Method for the operation of a gas turbine by active hydraulic gap adjustment

Patent metadata

Field	Value
Publication number	US-10450967-B2
Application number	US-201515118214-A
Country	US
Kind code	B2
Filing date	Feb 12, 2015
Priority date	Feb 25, 2014
Publication date	Oct 22, 2019
Grant date	Oct 22, 2019

Abstract

A method for operating a stationary gas turbine at partial load, having at least one compressor, at least one expansion turbine and a combustion chamber provided with at least one burner, which gas turbine further includes a hydraulic gap adjuster, wherein the method has the following steps: operating the gas turbine at partial load; operating the a hydraulic gap adjuster; during the operation of the hydraulic gap adjuster, increasing the fuel supply to the burner while increasing the temperature of the combustion gases which are guided to the expansion turbine.

First claim

The invention claimed is:

1. A method for operating a static gas turbine at partial load with at least one compressor, at least one expansion turbine and a combustion chamber that is provided with at least one burner, wherein the gas turbine further comprises a hydraulic gap adjuster, wherein the method comprises:
operating the gas turbine at partial load;
operating the hydraulic gap adjuster during partial load to shift a gas turbine rotor that connects the at least one compressor and the at least one expansion turbine in an axial direction, such that turbine blade tips of the at least one expansion turbine are displaced to have a smaller gap spacing with respect to an inner casing wall of the at least one expansion turbine;
while operating the hydraulic gap adjuster, increasing a fuel supply to the at least one burner, raising a temperature of combustion gases supplied to the at least one expansion turbine, wherein the temperature of the combustion gases is below a predetermined upper temperature limit for rated load operation.

2. The method as claimed in claim 1 , further comprising:
adjusting a guide vane adjustment device of the gas turbine while or after increasing the fuel supply to additionally increase the temperature of the combustion gases.

3. The method as claimed in claim 1 , further comprising:
recording, by measurement, of a physical operating parameter which correlates with the temperature of the combustion gases in order to determine the temperature of the combustion gases, and
initiating the increase in the fuel supply to the at least one burner when a recorded value of the physical operating parameter exceeds a predetermined limit value.

4. The method as claimed in claim 1 , wherein increasing the fuel supply to the at least one burner takes place in dependence on an ambient temperature and/or on an ambient pressure.

5. The method as claimed in claim 2 , wherein increasing the fuel supply to the at least one burner and/or the adjusting of the guide vane adjustment device takes place such that a turbine outlet temperature at partial load is below a turbine outlet temperature at rated load.

6. The method as claimed in claim 2 , wherein increasing the fuel supply to the at least one burner takes place in dependence on a setting of the guide vane adjustment device.

Assignees

• Siemens Ag

Inventors

• Larson Marco
• Savilius Nicolas

Classifications

• F05D2270/303

  Temperature · CPC title

• F05D2270/64

  Hydraulic actuators · CPC title

• F02C9/54 Primary

  by throttling the working fluid, by adjusting vanes · CPC title

• F02C9/48

  Control of fuel supply conjointly with another control of the plant (with nozzle section control F02K1/17) · CPC title

• F05D2250/34

  translated · CPC title