Aircraft Oxygen Mask Activation With Decentralized Flow Control

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Solution Overview

Problem

Current emergency oxygen systems in aircraft face challenges such as complexity, high power demand, electromagnetic interference, maintenance intensity, and difficulty in activating multiple face masks with a single motion, which increases installation costs and risks.

Innovation Solution

A decentralized system with a control unit integrated into each face mask, activated by a single pulling motion, eliminating the need for complex wiring and reducing power requirements, while ensuring electromagnetic compatibility and compliance with aviation regulations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a single central control system is used to control multiple face masks, then the system can be activated with a single motion, but the system complexity increases and the risk of multiple failures increases

Engineering Contradiction:
Improveactivation simplicityVSAvoidcontrol system complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The patent divides the single central control system into multiple independent control units, each integrated into a separate face mask. This segmentation allows each mask to function independently, eliminating the risk that a single control failure will disable all masks, while still maintaining simple activation through individual mask deployment

Inventive Principle:
Principle #1Segmentation

2Quantity of substance

If a single central control system with multiple valves is used, then multiple passengers can be served, but the power requirement increases necessitating connection to aircraft power supply

Engineering Contradiction:
Improvenumber of passengers servedVSAvoidpower consumption
Core Design Contradiction:
Quantity of substanceVSUse of energy by moving object

Solution Approach 1:

The patent segments the power consumption by providing each face mask with its own control unit and power source (battery). This eliminates the need for a high-power central system connected to aircraft power supply, as each mask operates independently with low power requirements suitable for battery operation

Inventive Principle:
Principle #1Segmentation

3Reliability

If sensors are connected to central control system by long wires, then breathing characteristics can be monitored, but electromagnetic interference with other aircraft systems occurs

Engineering Contradiction:
Improvebreathing monitoring capabilityVSAvoidelectromagnetic interference
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent extracts the control unit and sensors from the central control system and integrates them directly into each face mask. This eliminates the long connecting wires that act as aerials, thereby removing the source of electromagnetic interference while preserving the breathing monitoring function within each mask

Inventive Principle:
Principle #2Taking out (Extraction)

4Reliability

If complex redundant control systems are installed, then multiple fatalities can be avoided, but maintenance intensity increases and system becomes harder to install

Engineering Contradiction:
Improvesafety against fatalitiesVSAvoidinstallation ease
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent segments the safety function into multiple independent control units distributed across different face masks. This modular approach maintains safety through redundancy while simplifying installation, as each self-contained mask unit can be independently installed without complex system integration

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Each face mask with its integrated control unit operates as a self-service module, requiring minimal integration with aircraft systems. This self-contained design reduces maintenance intensity and simplifies both initial installation and subsequent servicing

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS20260034386A1A system for supplying a breathable gas to a user
Publication Date: 2026.02.05 AVIATION WORKS LTD
  • US20260034386A1 patent drawing
  • US20260034386A1 patent drawing
  • US20260034386A1 patent drawing

AI summary

A system for supplying a breathable gas to a user comprises: at least one face mask comprising: a gas feed tube for connection to a vessel containing a supply of breathable gas; and a control system for controlling a flow of the breathable gas from the vessel when the gas feed tube is connected thereto and the control system is in an operative condition; a holder for holding the at least one face mask in a location in space while the control system is in a non-operative condition; and an activation device responsive to displacement of the at least one face mask away from the location in space, so as to activate the flow of the breathable gas from the vessel and to activate the operative condition of the control system, thereby to activate a controllable flow of the breathable gas to the user.