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:
Feb. 22, 2022

Filed:

Feb. 20, 2018
Applicant:

Siemens Energy Global Gmbh & Co. KG, Munich, DE;

Inventors:

Kok-Mun Tham, Oviedo, FL (US);

Christian Keune, Heiligenhaus, DE;

Nicolas Benjamin Wappler, Düsseldorf, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 19/00 (2006.01); F01K 13/02 (2006.01); F02C 9/54 (2006.01);
U.S. Cl.
CPC ...
F01D 19/00 (2013.01); F01K 13/02 (2013.01); F02C 9/54 (2013.01); F05D 2220/32 (2013.01); F05D 2220/72 (2013.01); F05D 2260/85 (2013.01);
Abstract

The invention relates to a method for starting up a gas turbine engine of a combined cycle power plant. The method includes applying load to the gas turbine engine and increasing the load until a predetermined combustor firing temperature is reached, while keeping the adjustable inlet guide vanes in a start position adapted to reduce the mass flow of air into the compressor; further increasing the load of the gas turbine engine while opening the adjustable inlet guide vanes and keeping the predetermined combustor firing temperature constant until the inlet guide vanes reach an end position adapted to increase the mass flow of air into the compressor; further increasing the load of the gas turbine engine while keeping the adjustable inlet guide vanes in the end position until a predetermined load of the gas turbine engine is reached.


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