Reactive Magnetron Sputtering Hysteresis Control

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Solution Overview

Problem

Existing methods for controlling reactive magnetron sputtering processes face challenges in achieving high deposition rates due to hysteresis behavior, particularly when trying to maintain stable conditions for stoichiometric coatings, as they are sensitive to changes in process overall pressure and require precise calibration of vacuum gauges and gas flow control.

Innovation Solution

Implementing a PID algorithm for regulating the process overall pressure using the mean deviation of reactive gas flow, allowing the system to oscillate within a defined hysteresis zone and adjust the gas flow to maintain optimal stoichiometric conditions without requiring precise initial pressure settings or calibration, using a feedback loop that adapts to changes in chamber conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Manufacturing precision

If reactive magnetron sputtering is used to deposit stoichiometric coatings, then coating quality is improved, but deposition rate decreases due to hysteresis behavior

Engineering Contradiction:
Improvestoichiometric coating compositionVSAvoiddeposition rate
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The patent applies periodic pulsing of reactive gas flow to the magnetron sputtering system. The gas flow is periodically switched between on and off states with specific duty cycles (e.g., 50% or 70% on-time), creating oscillating conditions that traverse the hysteresis loop. This periodic action allows the system to spend sufficient time in the stoichiometric region while maintaining higher average deposition rates compared to continuous operation at fixed stoichiometric points.

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The patent dynamically changes the reactive gas flow rate parameter over time, varying it between minimum and maximum values according to a pulsed pattern. This parameter modulation allows the system to navigate through different compositional regions of the hysteresis loop, spending appropriate time in the stoichiometric zone to achieve desired coating composition while increasing overall productivity through higher average gas flow compared to static operation.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If high pumping speed is used to achieve high deposition rates, then productivity is improved, but system complexity and cost increase

Engineering Contradiction:
Improvedeposition rateVSAvoidpumping system requirements
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

By implementing periodic pulsing of reactive gas flow, the system can achieve high average deposition rates without requiring proportionally high pumping speeds. The pulsed operation creates transient conditions where deposition occurs rapidly during the on-phase, allowing the use of more moderate pumping systems while maintaining high overall productivity through time-averaged effects.

Inventive Principle:
Principle #19Periodic action

3Manufacturing precision

If precise calibration of vacuum gauges and gas flow control is implemented, then coating stoichiometry is improved, but device complexity and operation difficulty increase

Engineering Contradiction:
Improvecoating stoichiometryVSAvoidcalibration requirements
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The periodic pulsing method inherently compensates for system variations and drifts. The oscillating operation traverses the hysteresis loop repeatedly, and by adjusting the duty cycle of the pulse, the system self-regulates to achieve stoichiometric compositions without requiring precise initial calibration of vacuum gauges or gas flow controllers. The method is robust against variations in system parameters.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Instead of relying on precisely maintained static parameters, the patent uses dynamic parameter changes through periodic pulsing. The system achieves stoichiometric control through the time-averaged effect of oscillating gas flow rates rather than through precise calibration and maintenance of fixed flow rates, thereby reducing the need for complex calibration procedures.

Inventive Principle:
Principle #35Parameter changes

4Stability of the object's composition

If low frequency pulsing of power on target is used to stabilize hysteresis behavior, then stability is improved, but deposition rate decreases

Engineering Contradiction:
Improvehysteresis stabilizationVSAvoiddeposition rate
Core Design Contradiction:
Stability of the object's compositionVSProductivity

Solution Approach 1:

The patent applies periodic pulsing to the reactive gas flow rather than to the power on target. This approach stabilizes the hysteresis behavior while maintaining higher deposition rates because the gas flow pulsing directly controls the chemical composition of the plasma environment without significantly interrupting the physical sputtering process driven by continuous power delivery to the target.

Inventive Principle:
Principle #19Periodic action

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 method enables stable and reproducible deposition of stoichiometric coatings by maintaining the process within the optimal hysteresis zone, allowing for higher deposition rates and reducing the need for precise initial pressure settings or partial gas pressure regulation, thus achieving long-term stable conditions.

Implementation Method 1

reactive magnetron sputtering process

Methodology Applied
Scientific EffectSputtering: Sputtering

Implementation Method 2

reactive magnetron sputtering process

Methodology Applied
Scientific EffectPlasma: Plasma

Data Source

PatentUS9090961B2Magnetron sputtering process
Publication Date: 2015.07.28 PLATIT
  • US9090961B2 patent drawing
  • US9090961B2 patent drawing
  • US9090961B2 patent drawing

AI summary

To control reactive magnetron sputtering process using a reactive gas or reactive gases the process overall pressure is regulated by means of the flow of the reactive gas or the reactive gases, respectively. Oscillations of the flow of the reactive gas or the reactive gases, respectively are determined and used as feedback to determine the process overall pressure.