Absorption Chiller Cooling Exhaust Gas for SCR Systems

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Solution Overview

Problem

Heavy-duty gas turbine systems face challenges in cooling exhaust gases to suitable temperatures for selective catalytic reduction (SCR) systems, requiring significant tempering air that reduces efficiency and increases energy input, especially due to high exhaust gas temperatures exceeding acceptable operating ranges for SCR catalysts.

Innovation Solution

The implementation of an absorption chiller that utilizes exhaust gas heat to drive a cooling process, cooling a portion of the exhaust gas and reintroducing it to reduce overall exhaust gas temperature, potentially eliminating the need for tempering air by using an exhaust gas heat exchanger and absorption chiller configuration.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If tempering air is used to cool exhaust gas, then exhaust gas temperature is reduced to SCR operating range, but system efficiency decreases and energy input increases

Engineering Contradiction:
Improveexhaust gas temperatureVSAvoidsystem efficiency
Core Design Contradiction:
TemperatureVSUse of energy by moving object

Solution Approach 1:

The exhaust gas itself is used as the cooling medium through the absorption chiller system. The high-temperature exhaust gas drives the absorption cooling process, and the cooled exhaust gas is then reused to cool remaining exhaust gas, making the system self-sufficient without requiring external tempering air

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The absorption chiller utilizes phase transition of the refrigerant (evaporation and condensation) to absorb heat from the exhaust gas, converting thermal energy into useful cooling effect while maintaining system efficiency

Inventive Principle:
Principle #36Phase transitions

2Temperature

If tempering air is injected into exhaust gas, then exhaust gas temperature is reduced, but exhaust gas flow rate increases

Engineering Contradiction:
Improveexhaust gas temperatureVSAvoidexhaust gas flow rate
Core Design Contradiction:
TemperatureVSQuantity of substance

Solution Approach 1:

A portion of the high-temperature exhaust gas is extracted and routed through the absorption chiller to be cooled, then returned to the main exhaust stream. This avoids introducing external air while still achieving temperature reduction

Inventive Principle:
Principle #2Taking out (Extraction)

3Use of energy by moving object

If absorption chiller is used to cool exhaust gas, then tempering air requirement is reduced, but device complexity increases

Engineering Contradiction:
Improvesystem efficiencyVSAvoidcooling system complexity
Core Design Contradiction:
Use of energy by moving objectVSDevice complexity

Solution Approach 1:

The absorption chiller is integrated with the exhaust gas cooling system, combining the cooling function with the existing exhaust infrastructure. The chilled fluid path connects the absorption chiller to the exhaust duct assembly, creating a unified system that reduces overall complexity despite adding absorption cooling components

Inventive Principle:
Principle #5Merging (Combining)

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 approach enhances the efficiency of gas turbine systems by reducing the reliance on tempering air, achieving effective cooling of exhaust gases within acceptable temperature ranges for SCR systems, thereby improving plant efficiency and potentially eliminating the need for tempering air, while maintaining homogeneity and reducing energy input.

Implementation Method 1

The absorption chiller is configured to use the take-off stream of exhaust gas to drive at least a portion of an absorption cooling process to generate a cooled take-off stream of exhaust gas

Methodology Applied
Scientific EffectAbsorption cooling: Absorption (physical)

Implementation Method 2

The heat exchanger is positioned within the exhaust duct assembly or is part of a tempering air injection system configured to provide tempering air to the exhaust duct assembly

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Data Source

PatentUS10385779B2System for cooling exhaust gas with absorption chiller
Publication Date: 2019.08.20 GE INFRASTRUCTURE TECH LLC
  • US10385779B2 patent drawing
  • US10385779B2 patent drawing
  • US10385779B2 patent drawing

AI summary

A gas turbine system includes a gas turbine engine configured to combust a fuel and produce an exhaust gas. An exhaust duct assembly is coupled to the gas turbine engine and is configured to receive the exhaust gas. An absorption chiller is fluidly coupled to the exhaust duct assembly and is configured to receive a take-off stream of the exhaust gas. The absorption chiller is configured to use the take-off stream to drive at least a portion of an absorption cooling process to generate a cooled take-off stream of exhaust gas. The exhaust duct assembly is configured to receive the cooled take-off stream of exhaust gas from the absorption chiller and to mix the cooled take-off stream with exhaust gas present within the exhaust duct assembly to cool the exhaust gas.