Fuel Cell Airflow Fault Detection for Failed MAF Sensors

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Solution Overview

Problem

Mass air flow (MAF) sensors in fuel cells are unreliable due to susceptibility to contaminants, leading to incorrect air flow and pressure readings, which can cause interruptions in power generation or permanent damage to the fuel cell, posing safety risks in aircraft.

Innovation Solution

Detect MAF sensor failure by analyzing signals from non-MAF sensors, such as compressor RPM, pressure, and temperature, using a compressor map to estimate mass air flow and initiate a safe system response, such as limp mode, to maintain safe operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If MAF sensors are used to monitor air flow and pressure in fuel cells, then the fuel cell operation can be controlled, but the sensors are susceptible to contaminants causing clogging and performance degradation

Engineering Contradiction:
ImproveMAF sensor reliabilityVSAvoidcontaminant susceptibility
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent uses an intermediary approach by introducing a machine learning model that indirectly estimates MAF sensor readings through alternative measurements from other sensors (temperature, pressure, flow sensors). This intermediary estimation system bypasses the contaminated MAF sensor while still providing the necessary air flow data for fuel cell control.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent creates a virtual copy of the MAF sensor functionality by training a machine learning model to replicate the MAF sensor's measurement capabilities using data from other sensors. This digital twin approach allows the system to continue operating with accurate air flow estimates even when the physical MAF sensor is contaminated or failed.

Inventive Principle:
Principle #26Copying

2Ease of operation

If MAF sensor readings are used to control IGV positions, then fuel cell reactions can be regulated, but incorrect readings lead to incorrect IGV commands and potential fuel cell damage

Engineering Contradiction:
Improvefuel cell controlVSAvoidair flow reading accuracy
Core Design Contradiction:
Ease of operationVSMeasurement precision

Solution Approach 1:

The patent implements a feedback mechanism where the machine learning model continuously monitors alternative sensor readings and adjusts the estimated MAF values in real-time. This feedback loop ensures that even when the physical MAF sensor provides incorrect readings, the control system receives accurate estimated values for proper IGV positioning and fuel cell operation.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent replaces the mechanical MAF sensor measurement system with a computational machine learning model. Instead of relying on the physical sensor to provide accurate readings, the system uses algorithms to calculate and estimate the air flow parameters, substituting mechanical measurement with intelligent computation.

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

3Measurement precision

If multiple sensors are used to detect MAF failure, then detection accuracy improves, but system complexity increases

Engineering Contradiction:
Improvefailure detection accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent makes the existing sensors serve multiple functions: they not only monitor their primary parameters (temperature, pressure, flow) but also collectively contribute to estimating MAF sensor readings and detecting MAF failures. This multi-functionality approach allows accurate failure detection without adding dedicated MAF failure detection sensors, thereby avoiding increased system complexity.

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

Data Source

PatentUS20250323295A1Mass air flow sensor failure detection and management in aviation
Publication Date: 2025.10.16 ZEROAVIA INC
  • US20250323295A1 patent drawing
  • US20250323295A1 patent drawing
  • US20250323295A1 patent drawing

AI summary

A method and system of detecting mass air flow (MAF) sensor failure on an aircraft includes at least one signal from a non-MAF sensor received by a controller of a fuel cell system having at least one MAF sensor. The signal received by the controller is analyzed relative to a compressor map to estimate mass air flow. A MAF sensor failure is detected based on the estimated mass air flow. When a MAF sensor failure is detected, a safe operating mode of the fuel cell system may be activated to provide adequate power for operation of the aircraft to a safe landing while minimizing risk of damage to the fuel cell system.