3-Way Valve Inadvertent Slide Deployment Prevention

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Solution Overview

Problem

Inflatable aircraft emergency evacuation slides are prone to inadvertent in-flight deployment, leading to unpredictable and unsafe consequences such as additional drag, structural damage, and potential departure from the aircraft.

Innovation Solution

A system utilizing a 3-way valve with a compressed gas source and actuator that connects the gas supply to either a vent line or a supply line based on flight status, ensuring the inflatable slide only deploys safely on the ground by venting gas overboard during flight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If inflatable evacuation slides are installed in aircraft to provide emergency evacuation capability, then safety of occupants during emergency evacuation is improved, but the risk of inadvertent in-flight deployment increases

Engineering Contradiction:
Improveemergency evacuation safetyVSAvoidinadvertent deployment risk
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

A 3-way valve is introduced as an intermediary component between the compressed gas source and the inflatable slide. This valve acts as a mediator that controls gas flow based on aircraft status signals, preventing direct connection during flight and eliminating the harmful effect of inadvertent deployment while preserving emergency evacuation capability on the ground

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The system automatically responds to aircraft status conditions without requiring manual intervention. The 3-way valve receives control signals from aircraft systems and autonomously directs compressed gas either to the inflatable slide or to a vent, enabling the system to self-regulate based on whether the aircraft is in flight or on the ground

Inventive Principle:
Principle #25Self-service

2Speed

If compressed gas is continuously supplied to the inflatable slide for rapid deployment, then deployment speed is improved, but the danger of in-flight inflation increases

Engineering Contradiction:
Improvedeployment speedVSAvoidin-flight inflation hazard
Core Design Contradiction:
SpeedVSObject-affected harmful factors

Solution Approach 1:

The gas supply system transitions from a static continuous supply to a dynamic controlled supply. The 3-way valve dynamically adjusts the gas flow path based on real-time aircraft status, connecting the compressed gas source to the inflatable slide only when aircraft status indicates ground operation, thereby enabling rapid deployment when needed while preventing in-flight inflation

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system takes preliminary protective action by venting compressed gas to a safe location (overboard or to atmosphere) during flight conditions. This preliminary anti-action prevents the harmful effect of in-flight inflation by ensuring that compressed gas cannot reach the inflatable slide during flight, while still allowing rapid deployment when the valve switches to supply mode on the ground

Inventive Principle:
Principle #9Preliminary anti-action

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

Prevents inadvertent in-flight inflation of inflatable slides, ensuring safe aircraft operation by ensuring deployment only occurs on the ground, thereby avoiding drag and structural issues.

Implementation Method 1

A 3-way valve having an input port and a pair of output ports each being individually connectable to the input port. A supply line is provided to supply compressed gas from the source thereof to the input port of the 3-way valve while a vent and supply lines are provided to fluid connect first and second ones of the output ports of the 3-way valve to an outside environment and the inflatable slide, respectively.

Methodology Applied
Scientific EffectPneumatic control:

Implementation Method 2

The actuator may therefore be adapted to receive the control signal to operate the 3-way valve so as to fluid-connect the source of compressed gas with the supply line in response to a signal indicative of an operative ground condition of the aircraft.

Methodology Applied
Scientific EffectElectromechanical actuation:

Data Source

PatentUS10843805B2Systems to prevent inadvertent in-flight deployment of inflatable aircraft emergency evacuation slides
Publication Date: 2020.11.24 YABORA IND AERONAUTICA SA
  • US10843805B2 patent drawing
  • US10843805B2 patent drawing

AI summary

Inadvertent in-flight inflation of an inflatable slide associated with a non-co-located over-wing emergency door of an aircraft fuselage is prevented by a system having a source of compressed gas (e.g., a compress air cylinder) and a 3-way valve having an input port and a pair of output ports each being individually connectable to the input port. The 3-way valve is operable in response to a control signal so as to fluid-connect the source of compressed gas with either a vent line which vents the compress gas overboard or a supply line the inflatable slide. When the control signal fluid connects the gas source to the vent line, the system will be in a safe in-flight mode indicative of inflight operation of the aircraft in which case inadvertent inflation of the slide is prevented.