Accelerator Cavity Cooling Rings for Low-Resistance Cryogenic Cooldown

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Conventional conduction cooling methods for accelerator cavities face issues with thermal contact resistance due to material shrinkage and oxide formation, leading to prolonged cooldown times and performance degradation from magnetic fields.

Innovation Solution

A conduction cooling system using niobium cooling rings and copper conduction links with specific connection assemblies, along with a thermal switch and forced convective gas flow, to maintain mechanical pressure and reduce thermal resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If aluminum links are used for conduction cooling, then thermal conductivity is high, but thermal contact resistance increases due to material shrinkage and oxide formation

Engineering Contradiction:
Improvecooldown timeVSAvoidthermal contact resistance
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The patent changes the material parameters of the conduction cooling link from aluminum to copper, exploiting copper's superior thermal conductivity and resistance to oxide formation. This parameter change resolves the contradiction by maintaining low thermal contact resistance while achieving fast cooldown times.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs composite material construction with copper conduction links combined with specific connection assemblies. This composite approach optimizes both thermal performance and mechanical reliability, resolving the contradiction between cooldown speed and thermal contact stability.

Inventive Principle:
Principle #40Composite materials

2Reliability

If pressure retention devices such as disc springs are used, then mechanical pressure is maintained, but magnetic fields are introduced causing performance degradation

Engineering Contradiction:
Improvemechanical pressure retentionVSAvoidmagnetic field interference
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent extracts and removes the harmful disc spring component from the system, replacing it with a magnetic-field-compatible pressure retention mechanism. This elimination of the harmful element resolves the contradiction by maintaining mechanical pressure without introducing magnetic interference.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent introduces an intermediary component that provides mechanical pressure retention without magnetic properties. This intermediary replaces the problematic disc spring, resolving the contradiction between pressure maintenance and magnetic field avoidance.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Facilitates faster cooldown times and reduces magnetic interference, enhancing the efficiency and reliability of accelerator cavities.

Implementation Method 1

selecting the materials in the at least one connection assembly to experience greater thermal contraction than the cooling ring and the conduction link when cooled

Methodology Applied
Scientific EffectThermal contraction: Thermal Contraction

Implementation Method 2

a circulator configured to force gas through the heat exchanger

Methodology Applied
Scientific EffectForced convection: Forced Convection

Implementation Method 3

The series of interconnected cooling tubes are connected to the cavity via one of brazing and welding

Methodology Applied
Scientific EffectHeat conduction: Conduction (thermal)

Data Source

PatentUS20260032850A1Forced convective gas cooling for accelerator cavities
Publication Date: 2026.01.29 FERMI FORWARD DISCOVERY GROUP LLC
  • US20260032850A1 patent drawing
  • US20260032850A1 patent drawing
  • US20260032850A1 patent drawing

AI summary

Methods and systems for bolted joint conduction cooling of accelerator cavities comprises a conduction cooling system. The conduction cooling system comprises mounting at least one cooling ring to a cavity and a conduction link joined to the cooling ring with at least one connection assembly. The materials in the at least one connection assembly can be selected to experience greater thermal contraction than the cooling ring and the conduction link when cooled. A fast conduction cooling system can comprise a cryocooler in thermal communication with a conduction cooling apparatus affixed to a cavity via a conduction path and a thermal switch in the conduction path between the cryocooler and the conduction cooling apparatus wherein a thermal conductance of the thermal switch decreases as a function of temperature.