Multi-Stage Air Data Probe Prognostics for Real-Time RUL Prediction

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Solution Overview

Problem

Existing aircraft-based health monitoring systems lack the sophistication to analyze air data probe data in real-time for accurate prediction of remaining useful life and failure, requiring data transmission to a ground station and manual module updates.

Innovation Solution

A modular prognostics health monitoring system that includes edge devices for initial data processing, a smart coordinator for further analysis, and cloud infrastructure for detailed prediction of remaining useful life and failure using machine learning techniques.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If data is transmitted to a ground station for analysis, then complex health monitoring algorithms can be executed, but real-time prediction capability is reduced and operational time is lost

Engineering Contradiction:
Improveprediction accuracyVSAvoidoperational time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The health monitoring system is segmented into multiple levels: edge device for real-time local analysis, coordinator for data aggregation, and cloud infrastructure for comprehensive processing. This segmentation enables simultaneous real-time prediction at the edge and detailed ground station analysis, resolving the contradiction between real-time capability and prediction accuracy.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The edge device performs preliminary data processing and initial health assessments locally before transmitting processed data to the ground station. This preliminary action reduces the time required for ground-based analysis while maintaining prediction accuracy through pre-filtered and pre-processed data.

Inventive Principle:
Principle #10Preliminary action

2Adaptability or versatility

If the data acquisition module is updated, then monitoring capabilities are improved, but the module must be removed and reinstalled causing operational disruption

Engineering Contradiction:
Improvemonitoring capabilityVSAvoidupdate process
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The data acquisition module is extracted as a separate, removable component with standardized interfaces. This allows the module to be updated independently without affecting the core probe structure, enabling capability improvements while minimizing operational disruption through hot-swappable design.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The data acquisition module is designed with universal, standardized connection interfaces that allow different versions of the module to work with the same probe structure. This multi-functionality enables seamless updates and upgrades without requiring custom installation procedures, improving both adaptability and ease of operation.

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

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

Enables real-time, accurate prediction of air data probe failure and remaining useful life, reducing operational disruptions by allowing timely replacement of faulty probes and avoiding unnecessary replacements.

Implementation Method 1

resistive heating elements are installed in the air data probes to prevent ice formation. To heat the probe, an operational voltage is provided through the heating element.

Methodology Applied
Scientific EffectJoule heating: Joule Heating

Data Source

PatentUS12392796B2Dynamic multi-stage air data probe prognostics health monitoring system
Publication Date: 2025.08.19 ROSEMOUNT AEROSPACE INC
  • US12392796B2 patent drawing
  • US12392796B2 patent drawing
  • US12392796B2 patent drawing

AI summary

A method for monitoring a vehicle-borne probe includes receiving, by a first edge device in communication with the probe, sensed data related to a characteristic of a heating element of the probe, analyzing, by a first application of the first edge device, the sensed data to generate a first data output, receiving, by a coordinator in communication with the first edge device, the first data output, and incorporating the first data output into a data package, receiving, by a cloud infrastructure in communication with the coordinator, the data package via a data gateway, and analyzing, by one of the cloud infrastructure and a ground station, the data package to estimate a remaining useful life and a failure of the probe.