Dynamic Aircraft Threat Controller for Aircraft-Specific Icing and Turbulence

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Solution Overview

Problem

Existing weather monitoring systems provide generalized weather forecasts that do not account for specific aircraft airfoils, leading to inadequate icing and turbulence predictions, which can pose significant hazards during flights.

Innovation Solution

The Dynamic Aircraft Threat Controller Manager (DATCM) integrates comprehensive hazard modeling into flight planning tools, using aircraft-specific airfoil data to predict and avoid areas of turbulence and icing by generating optimized flight paths based on real-time and predictive data from various sources, including weather stations, satellites, and aircraft sensors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If generalized weather forecasts are used, then device complexity is reduced, but measurement precision of icing and turbulence predictions deteriorates

Engineering Contradiction:
Improveweather monitoring system complexityVSAvoidicing and turbulence prediction accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The system transitions from generalized weather forecasts to aircraft-specific predictions by incorporating airfoil geometry data. Each aircraft type receives customized icing and turbulence predictions based on its unique aerodynamic characteristics, thereby improving measurement precision without requiring complete system redesign.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The system changes the parameters of weather forecasts by integrating aircraft-specific variables such as airfoil shape, wing configuration, and aerodynamic coefficients. This parameter customization enables precise prediction of icing accumulation and turbulence effects tailored to each aircraft type.

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If aircraft-specific airfoil data is integrated, then measurement precision of hazard predictions improves, but device complexity increases

Engineering Contradiction:
Improveicing and turbulence prediction accuracyVSAvoidweather monitoring system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The system achieves aircraft-specific predictions through a universal platform that processes multiple aircraft types. The core algorithm remains generalizable while accepting airfoil geometry inputs, allowing one system to serve multiple aircraft configurations without requiring separate specialized systems for each aircraft type.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The system introduces an intermediary processing layer that translates generic weather data into aircraft-specific hazard predictions. This intermediary component integrates airfoil data with weather forecasts, acting as a mediator between general weather monitoring and specific aircraft performance prediction.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Reliability

If comprehensive hazard modeling is implemented, then reliability of flight safety improves, but device complexity increases

Engineering Contradiction:
Improveflight safetyVSAvoidflight planning system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system performs preliminary hazard assessment during flight planning by integrating comprehensive modeling of icing and turbulence conditions. By predicting hazards before flight departure and providing optimized flight paths, the system ensures safety reliability without requiring complex real-time intervention systems during actual flight operations.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20250225884A1Dynamic aircraft threat controller manager apparatuses, methods and systems
Publication Date: 2025.07.10 DTN LLC
  • US20250225884A1 patent drawing
  • US20250225884A1 patent drawing
  • US20250225884A1 patent drawing

AI summary

The present invention transforms flight profile information, terrain, weather/atmospheric data and flight parameter data via system components into comprehensive hazard avoidance optimized flight plans. Comprehensive hazard avoidance includes synergistic comprehensive flight condition data. In one implementation, the system comprises a processor and a memory disposed in communication with the processor and storing processor-issuable instructions to receive anticipated flight plan parameter data, obtain weather data based on the flight plan parameter data, obtain atmospheric data based on the flight plan parameter data, and determine a plurality of four-dimensional grid points based on the flight plan parameter data. The system may then determine comprehensive hazards mappings. With (near) real-time comprehensive hazard information and/or predictive flight condition specific to aircraft characteristics and/or profile parameters, the system may allow aircraft to avoid areas where comprehensive hazard is greater than a predetermined threshold and/or avoid areas where undesirable flight conditions are anticipated.