Annular Plate-Fin Core Layout for Compact Aerospace Heat Exchange

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Solution Overview

Problem

Aerospace heat exchangers face challenges in achieving a compact design with sufficient fluid flow and efficient heat transfer due to space and weight constraints, limiting the effectiveness of heat exchange systems in mobile applications.

Innovation Solution

An annular plate-fin heat exchanger with a core structure that includes radial and circumferential flow channels separated by plates, providing a compact design suitable for aerospace applications, enhancing fluid flow and heat transfer efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If a compact design is implemented to meet space constraints, then the heat exchanger size is reduced, but the fluid flow capability and heat transfer efficiency deteriorate

Engineering Contradiction:
Improveheat exchanger sizeVSAvoidheat transfer efficiency
Core Design Contradiction:
Volume of moving objectVSProductivity

Solution Approach 1:

The patent transitions from conventional planar plate-fin heat exchanger designs to a three-dimensional annular configuration with radial and circumferential flow channels. This dimensional change allows the heat exchanger to achieve compact footprint while maintaining extensive heat transfer surface area through vertical stacking of fin layers and radial expansion of flow paths.

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

Solution Approach 2:

The heat exchanger core is segmented into multiple stacked layers with alternating fin configurations. Each layer contains radial flow channels separated by circumferential partitions, creating multiple parallel flow paths that increase fluid throughput capacity within the compact annular volume.

Inventive Principle:
Principle #1Segmentation

2Weight of moving object

If the heat exchanger size is reduced to meet weight constraints, then the overall weight is decreased, but the fluid flow capacity and heat exchange effectiveness deteriorate

Engineering Contradiction:
Improveheat exchanger weightVSAvoidfluid flow capacity
Core Design Contradiction:
Weight of moving objectVSProductivity

Solution Approach 1:

The heat exchanger employs thin-walled annular cores with optimized fin structures that provide sufficient structural strength while minimizing weight. The thin-film separating walls define the flow channels and maintain pressure differential effectiveness without adding significant weight to the compact design.

Inventive Principle:
Principle #30Flexible shells and thin films

3Productivity

If multiple fin layers are stacked to increase heat transfer area, then the heat transfer efficiency is improved, but the device complexity and manufacturing difficulty increase

Engineering Contradiction:
Improveheat transfer efficiencyVSAvoidstructure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

Multiple fin layers with different orientations (radial and circumferential) are merged into a single integrated annular core structure. The separating walls and fin configurations are combined in such a way that they simultaneously define multiple flow channels and maximize heat transfer surface area within the unified compact geometry.

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

The annular design increases fluid flow and improves heat transfer efficiency in aerospace applications, addressing the constraints of space and weight limitations while maintaining effective heat exchange.

Implementation Method 1

Thermal energy is transferred between the flow circuits

Methodology Applied
Scientific EffectHeat transfer: Conduction (thermal)

Implementation Method 2

Each flow circuit can carry a different temperature fluid, which can be gas, liquid, or two-phase. Thermal energy is transferred between the flow circuits

Methodology Applied
Scientific EffectConvection: Convection

Data Source

PatentUS20260036374A1Annular plate-fin heat exchanger
Publication Date: 2026.02.05 HAMILTON SUNDSTRAND CORP
  • US20260036374A1 patent drawing
  • US20260036374A1 patent drawing
  • US20260036374A1 patent drawing

AI summary

A heat exchanger includes an exhaust shell and an annular core contained within the exhaust shell. The annular core includes a first end, a second end opposite the first end, an outer diameter, and an inner diameter. The annular core further includes a first plurality of fins extending in a first direction between the inner diameter and the outer diameter in a first set of layers. The annular core further includes a second plurality of fins extending in a second direction between the inner diameter and the outer diameter in a second set of layers. The second plurality of fins further includes a first inlet manifold comprising a second inlet and a first outlet manifold comprising a second outlet. The annular core further includes a plurality of plates separating the first set of layers and the second set of layers.