Actively Cooled Thermal Shield for Helium Transport Container

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Solution Overview

Problem

Current transport containers for helium, which are thermally insulated to prevent pressure increase, have limited helium holding times due to inefficiencies in thermal management, leading to a need for improved insulation and cooling methods.

Innovation Solution

A transport container design featuring an inner container for helium, a coolant container with cryogenic liquid, and an actively cooled thermal shield with oblique cooling lines and a phase separator, ensuring optimal thermal insulation and extended helium storage duration.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Duration of action of moving object

If conventional thermal insulation with high-vacuum multi-layer insulation is used, then the insulation performance is adequate, but the helium holding time is limited to 35-40 days

Engineering Contradiction:
Improvehelium holding timeVSAvoidcooling system complexity
Core Design Contradiction:
Duration of action of moving objectVSDevice complexity

Solution Approach 1:

The thermal shield is pre-cooled with liquid nitrogen before helium loading, establishing a cold thermal barrier in advance that delays heat ingress to the helium container, thereby extending the holding time beyond the conventional 35-40 days

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

An actively cooled thermal shield serves as an intermediary component between the outer environment and the inner helium container, absorbing and managing heat flux to protect the helium from thermal intrusion and extend storage duration

Inventive Principle:
Principle #24Intermediary (Mediator)

2Stress or pressure

If the thermal shield is passively insulated, then the structure is simpler, but heat transfer through radiation and gas conduction increases pressure rise

Engineering Contradiction:
Improvepressure increase rateVSAvoidheat transfer
Core Design Contradiction:
Stress or pressureVSLoss of energy

Solution Approach 1:

The cooling lines are designed with inclined sections at specific angles (5-15 degrees) to optimize two-phase flow characteristics of the cryogenic liquid, enhancing heat removal efficiency and controlling the pressure increase rate in the helium container

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

Active cooling systems replace passive insulation mechanisms by using flowing cryogenic liquid through cooling lines to dynamically manage heat transfer, effectively reducing both radiative and conductive heat flux to the helium

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Reliability

If cooling lines are arranged horizontally, then installation is easier, but cryogenic liquid distribution and cooling efficiency are insufficient

Engineering Contradiction:
Improvecooling efficiencyVSAvoidcooling line installation
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The cooling lines incorporate inclined sections with specific angles (5-15 degrees) rather than horizontal or vertical orientations, creating asymmetric geometry that optimizes cryogenic liquid distribution and two-phase flow patterns for enhanced cooling reliability

Inventive Principle:
Principle #4Asymmetry

Solution Approach 2:

The cooling lines transition from simple horizontal or vertical arrangements to three-dimensional inclined configurations, adding angular dimensionality to optimize fluid dynamics and heat transfer efficiency while maintaining manufacturing feasibility

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

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 design significantly extends helium holding time to at least 45 days, with sufficient cryogenic liquid supply for 40 days, by minimizing heat transfer through radiation and residual gas conduction, while maintaining effective cooling.

Implementation Method 1

The thermal shield has at least one cooling line for active cooling, in which the cryogenic liquid can be received

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 2

The thermal insulation of the transport container consists of high-vacuum multi-layer insulation

Methodology Applied
Scientific EffectThermal radiation: Thermal Radiation

Implementation Method 3

The thermal insulation of the transport container consists of high-vacuum multi-layer insulation

Methodology Applied
Scientific EffectVacuum insulation: Vacuum

Implementation Method 4

the at least one cooling line has inclined sections and sections running in a direction of gravity, and wherein the inclined sections have a slope relative to a horizontal

Methodology Applied
Scientific EffectGravity: Gravitation

Data Source

PatentEP3452750B1Transport container
Publication Date: 2022.03.16 LINDE AG
  • EP3452750B1 patent drawingFigure 1
  • EP3452750B1 patent drawingFigure 2
  • EP3452750B1 patent drawingFigure 3

AI summary

The invention relates to a transport container (1) for helium (He), comprising an inner container (6) for receiving the helium (He), a coolant container (14) for receiving a cryogenic liquid (N2), an outer container (2) in which the inner container (6) and the coolant container (14) are received, and a thermal shield (21) which can be actively cooled with the aid of the cryogenic liquid (N2), the thermal shield (21) comprising a tubular base section (22) in which the inner container (6) is received, and a cover section (23, 24) that closes the base section (22) at the front and that is arranged between the inner container (6) and the coolant container (14), wherein an intermediate space (20) is provided between the inner container (6) and the coolant container (14) and said cover section (23, 24) of the thermal shield (21) is arranged in this space.