Methods and systems for heavy fuel oil in gas turbines

Patent metadata

Field	Value
Publication number	US-2020088110-A1
Application number	US-201816133780-A
Country	US
Kind code	A1
Filing date	Sep 18, 2018
Priority date	Sep 18, 2018
Publication date	Mar 19, 2020
Grant date	—

Abstract

A control system for a gas turbine includes a controller. The controller includes a processor configured to receive a plurality of signals from sensors disposed in the gas turbine engine system, wherein the gas turbine system engine comprises a compressor section fluidly coupled to a gas turbine section. The processor is additionally configured to derive a vanadium content in a gas turbine engine fuel based on at least one of the plurality of signals. The processor is also configured to determine if a control curve should be adjusted based on the vanadium content in the gas turbine engine fuel, and if it is determined that the control curve should be adjusted, then deriving an adjustment to the control curve based on the vanadium content, and applying the adjustment to the control curve to derive an adjusted control curve.

First claim

1 . A control system for a gas turbine system, comprising:
a controller comprising a processor, wherein the processor is configured to: receive a plurality of signals from sensors disposed in the gas turbine engine system, wherein the gas turbine system engine comprises a compressor section fluidly coupled to a gas turbine section; derive a vanadium content in a gas turbine engine fuel based on at least one of the plurality of signals; determine if a control curve should be adjusted based on the vanadium content in the gas turbine engine fuel; and if it is determined that the control curve should be adjusted, then deriving an adjustment to the control curve based on the vanadium content, and applying the adjustment to the control curve to derive an adjusted control curve.

2 . The control system of claim 1 , wherein the control curve is plotted against a compressors pressure ratio (CPR) ordinate axis and an exhaust temperature abscissa axis.

3 . The control system of claim 2 , wherein the processor is configured to derive a CPR and a sensed exhaust temperature based on the plurality of signals, and to adjust fuel flow, air flow, or a combination thereof, of the gas turbine system by comparing the sensed exhaust temperature and the CPR to the adjusted control curve.

4 . The control system of claim 1 , wherein the processor is configured to derive an amount of an additive to add to the gas turbine engine fuel based on the vanadium content.

5 . The control system of claim 1 , wherein the additive comprises magnesium (Mg) and wherein the processor is configured to derive the amount of an additive to add to the gas turbine engine fuel based on the vanadium content Mg/V =X by weight where V comprises vanadium in heavy fuel oil used in operations as the gas turbine engine fuel.

6 . The control system of claim 4 , wherein deriving the adjustment to the control curve based on the vanadium content comprises deriving the adjustment to the control curve based on the vanadium content and based on the amount of the additive to add to the gas turbine fuel.

7 . The control system of claim 1 , wherein the deriving the adjustment to the control curve based on the vanadium content comprises deriving the adjustment so that the adjustment results in a shift of the adjusted control curve when compared to the control curve based on the vanadium content.

8 . The control system of claim 7 , wherein the processor is configured to increase a downwards shift of the adjusted control curve based on increasing vanadium content, and to increase an upwards shift of the adjusted control curve based on a decreasing vanadium content.

9 . The control system of claim 1 , wherein the processor is configured to determine if the adjusted control curve should be adjusted based on a second sensed vanadium content, and if it is determined that the adjusted control curve should be adjusted, then deriving a second adjustment and applying the second adjustment to the adjusted control curve to derive a second adjusted control curve.

10 . A method, comprising:
receiving a plurality of signals from sensors disposed in the gas turbine engine system, wherein the gas turbine system engine comprises a compressor section fluidly coupled to a gas turbine section; deriving a vanadium content in a gas turbine engine fuel based on at least one of the plurality of signals; determining if a control curve should be adjusted based on the vanadium content in the gas turbine engine fuel; and if it is determined that the control curve should be adjusted, then deriving an adjustment to the control curve based on the vanadium content, and applying the adjustment to the control curve to derive an adjusted control curve.

11 . The method of claim 10 , wherein the control curve is plotted against a compressors pressure ratio (CPR) ordinate axis and an exhaust temperature abscissa axis.

12 . The method of claim 10 , comprising deriving an amount of an additive to add to the gas turbine engine fuel based on the vanadium content.

13 . The method of claim 12 , wherein deriving the adjustment to the control curve based on the vanadium content comprises deriving the adjustment to the control curve based on the vanadium content and based on the amount of the additive to add to the gas turbine fuel.

14 . The method of claim 12 , wherein the additive comprises magnesium (Mg) and wherein deriving the amount of the additive to add to the gas turbine engine fuel based on the vanadium comprises adding Mg so that Mg/V=X by weight where V comprises vanadium in heavy fuel oil used in operations as the gas turbine engine fuel.

15 . The method of claim 10 , wherein the deriving the adjustment to the control curve based on the vanadium content comprises deriving the adjustment so that the adjustment results in a shift of the adjusted control curve when compared to the control curve based on the vanadium content.

16 . A non-transitory computer-readable medium having computer executable code stored thereon, the code comprising instructions to:
receive a plurality of signals from sensors disposed in the gas turbine engine system, wherein the gas turbine system engine comprises a compressor section fluidly coupled to a gas turbine section; derive a vanadium content in a gas turbine engine fuel based on at least one of the plurality of signals; determine if a control curve should be adjusted based on the vanadium content in the gas turbine engine fuel; and if it is determined that the control curve should be adjusted, then deriving an adjustment to the control curve based on the vanadium content, and applying the adjustment to the control curve to derive an adjusted control curve.

17 . The non-transitory computer-readable medium of claim 16 , wherein the control curve is plotted against a compressors pressure ratio (CPR) ordinate axis and an exhaust temperature abscissa axis.

18 . The non-transitory computer-readable medium of claim 16 , wherein the code comprises instructions to derive an amount of an additive to add to the gas turbine engine fuel based on the vanadium content.

19 . The non-transitory computer-readable medium of claim 16 , wherein the instructions to derive the adjustment to the control curve based on the vanadium content comprise instructions to derive the adjustment to the control curve based on the vanadium content and based on the amount of the additive to add to the gas turbine fuel.

20 . The non-transitory computer-readable medium of claim 16 , wherein the instructions to derive the adjustment to the control curve based on the vanadium content comprise instructions to derive the adjustment so that the adjustment results in a shift of the adjusted control curve when compared to the control curve based on the vanadium content.

Assignees

• Gen Electric

Inventors

• Nandagopal Pugalenthi
• Muralidharan Vikram
• Muthaiah Veerappan
• Jordan Jr Harold
• Aboujaib Maher Mohamad
• Vierling Matthieu Paul Frederic
• Njuki Sanyu Victoria Nakibuuka
• Montagne Pierre
• Catrin Sven Sébastien
• Saavedra Ezio M Pena
• Balcer Laurent
• Sokolov Dmitry

Classifications

• G05B19/042

  using digital processors (G05B19/05 takes precedence) · CPC title

• F05D2300/13

  Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W · CPC title

• F02C9/26

  Control of fuel supply (F02C9/48 takes precedence; fuel valves F02C7/232) · CPC title

• F02C9/00 Primary

  Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants (controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05) · CPC title

• F02C9/40 Primary

  specially adapted to the use of a special fuel or a plurality of fuels · CPC title