Fuel Isomerization for Aircraft Thermal Management

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

High-performance aircraft face thermal management challenges due to the need for cooling various systems and maintaining fuel tank temperature within design bounds, especially at high altitudes or ground operations, where existing methods like transferring waste heat to fuel become inefficient when the fuel tank temperature exceeds limits.

Innovation Solution

A system utilizing a heat source, an endothermic process module with a catalyst, and a fuel source to isomerize fuel, increasing its thermal carrying capacity without raising the fuel temperature, thereby enhancing the fuel's ability to absorb heat and manage thermal loads.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If waste heat is transferred to fuel in the fuel tank, then thermal management is improved, but fuel temperature exceeds design bounds

Engineering Contradiction:
Improvefuel tank temperatureVSAvoidthermal management effectiveness
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The patent applies parameter changes by isomerizing the fuel molecules, transforming them from a linear configuration to a branched configuration. This chemical structural change increases the fuel's thermal carrying capacity by approximately 30%, allowing the fuel to absorb more heat without exceeding temperature design bounds. The isomerization process fundamentally alters the fuel's thermal properties rather than simply adjusting operational parameters.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent utilizes an endothermic phase transition process where the fuel undergoes isomerization that absorbs thermal energy. The endothermic reaction absorbs heat from the fuel tank, effectively cooling the fuel while simultaneously increasing its thermal carrying capacity. This phase transition approach allows the system to manage thermal loads without raising fuel temperature.

Inventive Principle:
Principle #36Phase transitions

2Temperature

If fuel burning rate is increased to cool fuel tank, then thermal limits are maintained, but operational flexibility is reduced

Engineering Contradiction:
Improvefuel tank temperatureVSAvoidoperational flexibility
Core Design Contradiction:
TemperatureVSAdaptability or versatility

Solution Approach 1:

The patent implements self-service by enabling the fuel to cool itself through endothermic isomerization. The fuel tank system automatically absorbs excess heat through the isomerization process, eliminating the need for operational modifications such as increased fuel burning rates. The system self-regulates thermal management without requiring changes to flight operations or fuel consumption patterns.

Inventive Principle:
Principle #25Self-service

3Temperature

If thermal carrying capacity of fuel is increased through isomerization, then thermal management is improved, but device complexity increases

Engineering Contradiction:
Improvethermal carrying capacityVSAvoidendothermic process module
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent introduces an endothermic process module as an intermediary component that facilitates the isomerization process. This module contains the catalyst and provides the controlled environment needed for thermal carrying capacity enhancement. By concentrating the complexity in a dedicated, manageable module rather than distributing it throughout the entire fuel system, the overall device complexity is minimized while achieving the desired thermal management improvements.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 increases the thermal carrying capacity of fuel by up to 30%, allowing for improved thermal management and operational flexibility by absorbing waste heat without elevating fuel temperature, thus alleviating the need for frequent modifications in aircraft operations.

Implementation Method 1

The endothermic process module includes a catalyst that isomerizes fuel from the fuel source to increase the thermal carrying capacity of the fuel without raising the temperature of the fuel

Methodology Applied
Scientific EffectEndothermic reaction: Endothermic Reaction

Implementation Method 2

The endothermic process module includes a catalyst that isomerizes fuel from the fuel source

Methodology Applied
Scientific EffectCatalysis: Catalysis

Data Source

PatentUS8495880B2Thermal management using topological isomerization of fuel
Publication Date: 2013.07.30 LOCKHEED MARTIN CORP
  • US8495880B2 patent drawing
  • US8495880B2 patent drawing
  • US8495880B2 patent drawing

AI summary

Embodiments of a system are disclosed that include a heat source, an endothermic process module, and a fuel source configured to supply fuel to the endothermic process module and to receive isomerized fuel from the endothermic process module. A controller includes logic instructions operable to receive information regarding temperature of fuel received by the endothermic process module, and regulate application of heat from the heat source to the fuel at the endothermic process module. The endothermic process module includes a catalyst that increases the thermal carrying capacity of the fuel by isomerizing fuel from the fuel source.