Additive Mirror Core Bonded to ULE Faceplate

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Solution Overview

Problem

Current methods for manufacturing large lightweight mirrors for telescopes are time-consuming and costly, with traditional abrasive water jetting and precision machining resulting in long cycle times and high material wastage, while advanced ceramics and carbon composites face issues with thermal and hygroscopic stability.

Innovation Solution

The use of additive processes like 3D printing to create mirror cores, which are then bonded to faceplates using replication technology, allowing for the deposition of layers of core materials to form a structure with optimized properties such as low thermal expansion and high stiffness, reducing weight and manufacturing time and cost.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If traditional abrasive water jetting or precision machining is used to manufacture mirrors, then manufacturing precision can be achieved, but manufacturing time increases to 2-4 years and material wastage reaches 95%

Engineering Contradiction:
Improvemirror surface precisionVSAvoidmanufacturing cycle time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The mirror core structure is designed and prepared in advance with optimized topology and material distribution before the actual mirror assembly is constructed. This preliminary structuring allows the final mirror to achieve precise optical surfaces much faster than traditional machining approaches.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention changes the manufacturing approach from subtractive (machining) to additive (layer-by-layer construction), fundamentally altering the production parameters. This enables mirrors to be built up layer by layer with precise control over material placement, achieving both high precision and reduced manufacturing time.

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If traditional abrasive water jetting or precision machining is used to manufacture mirrors, then manufacturing precision can be achieved, but material wastage increases to 95%

Engineering Contradiction:
Improvemirror surface precisionVSAvoidglass boule material wastage
Core Design Contradiction:
Manufacturing precisionVSLoss of substance

Solution Approach 1:

The manufacturing method transitions from subtractive machining (removing 95% of material) to additive construction (building mirror layer by layer). This fundamental parameter change in the manufacturing process eliminates material wastage by only using the exact amount of material needed for the final mirror structure.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The mirror core structure is designed to be self-supporting and self-optimizing during the layer-by-layer construction process. Each layer is deposited only where structurally necessary, allowing the mirror to achieve precise dimensions without requiring excessive material removal or support structures.

Inventive Principle:
Principle #25Self-service

3Weight of moving object

If advanced ceramics or carbon composite materials are used to reduce weight and cost, then manufacturing cost and weight are reduced, but long term stability deteriorates due to thermal and hygroscopic absorption

Engineering Contradiction:
Improvemirror weightVSAvoidlong term stability
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The invention employs a composite structure consisting of a mirror core made from advanced materials (such as carbon composite or ceramic) bonded to a faceplate made from ultra-low expansion glass (ULE). This composite approach allows the lightweight core to reduce weight while the ULE faceplate provides thermal stability and long-term reliability, combining the advantages of both material types.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The mirror is divided into distinct functional segments: a lightweight core structure for mass reduction and a stable ULE faceplate for dimensional stability and optical performance. This segmentation allows each component to fulfill its specific function optimally, with the core providing structural support and the faceplate ensuring long-term stability against thermal and hygroscopic effects.

Inventive Principle:
Principle #1Segmentation

4Weight of moving object

If carbon fiber prepreg layering and autoclaving is used to fabricate composite core, then weight is reduced, but device complexity increases due to precise layering and machining requirements

Engineering Contradiction:
Improvemirror core weightVSAvoidfabrication process complexity
Core Design Contradiction:
Weight of moving objectVSDevice complexity

Solution Approach 1:

The fabrication process transitions from complex multi-step procedures (prepreg layering, autoclaving, precision machining) to a simplified additive manufacturing process. The mirror core is built layer by layer using digital modeling and automated deposition, eliminating the need for manual layering, autoclaving cycles, and subsequent machining operations.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

Traditional mechanical fabrication methods (manual layering, autoclaving pressure, precision machining) are replaced with digital manufacturing techniques. Computer-aided design and automated additive processes substitute for complex mechanical operations, significantly reducing device complexity while maintaining or improving weight efficiency.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 significantly reduces the weight and manufacturing time of mirrors by over 70% and costs by over 50%, while maintaining high stiffness and stability, enabling rapid and low-cost deployment of precision imaging capabilities.

Implementation Method 1

preparing a mirror core by successively depositing a plurality of layers of a core material to form a core structure

Methodology Applied
Scientific Effect3D Printing: 3D Printing

Implementation Method 2

bonding, using a bonding material, the mirror core to a front polishable faceplate and a back faceplate

Methodology Applied
Scientific EffectBonding: Adhesive

Data Source

PatentUS10422933B2Large lightweight mirror for a large telescope
Publication Date: 2019.09.24 HARRIS CORP
  • US10422933B2 patent drawing
  • US10422933B2 patent drawing
  • US10422933B2 patent drawing

AI summary

A process for manufacturing a mirror includes preparing a mirror core by successively depositing a plurality of layers of a core material to form a core structure; and bonding, using a bonding material, the mirror core to a front polishable faceplate and a back faceplate. A mirror includes a mirror core including a plurality of layers of a core material; a front polished faceplate; and a back faceplate. The front polished faceplate and the back faceplate are bonded to the mirror core with a bonding material.