Dual Pump Fuel Switching via Bypass Flow Sensing

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Solution Overview

Problem

Dual pump fuel supply systems in aircraft engines face challenges in reducing engine burn flow disturbances during transitions between pumping modes, leading to increased complexity and reduced reliability, while also wasting energy due to excess fuel return.

Innovation Solution

A dual pump fuel supply system that utilizes a flow sensing valve to regulate the amount of flow supplied to the fuel metering unit, minimizing engine burn flow disturbances by controlling the pressurization of the second pump and adding or subtracting its flow to the first pump based on bypass return flow from the fuel metering unit, thereby maintaining a nearly constant differential pressure and reducing energy consumption.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If a dual pump system is implemented to reduce thermal issues and match fuel demand, then fuel temperature control is improved, but engine burn flow disturbances increase during pump mode transitions

Engineering Contradiction:
Improvefuel temperatureVSAvoidengine burn flow stability
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The system performs preliminary pressurization of the second pump before adding its flow to the engine supply. The control system monitors fuel demand and progressively increases the second pump's output pressure to match the first pump's pressure before combining flows, preventing sudden flow disturbances that would affect engine burn stability

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system dynamically adjusts the operating mode of the dual pump system based on real-time fuel demand conditions. The control system continuously monitors engine fuel requirements and transitions between single-pump and dual-pump modes smoothly, adjusting flow rates and pressures dynamically to maintain stable engine operation while managing thermal conditions

Inventive Principle:
Principle #15Dynamics

2Reliability

If additional control mechanisms are added to minimize fuel flow disturbances during switching, then engine burn flow stability is improved, but system complexity increases

Engineering Contradiction:
Improveengine burn flow stabilityVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system uses the existing fuel bypass return flow from the fuel metering unit as a natural sensing mechanism. This bypass flow provides direct feedback about engine fuel demand conditions, allowing the control system to automatically adjust pump operations without requiring additional external sensors or complex control signals from the engine control unit

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The control system utilizes feedback from the fuel bypass return flow to monitor engine fuel demand in real-time. This feedback mechanism allows the system to detect when fuel demand exceeds the first pump's capability and automatically transitions to dual-pump mode, maintaining stable engine operation through continuous monitoring and adjustment

Inventive Principle:
Principle #23Feedback

3Use of energy by moving object

If the second pump operates with minimum pressure differential during low fuel demand, then energy consumption is reduced, but flow control precision decreases

Engineering Contradiction:
Improvepump energy consumptionVSAvoidflow control precision
Core Design Contradiction:
Use of energy by moving objectVSManufacturing precision

Solution Approach 1:

The second pump operates dynamically with variable pressure differential based on fuel demand conditions. During low fuel demand, the pump runs with minimum pressure differential to reduce energy consumption. As fuel demand increases and the system transitions to dual-pump mode, the pressure differential is progressively increased to provide precise flow control and match engine requirements

Inventive Principle:
Principle #15Dynamics

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

The system effectively reduces engine burn flow disturbances and minimizes energy waste by dynamically adjusting the flow from the second pump to match engine demand, ensuring adequate fuel supply while maintaining system reliability and efficiency.

Implementation Method 1

In one embodiment, a flow sensing valve senses the bypass return flow from the fuel metering unit and regulates the amount of flow supplied from the dual pump system to the fuel metering unit based on the flow sensing port's position

Methodology Applied
Scientific EffectFlow sensing:

Implementation Method 2

maintaining a nearly constant differential pressure

Methodology Applied
Scientific EffectPressure differential control:

Data Source

PatentEP2655857B1Flow sensing dual pump switching system and method
Publication Date: 2019.08.07 WOODWARD INC
  • EP2655857B1 patent drawingFigure 1
  • EP2655857B1 patent drawingFigure 2
  • EP2655857B1 patent drawingFigure 3

AI summary

A flow sensing dual pump switching system and method are provided that control the supply of fuel from a dual pump fuel system to a fuel metering unit. The system senses bypass pressure from the fuel metering unit to control the differential pressurization of the second pump. As the bypass is reduced, the pressure of the second pump is increased so that it may be added to that of the first pump to supply the increased fuel consumption needs of an engine. As the fuel consumption needs decrease, the flow from the second pump added to the first pump is reduced and the differential pressure of the second pump is similarly reduced. If the bypass pressure remains high, the switching system disconnects the output of the second pump from that of the first in favor of bypassing the flow to its input to reduce its differential pressure and conserve energy.