Mirror with increased form stability and longevity and a method of fabricating the same

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Solution Overview

Problem

Mirrors used in open air conditions, such as those for telescopes, suffer from rapid wear due to harsh weather conditions, leading to significant loss of reflectivity over time, necessitating frequent replacement or costly maintenance.

Innovation Solution

A mirror design featuring a carrier with a reflecting layer and a transparent protective layer, where the carrier can be made from materials with low density, porous, or honeycomb structures, and the reflective layer is applied using techniques like evaporation or sputtering, with additional layers for enhanced durability and protection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If mirrors are used in open air conditions for telescopes, then the telescopes can operate in harsh environments, but the mirrors wear rapidly and lose reflectivity within 3-4 years

Engineering Contradiction:
Improveoperation in open air conditionsVSAvoidreflectivity maintenance
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The mirror assembly uses a composite structure combining a lightweight carrier (made from materials with density 0.1-1.0 g/cm³, porous materials, or carbon fiber structures) with a transparent protective layer and reflective layer. This composite design provides both the mechanical support needed for harsh environment operation and the protective properties to maintain reflectivity over time.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

A transparent protective layer is applied over the reflective layer to protect it from environmental damage while maintaining optical performance. This thin film structure shields the reflective surface from harsh weather conditions (sand, moisture, temperature variations) without significantly affecting light reflection, thereby extending the operational life and maintaining reflectivity in open air conditions.

Inventive Principle:
Principle #30Flexible shells and thin films

2Reliability

If mirrors are replaced frequently due to wear, then operational reliability is maintained, but costs and time for production, transport, and installation increase significantly

Engineering Contradiction:
Improveoperational reliabilityVSAvoidtime for replacement operations
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The transparent protective layer is applied in advance to the reflective layer during manufacturing, creating a pre-protected mirror assembly. This preliminary protective measure prevents environmental damage before it occurs, eliminating the need for frequent replacements and reducing maintenance time and costs over the mirror's operational life.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The transparent protective layer acts as a cushioning barrier against environmental hazards (sand particles, moisture, UV radiation) before they can damage the reflective surface. This prior protection prevents wear and reflectivity loss, ensuring long-term operational reliability without requiring frequent interventions for replacement or maintenance.

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

3Strength

If heavy materials are used for the mirror carrier, then structural strength is improved, but the overall weight and complexity of the telescope array increases

Engineering Contradiction:
Improvecarrier structural strengthVSAvoidmirror assembly weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The carrier is constructed from porous materials or materials with closed-cell structures that provide high strength-to-weight ratios. These porous structures maintain the necessary mechanical strength to support the reflective and protective layers while significantly reducing the overall weight compared to solid dense materials, making the mirror assembly lighter and easier to install and maintain.

Inventive Principle:
Principle #31Porous materials

Solution Approach 2:

The patent specifies using materials with density in the range of 0.1-1.0 g/cm³, which is a significant reduction from traditional dense materials. This parameter change in material density achieves the dual goal of maintaining sufficient structural strength for the carrier while dramatically reducing the weight of the mirror assembly, benefiting large telescope arrays.

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 solution extends the longevity of mirrors by providing a durable and protective structure that maintains reflectivity, reducing the need for frequent replacements and lowering operational costs for large arrays like the Cherenkov Telescope Array.

Implementation Method 1

the reflective layer is applied using techniques like evaporation or sputtering

Methodology Applied
Scientific EffectEvaporation: Evaporation

Implementation Method 2

the reflective layer is applied using techniques like evaporation or sputtering

Methodology Applied
Scientific EffectSputtering: Sputtering

Data Source

PatentUS11550082B2Mirror with increased form stability and longevity and a method of fabricating the same
Publication Date: 2023.01.10 MEDIA LARIO SRL
  • US11550082B2 patent drawing
  • US11550082B2 patent drawing
  • US11550082B2 patent drawing

AI summary

A mirror includes a carrier, a reflecting layer disposed above a main face of the carrier, and a transparent layer disposed above the reflective layer. The carrier includes a base body, and the base body includes one or more of a material comprising a density in a range from 0.1 to 1.0 g/cm3, a porous material, a foamed material, a material comprising a structure containing closed cells, a material comprising a honeycomb structure, or a structure containing carbon fibers.