Fuel Tank Spray Cooling for Fuel Cell Waste Heat Dissipation

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Solution Overview

Problem

Traditional turbine engines in commercial aviation face high maintenance and fuel costs, contribute to particulate pollution, and generate excessive noise, while zero-emission aircraft using electric motors powered by hydrogen fuel cells struggle with low-grade waste heat rejection causing excessive drag.

Innovation Solution

An integrated hydrogen-electric engine system with a fuel cell stack, air compressor, and motor assembly, utilizing a fuel tank as a heat exchanger to dissipate low-grade waste heat without increasing drag, and employing phase change materials to manage thermal energy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If existing heat exchangers are used to reject low-grade waste heat from fuel cells, then heat dissipation is achieved, but excessive drag is generated

Engineering Contradiction:
Improvewaste heat rejectionVSAvoiddrag
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

The fuel tank is designed to serve dual functions: storing fuel and acting as a heat exchanger for waste heat rejection. The tank walls are equipped with cooling channels that allow coolant to flow through, absorbing heat from the fuel cell system. This eliminates the need for separate heat exchanger components that would increase drag, while effectively dissipating low-grade waste heat through the tank surface area.

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

Solution Approach 2:

The invention merges the fuel storage function with the thermal management function by integrating the heat exchanger capability directly into the fuel tank structure. The cooling channels are embedded within the tank walls, combining two previously separate systems (fuel storage and heat rejection) into a single integrated component, thereby reducing overall system drag while maintaining effective heat dissipation.

Inventive Principle:
Principle #5Merging (Combining)

2Loss of energy

If phase change materials are used to manage thermal energy, then thermal energy management efficiency is improved, but device complexity increases

Engineering Contradiction:
Improvethermal energy managementVSAvoidsystem complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The system utilizes phase change materials that undergo physical state transitions (phase changes) at specific temperature thresholds. When the coolant reaches the phase change temperature, the material automatically absorbs or releases latent heat, dynamically adjusting thermal parameters without requiring complex control mechanisms. This passive thermal management approach improves energy efficiency while minimizing system complexity.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The phase change materials provide self-regulating thermal management by automatically absorbing excess heat when temperatures rise and releasing heat when temperatures drop. This self-service capability eliminates the need for active control systems, pumps, or valves to manage thermal energy, thereby improving thermal efficiency without significantly increasing device complexity.

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

Reduces operating costs, minimizes environmental impact, and enhances mission capabilities by efficiently managing thermal energy without adding drag or noise, while repurposing fuel tanks for heat dissipation.

Implementation Method 1

utilizing a fuel tank as a heat exchanger to dissipate low-grade waste heat

Methodology Applied
Scientific EffectHeat exchanger: Heat Exchanger

Implementation Method 2

employing phase change materials to manage thermal energy

Methodology Applied
Scientific EffectPhase change: Phase Change

Data Source

PatentUS12542287B2Fuel tank heat dissipation system for fuel cell cooling
Publication Date: 2026.02.03 ZEROAVIA INC
  • US12542287B2 patent drawing
  • US12542287B2 patent drawing
  • US12542287B2 patent drawing

AI summary

A fuel tank heat dissipation system for fuel cell (FC) cooling is disclosed. In one example, at least one FC is in thermal communication with an intermediary heat exchanger. A fuel tank is also in fluid communication with the intermediary heat exchanger. A fluid is used to receive heat from the intermediary heat exchanger and flow along a first fluid path to the fuel tank. A nozzle is used to spray the fluid about an interior surface of the fuel tank, where the spray of the fluid about the interior of the fuel tank allows the fluid to dissipate the heat. A second fluid path from the fuel tank to the intermediary heat exchanger, the second fluid path to return the fluid that has dissipated the heat to the intermediary heat exchanger.