Fuel Cell Potential Monitoring for Stable Air Vehicle Flight

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Solution Overview

Problem

In air vehicles, insufficient fuel gas supply to fuel cells can cause the potential to become a reversal potential, leading to unstable flight due to limited fuel cell power generation, necessitating a method to stabilize power output and extend stable flight time.

Innovation Solution

A fuel cell system for air vehicles that includes a fuel cell, a fuel gas supplier, and a controller with a potential sensor to detect reversal potential and increase fuel gas supply, stabilizing power output and extending flight time by managing fuel gas supply based on potential state monitoring.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If fuel gas supply is increased to prevent reversal potential, then power generation stability is improved, but fuel consumption increases

Engineering Contradiction:
Improvepower generation stabilityVSAvoidfuel consumption
Core Design Contradiction:
ReliabilityVSLoss of substance

Solution Approach 1:

The control unit continuously monitors the potential of the fuel cell and dynamically adjusts the fuel gas supply rate based on real-time potential measurements. When the potential approaches reversal potential, the system increases fuel supply to maintain stable power generation, and reduces supply when potential is stable, creating a closed-loop feedback control system that balances reliability and fuel consumption

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system detects when the fuel cell potential is approaching reversal potential before actual reversal occurs, and proactively increases the fuel gas supply rate to prevent reversal potential from being reached. This preliminary action stabilizes power generation while avoiding excessive fuel consumption that would occur with continuous high supply

Inventive Principle:
Principle #10Preliminary action

2Stability of the object's composition

If fuel gas supply is increased to stabilize power output, then flight stability is improved, but fuel gas consumption increases

Engineering Contradiction:
Improveflight stabilityVSAvoidfuel gas consumption
Core Design Contradiction:
Stability of the object's compositionVSLoss of substance

Solution Approach 1:

The control unit uses real-time potential monitoring to dynamically adjust fuel gas supply, ensuring stable power output for flight stability while minimizing fuel gas consumption through precise, demand-based supply adjustment rather than continuous maximum supply

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The system dynamically adjusts the fuel gas supply rate based on real-time potential measurements and power demand conditions, transitioning between different supply rates to maintain flight stability while optimizing fuel gas consumption according to actual operational needs

Inventive Principle:
Principle #15Dynamics

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

The system effectively stabilizes fuel cell power output and extends the duration of stable flight by increasing fuel gas supply when a reversal potential is detected, preventing immediate output limitation and ensuring continued operation until the potential returns to a positive state.

Implementation Method 1

generates electrical energy by electrochemical reaction between fuel gas (e.g., hydrogen) and oxidant gas (e.g., oxygen)

Methodology Applied
Scientific EffectElectrochemical reaction:

Implementation Method 2

a potential sensor to detect a potential state of the fuel cell

Methodology Applied
Scientific EffectElectrical potential detection:

Data Source

PatentEP4080628B1Fuel cell system and air vehicle
Publication Date: 2024.11.13 TOYOTA JIDOSHA KK
  • EP4080628B1 patent drawingFigure 1
  • EP4080628B1 patent drawingFigure 2
  • EP4080628B1 patent drawingFigure 3

AI summary

A fuel cell system for air vehicles, wherein the fuel cell system comprises: a fuel cell, a fuel gas system for supplying fuel gas to the fuel cell, a potential sensor, and a controller; wherein the fuel gas system comprises a fuel gas supplier; wherein the controller determines whether or not a potential of the fuel cell measured by the potential sensor, is a reversal potential; and wherein, when the controller determines that the potential of the fuel cell is a reversal potential, the controller increases a fuel gas supply from the fuel gas supplier to the fuel cell.