Low-Modulus Epoxy Coating for Laminar Flow and Insect Adhesion

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Solution Overview

Problem

Existing aerodynamic surfaces face issues with insect residue and ice buildup, which disrupt laminar flow and increase aerodynamic drag, despite surface treatments like laser ablation, as these surfaces remain rough and interfere with airflow.

Innovation Solution

The method involves creating a subsurface topography using laser ablation micro-machining and coating with an epoxy-based resin to achieve a smooth aerodynamic surface that reduces adhesion and ice buildup, utilizing differential interfacial stresses to promote durotaxis and maintain laminar flow by forming a treated substrate surface with controlled roughness and a low-modulus epoxy layer.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If laser ablation is used to modify surface energy to reduce insect residue buildup, then adhesion resistance is improved, but surface roughness increases which disrupts laminar flow

Engineering Contradiction:
Improveinsect residue adhesionVSAvoidsurface roughness
Core Design Contradiction:
Object-affected harmful factorsVSShape

Solution Approach 1:

The invention separates the surface into two distinct layers: a rough subsurface layer created by laser ablation that provides adhesion resistance, and a smooth coating layer applied over it that maintains laminar flow. This segmentation allows each layer to perform its specific function without compromising the other.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The invention transitions from modifying only the surface topology (2D) to creating a multi-layer structure with distinct functional layers (3D). The rough subsurface is covered by a smooth coating, adding a dimensional layer that resolves the contradiction between roughness for adhesion resistance and smoothness for flow maintenance.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Reliability

If a rough ablated surface is used to reduce insect residue adhesion, then biological contamination resistance is improved, but aerodynamic flow is worsened due to surface roughness

Engineering Contradiction:
Improvebiological contamination resistanceVSAvoidaerodynamic drag
Core Design Contradiction:
ReliabilityVSObject-generated harmful factors

Solution Approach 1:

The aerodynamic surface is segmented into a rough subsurface layer for biological contamination resistance and a smooth flow-maintaining coating layer. This segmentation allows the rough surface to provide adhesion resistance while the smooth coating minimizes aerodynamic drag.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The smooth coating acts as an intermediary layer between the rough ablated subsurface and the airflow. It mediates the interaction by providing a smooth interface for laminar flow while the rough subsurface underneath provides the adhesion resistance properties.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Object-generated harmful factors

If a smooth surface is maintained for laminar flow, then aerodynamic drag is reduced, but insect residue and ice buildup adhesion is increased

Engineering Contradiction:
Improveaerodynamic dragVSAvoidbiological contamination adhesion
Core Design Contradiction:
Object-generated harmful factorsVSObject-affected harmful factors

Solution Approach 1:

The surface is divided into functional layers where the smooth outer coating reduces aerodynamic drag while the rough subsurface layer provides adhesion resistance. Each layer performs its designated function without compromising the other.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the surface structure have different properties: the outer coating layer has smooth properties for flow maintenance, while the subsurface layer has rough properties for adhesion resistance. This local differentiation of qualities resolves the contradiction.

Inventive Principle:
Principle #3Local quality

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

This approach effectively reduces insect residue adhesion and ice accumulation, maintaining laminar flow and minimizing aerodynamic drag by creating a smooth, low-modulus epoxy surface that deforms under impact, enhancing the durability and efficiency of aerodynamic surfaces in extreme environments.

Implementation Method 1

at least a selected portion of a surface of a substrate material is ablated utilizing a laser to form a treated substrate surface

Methodology Applied
Scientific EffectLaser ablation: Laser Ablation

Implementation Method 2

The solid layer of epoxy has a lower modulus of elasticity than the substrate material to provide durotaxis when an insect impacts the solid layer of epoxy material to thereby reduce adhesion of insect residue

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Data Source

PatentUS10501840B2Influence on surface interactions by substructure topography
Publication Date: 2019.12.10 UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR NAT AERONAUTICS & SPACE ADMINISTRATION
  • US10501840B2 patent drawing
  • US10501840B2 patent drawing
  • US10501840B2 patent drawing

AI summary

A method of forming a smooth aerodynamic surface that permits laminar flow of air over the smooth aerodynamic surface. Selected portions of a surface of a substrate material are ablated utilizing a laser to form a treated substrate surface having a predefined roughness. The treated substrate surface is coated to form a solid layer of material having a smooth aerodynamic surface that promotes laminar flow. The solid layer of material has a lower modulus of elasticity than the substrate material to provide durotaxis when an insect impacts the solid layer of epoxy material to thereby reduce adhesion of insect residue or other matter to the smooth aerodynamic surface.