Radio Altimeter Failure Prediction Using Altitude Difference Analytics

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Solution Overview

Problem

Current systems lack the capability to detect and predict radio altimeter failures, leading to potential flight delays, cancellations, and increased maintenance costs due to erroneous altitude readings and unforeseen failures.

Innovation Solution

A data analytics system that calculates a radio altimeter failure indicator by analyzing historical data from multiple radio altimeters, determining differences in altitude values, and evaluating these differences against thresholds to predict potential failures.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If radio altimeter systems operate without failure prediction capability, then the system structure remains simple, but flight operations experience delays and cancellations due to unforeseen failures

Engineering Contradiction:
Improveradio altimeter failure predictionVSAvoiddata analytics system
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system performs preliminary analysis of altitude data from multiple radio altimeters to calculate failure indicators before actual failures occur. By continuously monitoring and analyzing historical altitude values, the system predicts potential failures in advance, allowing preventive maintenance scheduling that avoids flight delays and cancellations.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent introduces a data analytics system as an intermediary layer between the radio altimeters and flight operations. This intermediary processes altitude data, calculates failure indicators, and provides predictions without requiring direct modification of the radio altimeter hardware, thus adding prediction capability while maintaining relative system simplicity.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If multiple radio altimeters are monitored with detailed data analysis, then failure prediction accuracy improves, but processing time and computational resources increase

Engineering Contradiction:
Improvefailure prediction accuracyVSAvoiddata processing time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The system extracts only the essential features from raw altitude data by calculating mode values and mode value differences. Instead of analyzing all raw altitude measurements in detail, the system extracts the statistically significant differences between altimeter readings, maintaining prediction accuracy while reducing processing time and computational resources.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent transforms raw altitude data into derived parameters such as mode values, mode value differences, and failure indicators. By changing the parameter representation from raw measurements to statistical features, the system achieves accurate failure prediction with reduced computational complexity and faster processing.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS11834201B2Methods, apparatuses and systems for predicting radio altimeter failure
Publication Date: 2023.12.05 HONEYWELL INTERNATIONAL INC
  • US11834201B2 patent drawing
  • US11834201B2 patent drawing
  • US11834201B2 patent drawing

AI summary

Methods, apparatuses, and systems for predicting radio altimeter failures are provided. An example method may include determining a first plurality of altitude values associated with a first radio altimeter, determining a second plurality of altitude values associated with a second radio altimeter, calculating a first level feature based at least in part on the first plurality of altitude values and the second plurality of altitude values, and determining a radio altimeter failure indicator based at least in part on the first level feature.