Material for inflatable safety products with high strength to weight ratio

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Solution Overview

Problem

Inflatable safety products for aircraft, such as evacuation slides and life rafts, face challenges with heavy materials that increase weight and compromise safety provisions, while lighter alternatives often fail to meet strength and heat resistance requirements set by Federal Aviation Administration (FAA) regulations.

Innovation Solution

Development of a low-weight, high-strength fabric or flexible composite material with a substrate weight of 3 ounces/yd² or less, featuring a tensile strength of at least 190 lbs/in and tear strength of 13 lbs/in, and radiant heat resistance of 180 seconds when exposed to 1.5 Btu/ft²-sec, utilizing materials like polyethylene (PE) or ultra-high molecular weight polyethylene (UHMWPE) with optional metallic layers for enhanced emissivity and heat management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If heavy fabric or flexible composite materials are used for inflatable safety products, then the mechanical strength and heat resistance requirements are met, but the weight of the safety provisions increases

Engineering Contradiction:
Improvemechanical strength and heat resistanceVSAvoidweight of safety provisions
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent changes the material parameters by using ultra-high molecular weight polyethylene (UHMWPE) with specific molecular weight (4.0 million to 10.0 million) and crystallinity (70% to 90%), achieving both high strength and low weight simultaneously

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent employs composite construction with UHMWPE substrate combined with thermoplastic polyurethane coating layers, creating a material that achieves both mechanical strength and weight reduction requirements

Inventive Principle:
Principle #40Composite materials

2Weight of moving object

If lighter substrate materials are used to reduce weight, then the weight of safety provisions decreases, but the mechanical strength and heat resistance may not meet FAA regulations

Engineering Contradiction:
Improveweight of safety provisionsVSAvoidmechanical strength and heat resistance
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The patent achieves weight reduction (3.0 to 8.0 ounces/yd²) while maintaining strength by precisely controlling UHMWPE molecular weight (4.0-10.0 million) and crystallinity (70%-90%), demonstrating that parameter optimization enables both lightness and strength

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The composite structure with UHMWPE substrate and thermoplastic polyurethane coating provides both the weight reduction and the mechanical strength/heat resistance needed to meet FAA regulations

Inventive Principle:
Principle #40Composite materials

3Temperature

If traditional coated fabrics are used to meet heat resistance requirements, then radiant heat resistance is achieved, but the weight and complexity of the material increases

Engineering Contradiction:
Improveradiant heat resistanceVSAvoidweight of material
Core Design Contradiction:
TemperatureVSWeight of moving object

Solution Approach 1:

The patent achieves radiant heat resistance (180 seconds at 1.5 Btu/ft²-sec) with reduced weight by optimizing the thermoplastic polyurethane coating thickness (0.5 to 2.0 mils) and formulation, rather than using heavier traditional fire-retardant coatings

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS12070930B2Material for inflatable safety products with high strength to weight ratio
Publication Date: 2024.08.27 AIR CRUISERS COMPANY LLC
  • US12070930B2 patent drawing
  • US12070930B2 patent drawing
  • US12070930B2 patent drawing

AI summary

An inflatable safety product may include a fabric or flexible composite material. The fabric or flexible composite material includes a low weight, high strength substrate. In certain embodiments, the fabric or flexible composite material has a tensile strength of at least 190 lbs/in and/or a tear strength of at least 13 lbs/in and/or a radiant heat resistance of at least 180 seconds, and a substrate weight of less than or equal to 3 ounces/yd2.