Wireless Evacuation Slide Lighting via Piezoelectric Energy Harvesting
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Solution Overview
Problem
Conventional aircraft evacuation slide lighting systems face challenges with compact packaging, leading to wiring damage and reliability issues, making it difficult to ensure adequate illumination during emergencies due to inaccessible components and complex deployment conditions.
Innovation Solution
A self-powered, wireless lighting system using piezoelectric sensors to generate electrical energy from vibrations and fluid pressure changes within the evacuation slide, powering independent lighting modules with LEDs, eliminating the need for traditional wiring and enhancing reliability.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If conventional wired lighting systems are used in evacuation slides, then illumination can be provided, but wiring damage and reliability issues occur during compact packaging and deployment
Solution Approach 1:
The patent extracts and removes the wiring harness from the lighting system, replacing it with a wireless power transmission system using electromagnetic fields. This eliminates the physical wires that cause damage during packaging and deployment, directly resolving the reliability issue while reducing device complexity.
Solution Approach 2:
The patent replaces the mechanical wiring system with an electromagnetic field-based power transmission system. Instead of using physical wires to transmit power and signals, the system uses electromagnetic induction to wirelessly power the LED lights, eliminating the mechanical wiring that causes reliability problems.
2Volume of moving object
If lighting components are made inaccessible to save space during stowing, then compact packaging is achieved, but component accessibility and maintenance become difficult
Solution Approach 1:
The patent implements a lighting system that requires no manual intervention for operation or maintenance. The wireless power system automatically activates upon slide deployment through detection of motion or pressure changes, and the solid-state LED components have long lifespans with no moving parts requiring maintenance, making the system self-sufficient.
Solution Approach 2:
The patent uses solid-state LED components that are inexpensive, durable, and have long operational lifespans. These components are designed to be replaced as simple units if needed, and their solid-state nature makes them highly resistant to damage from packaging and deployment stresses.
3Duration of action of moving object
If traditional battery-powered lighting systems are used, then illumination is provided, but energy supply duration and weight increase
Solution Approach 1:
The patent replaces the battery-powered electrical system with a wireless electromagnetic power transmission system. Power is transmitted through electromagnetic fields from a transmitter to receiver coils, eliminating the need for heavy battery packs while providing continuous illumination throughout the evacuation process.
Solution Approach 2:
The wireless power transmission system serves multiple functions: it provides power to the LED lights, detects slide deployment through motion sensing, and can potentially communicate system status. This multi-functionality reduces the overall system weight compared to separate battery, sensor, and communication components.
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
The solution provides reliable and efficient illumination for aircraft evacuation slides by eliminating wiring damage and single-point failures, ensuring consistent lighting during emergencies and reducing maintenance needs.
Implementation Method 1
a piezoelectric sensor operably connected to the light source and configured to generate electrical energy based upon a change in fluid pressure inside the evacuation slide
Data Source
AI summary
A self-powered, wireless lighting system for an aircraft evacuation system. The lighting system includes a piezoelectric sensor configured to generate electrical energy under an aircraft evacuation event when the aircraft evacuation system is deployed, and a first light source disposed on the aircraft evacuation system, the first light source configured to provide illumination to the aircraft evacuation system. The piezoelectric sensor is operably connected to the first light source and configured to supply electrical energy to the light source based on vibrations in the evacuation system during deployment of the evacuation system and during use of the evacuation system as passengers evacuate the aircraft.


