Gas turbine having fuel monitoring

Patent metadata

Field	Value
Publication number	US-9933336-B2
Application number	US-201414488686-A
Country	US
Kind code	B2
Filing date	Sep 17, 2014
Priority date	Mar 20, 2012
Publication date	Apr 3, 2018
Grant date	Apr 3, 2018

Abstract

The invention relates to a method for detecting a fuel leakage in the fuel distribution system between a fuel control valve and at least one burner of a gas turbine during the operation of the gas turbine. In order to detect a fuel leakage, the fuel consumption is approximated in accordance with the mechanical power of the gas turbine, the fuel amount fed to the fuel distribution system is determined, and the leakage flow is determined from the difference between the fed fuel amount and the fuel consumption. The invention further relates to a gas turbine for performing such a method.

First claim

The invention claimed is:

1. A method for detecting a fuel leakage during operation of a gas turbine, the gas turbine being controlled by a governor configured to compute an amount of a leakage flow of fuel in a fuel distribution system between a fuel control valve and at least one burner of the gas turbine, the method comprising:
in the governor:
approximating a fuel consumption of the gas turbine as a function of a mechanical power output of the gas turbine;
defining an amount of fuel supplied to the fuel distribution system;
computing the amount of the leakage flow from a difference between the defined amount of fuel supplied and the approximated fuel consumption; and

closing a trip valve in a fuel feed line of the fuel distribution system via a signal generated based on the computed amount of the leakage flow.

2. The method for detecting a fuel leakage as claimed in claim 1 , wherein approximating the fuel consumption of the gas turbine as a function of the mechanical power output of the gas turbine further comprises accounting for both an efficiency of the gas turbine and a heating value of the fuel.

3. The method for detecting a fuel leakage as claimed in claim 1 , wherein approximating the fuel consumption of the gas turbine as a function of the mechanical power output of the gas turbine comprises calculating a sum of a fuel mass flow in idling mode and a fuel mass flow in power output mode, wherein the fuel mass flow in power output mode is determined based on mechanical power output of the gas turbine, power output efficiency of the gas turbine, and a heating value of the fuel.

4. The method for detecting a fuel leakage as claimed in claim 1 , comprising:
approximating the mechanical power output of the gas turbine during steady-state load operation via a generator power output.

5. The method for detecting a fuel leakage as claimed in claim 1 , comprising:
measuring, during start-up of the gas turbine and during changes of a network frequency, acceleration of a shaft train of the gas turbine; and
approximating the mechanical power output of the gas turbine from a sum of generator power output and power for accelerating the shaft train.

6. The method for detecting a fuel leakage as claimed in claim 1 ,
wherein computing the amount of the leakage flow from the difference between the defined amount of fuel supplied and the approximated fuel consumption comprises calculating a time increment of the leakage flow; and
judging detection of fuel leakage when the calculated time increment exceeds a threshold value.

7. The method for detecting a fuel leakage as claimed in claim 6 , wherein the time increment of the leakage flow is calculated according to the equation:

m

leak
⁢
_
⁢
inc

=

m
leak

⁡

(

1
-

1
τ

⁢

∫

e

-

t
τ

⁢
d
⁢

⁢
t

)

=

m
leak

⁢

e

-

t
τ

,

wherein τ is an integration duration over time t of the time increment calculation.

8. The method for detecting a fuel leakage as claimed in claim 1 , comprising:
judging detection of fuel leakage when the computed amount of the leakage flow exceeds a threshold value.

9. The method for detecting a fuel leakage as claimed in claim 1 , wherein defining the amount of fuel supplied involves calculating the amount of fuel supplied as a function of at least a position of a fuel control valve and fuel pressure at the fuel control valve.

10. The method for detecting a fuel leakage as claimed in claim 1 , wherein defining the amount of fuel supplied involves setting a set point amount of fuel by the governor.

11. The method for detecting a fuel leakage as claimed in claim 1 , comprising:
deactivating detection of the fuel leakage when a change of operating conditions of the gas turbine occurs at a rate which exceeds a threshold.

12. The method for detecting a fuel leakage as claimed in claim 11 , wherein the operating conditions include a load shedding or an operating mode for frequency support.

13. The method for detecting a fuel leakage as claimed in claim 11 , wherein deactivating detection of the fuel leakage includes deactivating a threshold of the computed amount of the leakage flow, which occurs during operating conditions, wherein the operating conditions include a load shedding or an operating mode for frequency support.

14. A power plant comprising:
a gas turbine;
a governor configured to control the gas turbine;
a fuel distribution system between a fuel control valve and at least one burner of the gas turbine; and
a generator which is arranged to be driven by the gas turbine;
wherein the governor is further configured to:
detect a fuel leakage during operation of the gas turbine by:
(i) approximating a fuel consumption of the gas turbine as a function of a mechanical power output of the gas turbine,
(ii) defining an amount of fuel supplied to the gas turbine, and
(iii) computing an amount of a leakage flow of fuel in the fuel distribution system between the fuel control valve and the at least one burner from a difference between the defined amount of fuel supplied and the approximated fuel consumption; and

close a trip valve in a fuel feed line of the fuel distribution system via a signal generated based on the computed amount of the leakage flow.

Assignees

• Alstom Technology Ltd
• Ansaldo Energia Ip Uk Ltd

Inventors

• Zhang Mengbin
• Liedtke Klaus-Dieter
• Granados Gomez Wenceslao

Classifications

• G01M15/14 Primary

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• F23N2241/20

  Gas turbines · CPC title

• F05B2270/335

  Output power or torque · CPC title

• F02C9/32

  characterised by throttling of fuel (F02C9/38 takes precedence) · CPC title

• F02C7/228

  Dividing fuel between various burners · CPC title