Gas dosage control for gas engine

Patent metadata

Field	Value
Publication number	US-9581089-B2
Application number	US-201313891807-A
Country	US
Kind code	B2
Filing date	May 10, 2013
Priority date	May 10, 2013
Publication date	Feb 28, 2017
Grant date	Feb 28, 2017

Abstract

A gas engine assembly includes a compressor, a combustion system, a bypass line and a control system. The control system is configured to control gas supply parameters based on a transportation delay value. The transportation delay value corresponds to a delay between a time when a gas supply control mechanism is adjusted and a time that gas having a corresponding adjustment of a gas characteristic is received at a predetermined point downstream from the gas supply control mechanism.

First claim

The invention claimed is:

1. A gas engine assembly, comprising:
a compressor configured to receive a gas from a first gas supply line and to compress the gas;
a combustion system configured to receive the gas from the compressor via a second gas supply line and to combust the gas and a fuel;
a bypass line having one end connected to the first gas supply line and an opposite end connected to the second gas supply line to divert a portion of the gas less than all of the gas from one of the first and second gas supply lines to the other of the first and second gas supply lines; and
a control system configured to control gas supply parameters based on a transportation delay value, the transportation delay value corresponding to a delay between a time when a gas supply control mechanism is adjusted and a time that gas having a corresponding adjustment of a gas characteristic is received at a predetermined point downstream from the gas supply control mechanism, wherein the control system is configured to calculate the transportation delay value by determining a concentration of the gas along at least the second gas supply line over time.

2. The gas engine assembly of claim 1 , wherein the gas supply control mechanism is a gas/air mixer, and
the gas is a mixture of air and a non-air gas.

3. The gas engine assembly of claim 1 , wherein the gas supply control mechanism is a gas dosage valve configured to adjust an amount of a non-air gas provided to the first gas supply line.

4. The gas engine assembly of claim 1 , wherein the bypass line is configured to transmit the portion of the gas from the first gas supply line to the second gas supply line within the gas engine assembly comprising a turbocharger.

5. The gas engine assembly of claim 1 , wherein the control system is configured to calculate the concentration of the gas by measuring a pressure of the gas.

6. The gas engine assembly of claim 1 , further comprising:
a first sensor along the first gas supply line; and
a second sensor along the second gas supply line,
wherein the control system is configured to calculate the transportation delay value based on analyzing measurements from the first and second sensors over time.

7. The gas engine assembly of claim 6 , wherein analyzing the measurements from the first and second sensors over time includes detecting a first feature in the measurements from the first sensor corresponding to a first gas supply command signal, detecting a second feature in the measurements from the second sensor corresponding to the first gas supply command signal, and calculating the transportation delay value based on a difference in time between an occurrence of the first and second features, wherein the first feature and the second feature are indicative of the corresponding adjustment of the gas characteristic.

8. A gas engine control circuit, comprising:
a transportation delay calculation module configured to receive a measurement from at least one sensor along a gas supply path between a gas supply source and a combustion system and to calculate a transportation delay value corresponding to a delay between a time that a gas supply control mechanism is adjusted and a time that gas having a corresponding adjustment of a gas characteristic arrives at a predetermined point downstream from the gas supply control mechanism;
a gas supply mechanism control module configured to generate a gas supply control signal to control the gas supply control mechanism based on the transportation delay value;
a target value generator configured to generate a target value corresponding to a desired state of a gas turbine; and
a comparison unit configured to compare the target value with the measurement from the at least one sensor and to generate an error value based on a difference between the target value and the measurement,
wherein the gas supply mechanism control module is configured to generate the gas supply control signal to control the gas supply control mechanism based on the error value and the transportation delay value.

9. The gas engine control circuit of claim 8 , wherein the transportation delay calculation module is configured to receive at least two sets of measurements over time from at least two sensors along the gas supply path and to calculate the transportation delay value based on an analysis of the at least two sets of measurements over time.

10. The gas engine control circuit of claim 8 , wherein the transportation delay calculation module is configured to calculate the transportation delay value of the gas supply path of a gas turbine having a compressor configured to receive the gas from a gas supply source and to compress the gas, a combustion system configured to receive the gas from the compressor to combust the gas and a fuel, and a bypass line having one end connected along the gas supply path between the gas supply source and the compressor and an opposite end connected along the gas supply path between the compressor and the combustion system, and
the transportation delay calculation module is configured to calculate the transportation delay value by taking into account a diversion of a portion of the gas less than all of the gas through the bypass line.

11. A gas engine control circuit, comprising:
a transportation delay calculation module configured to receive a measurement from at least one sensor along a gas supply path between a gas supply source and a combustion system and to calculate a transportation delay value corresponding to a delay between a time that a gas supply control mechanism is adjusted and a time that gas having a corresponding adjustment of a gas characteristic arrives at a predetermined point downstream from the gas supply control mechanism; and
a gas supply mechanism control module configured to generate a gas supply control signal to control the gas supply control mechanism based on the transportation delay value, wherein the transportation delay calculation module is configured to receive at least two sets of measurements over time from at least two sensors along the gas supply path and to calculate the transportation delay value based on an analysis of the at least two sets of measurements over time.

12. The gas engine control circuit of claim 11 , wherein the transportation delay calculation module is configured to detect a first feature in a first set of measurements from a first sensor among the at least two sensors, the first feature corresponding to a first gas supply control signal,
the transportation delay calculation module is configured to detect a second feature in a second set of measurements from a second sensor among the at least two sensors, the second feature corresponding to the first gas supply control signal, and
the transportation delay calculation module is configured to calculate the transportation delay value based on a difference in time between an occurrence of the first and second features.

13. The gas engine control circuit of claim 11 , wherein the at least two sets of measurements are indicative of a pressure of gas in the gas supply path, a temperature of gas in the gas supply path, or a combination thereof.

14. The gas engine control circuit of claim 11 , wherein the transportation delay calculation module is configured to calculate the transportation delay value of the gas supply path of a gas turbine having a compressor configured to receive the gas from a gas supply source and to compress the gas, the combustion system configured to receive the gas from the compressor to combust the gas and a fuel, and a bypass line having one end connected along the gas supply path between the ga

Assignees

• Gen Electric

Inventors

• Sarmiento Penuela Oscar Eduardo
• Burgmair Raphael Rupert
• Huber Johannes
• Satria Medy
• Selga Rosa Castane
• Srinivasan Prashant

Classifications

• F05D2270/303

  Temperature · CPC title

• F02C9/18

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

• F02C9/52 Primary

  by bleeding or by-passing the working fluid · CPC title

• F05D2270/80

  Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges · CPC title

• F05D2260/606

  Bypassing the fluid · CPC title