High Pressure Gas Container Reinforcement Layer

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Solution Overview

Problem

The existing methods for forming gas guide passages in high pressure gas containers, such as those used in fuel cell systems, require a large number of microspheres between the resin liner and the reinforcement layer, leading to increased manufacturing costs and time.

Innovation Solution

A high pressure gas container design featuring a resin liner, a reinforcement layer with an inner side reinforcement layer formed by stacked sections of a metal-reinforced tape with gas permeability, and an outer side reinforcement layer, where gas guide passages are formed between sections of the reinforcing member, allowing gas to be easily released through vent holes in the caps.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If microspheres are provided between the liner and the reinforcement layer to form gas guide passages, then gas leakage is prevented, but manufacturing cost and time increase

Engineering Contradiction:
Improvegas leakage preventionVSAvoidmanufacturing cost and time
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The invention extracts the gas guide passage formation function from the microsphere assembly process and integrates it into the reinforcement layer structure itself. The reinforcing members are designed with inherent spacing that creates gas guide passages, eliminating the need for separate microsphere placement while maintaining gas leakage prevention functionality.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The invention merges the structural reinforcement function with the gas guide passage function into a single integrated component. The reinforcement layer both strengthens the container and provides gas guide passages through its construction, combining multiple functions into one element to simplify manufacturing.

Inventive Principle:
Principle #5Merging (Combining)

2Reliability

If a considerable number of microspheres are used to form gas guide passages, then gas guide passages are effectively formed, but the operation requires time and effort

Engineering Contradiction:
Improvegas guide passage effectivenessVSAvoidmanufacturing efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The reinforcement layer structure automatically creates gas guide passages through its own construction. The spacing between reinforcing members inherently forms the passages without requiring external assembly operations, allowing the structure to serve its own gas guide function.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The gas guide passages are pre-formed as part of the reinforcement layer design before final assembly. The reinforcing members are positioned and secured in a way that automatically creates the necessary spacing for gas guide passages, eliminating the need for subsequent microsphere placement operations.

Inventive Principle:
Principle #10Preliminary action

3Ease of manufacture

If sections of reinforcing member are arranged alongside one another and stacked to form gas guide passages, then manufacturing is simplified, but structural integrity must be maintained

Engineering Contradiction:
Improvegas guide passage formation simplicityVSAvoidcontainer structural integrity
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

The invention uses composite material construction where multiple layers of reinforcing members are stacked and secured together. This creates both the gas guide passages through inter-layer spacing and maintains structural integrity through the composite nature of the reinforcement layer, combining strength with functionality.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The gas guide passages are formed in the radial dimension through spacing between reinforcing member layers, while the circumferential stacking maintains structural integrity. This dimensional approach allows passage formation without compromising the tangential strength of the container.

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

This design simplifies the formation of gas guide passages, reduces manufacturing costs, and enables efficient gas discharge while maintaining structural integrity and thermal management through the use of high thermal conductivity materials.

Implementation Method 1

the hydrogen gas permeates through the resin liner and leaks

Methodology Applied
Scientific EffectPermeation: Permeation

Implementation Method 2

the gas guide passages guide the hydrogen gas that has permeated through the liner to the exterior of the high pressure gas container

Methodology Applied
Scientific EffectDiffusion: Diffusion

Implementation Method 3

enables efficient gas discharge while maintaining structural integrity and thermal management through the use of high thermal conductivity materials

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Data Source

PatentUS11473727B2High pressure gas container
Publication Date: 2022.10.18 HONDA MOTOR CO LTD
  • US11473727B2 patent drawing
  • US11473727B2 patent drawing
  • US11473727B2 patent drawing

AI summary

In a high pressure gas container including a liner, a reinforcement layer, bosses (caps), and openings (vent holes), the reinforcement layer includes an inner side reinforcement layer that surrounds the liner, and an outer side reinforcement layer that surrounds the inner side reinforcement layer, gas guide passages that guide, to the openings (vent holes), a gas leaking from the liner are formed in the inner side reinforcement layer, and the gas guide passages are voids formed between sections of a reinforcing member by arranging alongside one another and stacking the sections of the reinforcing member along the liner.