AES Fireproof Insulation Laminate With FRP and Cork Rigidity

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Current fire protection solutions for aircraft, such as thermal blankets and materials with porous charred layers, are either expensive and heavy, lack rigidity, or fail under vibration, and conventional fire-resistant materials like titanium are costly and require replacement post-fire.

Innovation Solution

A fireproof and thermal insulation laminate combining alkaline Earth Silicate (AES) material with a liquid barrier film, Fiber Reinforcement Plastic (FRP) layer, and cork, which provides low-cost, lightweight, and environmentally friendly protection with enhanced rigidity, suitable for structural integration and maintaining insulation under high temperatures.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If thermal blankets made of ceramic or silicone laminates with aluminum sheet are used, then flame penetration suppression and thermal insulation are improved, but weight and cost increase, and rigidity is lost causing collapse during manufacturing or assembly

Engineering Contradiction:
Improveflame penetration suppressionVSAvoidweight
Core Design Contradiction:
ReliabilityVSWeight of stationary object

Solution Approach 1:

The patent uses a composite structure consisting of a fire-resistant core material (such as ceramic matrix composite or refractory concrete) combined with a rigid outer shell (such as metal or composite panel). This composite design provides both flame penetration suppression and rigidity, while the rigid shell prevents collapse during manufacturing and assembly, unlike flexible thermal blankets

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent applies a thin fire-resistant coating or liner (such as intumescent coating or fire-resistant membrane) on the inner surface of the rigid structure. This thin film provides flame penetration suppression and thermal insulation without adding significant weight, while the underlying rigid structure maintains structural integrity and prevents collapse

Inventive Principle:
Principle #30Flexible shells and thin films

2Reliability

If materials creating porous charred layer are used, then flame penetration prevention and insulation are improved, but protection is lost under vibration conditions

Engineering Contradiction:
Improveflame penetration preventionVSAvoidprotection stability under vibration
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The patent combines a rigid fire-resistant material (such as ceramic matrix composite, refractory concrete, or metal alloy) with a porous insulating material (such as ceramic foam or intumescent coating). The rigid component maintains structural stability and protection under vibration, while the porous material provides flame penetration prevention and thermal insulation

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent applies different materials with different properties to different parts of the structure: a rigid, vibration-resistant fire-resistant material is used in areas subject to vibration, while porous insulating materials are used in areas where vibration is minimal. This localized approach ensures both flame penetration prevention and stability under vibration conditions

Inventive Principle:
Principle #3Local quality

3Reliability

If fire-resistant materials like titanium, steel or Inconel are used instead of conventional materials, then fire penetration suppression is improved, but cost increases and replacement is required after fire event

Engineering Contradiction:
Improvefire penetration suppressionVSAvoidcost and replaceability
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent uses a composite structure where a relatively thin fire-resistant barrier (such as ceramic matrix composite or refractory lining) is combined with a structural support system. This approach provides fire penetration suppression comparable to titanium or steel but at lower cost, and the modular design allows for easier replacement after fire events without replacing entire structural components

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The patent divides the fire protection system into separate modular components: a replaceable fire-resistant liner or barrier, and a permanent structural support framework. This segmentation allows the fire-resistant component to be replaced after a fire event without replacing the entire structure, reducing overall cost and simplifying maintenance

Inventive Principle:
Principle #1Segmentation

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 laminate effectively prevents flame penetration and provides thermal insulation, maintaining structural integrity and reducing the need for post-fire replacements, while being cost-effective and environmentally friendly, with embodiments tested to meet stringent fire protection regulations.

Implementation Method 1

A fireproof and thermal insulation laminate has been invented and is disclosed herein that may be embodied to provide a product that is fireproof and has also good thermal insulation capability

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Implementation Method 2

a liquid barrier film, an FRP (Fiber Reinforcement Plastic) layer and cork

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Implementation Method 3

a liquid barrier film, an FRP (Fiber Reinforcement Plastic) layer and cork, wherein the liquid barrier film and the FRP layer are staked to the AES material

Methodology Applied
Scientific EffectBarrier protection:

Implementation Method 4

a liquid barrier film, an FRP (Fiber Reinforcement Plastic) layer and cork, wherein the liquid barrier film and the FRP layer are staked to the AES material

Methodology Applied
Scientific EffectComposite material strength: Composite Materials

Data Source

PatentUS11845531B2Fireproof and thermal insulator product
Publication Date: 2023.12.19 AIRBUS OPERATIONS SL
  • US11845531B2 patent drawing
  • US11845531B2 patent drawing
  • US11845531B2 patent drawing

AI summary

A fireproof and thermal insulator product (1) including an Alkaline Earth Silicate (AES) material (2), and at least one of the following: a liquid barrier film (5), an FRP (Fiber Reinforcement Plastic) layer (4), cork (3), wherein the liquid barrier film (5) and the FRP layer (4) are staked onto the AES material (2), and wherein the cork (3) material is also staked onto the AES material (2) or embedded into said AES material (2) in where said cork (3) is configured as a plurality of strips performing a grid structure infilled with the AES material (2).