Systems and methods for radiant heat reflective aircraft evacuation systems

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Solution Overview

Problem

Current aircraft evacuation slide materials lack effective thermal management and flame retardancy, relying on chemical-based coatings that emit VOCs and require lengthy manufacturing processes.

Innovation Solution

A composite textile with a nylon fabric substrate, an inner polyurethane coating, and an outer heat reflective coating comprising nanofillers such as ceramic nanoparticles, carbon allotropes, graphene nanosheets, or nano metal particles, which improves thermal and mechanical properties, enabling hot air and RF welding without chemicals, and reduces manufacturing time.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If chemical-based coatings are used for thermal management and flame retardancy, then flame retardancy is improved, but VOC emissions increase and manufacturing time increases

Engineering Contradiction:
Improveflame retardancyVSAvoidVOC emissions
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The patent uses composite textile materials consisting of base fabric combined with polyurethane coatings containing dispersed aluminum particles. This composite structure provides flame retardancy through the aluminum particles that reflect thermal radiation, while avoiding harmful chemical coatings and VOC emissions entirely.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent replaces chemical-based flame retardant coatings with a physical/reflective mechanism using aluminum particles dispersed in polyurethane coating. The aluminum particles provide thermal management and flame retardancy through radiant heat reflection rather than chemical reactions, eliminating VOC emissions.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Reliability

If chemical-based coatings are used for thermal management, then flame retardancy is improved, but manufacturing time increases

Engineering Contradiction:
Improveflame retardancyVSAvoidmanufacturing time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent employs composite materials where aluminum particles are dispersed within polyurethane coating compounds that are integrated into the fabric structure. This composite approach provides flame retardancy as an inherent property of the material structure rather than requiring separate chemical coating applications, thereby reducing manufacturing time.

Inventive Principle:
Principle #40Composite materials

3Temperature

If radiant heat reflective coating is added to fabric substrate, then thermal radiant heat characteristics are improved, but device complexity increases

Engineering Contradiction:
Improvethermal radiant heat characteristicsVSAvoidcoating structure complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent merges the radiant heat reflective function with the structural fabric and polyurethane coating into a single integrated composite material. The aluminum particles are dispersed within the polyurethane coating that is already bonded to the fabric substrate, combining structural support, air retention, and thermal reflection functions in one unified structure rather than adding separate layers.

Inventive Principle:
Principle #5Merging (Combining)

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 enhances thermal radiant heat characteristics, mechanical properties, and flame retardancy, reducing VOC emissions and manufacturing time while supporting efficient welding techniques for aircraft evacuation slides.

Implementation Method 1

The outer coating may be a radiant heat reflective coating

Methodology Applied
Scientific EffectThermal radiation reflection: Reflection

Implementation Method 2

the outer heat reflective coating may comprise nanofillers

Methodology Applied
Scientific EffectThermal scattering: Scattering

Implementation Method 3

The inner coating may be an air retentive coating

Methodology Applied
Scientific EffectAir retention:

Data Source

PatentEP4253646A1Systems and methods for radiant heat reflective aircraft evacuation systems
Publication Date: 2023.10.04 GOODRICH CORP
  • EP4253646A1 patent drawingFigure 1
  • EP4253646A1 patent drawingFigure 2
  • EP4253646A1 patent drawingFigure 3

AI summary

An aircraft evacuation slide assembly may be comprised of a plurality of composite textiles (300). Each composite textile may comprise a fabric substrate (302), an inner polyurethane coating (304), and an outer heat reflective coating (306). The outer heat reflective coating may comprise nanofillers that improve polymer properties, such as mechanical, barrier, thermal, flame retardancy, and electrical properties. Moreover, the outer heat reflective coating may comprise nanofillers that enable hot air welding and radio frequency welding of the plurality composite textiles to form the aircraft evacuation slide assembly.