Radially Cut Torus Spring Seal for Cryogenic Leakage Control

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Solution Overview

Problem

Seals used in extreme operating conditions, such as cryogenic temperatures, experience reduced contact pressure due to shrinkage or deformation, leading to increased leakage between components.

Innovation Solution

A seal design featuring a metallic annular spring with radially cut perforations disposed about the inner and/or outer diameter, maintaining contact pressure through a differential pressure profile.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a traditional seal is used at cryogenic temperatures, then the seal material remains flexible and sealable, but the seal shrinks or deforms significantly away from the hardware, reducing contact pressure

Engineering Contradiction:
Improvesealing functionVSAvoidcontact pressure
Core Design Contradiction:
ReliabilityVSStress or pressure

Solution Approach 1:

The seal is segmented into multiple functional zones including an enlarged shoulder portion, a body portion, and an O-ring groove. The radially-cut torus spring is also segmented into multiple independent segments that can deform independently. This segmentation allows different portions of the seal to perform different functions - the shoulder maintains positioning while the segmented spring compensates for shrinkage through independent deformation of each segment.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The radially-cut torus spring provides dynamic compensation for thermal shrinkage. As the seal contracts at cryogenic temperatures, the spring segments deform elastically to maintain constant contact pressure. The spring's dynamic elastic deformation allows it to adapt to dimensional changes in the seal and hardware, ensuring continuous sealing force despite temperature-induced shrinkage.

Inventive Principle:
Principle #15Dynamics

2Reliability

If the seal shrinks at cryogenic temperatures, then the seal material maintains its sealing properties, but the contact pressure between seal and hardware decreases, leading to increased leakage

Engineering Contradiction:
Improvesealing performanceVSAvoidleakage
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The radially-cut torus spring is pre-loaded during assembly to exert outward radial force on the seal before thermal shrinkage occurs. This preliminary compressive force counteracts the subsequent shrinkage effect, ensuring that when the seal contracts at cryogenic temperatures, the spring maintains adequate contact pressure. The pre-compression creates a force reserve that actively opposes the harmful shrinkage effect.

Inventive Principle:
Principle #9Preliminary anti-action

Solution Approach 2:

The spring's physical parameters - particularly its radial width, wall thickness, and segment geometry - are optimized to provide appropriate stiffness and force characteristics. By carefully selecting these parameters, the spring generates sufficient contact pressure to compensate for seal shrinkage while avoiding excessive force that could damage the seal or hardware. The parameter optimization ensures the spring's elastic deformation produces the desired compensating effect.

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

The seal maintains improved contact pressure and reliability at cryogenic temperatures, reducing leakage and enhancing sealing performance compared to traditional designs.

Implementation Method 1

a radially-cut torus spring which maintains a differential pressure profile between the metallic annular body of the spring and the radially cut perforations

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Data Source

PatentUS12510159B2Seal with radial cut torus spring
Publication Date: 2025.12.30 SAINT GOBAIN PERFORMANCE PLASTICS CORP
  • US12510159B2 patent drawing
  • US12510159B2 patent drawing
  • US12510159B2 patent drawing

AI summary

Systems and methods include providing a seal for an assembly. The seal includes a jacket having a base, an inner sealing leg, and an outer sealing leg, and further includes a spring disposed within the jacket between and in contact with the inner sealing leg and the outer sealing leg. The spring includes a metallic annular body comprising an inner diameter and an outer diameter, and a plurality of radially cut perforations disposed about at least one of the inner diameter and the outer diameter of the metallic annular body.