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:
Mar. 13, 2018

Filed:

Feb. 20, 2014
Applicant:

Siemens Aktiengesellschaft, Munich, DE;

Inventors:

Thorsten Engler, Moers, DE;

Markus Gorynski, Bochum, DE;

Manuel Gutermuth, Essen, DE;

Philipp Kreutzer, Haltern am See, DE;

Marco Link, Mulheim, DE;

Nicolas Savilius, Essen, DE;

Kai Suselbeck, Oberhausen, DE;

Marc Tertilt, Hattingen, DE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/02 (2006.01); F01D 17/16 (2006.01); F01D 17/08 (2006.01); F02C 7/057 (2006.01); F01D 9/04 (2006.01); F02C 7/04 (2006.01);
U.S. Cl.
CPC ...
F01D 17/16 (2013.01); F01D 9/041 (2013.01); F01D 17/08 (2013.01); F01D 17/085 (2013.01); F01D 25/02 (2013.01); F02C 7/04 (2013.01); F02C 7/057 (2013.01); F05D 2220/32 (2013.01); F05D 2240/12 (2013.01); F05D 2270/301 (2013.01); F05D 2270/303 (2013.01); F05D 2270/311 (2013.01);
Abstract

A gas turbine includes an intake tract and a compressor having a compressor flow channel. The compressor further includes an inlet guide vane row positioned in the compressor flow channel having inlet guide vanes that can be adjusted. The gas turbine has an icing sensor unit having at least one sensor arranged between a first compressor blade row and a first compressor guide vane row. The first compressor blade row is thereby arranged in the compressor flow channel directly downstream of the inlet guide vane row, and the first compressor guide vane row is arranged directly downstream of the first compressor blade row. A method detects an imminent icing of the compressor, and the compressor is safeguarded therefrom such that at least inlet guide vanes of the inlet guide vane row are adjusted such that the acceleration of an intake air mass flow is reduced.


Find Patent Forward Citations

Loading…