Single Coolant Loop for Fuel Cell and Electronics Cooling

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Solution Overview

Problem

The existing cooling systems for fuel cell systems and their related electronic components on aircraft require two separate cooling loops, which increase weight and complexity, and are inefficient due to energy consumption and emissions.

Innovation Solution

A single coolant loop is used to cool both the fuel cell system and electronic components, utilizing a coolant pump, distributor, and mixer to route and mix coolant at different temperatures, reducing the need for separate cooling systems and harnessing heat for storage or reuse.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If two separate cooling loops are used for fuel cell system and electronic components, then each system can be cooled at its optimal temperature, but weight and system complexity increase

Engineering Contradiction:
Improvecooling temperature controlVSAvoidcooling system complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent combines two separate cooling loops into a single integrated cooling system that serves both the fuel cell system and electronic components. The single loop uses a coolant pump, distributor with temperature sensors, and mixer to route coolant to different systems, reducing the number of pumps, heat exchangers, and control systems while maintaining appropriate cooling for each component

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The single coolant loop is designed to perform multiple functions: cooling the fuel cell system, cooling electronic components, and providing heated coolant to the cabin. The distributor and mixer enable the system to dynamically allocate coolant to different destinations based on temperature requirements, making the cooling system multi-functional and adaptable

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

2Temperature

If two separate cooling loops are used for fuel cell system and electronic components, then each system can be cooled independently, but weight increases

Engineering Contradiction:
Improvecooling temperature controlVSAvoidcooling system weight
Core Design Contradiction:
TemperatureVSWeight of moving object

Solution Approach 1:

The patent merges two separate cooling loops into one unified system, eliminating duplicate components such as second coolant pumps, additional heat exchangers, and redundant control systems. This consolidation directly reduces the overall weight of the cooling system while maintaining the capability to cool both the fuel cell system and electronic components at their respective optimal temperatures

Inventive Principle:
Principle #5Merging (Combining)

3Productivity

If thermal power from fuel cell is not utilized, then system operation is simplified, but energy efficiency decreases and waste heat is generated

Engineering Contradiction:
Improvesystem operation simplicityVSAvoidthermal energy waste
Core Design Contradiction:
ProductivityVSLoss of energy

Solution Approach 1:

The patent converts the previously wasted thermal power (heat) from the fuel cell system into a useful resource by routing heated coolant from the fuel cell to the cabin heating system. This transforms waste heat into a beneficial output, improving overall energy efficiency and reducing the need for separate heating systems, while the system remains operationally manageable through integrated control

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

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 solution reduces weight and complexity by using a single coolant loop, improves energy efficiency by reusing heat, and decreases emissions by integrating cooling systems for fuel cell and electronic components, while maintaining optimal operating temperatures.

Implementation Method 1

a heat exchanger to cool the coolant fluid

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 2

a coolant pump to move the coolant fluid through the loop

Methodology Applied
Scientific EffectPumping: Pump

Data Source

PatentEP3025387B1Fuel cell system with one coolant loop
Publication Date: 2022.09.07 SAFRAN AEROTECHNICS SAS
  • EP3025387B1 patent drawingFigure 1
  • EP3025387B1 patent drawingFigure 2
  • EP3025387B1 patent drawingFigure 3

AI summary

Embodiments of the present invention provide a single coolant loop (40) that can be used for cooling at least two systems (100, 26) that are generally operable at two different temperatures. Rather than providing two separate cooling loops that can provide the two different cooling temperatures, there is provided a single cooling loop (40) that can route, harness, and mix heated coolant so that the two system can be served by a single loop.