Cryocooler Expansion Space Annular Structure for Lower Pressure Loss

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Solution Overview

Problem

Current cryocoolers, such as Gifford-McMahon cryocoolers, face limitations in refrigerating performance due to inefficiencies in heat exchange and pressure loss within the expansion space.

Innovation Solution

The design incorporates a displacer with annular protruding and recessed portions on the bottom surface of the expansion space, creating a multiplex structure that increases the heat exchange area and reduces pressure loss by optimizing the clearance between these features, allowing for improved heat transfer and gas flow.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If a conventional smooth bottom surface is used in the expansion space, then the device structure is simple, but the heat exchange area is insufficient and pressure loss is high

Engineering Contradiction:
Improverefrigerating performanceVSAvoidstructure complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The bottom surface of the expansion space is segmented into multiple annular protruding portions with different diameters, dividing the previously smooth surface into distinct functional zones. This segmentation increases the effective heat exchange area while maintaining a relatively simple overall structure that can be manufactured using conventional techniques.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention transitions from a two-dimensional smooth bottom surface to a three-dimensional structured surface with annular protrusions of varying diameters. This dimensional change creates additional heat exchange surfaces and optimizes gas flow paths, thereby improving heat exchange efficiency and reducing pressure loss without proportionally increasing structural complexity.

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

2Loss of energy

If the clearance between protruding portions is increased, then pressure loss is reduced, but heat exchange area is decreased

Engineering Contradiction:
Improvepressure lossVSAvoidheat exchange area
Core Design Contradiction:
Loss of energyVSArea of stationary object

Solution Approach 1:

The invention optimizes the clearance parameter between annular protruding portions to achieve a balance between pressure loss reduction and heat exchange area maintenance. By carefully controlling the dimensional parameters of the protrusions and their spacing, the design minimizes pressure loss while preserving sufficient heat exchange surface area for effective thermal transfer.

Inventive Principle:
Principle #35Parameter changes

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 the heat exchange efficiency between the working gas and the cooling stage, leading to improved refrigerating performance and reduced pressure losses, thereby increasing the overall efficiency of the cryocooler.

Implementation Method 1

using a high-pressure working gas supplied from a compression device, set up Simon expansion to give rise to cryogenic coldness

Methodology Applied
Scientific EffectSimon expansion: Joule-Thomson Effect

Implementation Method 2

a plurality of annular protruding portions provided on a bottom surface of the expansion space such as to form a multiplex structure

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS10274230B2Annular portions protruding from a displacer and expansion space of a cryocooler
Publication Date: 2019.04.30 SUMITOMO HEAVY IND LTD
  • US10274230B2 patent drawing
  • US10274230B2 patent drawing
  • US10274230B2 patent drawing

AI summary

In a cryocooler, a displacer includes an internal space, and a working gas flows through the internal space. A cylinder reciprocally accommodates the displacer, and an expansion space for the working gas is formed between the cylinder and a bottom portion of the displacer. A plurality of annular protruding portions are provided on a bottom surface of the expansion space such as to form a multiplex structure. A plurality of annular recessed portions are provided on the bottom portion of the displacer such as to receive the plurality of annular protruding portions.