Redundant Axial Gap Motor Fuel System for Gas Turbine Reliability

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Solution Overview

Problem

Current direct metering fuel control systems for gas turbine engines face challenges such as fuel supply variations, unpredictable engine transients, reduced thermal efficiency, and increased complexity and cost, along with insufficient redundancy and reliability.

Innovation Solution

A direct metering fuel supply system utilizing axial gap motors with permanent magnet rotors and stators, coupled with a fixed displacement, variable speed positive displacement piston pump, and a gas turbine engine control to manage fuel flow, ensuring redundancy and efficiency by selectively energizing and deenergizing motors based on operational status.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If direct metering fuel control systems are implemented to reduce system weight and complexity, then system weight and complexity are reduced, but fuel supply variations and reliability issues occur

Engineering Contradiction:
Improvesystem complexityVSAvoidfuel supply reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The system incorporates a standby motor that remains ready to take over immediately if the primary motor fails. This redundant component is pre-positioned and pre-configured to prevent fuel supply interruptions, thereby maintaining reliability while using a simplified direct metering architecture.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Solution Approach 2:

The system changes the operational state of the motor from a single continuous operation mode to a selectable mode with hot standby. The control system can switch between primary and standby motors based on operational status, changing the system's redundancy parameter without increasing overall complexity.

Inventive Principle:
Principle #35Parameter changes

2Device complexity

If single motor configuration is used to simplify system structure, then system structure is simplified, but system redundancy and reliability are reduced

Engineering Contradiction:
Improvemotor configuration complexityVSAvoidsystem redundancy
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The motor function is segmented into multiple independent units (primary motor and standby motor) that can operate independently. This segmentation allows the system to maintain simplified control logic while achieving redundancy through parallel independent components.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Both the primary and standby motors are designed with identical capabilities and interfaces, making them universally interchangeable. Either motor can perform the fuel pumping function, providing multi-functionality that enhances reliability without increasing operational complexity.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Ease of operation

If fuel is used to drive fluid-operated actuators, then actuator operation is enabled, but fuel supply droop and engine speed droop occur

Engineering Contradiction:
Improveactuator operationVSAvoidengine speed stability
Core Design Contradiction:
Ease of operationVSSpeed

Solution Approach 1:

The control system continuously monitors fuel flow and engine parameters, detecting any droop caused by actuator operation. Based on this feedback, the control system adjusts the motor operation to compensate for fuel consumption by actuators, maintaining stable engine speed.

Inventive Principle:
Principle #23Feedback

4Manufacturing precision

If direct metering control is implemented to improve thermal efficiency, then fuel metering precision is improved, but system cost and manufacturing complexity increase

Engineering Contradiction:
Improvefuel metering precisionVSAvoidsystem manufacturing
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The system replaces complex mechanical metering mechanisms with an electronically controlled motor-driven pump. This substitution achieves precise fuel metering through electronic control while simplifying manufacturing, as the motor and pump are standard components that can be mass-produced.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 minimizes fuel supply variations, enhances thermal efficiency and cost-effectiveness, and provides sufficient redundancy and reliability in fuel delivery to gas turbine engines.

Implementation Method 1

Each axial gap motor is configured to be selectively energized and is operable, upon being energized, to supply a drive torque at a drive speed

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 2

The fixed displacement, variable speed positive displacement piston pump is coupled to each of the axial gap motors to receive the drive torque selectively supplied therefrom and is operable, upon receipt of the drive torque, to supply fuel at a flow rate dependent on the drive speed

Methodology Applied
Scientific EffectPositive displacement: Pump

Data Source

PatentUS7841164B2Direct metering fuel system with an integral redundant motor pump
Publication Date: 2010.11.30 HONEYWELL INTERNATIONAL INC
  • US7841164B2 patent drawing
  • US7841164B2 patent drawing
  • US7841164B2 patent drawing

AI summary

A direct metering fuel supply system includes a plurality of axial gap motors, a fixed displacement, variable speed positive displacement piston pump, and a gas turbine engine control. Each axial gap motor is configured to be selectively energized and is operable, upon being energized, to supply a drive torque at a drive speed. The fixed displacement, variable speed positive displacement piston pump is coupled to each of the axial gap motors to receive the drive torque selectively supplied therefrom and is operable, upon receipt of the drive torque, to supply fuel at a flow rate dependent on the drive speed. The gas turbine engine control is adapted to receive fuel flow commands and is operable, in response to the fuel flow commands, to energize one of the plurality of axial gap motors.