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 9920644 B1

PDF
Full Text
Expired
Date of Patent:
Mar. 20, 2018

Filed:

Jan. 23, 2014
Applicant:

Siemens Aktiengesellschaft, Munich, DE;

Inventor:

Mike McKenna, Newark, GB;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 11/00 (2006.01); F01D 11/02 (2006.01); F01D 5/12 (2006.01);
U.S. Cl.
CPC ...
F01D 11/008 (2013.01); F01D 5/12 (2013.01); F01D 9/041 (2013.01); F01D 11/005 (2013.01); F01D 11/006 (2013.01); F01D 11/02 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2240/30 (2013.01); F05D 2240/55 (2013.01); F05D 2240/57 (2013.01); F05D 2240/80 (2013.01); F05D 2250/294 (2013.01); F05D 2250/611 (2013.01);
Abstract

A seal of a turbomachine reduces a leakage flow between a first and second component of the turbomachine. The first component has a first surface and the second component has a second surface, wherein the first component is stiff with regard to a first force exerted perpendicularly thereto and the second component is stiff with regard to a second force exerted perpendicularly thereto. The first surface is opposite the second surface, together defining boundaries of a fluid passage for the leakage flow. The first surface has a first surface riffle. A turbomachine has a seal described above, wherein the turbomachine is a gas turbine engine. A method of manufacturing a first component of a turbomachine with a reduced leakage flow between the first component and a second component of the turbomachine includes fabrication of a first surface riffle, in particular by grinding and/or by electrical discharge machining.


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