Hydrogen Fuel Leak Detection System for Aircraft Safety

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Solution Overview

Problem

Hydrogen fuel systems in aircraft pose challenges due to hydrogen's low boiling point, low power density in gaseous form, tendency to seep through materials, and its colorless, odorless, and invisible flame, making it difficult to detect leaks effectively.

Innovation Solution

A hydrogen fuel system with a fuel tank, power generator, and fuel delivery assembly, equipped with a leak detection system that includes sensors to monitor parameters corresponding to hydrogen fuel leaks and a controller to determine and indicate the occurrence of leaks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If hydrogen fuel is used to reduce carbon dioxide emissions, then environmental performance is improved, but leak detection difficulty increases due to hydrogen's colorless, odorless, and invisible flame properties

Engineering Contradiction:
Improvecarbon dioxide emissionsVSAvoidleak detection difficulty
Core Design Contradiction:
Object-affected harmful factorsVSDifficulty of detecting and measuring

Solution Approach 1:

The patent introduces sensor systems as intermediary devices that detect hydrogen leakage through physical parameters such as thermal conductivity, pressure changes, or acoustic signals. These sensors act as mediators between the invisible hydrogen gas and the detection system, converting undetectable hydrogen presence into measurable signals that can be monitored and alarmed.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces traditional mechanical or chemical detection methods (which rely on visible or olfactory cues) with electronic sensing systems. The sensor-based detection system uses electrical or optical fields to detect hydrogen's unique physical properties, substituting human sensory limitations with electronic measurement capabilities.

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

2Quantity of substance

If hydrogen fuel is stored and transported in aircraft, then energy density is improved, but safety risks increase due to hydrogen's tendency to seep through materials

Engineering Contradiction:
Improveenergy densityVSAvoidsafety risk
Core Design Contradiction:
Quantity of substanceVSReliability

Solution Approach 1:

The patent implements leak detection sensors and monitoring systems before actual leakage occurs. The system continuously monitors for signs of hydrogen escape through seals and materials, enabling early detection and preventive action before the leakage becomes significant enough to compromise safety.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent establishes a feedback loop where sensor data about hydrogen pressure, temperature, and presence is continuously monitored and fed back to the control system. This feedback mechanism allows real-time adjustment of storage conditions and immediate alerting when anomalies suggest potential leakage through materials.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS12241424B2Hydrogen fuel leak detection system
Publication Date: 2025.03.04 GENERAL ELECTRIC CO
  • US12241424B2 patent drawing
  • US12241424B2 patent drawing
  • US12241424B2 patent drawing

AI summary

A fuel leak detection system for hydrogen fuel system including a monitored component. The fuel leak detection system including a sensor and controller communicatively coupled to the sensor. The sensor is positioned to monitor at least a portion of the monitored component. The sensor is configured (i) to sense a parameter corresponding to a hydrogen fuel leak of the monitored component and (ii) to generate an output. The controller is configured (i) to receive the output of the sensor, (ii) to determine, based on the output of the sensor, if a leak has occurred in the monitored component, and (iii) to generate an output indicating a fuel system leak when the controller determines that the leak has occurred in the monitored component. The monitored component may be a component of one of a fuel tank, a power generator, and a fuel delivery assembly.