Gas-Lifted Substrate Support for Rapid Rotation Braking

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Solution Overview

Problem

Existing substrate processing apparatuses face challenges in rapidly decelerating and stopping substrates after the acceleration gas supply is stopped, leading to prolonged processing times.

Innovation Solution

A substrate supporting assembly that includes a susceptor plate with substrate seats and gas flow lines for supplying lifting, acceleration, and deceleration gases, where the satellite is lifted, rotated, and decelerated using these gases to control the substrate's rotation speed and stop it quickly.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If the substrate is rotated using acceleration gas supply, then the substrate rotation speed is improved, but the stopping time becomes excessively long

Engineering Contradiction:
Improvesubstrate rotation speedVSAvoidstopping time
Core Design Contradiction:
SpeedVSLoss of time

Solution Approach 1:

The patent applies preliminary anti-action by introducing a deceleration gas flow line that supplies gas in the opposite direction to substrate rotation before the substrate comes to a natural stop. This counter-directional gas flow creates a braking effect that actively opposes the rotation, significantly reducing the stopping time from a prolonged natural deceleration to a controlled rapid stop while maintaining the benefits of acceleration gas-driven rotation speed

Inventive Principle:
Principle #9Preliminary anti-action

2Manufacturing precision

If the satellite is lifted by lifting gas, then the substrate processing uniformity is improved, but the system complexity increases

Engineering Contradiction:
Improvesubstrate processing uniformityVSAvoidsystem complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent merges the lifting gas supply function into the existing satellite structure by integrating lifting gas flow lines that supply gas to the substrate seat, allowing the satellite to be lifted off the substrate seat during rotation. This combination achieves uniform substrate processing through satellite lifting while utilizing the existing mechanical structure, thereby reducing overall system complexity compared to separate lifting mechanisms

Inventive Principle:
Principle #5Merging (Combining)

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 enables fast deceleration and stopping of substrates within a short time, reducing processing times and increasing productivity in semiconductor and solar cell manufacturing.

Implementation Method 1

a plurality of gas flow lines for supplying a lifting gas, an acceleration gas, and a deceleration gas to the substrate seat

Methodology Applied
Scientific EffectGas pressure: Pressure Increase

Implementation Method 2

is rotated relative to the susceptor plate by the acceleration gas supplied in a forward direction of rotation

Methodology Applied
Scientific EffectGas impact force: Impact Force

Implementation Method 3

is decelerated or stopped by the deceleration gas supplied in a reverse direction of rotation

Methodology Applied
Scientific EffectGas impact force: Impact Force

Data Source

PatentUS12249536B2Substrate supporting assembly and substrate processing apparatus
Publication Date: 2025.03.11 WONIK IPS CO LTD
  • US12249536B2 patent drawing
  • US12249536B2 patent drawing
  • US12249536B2 patent drawing

AI summary

A substrate supporting assembly includes a susceptor plate including at least one substrate seat, and a plurality of gas flow lines for supplying a lifting gas, an acceleration gas, and a deceleration gas to the substrate seat, and at least one satellite on the at least one substrate seat and including an upper surface, and a lower surface where a rotation pattern for receiving a rotational force and a braking force from the acceleration gas and the deceleration gas is provided. The at least one satellite is lifted from the at least one substrate seat by the lifting gas supplied from the at least one substrate seat, is rotated relative to the susceptor plate by the acceleration gas supplied in a forward direction of rotation, to rotate the substrate, and is decelerated or stopped by the deceleration gas supplied in a reverse direction of rotation.