Aircraft FOHE Failure Detection via Cross-Referenced Temperature Signals

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Solution Overview

Problem

Existing systems for monitoring the health of a Fuel Oil Heat Exchanger (FOHE) in aircraft engines are insufficient as they only provide notification of fuel temperature being outside a predetermined range, failing to distinguish between FOHE failure and sensor faults, leading to potential safety issues like fuel system fires or icing.

Innovation Solution

A method and system that detect out-of-range fuel temperatures downstream of the heat exchanger by monitoring fuel tank and main oil temperatures, using a processing unit to differentiate between FOHE failures and sensor faults, and outputting alerts via a Crew-Alerting System.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a fuel temperature switch is used to monitor the health of the FOHE, then a notification is provided when fuel temperature is outside a predetermined range, but the information is insufficient to determine if the FOHE or the fuel temperature switch itself is at fault

Engineering Contradiction:
Improvefault detection reliabilityVSAvoidfault identification information
Core Design Contradiction:
ReliabilityVSLoss of information

Solution Approach 1:

The patent introduces an intermediary processing system that receives the fuel temperature switch signal and cross-references it with fuel tank temperature and main oil temperature signals. This intermediary processing layer analyzes the relationships between multiple temperature parameters to determine whether an out-of-range reading indicates actual FOHE failure or sensor fault, thereby resolving the information insufficiency problem

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system implements feedback by continuously monitoring multiple temperature signals (fuel tank temperature, main oil temperature, and fuel temperature downstream of FOHE) and using this feedback information to validate each other's readings. When discrepancies are detected, the system uses the feedback from multiple sources to identify the faulty component, improving fault detection reliability

Inventive Principle:
Principle #23Feedback

2Device complexity

If only fuel temperature downstream of FOHE is monitored, then the system is simple, but it cannot distinguish between FOHE failure and sensor faults

Engineering Contradiction:
Improvemonitoring system complexityVSAvoidfault detection precision
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The monitoring system is designed to serve multiple functions: it not only detects out-of-range fuel temperatures but also identifies the source of the problem (FOHE failure versus sensor fault). By making the system multi-functional through the use of multiple temperature sensors and a processing unit that analyzes relationships between them, the patent achieves both acceptable complexity and high measurement precision

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

This approach allows for reliable detection of FOHE failures, including excessive or insufficient heating conditions, and sensor faults, enhancing safety by providing accurate fault identification and enabling appropriate actions.

Implementation Method 1

The fuel is indeed circulated in the FOHE, where the heat generated by the engine's oil system is transferred to the fuel

Methodology Applied
Scientific EffectHeat transfer: Conduction (thermal)

Data Source

PatentUS10676206B2System and method for heat exchanger failure detection
Publication Date: 2020.06.09 PRATT & WHITNEY CANADA CORP
  • US10676206B2 patent drawing
  • US10676206B2 patent drawing
  • US10676206B2 patent drawing

AI summary

A system and a method for detecting a failure of a heat exchanger provided on an engine of an aircraft. An out-of-range fuel temperature downstream of an outlet of the heat exchanger is detected. A health of a fuel tank temperature signal indicative of a temperature of at least one fuel tank of the aircraft is monitored. A main oil temperature signal indicative of a temperature of oil in the engine is received. The failure is detected based on the main oil temperature and on the health of the fuel tank temperature signal.