Toroidal Multi-Stage Thermoacoustic Engine Layout for Compact Power Gain

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Solution Overview

Problem

Existing multi-stage thermoacoustic heat engines are thermally and mechanically cumbersome, volumetrically inefficient, and prone to high thermal stresses due to the repeated exposure of the gaseous working fluid's acoustic power path to common thermal interfaces, limiting their scalability and efficiency.

Innovation Solution

A multi-stage traveling wave thermoacoustic engine with a topologically folded acoustic power path that re- accesses the same thermal interfaces multiple times within a single domed pressure vessel, minimizing hot joints and improving manufacturing simplicity and reliability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If multiple heat engine stages are connected in series with common thermal interfaces, then the overall gain of the engine is increased, but the device becomes thermally and mechanically cumbersome with high thermal stresses

Engineering Contradiction:
Improveoverall gainVSAvoidthermal and mechanical complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The engine is divided into multiple discrete stages (first stage with first hot/cold heat exchangers, second stage with second hot/cold heat exchangers, etc.), where each stage operates independently with its own thermal interfaces. This segmentation allows the acoustic power to be processed through multiple stages without subjecting a common thermal interface to repeated exposure, thereby reducing thermal and mechanical complexity while maintaining increased overall gain.

Inventive Principle:
Principle #1Segmentation

2Power

If a folded loop topology is used to provide common thermal interface points, then multi-stage operation is achieved, but the device becomes very large and volumetrically inefficient

Engineering Contradiction:
Improvemulti-stage operationVSAvoiddevice volume
Core Design Contradiction:
PowerVSVolume of moving object

Solution Approach 1:

The patent transitions from a planar folded loop topology to a three-dimensional stacked configuration where stages are arranged vertically one above another. Each stage occupies a separate vertical level within the pressure vessel, allowing multiple stages to coexist in a compact volume without requiring the extensive horizontal spacing needed for folded loop topologies.

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

3Reliability

If stages are physically separated, then thermal stress is reduced, but volumetric efficiency and scalability are compromised

Engineering Contradiction:
Improvethermal stress resistanceVSAvoidvolumetric efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent employs a nested arrangement where multiple stages are stacked concentrically within the pressure vessel, with each stage containing its own thermal interfaces and acoustic processing components. This nesting allows stages to be physically separated for thermal stress reduction while maintaining compact volumetric efficiency through hierarchical spatial organization.

Inventive Principle:
Principle #7Nested doll (Nesting)

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 configuration enhances volumetric and thermal efficiency, improves scalability, and reduces thermal stresses, resulting in a more efficient and reliable power generation system.

Implementation Method 1

Thermal buffer tube 112 provides a thermal buffer between hot heat exchanger 110 and the cold side (114 and 116) by providing space for the heated helium gas to oscillate without reaching the cold side

Methodology Applied
Scientific EffectThermal buffer: Thermal Insulation

Implementation Method 2

A flow straightener and heat exchanger 114 suppress prevent certain types of gas flow and reduces heat loss thereby improving the thermal efficiency of the heat engine

Methodology Applied
Scientific EffectHeat exchanger: Heat Exchanger

Implementation Method 3

Jet pump 120 is used to reduce gas streaming and thereby improve thermal efficiency

Methodology Applied
Scientific EffectJet pump: Jet

Implementation Method 4

Applying heat at one end of the tube creates a heat differential along the length of the tube and induces sound waves which can be used to convert the heat into mechanical energy

Methodology Applied
Scientific EffectThermoacoustic effect: Thermoacoustic Effect

Data Source

PatentEP3701146B1Toroidal spiral cascading of multiple heat engine stages in traveling wave thermoacoustic engines
Publication Date: 2024.12.04 NORTHROP GRUMMAN SYSTEMS CORP
  • EP3701146B1 patent drawingFigure 1
  • EP3701146B1 patent drawingFigure 2
  • EP3701146B1 patent drawingFigure 3

AI summary

A multi-stage traveling wave thermoacoustic engine is disclosed. A plurality of heat engine stages are formed as a toroidal spiral cascade of N stages inside a pressure vessel. Each stage feeds into the next stage such that all of the thermoacoustic power cycles past a common set of thermal interfaces multiple times with the single domed pressure vessel. The inventive thermoacoustic engine is simpler and cheaper to manufacture and more reliable due to the minimization of hot joints.