Composite Laminate for Aircraft Thermal Insulation

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Solution Overview

Problem

There is a need for thermal and acoustic blankets for aircraft structures that have reduced weight and improved resistance to flame spread, as existing solutions do not adequately address these requirements.

Innovation Solution

A composite laminate comprising a polymeric film layer capable of withstanding 200°C for at least 10 minutes, an adhesive layer with a specific areal weight and activation temperature range, and an inorganic refractory layer with a high percentage of platelets, which provides mechanical strength and acts as a flame and hot gas impermeable barrier.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If existing thermal and acoustic blanket solutions are used, then basic insulation function is provided, but weight is excessive and flame spread resistance is insufficient

Engineering Contradiction:
Improveflame spread resistanceVSAvoidblanket weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent employs a composite laminate structure combining organic polymer layers with inorganic refractory platelet layers. The refractory platelets (such as vermiculite, mica, or alumina) are dispersed within the polymer matrix to create a material that leverages both the flexibility and bonding capability of polymers and the fire resistance and thermal insulation of inorganic refractories. This composite approach enables flame spread resistance without requiring excessive weight, as the refractory platelets provide fire protection at relatively low concentrations within the polymer structure.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The invention incorporates flame retardant additives and refractory platelets specifically within the polymer layers at controlled concentrations and distributions. Rather than making the entire blanket structure heavy and fire-resistant, the fire-resistant properties are localized to specific layers and regions where they are most needed for flame spread prevention. This localized enhancement allows weight reduction in non-critical areas while maintaining adequate flame resistance where required.

Inventive Principle:
Principle #3Local quality

2Temperature

If existing thermal and acoustic blanket solutions are used, then basic insulation function is provided, but thermal insulation performance is insufficient

Engineering Contradiction:
Improvethermal insulation performanceVSAvoidblanket weight
Core Design Contradiction:
TemperatureVSWeight of moving object

Solution Approach 1:

The composite laminate structure combines organic polymer layers with inorganic refractory platelet layers to achieve superior thermal insulation. The refractory platelets (vermiculite, mica, alumina) inherently possess high thermal resistance and low thermal conductivity. When dispersed within the polymer matrix, they create tortuous heat flow paths and reduce thermal conduction through the material. This composite approach provides enhanced thermal insulation performance without proportionally increasing weight, as the refractory platelets contribute both thermal resistance and structural integrity.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The refractory platelet-containing polymer layers create a microstructure with inherent porosity and air pockets between the platelets and polymer chains. Air is a poor thermal conductor, and these trapped air pockets significantly reduce heat transfer through the blanket material. The platelet structure itself creates a tortuous path for heat flow, further enhancing thermal insulation. This porous microstructure achieves high thermal resistance at low material density, improving insulation performance without adding excessive weight.

Inventive Principle:
Principle #31Porous materials

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 composite laminate effectively resists flame propagation and provides improved thermal insulation while maintaining mechanical integrity, making it suitable for use in aircraft and other applications where flame resistance is critical.

Implementation Method 1

an inorganic refractory layer with a high percentage of platelets, which provides mechanical strength and acts as a flame and hot gas impermeable barrier

Methodology Applied
Scientific EffectFlame barrier:

Implementation Method 2

a polymeric film layer capable of withstanding a temperature of at least 200 C for at least 10 min

Methodology Applied
Scientific EffectThermal resistance:

Implementation Method 3

an adhesive layer having an areal weight of from 2 to 40 gsm capable of activation at a temperature of from 75 to 200 degrees C.

Methodology Applied
Scientific EffectAdhesive bonding: Adhesive

Data Source

PatentUS9238505B2Composite laminate for a thermal and acoustic insulation blanket
Publication Date: 2016.01.19 DUPONT SAFETY & CONSTRUCTION INC
  • US9238505B2 patent drawing
  • US9238505B2 patent drawing

AI summary

A multilayer laminate comprising in order, a polymeric film layer capable of withstanding a temperature of at least 200 C for at least 10 min, an adhesive layer having an areal weight of from 2 to 40 gsm capable of activation at a temperature of from 75 to 200 degrees C. and an inorganic refractory layer wherein the refractory layer comprises platelets in an amount at least 85% by weight with a dry areal weight of 15 to 50 gsm and has a residual moisture content of no greater than 10 percent by weight.