Aircraft Transparent Wall Mounting for Bird-Strike Energy Absorption

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing aircraft transparent walls, such as windscreens or windows, are not efficiently designed to absorb the energy from bird strikes, leading to potential damage and the need for thicker, heavier structures to meet certification requirements.

Innovation Solution

Aircraft transparent walls are fixed to a supporting structure using a fixation system with martyr energy-absorbing pads that deform plastically to absorb impact energy, allowing for thinner and potentially lighter walls.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the transparent wall is made thicker to withstand bird strikes, then the strength and reliability are improved, but the weight increases

Engineering Contradiction:
ImprovestrengthVSAvoidweight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent introduces energy-absorbing pads as intermediary elements between the transparent wall and the supporting structure. These pads deform plastically during bird strikes to absorb impact energy, protecting the transparent wall from direct damage. This allows the use of thinner, lighter transparent walls while maintaining the required strength and reliability certification standards.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Weight of moving object

If the transparent wall is made thinner to reduce weight, then the weight is reduced, but the ability to withstand bird strikes deteriorates

Engineering Contradiction:
ImproveweightVSAvoidstrength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The patent implements energy-absorbing pads that are pre-installed between the transparent wall and the supporting structure. These pads are designed to deform plastically under impact loads, cushioning the transparent wall against bird strike forces before the wall can be damaged. This beforehand cushioning enables the use of thinner, lighter transparent walls while maintaining certification standards for bird strike resistance.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

3Device complexity

If conventional fixation methods (screws, glue) are used, then the device complexity is reduced, but the energy absorption capability deteriorates

Engineering Contradiction:
ImprovecomplexityVSAvoidenergy absorption
Core Design Contradiction:
Device complexityVSLoss of energy

Solution Approach 1:

The patent changes the mechanical parameters of the fixation system by replacing rigid connections (screws, glue) with plastically deformable energy-absorbing pads. These pads are designed with specific material properties and geometric configurations that enable controlled plastic deformation during impact, transforming the fixation system from a rigid structure into an energy-dissipating system. This parameter change allows the system to absorb bird strike energy while maintaining reasonable structural complexity.

Inventive Principle:
Principle #35Parameter changes

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 system effectively absorbs impact energy from bird strikes, enabling thinner and lighter transparent walls while meeting certification standards, with the pads being replaceable during maintenance.

Implementation Method 1

at least one martyr energy-absorbing pad configured to deform according to an irreversible plastic deformation

Methodology Applied
Scientific EffectPlastic deformation: Plasticity

Data Source

PatentUS20250388313A1Aircraft with a transparent wall fixed to a structure via a shock protection system
Publication Date: 2025.12.25 EUROCOPTER FRANCE SA
  • US20250388313A1 patent drawing
  • US20250388313A1 patent drawing
  • US20250388313A1 patent drawing

AI summary

An aircraft provided with a transparent wall interposed between an internal environment located in the aircraft and an external environment, the transparent wall being fixed to a supporting structure of the aircraft by a fixing system, the transparent wall having an internal face facing the internal environment and an external face facing the external environment. The fixing system comprises at least one martyr energy-absorbing pad, the energy-absorbing pad comprising at least one energy absorber connected to the transparent wall and to the supporting structure, the at least one energy absorber comprising an internal absorber attached against the internal face.