Glassy Carbon Composite Substrate for Smooth SiC Direct Bonding

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Solution Overview

Problem

Substrates made of polycrystalline silicon carbide (p-SiC) are difficult to polish and exhibit residual surface roughness, which complicates direct bonding and affects the quality of composite structures used in microelectronics.

Innovation Solution

A process involving the deposition of a polymer resin layer with preformed carbon-carbon bonds by centrifugal coating on a p-SiC substrate, followed by annealing to form a glassy carbon film, which improves surface smoothness and facilitates direct bonding.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If direct bonding is performed on polycrystalline SiC substrates, then bonding interface quality is required to be high, but surface roughness prevents successful bonding

Engineering Contradiction:
Improvebonding interface qualityVSAvoidsurface roughness
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

A glassy carbon intermediate layer is deposited on the polycrystalline SiC substrate surface. This intermediate layer serves as a mediator that provides the required surface smoothness and quality for direct bonding, while the underlying polycrystalline SiC substrate maintains its structural properties. The glassy carbon layer effectively decouples the rough substrate surface from the bonding interface requirements.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The surface properties of the substrate are modified by changing the material parameter at the surface level. Instead of attempting to polish the polycrystalline SiC to achieve smoothness, a glassy carbon layer is deposited that inherently provides the required surface smoothness parameter, thereby achieving bonding compatibility without modifying the bulk substrate.

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If polycrystalline SiC substrates are polished to reduce roughness, then bonding quality improves, but the hardness and polycrystalline structure make polishing difficult and time-consuming

Engineering Contradiction:
Improvesurface smoothnessVSAvoidpolishing difficulty
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

Rather than directly modifying the difficult-to-process polycrystalline SiC surface through polishing, a glassy carbon intermediate layer is deposited. This layer is much easier to process and polish to the required smoothness, thereby transferring the manufacturing ease from the intermediate layer to the overall substrate surface preparation process.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The mechanical polishing process is replaced by a deposition process. Instead of mechanically removing material from the hard polycrystalline SiC surface, a glassy carbon layer is deposited and then polished, substituting the difficult mechanical removal process with a more manageable deposition and light polishing sequence.

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

The glassy carbon film achieves a low surface roughness, enhancing the electrical and thermal properties of the support substrate, thereby improving the quality and integrity of the composite structure for microelectronic applications.

Implementation Method 1

a second annealing at a temperature of greater than 600° C., under a neutral atmosphere, in order to transform the crosslinked polymer resin layer into a glassy carbon film

Methodology Applied
Scientific EffectAnnealing: Annealing

Implementation Method 2

the deposition, by centrifugal coating, at least on a front face of the starting substrate, of a polymer resin layer

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentUS20250140602A1Composite structure and manufacturing method thereof
Publication Date: 2025.05.01 SOITEC SA
  • US20250140602A1 patent drawing
  • US20250140602A1 patent drawing
  • US20250140602A1 patent drawing

AI summary

A method of manufacturing a composite structure including a thin layer of a first monocrystalline material arranged on a carrier substrate, the method including: providing an initial substrate of a second polycrystalline material; and depositing, by spin coating, at least on one front surface of the initial substrate, a layer of polymer resin including preformed 3D carbon-carbon bonds; performing a first annealing step at a temperature between 120° C. and 180° C. on the initial substrate provided with the polymer resin layer, to form a layer of cross-linked polymer resin; and performing a second annealing step at a temperature greater than 600° C., in a neutral atmosphere, to convert the layer of cross-linked polymer resin into a glassy carbon film. a composite structure includes a thin layer of a first monocrystalline material on a carrier substrate, which includes a glassy carbon film on an initial substrate of a second polycrystalline.