Aircraft Hydrogen Casing Inerting with Recirculated Nitrogen

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Solution Overview

Problem

Existing aircraft inerting systems for hydrogen-based systems are inefficient in space and weight usage, and rely on halon for fire suppression, which is environmentally problematic and unsuitable for smaller volumes.

Innovation Solution

An inerting system that recirculates inert gas within the hydrogen system casing, using sensors to monitor oxygen and hydrogen concentrations and control the flow of pure inert gas and recirculated fluid to maintain safe levels, reducing the need for external inert gas storage and eliminating the need for halon.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If nitrogen bottles or nitrogen generation system are used to supply inert gas, then the inerting function is ensured, but the space occupation and on-board weight increase

Engineering Contradiction:
Improveinerting functionVSAvoidon-board weight
Core Design Contradiction:
ReliabilityVSWeight of stationary object

Solution Approach 1:

The system recirculates and reuses the inert gas atmosphere after it has performed its inerting function. The atmosphere is extracted from the casing, recirculated through the hydrogen system, and reused to maintain inert conditions, thereby eliminating the need for continuous fresh nitrogen supply and reducing the size of nitrogen storage bottles or generation systems.

Inventive Principle:
Principle #34Discarding and recovering

Solution Approach 2:

The system uses its own exhaust atmosphere to perform the inerting function again. By recirculating the gas that has already been inside the casing, the system makes the atmosphere serve dual purposes: initial inerting and continuous maintenance of inert conditions, reducing dependency on external nitrogen sources.

Inventive Principle:
Principle #25Self-service

2Reliability

If nitrogen bottles or nitrogen generation system are used to supply inert gas, then the inerting function is ensured, but the space occupation increases

Engineering Contradiction:
Improveinerting functionVSAvoidspace occupation
Core Design Contradiction:
ReliabilityVSArea of stationary object

Solution Approach 1:

The system recirculates and reuses the inert gas atmosphere after it has performed its inerting function. The atmosphere is extracted from the casing, recirculated through the hydrogen system, and reused to maintain inert conditions, thereby eliminating the need for continuous fresh nitrogen supply and reducing the size of nitrogen storage bottles or generation systems.

Inventive Principle:
Principle #34Discarding and recovering

3Reliability

If halon is used as fire extinguishing agent, then fire suppression capability is provided, but environmental harm occurs and the solution is unsuitable for small volumes

Engineering Contradiction:
Improvefire suppression capabilityVSAvoidenvironmental harm
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The system converts the potentially harmful recirculated atmosphere (which could contain leaked hydrogen) into a beneficial fire suppression mechanism. By monitoring and controlling the recirculated gas composition, the system ensures that hydrogen concentrations remain below flammable limits, thereby using the atmosphere itself to prevent combustion rather than requiring separate fire suppression agents.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

Solution Approach 2:

The system maintains a permanently inert atmosphere through continuous recirculation and monitoring. By keeping hydrogen concentrations below 4% (the lower flammable limit) through controlled recirculation, the system creates an inherently fire-safe environment that eliminates the need for halon or other fire suppressants.

Inventive Principle:
Principle #39Inert atmosphere (Inert environment)

4Reliability

If nominal rate of nitrogen circulation is used based on worst case scenario, then safety limits are ensured, but the system efficiency decreases

Engineering Contradiction:
Improvesafety policy limitsVSAvoidsystem efficiency
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The system transitions from static nominal circulation to dynamic adaptive recirculation. The recirculation rate is continuously adjusted based on real-time hydrogen concentration measurements and leak detection, allowing the system to operate at minimum necessary rates during normal conditions and increase recirculation only when needed, thereby optimizing efficiency while maintaining safety.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system implements continuous feedback control by monitoring hydrogen concentrations and adjusting recirculation rates accordingly. Sensors detect hydrogen levels, and the control system modulates the recirculation pump speed to maintain safe concentrations, avoiding unnecessary high-rate circulation during low-risk periods and ensuring rapid response when leaks are detected.

Inventive Principle:
Principle #23Feedback

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 system reduces the amount of inert gas required, minimizing space and weight while effectively preventing fires by maintaining safe oxygen and hydrogen concentrations, and quickly detecting and extinguishing flammable mixtures.

Implementation Method 1

a fluid recirculation system configured to recirculate part of the fluid located inside the casing to the inlet conduct for supplying the recirculated fluid mixed with the pure inert gas to the inside of the casing

Methodology Applied
Scientific EffectFluid recirculation:

Implementation Method 2

sensing means configured to measure the concentration of oxygen and the concentration of hydrogen of a fluid located inside the casing

Methodology Applied
Scientific EffectGas concentration detection:

Implementation Method 3

The present invention provides a solution for the aforementioned problems, with an inerting system according to one or more embodiments described herein... configured to independently control at least the outlet valve and the fluid recirculation system based on the concentration of oxygen and the concentration of hydrogen inside the casing

Methodology Applied
Scientific EffectInerting:

Data Source

PatentUS20250100706A1Inerting system for an aircraft
Publication Date: 2025.03.27 AIRBUS OPERATIONS SL
  • US20250100706A1 patent drawing
  • US20250100706A1 patent drawing
  • US20250100706A1 patent drawing

AI summary

An inerting system for an aircraft and a method of inerting a hydrogen system in an aircraft. Also an aircraft with such an inert system. In the inerting system, a part of an inerting gas that has already been supplied to the casing of the hydrogen system is mixed with pure inerting gas through a fluid recirculation system.