Common Cooling Circuit for Fuel Cell and Aircraft Hydraulic Systems

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current aircraft hydraulic systems face reliability issues due to high temperatures under load, which can damage components, while fuel cells require thermal management to prevent overheating.

Innovation Solution

A system coupling a fuel cell system with a heat generating system through a common cooling circuit, utilizing heat exchangers, a pump, reservoir, and a liquid/air cooler to manage heat and maintain the fuel cell at optimal operating temperature, with the option of different operating windows for hydraulic and fuel cell systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If a common cooling circuit is used to cool both the fuel cell and hydraulic system, then heat management efficiency is improved, but system complexity increases

Engineering Contradiction:
Improveheat management efficiencyVSAvoidsystem complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The patent merges the cooling circuits of the fuel cell system and hydraulic system into a single common cooling circuit. The coolant flows through heat exchangers connected to both systems, allowing simultaneous cooling of both components through one integrated circuit rather than separate independent circuits.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The common cooling circuit serves multiple functions: it cools the fuel cell stack, cools the hydraulic system components, and can selectively direct coolant flow to different heat exchangers based on thermal demands. This multi-functional design eliminates the need for separate cooling systems.

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

2Reliability

If the hydraulic system is cooled continuously, then component reliability is improved, but energy consumption increases

Engineering Contradiction:
Improvecomponent reliabilityVSAvoidenergy consumption
Core Design Contradiction:
ReliabilityVSUse of energy by moving object

Solution Approach 1:

The system employs dynamic control of coolant flow through the hydraulic heat exchanger. A control unit monitors the temperature and operational state of the hydraulic system, activating or deactivating the coolant flow through the hydraulic heat exchanger based on real-time thermal demands, rather than continuous cooling.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The cooling of the hydraulic system is performed periodically or on-demand rather than continuously. The system activates cooling only when thermal thresholds are exceeded or when hydraulic components are actively operating, reducing unnecessary energy consumption from continuous coolant circulation.

Inventive Principle:
Principle #19Periodic action

3Ease of operation

If the fuel cell is preheated to operating temperature, then starting properties are improved, but system complexity increases

Engineering Contradiction:
Improvestarting propertiesVSAvoidsystem complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The heating function is integrated into the existing common cooling circuit. The same coolant loop that cools the fuel cell during operation can reverse or redirect flow to heat the fuel cell during startup, eliminating the need for a separate heating system.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fuel cell system uses its own cooling circuit infrastructure to provide heating during startup. The coolant, circulated through the fuel cell heat exchanger, transfers thermal energy to preheat the fuel cell membranes and components, allowing the system to serve its own heating needs without external equipment.

Inventive Principle:
Principle #25Self-service

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 enhances the starting properties of the fuel cell, improves system reliability by efficiently managing heat, and allows for flexible operation during normal and emergency conditions, reducing the risk of component damage.

Implementation Method 1

The heat generating system has at least one heat exchanger, which can effectuate heat transfer between the heat generating system and the cooling circuit system

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 2

A coolant may circulate in the cooling circuit system, absorbing heat from the heat generating system and keeping the fuel cell at a predetermined operating temperature

Methodology Applied
Scientific EffectHeat absorption: Absorption (physical)

Implementation Method 3

The cooler is a liquid-/air cooler with a fan. The heat of the coolant is transferred to the ambient via the cooler and via an out flow valve

Methodology Applied
Scientific EffectConvection cooling: Convection

Data Source

PatentUS8192882B2Fuel cell and aircraft hydraulic system having a common cooling circuit
Publication Date: 2012.06.05 AIRBUS OPERATIONS GMBH
  • US8192882B2 patent drawing
  • US8192882B2 patent drawing

AI summary

A system utilizing synergetic potentials at different systems such as of a fuel cell system and of an aircraft hydraulic system, through coupling them via a common cooling circuit system.