Thin Disk Laser Cooling Barrier Sapphire

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Solution Overview

Problem

Existing thin disk lasers face degradation of the high reflectivity coating due to liquid cooling, with previous solutions like ion-beam sputtering and synthetic diamond coatings failing to provide long-term protection and thermal conductivity matching, especially over a wide range of coolant temperatures.

Innovation Solution

A thin disk laser assembly with a protective barrier material, such as crystalline sapphire, attached to the high-reflectivity coating, which matches the coefficient of thermal expansion and provides improved adhesion through an intermediate layer, ensuring effective thermal conductivity and durability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If liquid cooling is applied directly against the high reflectivity coating, then cooling effectiveness is improved, but the reflectivity performance of the coating degrades

Engineering Contradiction:
Improvecooling effectivenessVSAvoidreflectivity performance
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

A barrier layer is introduced as an intermediary between the liquid coolant and the high reflectivity coating. This barrier layer protects the coating from direct contact with the coolant while still allowing thermal energy to pass through, thus maintaining both cooling effectiveness and coating reflectivity performance.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If hard durable coatings are deposited by ion-beam sputtering, then protection against degradation is improved, but long-term protection is insufficient

Engineering Contradiction:
Improveprotection against degradationVSAvoidduration of protection
Core Design Contradiction:
ReliabilityVSDuration of action of stationary object

Solution Approach 1:

The solution uses a composite structure combining the high reflectivity coating with a barrier layer made of material such as crystalline sapphire or diamond-like carbon. This composite structure provides both the optical properties of the HR coating and the mechanical/chemical protection of the barrier material, achieving long-term durability.

Inventive Principle:
Principle #40Composite materials

3Reliability

If thick protective material such as CVD diamond is used, then protection against degradation is improved, but thermal conductivity and coefficient of thermal expansion matching deteriorate

Engineering Contradiction:
Improveprotection against degradationVSAvoidcoefficient of thermal expansion matching
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The invention selects barrier layer materials with specific physical parameters - particularly coefficient of thermal expansion and thermal conductivity - that closely match the substrate material. By changing the material parameters to match the substrate, the system achieves both protection and thermal stability over large temperature ranges.

Inventive Principle:
Principle #35Parameter changes

4Reliability

If barrier material is attached to prevent degradation, then protection against coolant degradation is improved, but adhesion to the HR layer deteriorates

Engineering Contradiction:
Improveprotection against coolant degradationVSAvoidadhesion to HR layer
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

An intermediate layer is introduced as a mediator between the barrier material and the high reflectivity coating. This intermediate layer provides a bonding interface that ensures strong adhesion between the barrier layer and the HR coating, while the barrier layer itself provides protection against coolant degradation.

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 solution effectively prevents degradation of the high reflectivity coating during liquid cooling, maintaining thermal conductivity and allowing operation over a large coolant temperature range, thereby enhancing the longevity and performance of thin disk lasers.

Implementation Method 1

a protective barrier material, such as crystalline sapphire, attached to the high-reflectivity coating, which matches the coefficient of thermal expansion and provides improved adhesion

Methodology Applied
Scientific EffectPhysical barrier protection: Physical Containment

Implementation Method 2

providing good thermal conductivity and the ability to operate over a large range of coolant temperatures

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Implementation Method 3

provides improved adhesion through an intermediate layer

Methodology Applied
Scientific EffectAdhesion: Adhesive

Data Source

PatentUS8379680B1Direct cooling of thin disk lasers
Publication Date: 2013.02.19 THE BOEING CO
  • US8379680B1 patent drawing
  • US8379680B1 patent drawing
  • US8379680B1 patent drawing

AI summary

The present embodiment provides a thin disk laser disk element having improved direct cooling through the use of a barrier material directly attached to the high reflectivity layer of the thin disk element. This barrier is needed due to noticeable degradation of the reflectivity of the thin disk element without the barrier material. A barrier material of sapphire (crystalline Al2O3) is preferable, given a desire to have adequate thermal conductivity through the barrier material, proper matching of the coefficient of thermal expansion with the other components of the thin disk, and to save monetary costs. In another preferred embodiment, an intermediate layer is interposed between the thin disk element and the barrier material to provide improved adhesion between the barrier material and the thin disk element. Preferred crystallographic orientations for sapphire barrier material are provided as well.