Gas turbine fuel flow measurement using inert gas

Patent metadata

Field	Value
Publication number	US-9777637-B2
Application number	US-201213719714-A
Country	US
Kind code	B2
Filing date	Dec 19, 2012
Priority date	Mar 8, 2012
Publication date	Oct 3, 2017
Grant date	Oct 3, 2017

Abstract

The fuel flow rate to a gas turbine is measured using an inert gas. The inert gas is injected into the fuel flow and the concentration of the inert gas in the fuel/inert gas mixture is later measured. The concentration of the inert gas in the fuel/inert gas mixture is then used to calculate the mass flow rate of the fuel.

First claim

What is claimed is:

1. A system, comprising:
a transport medium to convey a fuel flow;
an injection device to inject an inert gas into the fuel flow to form a gas mixture; and
a gas composition measuring device downstream of the injection device to measure a concentration of the inert gas in the gas mixture,
wherein a flow rate of the fuel flow is calculated based on the measured concentration of the inert gas in the gas mixture.

2. The system of claim 1 , wherein the transport medium is configured to convey the fuel flow to a gas turbine for combustion, and wherein the gas composition measuring device is arranged to measure the concentration of the inert gas in the gas mixture upstream of the gas turbine.

3. The system of claim 1 , wherein the fuel flow powers at least one gas turbine.

4. The system of claim 1 , further comprising a controller to control a device based on the calculated flow rate of the fuel flow.

5. The system of claim 1 , further comprising a flow meter to measure an amount of the inert gas injected into the fuel flow, wherein the flow rate of the fuel flow is calculated based on the amount of the inert gas injected into the fuel flow and the measured concentration of the inert gas in the gas mixture.

6. The system of claim 1 , further comprising a controller to control a device based on the measured concentration of the inert gas.

7. The system of claim 4 , wherein the device is a gas turbine.

8. The system of claim 1 , wherein the inert gas is neon.

9. A method of measuring the flow rate of a gas, comprising:
injecting an inert gas into a fuel flow at an injection location;
mixing the inert gas with the fuel flow to form a gas mixture;
measuring a concentration of the inert gas in the gas mixture downstream of the injection location; and
calculating a flow rate of the fuel flow based on the measured concentration of the inert gas in the gas mixture.

10. The method of claim 9 , further comprising conveying the fuel flow to a gas turbine for combustion,
wherein the concentration of the inert gas in the gas mixture is measured upstream of the gas turbine.

11. The method of claim 9 , wherein the fuel flow powers at least one gas turbine.

12. The method of claim 9 , further comprising controlling, with a controller, a device based on the calculated flow rate of the fuel flow.

13. The method of claim 9 , further comprising measuring an amount of the inert gas injected into the fuel flow, wherein the flow rate of the fuel flow is calculated based on the amount of the inert gas injected into the fuel flow and the measured concentration of the inert gas in the gas mixture.

14. The method of claim 9 , wherein the inert gas is neon.

15. A gas turbine system, comprising;
a fuel line to convey a flow of fuel to a combustor section of a gas turbine;
an injection device to inject an inert gas into the fuel flow to form a gas mixture; and
a gas composition measuring device downstream of the injection device to measure a concentration of the inert gas in the gas mixture,
wherein a flow rate of the fuel flow is calculated based on the measured concentration of the inert gas in the gas mixture.

16. The gas turbine system of claim 15 , further comprising a controller to control the gas turbine based on the calculated flow rate of the fuel flow.

17. The gas turbine system of claim 15 , further comprising a flow meter to measure an amount of the inert gas injected into the fuel flow, wherein the flow rate of the fuel flow is calculated based on the amount of the inert gas injected into the fuel flow and the measured concentration of the inert gas in the gas mixture.

18. The gas turbine system of claim 15 , further comprising a controller is control the gas turbine based on the measured concentration of the inert gas.

19. The gas turbine system of claim 15 , wherein the inert gas is neon.

Assignees

• Gen Electric

Inventors

• Tillery Steven William
• Cook Jason Nathaniel

Classifications

• F05D2270/306

  Mass flow · CPC title

• G01F1/704

  using marked regions or existing inhomogeneities within the fluid stream, e.g. statistically occurring variations in a fluid parameter (G01F1/76, G01F25/00 take precedence) · CPC title

• F02C7/22 Primary

  Fuel supply systems · CPC title

• F17D3/00

  Arrangements for supervising or controlling working operations · CPC title

• Y10T137/8376

  Combined · CPC title