SiC Crystal Growth Radial Temperature Gradient Control

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing methods for manufacturing silicon carbide single crystals, such as HTCVD, fail to effectively suppress the conversion of threading edge dislocations into prismatic plane dislocations and subsequent conversions into basal plane dislocations, which affects the quality of semiconductor devices.

Innovation Solution

A method involving HTCVD with a controlled temperature gradient in the radial direction, specifically 15° C./mm or lower, and strategic management of shear stress regions on the silicon carbide single crystal layer to minimize the areas where high shear stresses overlap, thereby reducing dislocation conversions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If HTCVD method is used to grow silicon carbide single crystal, then crystal growth is achieved, but threading edge dislocations are converted into prismatic plane dislocations which further convert into basal plane dislocations

Engineering Contradiction:
Improvedislocation controlVSAvoiddislocation conversion
Core Design Contradiction:
Manufacturing precisionVSReliability

Solution Approach 1:

The patent applies parameter changes by controlling the temperature gradient in the radial direction during HTCVD crystal growth. Specifically, maintaining the temperature gradient at 15°C/mm or lower prevents the conversion of threading edge dislocations into prismatic plane dislocations, and subsequently prevents conversion into basal plane dislocations. This parameter control directly addresses the dislocation conversion problem while enabling successful crystal growth.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If temperature gradient in radial direction is not controlled, then crystal growth proceeds, but dislocation conversions occur affecting device quality

Engineering Contradiction:
Improvecrystal growthVSAvoiddislocation density
Core Design Contradiction:
ProductivityVSManufacturing precision

Solution Approach 1:

The patent implements parameter changes by establishing a specific temperature gradient condition (15°C/mm or lower) in the radial direction during crystal growth. This parameter control enables simultaneous achievement of productive crystal growth and low dislocation density, resolving the contradiction between productivity and manufacturing precision.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent applies equipotentiality by creating a uniform temperature distribution in the radial direction through controlled gradient. This uniform thermal field prevents localized stress variations that would otherwise cause dislocation conversions, enabling both efficient growth and high crystal quality.

Inventive Principle:
Principle #12Equipotentiality

3Stability of the object's composition

If threading edge dislocations are converted into prismatic plane dislocations, then crystal structure changes, but device performance deteriorates

Engineering Contradiction:
Improvecrystal structureVSAvoiddevice performance
Core Design Contradiction:
Stability of the object's compositionVSReliability

Solution Approach 1:

The patent uses parameter changes by controlling the temperature gradient to prevent the crystal structure transitions that lead to device performance deterioration. By maintaining the gradient at 15°C/mm or lower, the crystal structure remains stable in the desired configuration, avoiding harmful dislocation conversions.

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

This approach effectively suppresses the conversion of threading edge dislocations into prismatic plane dislocations and prismatic plane dislocations into basal plane dislocations, resulting in improved quality silicon carbide single crystal ingots and wafers suitable for high-performance semiconductor devices.

Implementation Method 1

high temperature chemical vapor deposition (hereinafter called HTCVD or the HTCVD method) is known (see, for example, Patent Document 1). With the HTCVD method, many of basal plane dislocations (may hereinafter be referred to as BPDs) contained in a seed substrate are converted into threading edge dislocations (may hereinafter be referred to as TEDs) by epitaxial growth.

Methodology Applied
Scientific EffectEpitaxial growth: Epitaxy

Implementation Method 2

growing the silicon carbide single crystal so that a temperature gradient in a radial direction is a predetermined value or lower

Methodology Applied
Scientific EffectTemperature gradient: Temperature Gradient

Data Source

PatentUS20240110308A1Silicon carbide single crystal ingot, silicon carbide wafer, and method for manufacturing silicon carbide single crystal
Publication Date: 2024.04.04 MIRISE TECH CORP
  • US20240110308A1 patent drawing
  • US20240110308A1 patent drawing
  • US20240110308A1 patent drawing

AI summary

Provided are a method for manufacturing a silicon carbide single crystal, which can suppress conversion of threading edge dislocations into prismatic plane dislocations and conversion of the prismatic plane dislocations into basal plane dislocations; and a silicon carbide single crystal ingot and a silicon carbide wafer, in which conversion from threading edge dislocations into prismatic plane dislocations and conversion from the prismatic plane dislocations into basal plane dislocations have been suppressed. A silicon carbide single crystal is grown on the surface of a seed substrate by a gas method so that a temperature gradient in the radial direction of the seed substrate takes a predetermined value or lower during the growth. The area of regions T1 to T4, where regions R1 to R3 of a basal plane whose shear stresses exceed critical resolved shear stress, and regions S1 to S4 of a prismatic plane whose shear stresses exceed critical resolved shear stress overlap, is less than a half of the area of a crystal growth surface. Furthermore, the area of the regions T1 to T4 is smaller than the area of regions V1 to V4 where a region R4 of the basal plane whose shear stress does not exceed the critical resolved shear stress overlaps the regions S1 to S4.