Fuel Gas Heater Flow Control for Combined Cycle Stability

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Solution Overview

Problem

Gas turbine combined cycle plants face challenges in managing fuel gas temperature fluctuations due to sudden load changes, which can lead to inefficient heat transfer and pressure issues when using heated water from an exhaust heat recovery boiler as a heat source.

Innovation Solution

A control unit manages the operation of return and dump valves to regulate the flow rate of heated water in the fuel gas heater, closing the return valve and maintaining a specified opening degree of the dump valve during reduced load conditions to prevent sharp temperature rises, and stepwise increasing the dump valve opening as needed to adjust fuel gas temperature accurately.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If the flow rate of heated water is reduced to control sharp temperature rise in fuel gas, then fuel gas temperature stability is improved, but heated water supply pressure increases

Engineering Contradiction:
Improvefuel gas temperature stabilityVSAvoidheated water supply pressure
Core Design Contradiction:
TemperatureVSStress or pressure

Solution Approach 1:

The patent introduces a flow control valve as an intermediary device on the heated water supply line to regulate the flow rate of heated water to the fuel gas heater. This mediator allows independent control of heated water flow rate separate from the return line valves, enabling temperature stability without excessive pressure buildup by dissolving the coupling between temperature control and pressure management.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent segments the heated water flow control into independent components: a supply line with a flow control valve, a return line with return valve, and a bypass with dump valve. This segmentation allows the supply pressure and flow rate to be controlled independently, resolving the contradiction between maintaining temperature stability (requiring low flow rate) and managing supply pressure (requiring adequate flow rate).

Inventive Principle:
Principle #1Segmentation

2Temperature

If the return valve is closed and dump valve is opened to reduce heated water flow rate during load reduction, then fuel gas temperature rise is controlled, but system complexity increases due to valve coordination requirements

Engineering Contradiction:
Improvefuel gas temperature controlVSAvoidvalve coordination system
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent implements feedback control by monitoring the outlet temperature of the fuel gas heater and using this information to automatically adjust the flow control valve opening degree. The control unit continuously compares the actual temperature with the target temperature and modifies the heated water flow rate accordingly, eliminating the need for complex manual valve coordination while maintaining precise temperature control during load changes.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system performs self-service through automatic control where the control unit independently manages the flow control valve based on temperature feedback without requiring operator intervention to coordinate multiple valves. The system self-regulates the heated water flow rate to maintain temperature stability, reducing operational complexity while achieving the desired temperature control during gas turbine load changes.

Inventive Principle:
Principle #25Self-service

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This configuration effectively controls fuel gas temperature fluctuations during load changes, ensuring efficient heat transfer and reducing pressure issues by managing the flow rate of heated water, thus enhancing the operational stability of the gas turbine combined cycle plant.

Implementation Method 1

an exhaust heat recovery boiler configured to recover exhausted heat of the gas turbine to generate steam

Methodology Applied
Scientific EffectHeat recovery: Heat Exchanger

Implementation Method 2

a fuel gas heater configured to heat fuel gas to be supplied to a combustor of the gas turbine using heated water that has been heated by the exhaust heat recovery boiler to serve as a heat source

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Data Source

PatentUS10975771B2Gas turbine combined cycle plant and method for controlling gas turbine combined cycle plant
Publication Date: 2021.04.13 MITSUBISHI POWER LTD
  • US10975771B2 patent drawing
  • US10975771B2 patent drawing
  • US10975771B2 patent drawing

AI summary

A gas turbine combined cycle plant includes a fuel gas heater configured to heat fuel gas to be supplied to a combustor of a gas turbine using heated water heated by an exhaust heat recovery boiler; a return valve disposed on a heated water returning line to return heated water passing through the heater to the boiler; a dump valve disposed on a condensate line bifurcated from the heated water returning line between the return valve and the heater to return the heated water to a condenser; and a control unit configured to control operation of the return and dump valves. When load of the turbine falls below a lower limit, the control unit closes the return valve and keeps the opening degree of the dump valve at a specified degree to reduce a flow rate of the heated water flowing in the heater for a predetermined time.