Aircraft Oxygen Conservation System Using Respiratory Timing

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Emergency oxygen supply systems on aircraft are inefficient, leading to the need for excessive oxygen storage and generation, which increases weight and reduces payload capacity and safety margins.

Innovation Solution

The system adjusts oxygen delivery to each passenger based on their actual demand, timing it for maximum absorption in the lungs and using cabin air to supplement, thereby minimizing the volume and weight of oxygen required.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If continuous oxygen flow is provided at a rate calculated to accommodate worst case scenario, then all passengers are sustained until cabin pressure is reestablished, but oxygen storage weight increases significantly

Engineering Contradiction:
Improveoxygen supply reliabilityVSAvoidoxygen storage weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The system switches from continuous oxygen flow to periodic/demand-based flow by detecting patient respiratory cycles. Oxygen is delivered during inhalation phases and stopped during exhalation phases, converting continuous action into periodic action that matches actual physiological needs, thereby reducing overall oxygen consumption while maintaining adequate oxygenation.

Inventive Principle:
Principle #19Periodic action

Solution Approach 2:

The system uses feedback from respiratory cycle detection (via flow sensors or pressure sensors monitoring inhalation/exhalation patterns) to dynamically control oxygen delivery. The detected respiratory signals feed back to the oxygen flow control mechanism, adjusting flow rates in real-time to match actual demand rather than relying on fixed worst-case calculations.

Inventive Principle:
Principle #23Feedback

2Reliability

If oxygen flow rate is increased to satisfy passengers with larger than average tidal volume and faster respiration rate, then oxygenation needs are met, but oxygen consumption increases

Engineering Contradiction:
Improveoxygenation adequacyVSAvoidoxygen consumption
Core Design Contradiction:
ReliabilityVSQuantity of substance

Solution Approach 1:

The system transitions from static fixed flow rates to dynamic flow rates that adapt to individual patient characteristics. By continuously monitoring respiratory parameters (tidal volume, respiration rate, inhalation/exhalation timing) and adjusting oxygen flow accordingly, the system optimizes delivery for each patient's actual needs rather than using universal worst-case parameters.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes oxygen delivery parameters (flow rate, timing, duration) based on detected respiratory cycle characteristics. Flow rate is modulated according to inhalation flow demands, and delivery timing is synchronized with respiratory phases, allowing parameter optimization that reduces total oxygen consumption while maintaining adequate oxygenation.

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If constant flow of oxygen is directed into reservoir bag upon deployment, then oxygen is always available for inhalation, but system efficiency decreases

Engineering Contradiction:
Improveoxygen availabilityVSAvoidsystem efficiency
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

The system maintains continuous monitoring of respiratory cycles and continuous readiness to deliver oxygen, but actual oxygen flow is interrupted to coincide only with useful inhalation phases. This preserves the continuous availability capability while eliminating wasteful continuous flow during exhalation phases when oxygen cannot be utilized.

Inventive Principle:
Principle #20Continuity of useful action

Solution Approach 2:

The system allows the patient's own respiratory cycle to trigger and control oxygen delivery timing. The patient's inhalation action automatically initiates oxygen flow without external intervention, making the system self-regulating and eliminating the need for continuous external control while maintaining adequate oxygen supply.

Inventive Principle:
Principle #25Self-service

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 approach reduces oxygen consumption, allowing for a significant weight savings or increased safety margin by optimizing oxygen use, matching delivery to individual respiratory needs and using compressed oxygen for efficient distribution.

Implementation Method 1

a pressure sensor fitted to each mask to detect when the patient is exhaling

Methodology Applied
Scientific EffectPressure detection: Pressure Gradient

Implementation Method 2

an inlet valve on the oxygen supply line for each reservoir to be controlled by a controller to deliver an allotment of oxygen to each reservoir upon detection of exhalation by the pressure sensor

Methodology Applied
Scientific EffectGas flow control: Valve

Implementation Method 3

timing it for maximum absorption in the lungs

Methodology Applied
Scientific EffectOxygen absorption: Absorption (physical)

Implementation Method 4

using cabin air to supplement, thereby minimizing the volume and weight of oxygen required

Methodology Applied
Scientific EffectGas mixing: Diffusion

Data Source

PatentUS7588032B2Oxygen conservation system for commercial aircraft
Publication Date: 2009.09.15 BE INTELLECTUAL PROPERTY INC
  • US7588032B2 patent drawing
  • US7588032B2 patent drawing
  • US7588032B2 patent drawing

AI summary

An emergency oxygen supply system for use on aircraft in the event of a loss in cabin pressure is configured for delivering allotments of oxygen and timing the delivery such allotments to each passenger so as maximize the efficiency of the transfer of such oxygen into the passenger's bloodstream. The delivery of each allotment is selected so that the entire allotment is available for inhalation into the region of the lung most efficient at oxygen transfer while the volume of the allotment is selected to substantially coincide with the volume of such region of the lung.