Technical Description
The invention is a system to capture real-time dynamic pressure or acoustic time-series signals from high-flow combustion, aeroelastic, or acoustic. It processes data through non-linear mathematical frameworks to foresee and actively mitigate impending oscillatory instabilities before they occur by altering operational parameters.
Problems Addressed
- Elevated NOx Emissions
- Intrusive Hardware Dependency
- Reactive Post-Instability Intervention
- Combustion Chamber Acoustic Noise
- Oscillation-Driven Structural Degradation
Tech Features
- 0-1 Test Instability Tracking
- Mutual Information Down sampling
- Burst Fraction Proximity Tracking
- Preemptive Valve-Control Triggering
Target Audience
- Furnace & Industrial Burner Operators
- Turbine & Jet Propulsion Manufacturers
- Aerodynamic & Aeroelastic Researchers
Tech ID: P16-2104 TRL 3 Patent Status: Granted Available For Exclusive and Non-exclusive License
