Real-Time Ice Estimation Algorithm for Aircraft Safety

The patent replaces complex mechanical ice detection systems with an algorithmic approach that processes sensor data (temperature, humidity, precipitation rate) through mathematical models to estimate ice accumulation. This substitutes direct mechanical measurement with computational estimation, reducing hardware complexity while maintaining monitoring capability.

The patent introduces an intermediary computational model that processes raw sensor data and translates it into ice formation predictions. This intermediary layer (the algorithm) mediates between simple sensors and the complex task of ice monitoring, allowing basic sensors to provide accurate ice estimates through sophisticated data processing rather than requiring complex direct ice sensors.

The patent replaces direct physical ice sensors with an algorithmic estimation system that uses readily available atmospheric and flight data. Instead of attempting to directly measure ice accumulation through complex sensors, the system substitutes this with computational models that process temperature, humidity, and precipitation rate to predict ice formation, achieving measurement precision through information processing rather than physical measurement.

The patent creates a virtual copy of the ice accumulation state through algorithmic estimation. Rather than directly measuring the physical ice layer, the system generates a computational representation of ice quantity by processing related atmospheric parameters, effectively copying the ice state information from indirect measurements and flight data.

The patent implements continuous feedback monitoring where the estimated ice quantity is constantly compared against predefined thresholds. This feedback mechanism allows the system to provide real-time warnings and recommendations to pilots, enabling adaptive operational decisions that balance flexibility with safety based on current ice accumulation rates and aircraft conditions.

The patent establishes preliminary safety thresholds below the maximum certified ice limits before ice accumulation reaches dangerous levels. By setting these advance warning thresholds, the system enables preliminary corrective actions (such as activating deicing systems or adjusting flight plans) before the aircraft reaches its absolute safety limits, thereby maintaining both operational flexibility and safety margins.