Composite Cryogenic Tank Liner Eliminates Metallic Weight

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Solution Overview

Problem

Existing cryogenic tanks face challenges due to materials not specifically designed for cryogenic conditions, leading to issues with aero-thermal heating, vibrational loads, and potential cracking and leakage during space launch and travel.

Innovation Solution

A cryogenic tank construction using a composite liner with a fiber-resin matrix and a filament-wound outer layer, eliminating the need for a metallic liner, which allows for weight savings and scalable manufacturing, and is adaptable to various environments.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a metallic liner is used in traditional composite over-wrapped vessels, then the tank can contain cryogenic fluids, but the weight increases and manufacturing complexity increases due to weld joints and tooling requirements

Engineering Contradiction:
Improveability to contain cryogenic fluidsVSAvoidtank weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent removes the metallic liner component from the traditional composite over-wrapped vessel construction. The inner liner function is replaced entirely by a composite material system consisting of a cryogenic-compatible resin matrix and fiber reinforcement, eliminating the need for metal parts and their associated weight and manufacturing complexity

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent uses a composite material system (fiber-reinforced polymer matrix) to replace the metallic liner. The composite inner liner is constructed using cryogenic-compatible resins and fibers that can withstand low temperatures, providing both containment and structural functionality without the weight penalty of metal

Inventive Principle:
Principle #40Composite materials

2Reliability

If a metallic liner is used in traditional composite over-wrapped vessels, then the tank can contain cryogenic fluids, but the manufacturing complexity and tooling requirements increase

Engineering Contradiction:
Improveability to contain cryogenic fluidsVSAvoidmanufacturing complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent removes the metallic liner component from the traditional composite over-wrapped vessel construction. The inner liner function is replaced entirely by a composite material system consisting of a cryogenic-compatible resin matrix and fiber reinforcement, eliminating the need for metal parts and their associated weight and manufacturing complexity

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent changes the material parameters by selecting resins and fibers specifically designed for cryogenic service. The resin matrix is chosen to remain ductile at low temperatures, and the fiber-reinforced composite structure is designed to maintain mechanical integrity across the temperature range, eliminating the need for metal while maintaining containment reliability

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If traditional materials are used in cryogenic tanks, then the materials are readily commercially available, but they are not specifically designed for cryogenic conditions leading to potential cracking and leakage

Engineering Contradiction:
Improvematerial availabilityVSAvoidresistance to cracking and leakage
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent changes the material parameters by selecting resins and fibers specifically designed for cryogenic service. The resin matrix is chosen to remain ductile at low temperatures, and the fiber-reinforced composite structure is designed to maintain mechanical integrity across the temperature range, eliminating the need for metal while maintaining containment reliability

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent uses a composite material system (fiber-reinforced polymer matrix) to replace the metallic liner. The composite inner liner is constructed using cryogenic-compatible resins and fibers that can withstand low temperatures, providing both containment and structural functionality without the weight penalty of metal

Inventive Principle:
Principle #40Composite materials

4Weight of moving object

If a composite liner is used instead of a metallic liner, then weight is reduced and manufacturing is simplified, but the material must be specifically designed for cryogenic conditions

Engineering Contradiction:
Improvetank weightVSAvoidmaterial adaptability to cryogenic conditions
Core Design Contradiction:
Weight of moving objectVSAdaptability or versatility

Solution Approach 1:

The patent changes the material parameters by selecting resins and fibers specifically designed for cryogenic service. The resin matrix is chosen to remain ductile at low temperatures, and the fiber-reinforced composite structure is designed to maintain mechanical integrity across the temperature range, eliminating the need for metal while maintaining containment reliability

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 solution provides a lightweight, high-pressure cryogenic tank that effectively contains fluids without cracking or leaking, offering superior performance in cryogenic conditions and reducing tooling costs and complexity.

Implementation Method 1

infusing the preform with a resin having high ductibility at low temperatures

Methodology Applied
Scientific EffectVacuum pressure infusion: Vacuum

Implementation Method 2

the infusing of the preform comprises a vacuum assisted resin transfer molding operation

Methodology Applied
Scientific EffectResin transfer molding:

Implementation Method 3

providing for curing of the inner layer and the outer layer

Methodology Applied
Scientific EffectCuring:

Data Source

PatentUS7867589B2Hybrid cryogenic tank construction and method of manufacture therefor
Publication Date: 2011.01.11 UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR NAT AERONAUTICS & SPACE ADMINISTRATION
  • US7867589B2 patent drawing
  • US7867589B2 patent drawing

AI summary

A lightweight, high-pressure cryogenic tank construction includes an inner layer comprising a matrix of fiber and resin suitable for cryogenic use. An outer layer in intimate contact with the inner layer provides support of the inner layer, and is made of resin composite. The tank is made by placing a fiber preform on a mandrel and infusing the preform with the resin. The infused preform is then encapsulated within the outer layer.