Aircraft Emergency Oxygen Power Backup Using a Single Harness
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Solution Overview
Problem
The installation of two independent power harnesses in aircraft for emergency oxygen supply systems is cumbersome and expensive, and existing systems are not reliably operable in case of failure of the electric power supply system.
Innovation Solution
An aircraft emergency oxygen supply device with a backup electric power supply system, including an electric power storage device and a controller, that allows operation independent of the primary power supply, eliminating the need for an additional emergency power harness and simplifying installation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If two independent power harnesses are installed for emergency oxygen supply systems, then reliability is improved, but device complexity and installation cost increase
Solution Approach 1:
The patent combines the emergency power supply function with the existing primary power supply system by integrating a backup power storage device into the same power harness infrastructure. This merging approach eliminates the need for a completely separate emergency power harness while ensuring operational reliability during primary system failures.
Solution Approach 2:
The power harness is designed to serve dual functions: it operates as the primary power supply during normal conditions and automatically switches to backup power storage mode when primary power fails. This multi-functionality reduces the need for dedicated separate harnesses while maintaining reliability requirements.
2Reliability
If two independent power harnesses are installed for emergency oxygen supply systems, then reliability is improved, but installation cost increases
Solution Approach 1:
The patent combines the emergency power supply function with the existing primary power supply system by integrating a backup power storage device into the same power harness infrastructure. This merging approach eliminates the need for a completely separate emergency power harness while ensuring operational reliability during primary system failures.
Solution Approach 2:
The power harness is designed to serve dual functions: it operates as the primary power supply during normal conditions and automatically switches to backup power storage mode when primary power fails. This multi-functionality reduces the need for dedicated separate harnesses while maintaining reliability requirements.
3Device complexity
If existing power supply is used for charging backup power storage device, then device complexity is reduced, but power supply reliability may be affected
Solution Approach 1:
The backup power storage device is charged in advance during normal operation when the primary power supply is functional. This preliminary charging action ensures that sufficient energy is stored before any potential failure occurs, enabling immediate switch to backup power without compromising reliability when needed.
Solution Approach 2:
The system maintains a charged backup power storage device as a cushion against potential primary power failures. By continuously or periodically charging the backup storage during normal operation, the system prepares in advance to cushion against future power supply disruptions, ensuring operational continuity.
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
Ensures reliable operation of emergency oxygen supply devices even in power supply failures without additional harnesses, reducing complexity and cost by using existing power for charging and providing backup power as needed.
Implementation Method 1
a backup electric power supply system, which includes at least one electric power storage device
Data Source
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AI summary
An aircraft emergency oxygen supply device (2) comprises an oxygen source (20) for supplying oxygen gas; a backup electric power supply system (28), comprising at least one electric power storage device (29); and a controller (26) for controlling the operation of the aircraft emergency oxygen supply device (2). The aircraft emergency oxygen supply device (2) is electrically connectable to an aircraft electric power supply system (34) for being supplied with electric power provided by the aircraft electric power supply system (34); the at least one electric power storage device (29) is chargeable by electric power provided by the aircraft electric power supply system (34); and the aircraft emergency oxygen supply device (2) is operational with electric power provided by the backup electric power supply system (28).