Gas Turbine Feedforward Control for Compressor Failure

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Solution Overview

Problem

Existing power plant control systems are too slow to respond to unexpected transients, leading to sudden shutdowns of major rotating equipment when a fuel gas compressor fails, resulting in high stress and potential delays in restarting the plant.

Innovation Solution

A method that rapidly reduces the power output of gas turbine engines to an emergency power output upon detection of a fuel gas compressor failure, using feedforward control signals to quickly adjust fuel flow and maintain operation until redundant compressors can take over.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If pressure controllers and load control systems are designed to work slowly to avoid steep pressure gradients and oscillations, then stable operation of gas turbine engines is achieved, but the control systems cannot respond quickly enough to unexpected transients such as fuel gas compressor failures

Engineering Contradiction:
Improvestable operationVSAvoidresponse speed
Core Design Contradiction:
Stability of the object's compositionVSSpeed

Solution Approach 1:

The control system is equipped with feedforward control that anticipates compressor failures and preemptively adjusts fuel control valve positions and gas turbine power output before the failure fully impacts the system. This preliminary action prevents the transient pressure drops that would otherwise cause sudden shutdowns, thereby maintaining stability while enabling fast response to failures.

Inventive Principle:
Principle #10Preliminary action

2Productivity

If fuel gas compressors are operated close to full load to improve plant economics, then investment cost and self-consumption are optimized, but failure of a compressor results in fast drop of fuel gas supply pressure causing sudden shutdown of gas turbine engines

Engineering Contradiction:
Improveplant economicsVSAvoidcontinuous operation
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

Upon detection of compressor failure, the feedforward control system immediately reduces gas turbine power output to match the reduced fuel gas supply capacity. This prevents fuel gas pressure from dropping below the minimum required pressure threshold, allowing the gas turbine engines to continue operating reliably at reduced capacity rather than shutting down suddenly.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The control system dynamically adjusts the operating point of the gas turbine engines in response to compressor failure. By continuously modulating fuel control valve positions and power output based on real-time compressor status, the system maintains reliable operation across varying conditions, transitioning smoothly from full-load operation to failure-mode operation without sudden shutdowns.

Inventive Principle:
Principle #15Dynamics

3Duration of action of stationary object

If sudden shutdown of gas turbine engines is prevented through fast control response, then lifetime consumption of thermally loaded parts is reduced, but the control system complexity increases

Engineering Contradiction:
Improveequipment lifetimeVSAvoidcontrol system complexity
Core Design Contradiction:
Duration of action of stationary objectVSDevice complexity

Solution Approach 1:

The feedforward control system uses pre-programmed control strategies and lookup tables that define the relationship between compressor failure scenarios and required gas turbine power adjustments. This approach provides fast protective action to preserve equipment lifetime while avoiding the need for complex real-time calculations or advanced control algorithms, thereby limiting control system complexity.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP3862549B1Method for operating a power plant, and power plant
Publication Date: 2025.05.07 GENERAL ELECTRIC TECH GMBH
  • EP3862549B1 patent drawingFigure 1
  • EP3862549B1 patent drawingFigure 2

AI summary

Disclosed is a method for operating a power plant (1) comprising at least one gas turbine engine (10, 20) and at least one fuel gas compressor (53. 54, 55). The method comprises supplying fuel gas (5) through a utility supply line (51), compressing the fuel gas to a plant supply pressure in at least one operating fuel gas compressor and supplying the compressed fuel gas to a plant supply line (52). The at least one gas turbine engine is operated at a set power output according to a power demand signal. If a failure of an operating fuel gas compressor is detected, the power output of the at least one gas turbine engine is reduced to an emergency power output which is lower than the set power output and the power output of the at least one gas turbine engine is restricted to the emergency power output. The reduction of the power output is performed in one single step and controlled by at least one feedforward control signal.