Microtube Heat Exchanger Array for Compact Aerospace Cooling

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Solution Overview

Problem

Aerospace applications require more efficient and compact heat exchangers to manage increasing thermal loads and smaller size requirements in environmental control systems, as traditional heat exchangers are limited by efficiency and size constraints.

Innovation Solution

The use of microtube heat exchangers, comprising an array of microtubes with specific geometries and arrangements, to enhance heat transfer efficiency by replacing traditional heat exchangers, allowing for improved heat exchange in aerospace systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If traditional heat exchangers are used, then system reliability is maintained, but heat exchange efficiency is insufficient and size requirements cannot be met

Engineering Contradiction:
Improveheat exchange efficiencyVSAvoidheat exchanger size
Core Design Contradiction:
ProductivityVSVolume of stationary object

Solution Approach 1:

The heat exchanger is divided into multiple microtubes arranged in an array, where each microtube functions as an independent heat transfer unit. This segmentation increases the total heat transfer surface area within a compact volume, thereby improving heat exchange efficiency while reducing overall system size. The microtubes are arranged in rows and columns to maximize surface area utilization.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from traditional macro-scale heat exchanger design to micro-scale tube design, utilizing dimensional scaling to increase surface area to volume ratio. The microtubes with diameters in the range of 0.005 to 0.05 inches provide enhanced heat transfer surface area within a compact footprint, effectively addressing both efficiency and size requirements.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Volume of stationary object

If heat exchanger size is reduced to meet aerospace requirements, then system compactness is improved, but heat exchange efficiency decreases

Engineering Contradiction:
Improveheat exchanger sizeVSAvoidheat exchange efficiency
Core Design Contradiction:
Volume of stationary objectVSProductivity

Solution Approach 1:

The microtubes are designed with specific local characteristics including optimized diameters (0.005 to 0.05 inches), wall thicknesses, and spacing arrangements that maximize heat transfer efficiency within each individual tube. The local geometry of each microtube is optimized to provide high surface area to volume ratio, enabling efficient heat exchange in compact configurations.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent employs parameter optimization by varying microtube diameter, length, wall thickness, and spacing to achieve optimal heat exchange performance. By carefully selecting and adjusting these parameters, the system achieves high heat exchange efficiency while maintaining a compact overall size, resolving the contradiction between size reduction and efficiency maintenance.

Inventive Principle:
Principle #35Parameter changes

3Productivity

If microtube heat exchangers are implemented, then heat exchange efficiency and system compactness are improved, but manufacturing complexity increases

Engineering Contradiction:
Improveheat exchange efficiencyVSAvoidmanufacturing complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

Multiple microtubes are merged into a single heat exchanger assembly that functions as an integrated unit. The microtubes are arranged in a structured array and connected through common inlet and outlet manifolds, creating a unified heat exchange system. This merging approach maintains manufacturing feasibility while achieving the performance benefits of micro-scale heat transfer.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The microtube heat exchanger design provides multi-functionality by serving various aerospace applications including environmental control systems, engine cooling, hydraulic cooling, and avionics cooling. The universal design approach allows the same basic microtube structure to be adapted for different thermal management requirements, reducing overall manufacturing complexity through standardization.

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

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

Microtube heat exchangers increase heat exchange efficiency, reduce component size and weight, and decrease demand on compressors and pumps, leading to more compact and efficient systems.

Implementation Method 1

The use of microtube heat exchangers, comprising an array of microtubes with specific geometries and arrangements, to enhance heat transfer efficiency

Methodology Applied
Scientific EffectHeat transfer: Conduction (thermal)

Implementation Method 2

Microtube heat exchangers increase heat exchange efficiency, reduce component size and weight

Methodology Applied
Scientific EffectConvection: Convection

Data Source

PatentUS20250383155A1Microtube heat exchanger devices, systems, and methods
Publication Date: 2025.12.18 INTERGALACTIC SPACEWORX LLC
  • US20250383155A1 patent drawing
  • US20250383155A1 patent drawing
  • US20250383155A1 patent drawing

AI summary

A microtube heat exchanger is disclosed for an aerospace system including two end plates with an array of holes or openings and an array of microtubes disposed in the array of openings between the two end plates. The heat exchanger can be used in environmental control systems, including systems for aerospace applications.