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:
Aug. 01, 2017

Filed:

Dec. 16, 2013
Applicant:

Siemens Aktiengesellschaft, Munich, DE;

Inventors:

Steve Hannam, North Hykeham, GB;

Paul Jenkinson, Lincoln, GB;

Paul Padley, Tattershall, GB;

Paul Mathew Walker, Dunholme, GB;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 25/08 (2006.01); C23C 14/22 (2006.01); F01D 9/02 (2006.01); C25D 3/56 (2006.01); F01D 9/04 (2006.01); C23C 4/134 (2016.01);
U.S. Cl.
CPC ...
F01D 25/08 (2013.01); C23C 4/134 (2016.01); C23C 14/22 (2013.01); C25D 3/56 (2013.01); F01D 5/288 (2013.01); F01D 9/02 (2013.01); F01D 9/041 (2013.01); F05D 2220/32 (2013.01); F05D 2230/311 (2013.01); F05D 2230/312 (2013.01); F05D 2230/313 (2013.01); F05D 2240/12 (2013.01); F05D 2240/15 (2013.01); F05D 2260/231 (2013.01);
Abstract

A vane device for a gas turbine is provided. The vane device includes a first airfoil having a first suction side and a first pressure side, a second airfoil having a second suction side and a second pressure side, an inner shroud and an outer shroud. The first airfoil and the second airfoil are arranged between the inner shroud and the outer shroud, wherein the first airfoil and the second airfoil are at least partially coated with a MCrAlY coating. At least the first suction side has a first coated surface section which is coated with a thermal barrier coating and which represents at least a part of the total surface of the first suction side. At least the inner shroud or the outer shroud has a further coated surface section which is coated with a further thermal barrier coating. A corresponding method of manufacturing is also provided.


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