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:
Nov. 29, 2016

Filed:

Sep. 03, 2013
Applicant:

Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, DE;

Inventors:

Knut Lehmann, Berlin, DE;

Tijana Filipova, Berlin, DE;

Assignee:

Rolls-Royce Deutschland Ltd & Co KG, Blankenfelde-Mahlow, DE;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 5/08 (2006.01); B23P 15/02 (2006.01); B23P 15/04 (2006.01);
U.S. Cl.
CPC ...
F01D 5/188 (2013.01); B23P 15/02 (2013.01); B23P 15/04 (2013.01); F01D 5/186 (2013.01); F05D 2240/127 (2013.01); F05D 2260/2212 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01); Y10T 29/49336 (2015.01); Y10T 29/49337 (2015.01); Y10T 29/49339 (2015.01);
Abstract

The present invention relates to a turbine blade of a gas turbine with an airfoil arranged on a blade root and having at least one cooling air duct running in the longitudinal direction of the turbine blade, arranged inside the turbine blade and extending through the blade root, characterized in that at least one swirl-generating element is arranged in the transitional area between blade root and airfoil in the cooling air duct, with the swirl-generating element including an outer ring and several swirl-generating stator vanes arranged thereon, which are connected to a centric area, as well as to a method for its manufacture.


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