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:
Sep. 17, 2019

Filed:

Nov. 28, 2014
Applicant:

Siemens Aktiengesellschaft, Munich, DE;

Inventors:

Stefan Braun, Neukirchen-Vluyn, DE;

Tjark Eisfeld, Mettmann, DE;

Marco Larson, Mülheim, DE;

Ulrich Waltke, Mülheim an der Ruhr, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/56 (2006.01); F02C 9/20 (2006.01); F02C 9/28 (2006.01); F01D 25/02 (2006.01); G01K 13/00 (2006.01); F04D 29/54 (2006.01); F04D 29/32 (2006.01); F04D 27/00 (2006.01); F04D 19/00 (2006.01);
U.S. Cl.
CPC ...
F04D 27/001 (2013.01); F01D 25/02 (2013.01); F02C 9/20 (2013.01); F02C 9/28 (2013.01); F04D 19/00 (2013.01); F04D 27/002 (2013.01); F04D 29/324 (2013.01); F04D 29/542 (2013.01); F04D 29/563 (2013.01); G01K 13/00 (2013.01); F05B 2220/302 (2013.01); F05B 2240/12 (2013.01);
Abstract

An ascertainment method for determining a final angle of vanes that are adjustable between an initial angle and the final angle and are part of a row of leading vanes which are arranged upstream of a row of trailing vanes of a compressor in a gas turbine, in order to prevent ice from forming in the compressor. During operation of the gas turbine, a current value of at least one process parameter is determined in a parameter ascertainment step, whereupon the final angle is defined in accordance with the value in a final-angle defining step, an aerodynamic speed being determined as the process parameter.


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