Balloon Seal Stress Reduction via Load Sharing Member

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Solution Overview

Problem

Balloon catheters face high failure rates due to excessive hoop stress on the seal portion, particularly at high pressures, and in balloons with non-tapering shoulder geometries that lead to increased stress on adjacent seals.

Innovation Solution

The introduction of a load sharing member with a stepped or tapered geometry, using materials like expanded polytetrafluoroethylene (ePTFE) and structural reinforcements, to reduce stress on the seal portion by offsetting the outer and inner edges of the body and seal portions and incorporating less distensible materials or reinforcements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If high balloon pressures are used for medical treatments, then treatment effectiveness is improved, but seal stress increases leading to balloon failure

Engineering Contradiction:
Improveballoon pressureVSAvoidballoon seal durability
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The balloon is divided into distinct functional zones: a body portion made of distensible material for expansion, and a seal portion made of less distensible material for maintaining the seal. This segmentation allows the body to expand under high pressure while the seal maintains its integrity by resisting excessive deformation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different materials with different distensibility properties are used in different regions of the balloon. The body portion uses highly distensible material to accommodate high pressure expansion, while the seal portion uses less distensible material to maintain seal integrity under the same pressure conditions.

Inventive Principle:
Principle #3Local quality

2Ease of manufacture

If non-tapering shoulder geometry is used in balloons, then manufacturing is simplified, but seal stress increases due to vertical shoulder walls

Engineering Contradiction:
Improveballoon geometry fabricationVSAvoidseal stress
Core Design Contradiction:
Ease of manufactureVSStress or pressure

Solution Approach 1:

The shoulder region incorporates a tapered geometry that transitions from the body portion to the seal portion at an angle. This localized geometric modification in the shoulder region redistributes stress away from the seal while maintaining the overall simplicity of the balloon structure.

Inventive Principle:
Principle #3Local quality

3Adaptability or versatility

If distensible materials are used in shoulder regions, then balloon compliance is improved, but shoulder geometry becomes non-tapering increasing seal stress

Engineering Contradiction:
Improveballoon complianceVSAvoidseal stress
Core Design Contradiction:
Adaptability or versatilityVSStress or pressure

Solution Approach 1:

The shoulder region uses a tapered geometric configuration that maintains compliance through its angled transition while simultaneously reducing seal stress. The taper angle is specifically designed to allow material compliance while directing stresses away from the seal portion.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The balloon employs composite construction with different materials in different regions: distensible materials in the body for compliance, and less distensible materials in the seal portion for stress resistance. The shoulder region transitions between these materials to balance compliance and stress reduction.

Inventive Principle:
Principle #40Composite materials

Data Source

PatentEP2968859B1Balloon with seal stress reduction and method of production
Publication Date: 2021.10.13 WL GORE & ASSOC INC
  • EP2968859B1 patent drawingFigure 1~2A
  • EP2968859B1 patent drawingFigure 2B~2C
  • EP2968859B1 patent drawingFigure 3A~3C

AI summary

The present disclosure is directed toward devices, systems and method of production that reduce stress being exerted directly onto balloon seals (130) having a load sharing member (115) located at the shoulders (110) between the seals (130) and the body portion (120) of the balloon (100).