Liquid Hydrogen Aircraft Power Generation from Fuel Warming

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Solution Overview

Problem

Hydrogen fueled vehicles face inefficiencies in warming liquid hydrogen from storage temperature to operational temperature, leading to energy waste, as existing systems do not effectively utilize excess energy within the system.

Innovation Solution

A power system with a liquid hydrogen fuel source and vacuum insulation layers, utilizing a heat exchanger to warm a portion of the hydrogen fuel, which is then expanded through a thermal engine to generate additional power, with a turbine and electrical generator converting this thermal energy into electrical or mechanical power.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If liquid hydrogen is warmed from storage temperature (20K) to operational temperature (300K), then the hydrogen becomes usable in fuel cells, but significant energy is wasted in the warming process

Engineering Contradiction:
Improvehydrogen temperatureVSAvoidenergy waste
Core Design Contradiction:
TemperatureVSLoss of energy

Solution Approach 1:

The patent converts the harmful thermal energy that would otherwise be wasted during hydrogen warming into useful work by employing a thermal engine (Stirling engine) to capture and utilize the temperature differential between the warming hydrogen and the environment, transforming energy loss into additional power generation

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

Solution Approach 2:

The system changes the temperature parameter of the hydrogen fuel from 20K to 300K in a controlled manner, utilizing the temperature gradient as a resource rather than a loss, and employs phase change (liquid to gas) as part of the energy extraction process

Inventive Principle:
Principle #35Parameter changes

2Device complexity

If excess thermal energy is dissipated during hydrogen warming, then the system operates simply, but energy efficiency deteriorates

Engineering Contradiction:
Improvesystem complexityVSAvoidenergy efficiency
Core Design Contradiction:
Device complexityVSUse of energy by moving object

Solution Approach 1:

The thermal engine serves multiple functions: it generates additional power during hydrogen warming, utilizes the temperature differential that would otherwise be wasted, and can potentially provide cooling during certain operational phases, making the system multi-functional without proportionally increasing complexity

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

3Power

If a thermal engine is added to capture thermal energy, then additional power is generated, but system complexity increases

Engineering Contradiction:
Improvepower generationVSAvoidsystem complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The patent merges the thermal engine with the existing hydrogen storage and fuel cell system, integrating the Stirling engine into the thermal management architecture so that components serve dual purposes: the heat exchanger既是 warming device又是 thermal engine heat source, reducing overall system complexity despite added power generation capability

Inventive Principle:
Principle #5Merging (Combining)

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 approach reduces overall power consumption and improves hydrogen-powered vehicle efficiency by utilizing thermal energy for additional onboard power generation and enhancing combustion efficiency through oxygen/nitrogen enrichment.

Implementation Method 1

a heat exchanger is configured to heat the first portion of the liquid insulation material via thermal energy exchange with a relatively warm fluid

Methodology Applied
Scientific EffectThermal energy exchange: Heat Exchanger

Implementation Method 2

a thermal engine is configured to expand the liquid insulation material into gaseous form via interaction between a heated first portion of the liquid insulation material and a second portion of the liquid insulation material

Methodology Applied
Scientific EffectPhase change: Phase Change

Implementation Method 3

The heated first portion of the liquid insulation material is directed through a turbine, where it expands and drives the turbine to generate mechanical power

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Implementation Method 4

an electrical generator is operably connected to the turbine to generate electrical power via rotation of the turbine

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 5

The fuel tank includes two or more vacuum insulation layers, and a liquid insulation material positioned between the two or more vacuum insulation layers

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS11845562B1Auxiliary power generation and cooling systems on liquid hydrogen fueled aircraft
Publication Date: 2023.12.19 HAMILTON SUNDSTRAND CORP
  • US11845562B1 patent drawing
  • US11845562B1 patent drawing
  • US11845562B1 patent drawing

AI summary

A power system includes a liquid hydrogen fuel source including a fuel tank containing a volume of hydrogen fuel. The fuel tank includes two or more vacuum insulation layers, and a liquid insulation material positioned between the two or more vacuum insulation layers. A first power generator located fluidly downstream of the hydrogen fuel source. The first power generator utilizes a flow of hydrogen fuel from the volume of hydrogen fuel to generate electrical or mechanical power.