Distributed Fuel Control System for Turbine Engine

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Solution Overview

Problem

Turbine engines face challenges in controlling fuel flow due to limited controllability of multiplex fuel delivery units, leading to uneven fuel distribution and variations in fuel pressure, volume, and velocity across the engine.

Innovation Solution

A distributed fuel control system comprising a controller, fuel delivery system, and sensors that allow individualized control and monitoring of fuel flow to each multiplex fuel delivery unit, using a processor and tangible memory to regulate fuel passage based on inputs from sensors and aircraft systems, ensuring precise fuel pressure, volume, and velocity delivery.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If traditional centralized fuel control is used, then system simplicity is maintained, but fuel flow controllability and distribution uniformity deteriorate

Engineering Contradiction:
Improvecontrol system structureVSAvoidfuel flow controllability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The fuel control system is segmented into multiple independent control units, each responsible for a specific multiplex fuel delivery unit. This segmentation allows individualized control of fuel flow to each delivery unit, improving controllability and distribution uniformity while maintaining overall system manageability through modular architecture.

Inventive Principle:
Principle #1Segmentation

2Measurement precision

If individualized control of each multiplex fuel delivery unit is implemented, then fuel flow precision is improved, but system complexity increases

Engineering Contradiction:
Improvefuel flow control precisionVSAvoidcontrol system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The control system dynamically adjusts fuel flow parameters for each multiplex fuel delivery unit based on real-time sensor feedback and operational conditions. This dynamic control enables precise fuel flow regulation while the system adapts to varying engine conditions, maintaining precision without requiring overly complex static control mechanisms.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

Sensor feedback from each multiplex fuel delivery unit is integrated into the control system, allowing real-time monitoring and adjustment of fuel flow parameters. This feedback mechanism enables precise control by continuously comparing actual fuel delivery against target parameters and making corrective adjustments.

Inventive Principle:
Principle #23Feedback

3Device complexity

If centralized fuel control is used, then system simplicity is maintained, but fuel distribution uniformity deteriorates

Engineering Contradiction:
Improvecontrol system structureVSAvoidfuel distribution uniformity
Core Design Contradiction:
Device complexityVSStability of the object's composition

Solution Approach 1:

Each control unit is configured with local quality characteristics tailored to its specific multiplex fuel delivery unit, accounting for variations in delivery unit performance and positioning. This localized control approach ensures uniform fuel distribution across all delivery units by compensating for individual unit variations through customized control parameters.

Inventive Principle:
Principle #3Local quality

Data Source

PatentEP2985439B1Distributed fuel control system
Publication Date: 2020.03.25 HAMILTON SUNDSTRAND CORP
  • EP2985439B1 patent drawingFigure 1
  • EP2985439B1 patent drawingFigure 2
  • EP2985439B1 patent drawingFigure 3A

AI summary

Distributed fuel control system (2) and methods are disclosed. A distributed fuel control system (2) may comprise a controller (4), a fuel delivery system (6), and fuel delivery system sensors (8) and combustion sensors (10). The controller may output a control signal (5) in response to at least one of the fuel delivery system sensor (8) or the combustion sensors (10). In response, the fuel flow to an individual multiplex fuel delivery unit (25-1 to 25-n) may be controlled according to various methods. One such method includes determining a desired fuel pressure differential, directing a torque motor (15) to set a pressure regulator (14) to a position corresponding to the desired fuel pressure differential, determining a sensed fuel pressure differential, and adjusting the torque motor (15) in response to a difference between the sensed fuel pressure differential and the desired fuel pressure differential.