Wind Shear Safety Tool for Aircraft Configuration
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Solution Overview
Problem
Current methods for operating aircraft in wind shear conditions rely on pilot memory, manual calculations, and external resources, which are time-consuming, prone to errors, and lack comprehensive guidance for identifying appropriate aircraft configurations, increasing the risk of accidents.
Innovation Solution
A wind shear safety performance tool that uses a processor unit to receive operation information and wind shear indications, applying stored rules to identify a recommended aircraft configuration, providing customized guidance for flight crews through an onboard system.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If pilot memory and manual calculations are used to determine aircraft configuration in wind shear conditions, then flexibility in handling various operational scenarios is maintained, but the time required to determine safe configuration increases and error risk increases
Solution Approach 1:
The patent replaces manual mechanical calculations and memory-based decision-making with an automated computer-based system. The flight management system automatically calculates aircraft configuration recommendations by processing operational parameters through stored algorithms, eliminating the need for pilots to perform manual computations while maintaining adaptability to various wind shear scenarios.
Solution Approach 2:
The patent introduces a computer-based intermediary system that acts as a mediator between operational conditions and configuration decisions. This intermediary automatically processes operational parameters, applies relevant rules and constraints, and generates configuration recommendations, reducing the cognitive burden on pilots while maintaining flexibility.
2Reliability
If manual calculations and external resources are used to determine aircraft configuration, then comprehensive guidance can be provided, but the complexity of the process increases and error susceptibility increases
Solution Approach 1:
The patent merges multiple functions into a single integrated flight management system. It combines operational parameter input, wind shear detection, configuration calculation, and recommendation generation into one unified system, reducing process complexity while maintaining comprehensive guidance capabilities and improving reliability through systematic integration.
Solution Approach 2:
The flight management system performs self-service by automatically determining aircraft configuration recommendations without requiring external resources or manual intervention. The system autonomously processes operational parameters, applies relevant rules, and generates configuration guidance, reducing error susceptibility while maintaining comprehensive coverage.
3Measurement precision
If pilots rely on memory and manual resources during wind shear operations, then no additional equipment complexity is introduced, but the consistency and accuracy of configuration determination deteriorates
Solution Approach 1:
The patent replaces human memory and manual resources with an automated computer-based system that consistently and accurately determines aircraft configuration. The flight management system uses standardized algorithms and stored operational data to eliminate variability in configuration determination, significantly improving precision while accepting the introduction of computational equipment.
Data Source
AI summary
A system and method for identifying a recommended configuration for operating an aircraft in wind shear conditions. A processor unit receives information associated with an operation to be performed by the aircraft. The processor unit receives an indication that wind shear may be present during the operation. Responsive to receiving the indication that the wind shear may be present during the operation, the processor unit identifies the recommended configuration for the aircraft to perform the operation using the information associated with the operation to be performed by the aircraft and rules for operating the aircraft in the wind shear conditions.