Perforated Heavy Layer Aircraft Insulation

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Solution Overview

Problem

Conventional aircraft insulation structures fail to effectively dampen low-frequency noises while maintaining thermal insulation and preventing condensation, as they often rely on heavy foils that act as vapor barriers and create resonant frequencies that reduce sound damping and allow water vapor accumulation.

Innovation Solution

A perforated heavy layer with an absorption layer on the cabin side, where the perforation ratio allows the layer to be transparent to sound below the double-wall frequency, preventing the formation of an oscillatory spring-mass system and maintaining water vapor transport, thus avoiding condensation and enhancing sound absorption.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If a heavy foil is used in the insulation structure to dampen low-frequency noises, then sound damping is improved, but water vapor transport is blocked causing condensation

Engineering Contradiction:
Improvelow-frequency noiseVSAvoidcondensation
Core Design Contradiction:
Object-affected harmful factorsVSObject-generated harmful factors

Solution Approach 1:

The heavy foil is designed with a porous structure that allows water vapor to pass through while maintaining its sound damping functionality. The pores enable vapor transport to prevent condensation, while the overall structure retains sufficient mass to dampen low-frequency noises effectively.

Inventive Principle:
Principle #31Porous materials

Solution Approach 2:

The insulation structure combines the heavy foil with porous absorption materials to create a composite system. This composite approach allows the heavy foil to provide sound damping while the porous materials facilitate vapor transport, resolving the contradiction between noise reduction and condensation prevention.

Inventive Principle:
Principle #40Composite materials

2Object-affected harmful factors

If a heavy foil is used to increase sound damping, then acoustic comfort is improved, but weight of the aircraft increases

Engineering Contradiction:
Improvenoise levelVSAvoidaircraft weight
Core Design Contradiction:
Object-affected harmful factorsVSWeight of moving object

Solution Approach 1:

Instead of uniformly distributing heavy material throughout the insulation structure, the heavy foil is applied selectively in specific areas where sound damping is most needed. This localized approach reduces overall weight while maintaining acoustic comfort in critical regions.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent combines heavy foil with lighter porous absorption materials to create a composite insulation structure. This allows the system to achieve effective sound damping with reduced overall weight compared to using solid heavy materials throughout.

Inventive Principle:
Principle #40Composite 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 solution effectively dampens low-frequency noises without increasing weight or causing condensation, while allowing the insulation to dry and maintaining thermal performance by preventing the heavy layer from acting as a vapor barrier and optimizing sound absorption with a porous material.

Implementation Method 1

the ratio of its perforated area is adapted in such a way that the heavy layer is essentially transparent to sound for frequencies below a double-wall frequency of the insulation structure

Methodology Applied
Scientific EffectSound wave transmission: Sound

Implementation Method 2

an absorption layer that is preferably arranged on the cabin side of the heavy layer

Methodology Applied
Scientific EffectSound absorption: Acoustic Absorption

Implementation Method 3

maintaining water vapor transport, thus avoiding condensation

Methodology Applied
Scientific EffectVapor transport: Permeation

Implementation Method 4

Insulation design for thermal and acoustic insulation of an aircraft

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS8327976B2Insulation design for thermal and acoustic insulation of an aircraft
Publication Date: 2012.12.11 AIRBUS OPERATIONS GMBH
  • US8327976B2 patent drawing
  • US8327976B2 patent drawing
  • US8327976B2 patent drawing

AI summary

The invention pertains to an insulation structure for thermally and acoustically insulating an aircraft that features at least one heavy layer, wherein the insulation structure according to the invention is characterized in that the insulation structure comprises an additional absorption layer, in that the heavy layer is perforated at least in certain areas, and in that the perforated area ratio of the heavy layer is adapted in such a way that the heavy layer is essentially transparent to sound for frequencies below a double-wall frequency of the insulation structure. This makes it possible to dampen sound with low frequencies below the double-wall frequency as effectively as possible.