Duplex Coating for Aircraft Windows Resolving Wear and Transmittance Trade-offs

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Solution Overview

Problem

Aircraft acrylic windows face issues with erosion, crazing, and coating durability due to differential pressures, chemical exposure, and UV degradation, with existing sol-gel polysiloxane coatings offering limited durability and wear resistance.

Innovation Solution

A duplex coating scheme combining a polysiloxane adherent coating with a plasma CVD-based SiOxCy hard coating is applied to the acrylic substrate, enhancing adhesion, flexibility, and chemical resistance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Illumination intensity

If sol-gel polysiloxane coatings are applied to acrylic windows, then high transmittance is achieved, but durability against wear and UV degradation is limited

Engineering Contradiction:
Improvelight transmittanceVSAvoiddurability against wear and UV degradation
Core Design Contradiction:
Illumination intensityVSReliability

Solution Approach 1:

The patent applies a duplex coating system combining sol-gel polysiloxane coating (providing optical clarity and UV protection) with a plasma-enhanced siloxane coating (providing enhanced hardness and wear resistance). This composite structure allows the window to simultaneously achieve high light transmittance through the polysiloxane layer while gaining superior durability from the plasma coating layer, resolving the contradiction between optical performance and wear resistance.

Inventive Principle:
Principle #40Composite materials

2Adaptability or versatility

If differential pressure causes windows to flex, then the window adapts to pressure changes, but coatings crack and delaminate from the acrylic substrate

Engineering Contradiction:
Improveflexibility under pressureVSAvoidcoating integrity
Core Design Contradiction:
Adaptability or versatilityVSStability of the object's composition

Solution Approach 1:

The patent modifies the coating composition by incorporating specific siloxane crosslinking densities and using plasma treatment to create a more flexible yet durable coating structure. The plasma-enhanced siloxane coating has optimized crosslinking that allows it to flex with the acrylic substrate under differential pressure while maintaining coating integrity and preventing delamination, thus resolving the contradiction between adaptability and stability.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If acrylic windows are used due to light weight and flexibility, then ease of manufacture is improved, but susceptibility to particle erosion and water induced crazing increases

Engineering Contradiction:
Improveflexibility and formabilityVSAvoidparticle erosion and water induced crazing
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The patent introduces a duplex coating system as an intermediary protective layer between the acrylic substrate and the external environment. The plasma-enhanced siloxane coating acts as a mediator that provides resistance to particle erosion and water-induced crazing, while the underlying polysiloxane layer maintains compatibility with the acrylic substrate. This intermediary coating system protects the acrylic window from harmful factors while preserving the substrate's inherent flexibility and ease of manufacture.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 duplex coating significantly improves wear resistance, chemical resistance, and flexing-induced crazing resistance, maintaining optical quality and extending the lifespan of aircraft windows.

Implementation Method 1

a plasma CVD based coating containing silicon

Methodology Applied
Scientific EffectPlasma CVD: Plasma Enhanced Chemical Vapour Deposition

Data Source

PatentUS8313812B2Durable transparent coatings for aircraft passenger windows
Publication Date: 2012.11.20 THE BOEING CO
  • US8313812B2 patent drawing
  • US8313812B2 patent drawing
  • US8313812B2 patent drawing

AI summary

A duplex coating scheme and associated method of formation, which includes a siloxane based soft coating and a plasma based SiOxCy hard coating used in combination to improve the durability of acrylic substrates used in aircraft window applications.