Liquid Fuel Modeling for Gas Turbine Consistency

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Solution Overview

Problem

Gas turbine systems consuming liquid fuel face inconsistency due to variations in fuel composition, which can affect operational parameters like rotational speed, flame temperature, and energy output, especially when the exact fuel composition is unknown.

Innovation Solution

A model-based control system uses a processor to determine the specific gravity and hydrocarbon ratio of the liquid fuel based on its lower heating value, identifying a mixture of methane and ethylene as a model to simulate the fuel composition and adjust system parameters for consistent operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If liquid fuel is used in gas turbine systems, then the system can operate with flexible fuel sources, but the variation in fuel composition causes inconsistency in operational parameters

Engineering Contradiction:
Improvefuel source flexibilityVSAvoidoperational consistency
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The system dynamically adjusts operational parameters (air-fuel ratio, combustion timing, turbine inlet temperature) based on real-time fuel composition analysis. By changing these parameters in response to fuel variations, the system maintains consistent performance despite using variable liquid fuel sources.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The system creates a virtual model or representation of the actual fuel composition using spectroscopic analysis. This digital copy of the fuel's chemical properties allows the control system to predict and compensate for combustion behavior without physically testing each fuel batch.

Inventive Principle:
Principle #26Copying

2Adaptability or versatility

If the exact fuel composition is unknown, then the system can operate with varied fuel sources, but the operational parameters such as rotational speed and flame temperature become inconsistent

Engineering Contradiction:
Improvefuel source flexibilityVSAvoidparameter control precision
Core Design Contradiction:
Adaptability or versatilityVSManufacturing precision

Solution Approach 1:

The system performs preliminary fuel analysis using spectroscopic sensors before combustion. By identifying the fuel composition in advance, the control system can pre-calculate the optimal operational parameters needed to maintain consistent performance, rather than reacting to variations after they occur.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system continuously monitors fuel composition and compares it against target values, then adjusts operational parameters in real-time based on the deviation. This closed-loop feedback ensures that rotational speed, flame temperature, and other critical parameters remain within specified tolerances despite fuel variations.

Inventive Principle:
Principle #23Feedback

3Adaptability or versatility

If fuel composition varies over time, then the system can adapt to different fuel batches, but the inconsistency affects energy output and combustion efficiency

Engineering Contradiction:
Improvefuel batch adaptabilityVSAvoidenergy output consistency
Core Design Contradiction:
Adaptability or versatilityVSProductivity

Solution Approach 1:

The system transitions from static operational settings to dynamic parameter adjustment. Operational parameters are continuously modified in real-time based on incoming fuel composition data, allowing the system to maintain optimal energy output and combustion efficiency across different fuel batches rather than relying on fixed settings.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS9149776B2Systems and methods for liquid fuel modeling
Publication Date: 2015.10.06 GE INFRASTRUCTURE TECH LLC
  • US9149776B2 patent drawing
  • US9149776B2 patent drawing
  • US9149776B2 patent drawing

AI summary

A system includes a model-based control unit configured to receive a lower heating value for a liquid fuel having a composition. The processor is configured to determine a specific gravity, a hydrocarbon ratio, or both, for the liquid fuel based, at least in part, on the lower heating value of the liquid fuel. The processor is configured to compare the hydrocarbon ratio, the specific gravity, and/or the lower heating value of the liquid fuel to a collection of hydrocarbon ratios, specific gravities, and/or lower heating values for a plurality of mixtures of methane and ethylene. The processor is configured to identify a mixture of methane and ethylene from the collection that best matches the hydrocarbon ratio, the specific gravity, and/or the lower heating value of the liquid fuel and configured to use the identified mixture of methane and ethylene as a model for the composition of the liquid fuel.