Aircraft Soundproofing Trim Panel With Decoupled Walls

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Aircrafts face challenges in achieving both acoustic insulation and mechanical strength in soundproofing trim panels, with existing solutions either being costly or resulting in panels with critical frequencies within the audible range, leading to compromised sound comfort and mechanical integrity.

Innovation Solution

A self-supporting trim panel design featuring a visible and invisible wall separated by a porous core, with connecting elements that decouple the walls to enhance mechanical strength while minimizing mass and manufacturing costs, using inexpensive materials and manufacturing techniques.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a panel uses composite materials with woven fibers to achieve sufficient rigidity and mechanical strength, then the panel can be self-supporting and meet aircraft certification regulations, but the manufacturing cost increases significantly

Engineering Contradiction:
Improvemechanical strengthVSAvoidmanufacturing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The patent employs a composite structure combining a polymer foam core with a thin polymer skin layer. This composite approach provides sufficient mechanical strength and rigidity while using less expensive materials and simpler manufacturing processes compared to traditional woven fiber composite panels. The foam core provides structural support and the thin skin provides surface integrity, achieving a cost-effective balance between performance and manufacturing complexity.

Inventive Principle:
Principle #40Composite materials

2Ease of manufacture

If a panel uses inexpensive polymer forming methods without woven fibers to reduce manufacturing cost, then the panel can be produced economically, but the panel mass increases and stiffness decreases

Engineering Contradiction:
Improvemanufacturing costVSAvoidpanel mass
Core Design Contradiction:
Ease of manufactureVSWeight of moving object

Solution Approach 1:

The patent uses a thin polymer skin (film) that is formed over or bonded to a lightweight foam core. This thin film approach provides the necessary surface integrity and aerodynamic smoothness while minimizing added mass. The foam core provides the primary structural support, allowing the thin skin to be much lighter than traditional solid polymer panels while maintaining stiffness through the composite action of the foam-skin system.

Inventive Principle:
Principle #30Flexible shells and thin films

3Strength

If a panel increases thickness to achieve self-supporting characteristics using inexpensive materials, then the panel gains mechanical strength, but the mass increases significantly

Engineering Contradiction:
Improvemechanical strengthVSAvoidpanel mass
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent segments the panel into two functional components: a foam core that provides structural support and rigidity, and a thin polymer skin that provides surface integrity and aerodynamic properties. This segmentation allows each component to be optimized independently - the foam core can be engineered for maximum stiffness-to-weight ratio while the thin skin minimizes mass. The combined structure achieves self-supporting characteristics without the excessive mass that would result from using a single thick polymer panel.

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 panel achieves effective acoustic insulation, particularly at high frequencies, while maintaining mechanical strength and reducing mass, thus optimizing sound comfort and manufacturing efficiency.

Implementation Method 1

a porous core arranged between the first wall and the second wall

Methodology Applied
Scientific EffectAcoustic absorption: Acoustic Absorption

Implementation Method 2

each connecting element having the function of separating the visible wall from the invisible wall and of mechanically linking the visible wall and the invisible wall by acoustically decoupling the visible wall and the invisible wall

Methodology Applied
Scientific EffectVibration decoupling: Damping

Data Source

PatentEP3043347B1Soundproofing trim panel, and aircraft
Publication Date: 2020.03.04 EUROCOPTER FRANCE SA
  • EP3043347B1 patent drawingFigure 1~2
  • EP3043347B1 patent drawingFigure 3
  • EP3043347B1 patent drawingFigure 4

AI summary

The present invention relates to a self-supporting, acoustically insulating panel (1) comprising a visible (3) non-self-supporting wall and an invisible (2) non-self-supporting wall facing a sound wave source (50). A porous core (20) is arranged between the visible wall (3) and the invisible wall (2), a plurality of connecting elements (5) each extending from the invisible wall (2) to the visible wall (3), each connecting element (5) passing through an orifice (21) of said core (20) and being connected to the visible wall (3) and the invisible wall (2), each connecting element (5) separating the visible wall (3) from the invisible wall (2) and mechanically linking the visible wall (3) and the invisible wall (2) while acoustically decoupling the visible wall (3) and the invisible wall (2).