Prognostic Processor for Avionics Failure Prediction

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Solution Overview

Problem

Current methods for failure analysis of avionic electronic systems, particularly Line Replacement Units (LRUs), lack real-time predictive capabilities, relying on manual estimation and post-data analysis, which is inefficient and costly, especially considering the high operational costs associated with unscheduled delays in aircraft operations.

Innovation Solution

A prognostic processor system integrated with LRUs, utilizing a predictive failure analysis model that interacts with sensors and historic log information to predict failures in real-time, employing a hierarchical processing approach with multiple processors interconnected via a system bus for enhanced fault prediction.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If manual failure analysis methods are used for LRUs, then system cost is reduced, but failure prediction accuracy and timeliness deteriorate

Engineering Contradiction:
Improvefailure prediction accuracyVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The LRU performs self-diagnosis and self-monitoring through integrated sensors and processing units that continuously assess its own health status, eliminating the need for external manual inspection while maintaining high prediction accuracy

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

Manual failure analysis is replaced by an automated electronic system comprising sensors, processing units, and algorithms that continuously monitor LRU parameters and predict failures, transitioning from mechanical/manual methods to automated electronic diagnostics

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Productivity

If real-time failure prediction systems are implemented, then operational efficiency is improved, but system cost increases

Engineering Contradiction:
Improveoperational efficiencyVSAvoidsystem cost
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The failure prediction system is segmented into modular components including sensors, processing units, and communication interfaces that can be independently implemented or scaled, allowing gradual deployment and cost management

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The prognostic system is designed to monitor multiple LRU types and parameters using a unified architecture, enabling the same system to serve multiple functions and reducing overall system cost through reuse of components and algorithms

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

3Loss of time

If manual failure analysis is used, then system simplicity is maintained, but response time to failures deteriorates

Engineering Contradiction:
Improveresponse timeVSAvoidautomation level
Core Design Contradiction:
Loss of timeVSExtent of automation

Solution Approach 1:

The system implements continuous monitoring of LRU parameters through always-active sensors and processing, ensuring that failure prediction is performed without interruption and providing immediate response when degradation patterns are detected

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The system performs preliminary failure prediction by continuously analyzing trends and patterns before actual failure occurs, enabling proactive maintenance scheduling and preventing unexpected downtime

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS7509537B1Prognostic processor system for real-time failure analysis of line replaceable units
Publication Date: 2009.03.24 ROCKWELL COLLINS INC
  • US7509537B1 patent drawing
  • US7509537B1 patent drawing
  • US7509537B1 patent drawing

AI summary

A prognostic processor for predicting machine failure in avionics electronics comprises prognostic capabilities in a single integrated circuit, with a processor, volatile and non-volatile memory, clock, on-chip and off-chip sensors and transducers, A/D converters, a common I/O interface adapted to be employed in a network of similar prognostic processors, and predictive Failure Analysis (FA) model software, which may be distributed throughout the network. The FA software employs a log file history, with the log file history storing data collected by the prognostic processor, real-time execution of a predictive model, with the ability to update the FA model with data from field failures. The prognostic processor network supports hierarchical processing to work with multiple prognostic processors. The prognostic processor system is applicable to FA monitoring of a wide range of avionics electronic equipment, in particular, Line Replacement Units (LRUs).