Aircraft Oxygen Mask Dynamic Flow Control

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Solution Overview

Problem

Current oxygen mask systems for aircraft do not accurately determine the minimum oxygen flow required to maintain safe blood-oxygen saturation levels at varying altitudes, leading to oversupply and inefficient use of oxygen.

Innovation Solution

A method using sensors and a controller to detect blood-oxygen saturation levels at different altitudes and determine a minimum oxygen flow rate, adjusting the oxygen concentration and duration to match baseline levels, thereby optimizing oxygen supply.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If continuous flow oxygen masks are used to supply oxygen at altitude, then passengers receive supplemental oxygen to prevent hypoxia, but oxygen is oversupplied and consumed inefficiently

Engineering Contradiction:
Improveoxygen supply reliabilityVSAvoidoxygen consumption efficiency
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The system dynamically adjusts oxygen flow rate based on real-time blood oxygen saturation levels and altitude data. Instead of continuous fixed flow, the controller modulates flow to match actual physiological needs, maintaining safety while reducing waste

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system uses blood oxygen saturation sensors to provide feedback to the controller, which then adjusts oxygen delivery accordingly. This closed-loop control ensures oxygen is supplied only when and at the rate needed, preventing oversupply and improving efficiency

Inventive Principle:
Principle #23Feedback

2Reliability

If oxygen flow rate is increased to ensure adequate oxygen supply at higher altitudes, then blood-oxygen saturation levels are maintained, but oxygen consumption increases

Engineering Contradiction:
Improveblood-oxygen saturation maintenanceVSAvoidoxygen quantity consumed
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The system changes oxygen flow rate parameters based on detected altitude and blood oxygen saturation levels. At higher altitudes or when saturation drops, flow rate increases; when conditions improve, flow rate decreases, optimizing the balance between safety and consumption

Inventive Principle:
Principle #35Parameter changes

3Device complexity

If fixed oxygen flow rates are used in oxygen masks, then system design is simplified, but oxygen supply does not adapt to varying altitude conditions

Engineering Contradiction:
Improveoxygen mask system complexityVSAvoidaltitude adaptation capability
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The oxygen mask system transitions from static fixed flow to dynamic adjustable flow based on altitude and physiological feedback. The controller and sensor integration enables real-time adaptation while maintaining relatively simple overall system architecture

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system uses onboard sensors to automatically detect altitude and blood oxygen levels, and the controller automatically adjusts flow rates without requiring manual intervention. The system serves itself by monitoring and adapting to changing conditions

Inventive Principle:
Principle #25Self-service

Data Source

PatentUS12121759B2Method of supplying oxygen to an aircraft oxygen mask
Publication Date: 2024.10.22 AVOX SYSTEMS INC
  • US12121759B2 patent drawing
  • US12121759B2 patent drawing

AI summary

A method of supplying oxygen to an oxygen mask for an aircraft includes detecting, with at least one sensor and during a first time period, a first blood-oxygen saturation level at a first altitude. The method may also include detecting, with the at least one sensor and during a second time period, a second blood-oxygen saturation level at a second altitude that is different from the first altitude. The method may include determining a minimum flow rate of a gas that includes oxygen for the second altitude such that the second blood-oxygen saturation level at least matches the first blood-oxygen saturation level at the same altitude.