on each side of the top surface and connecting said top surface with adjacent surface of the outer side of the shroud platform. The form of the stiffening rib allows to obtain an improved shroud configuration of reduced overall blade mass, capable of providing sufficient stiffening of the shroud, reducing vibrations of the shroud platform, creep curling of the shroud edges and bending stress at the intersection of the airfoil and of the shroud.


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