Movable Passenger Seats for Sequential Emergency Ejection

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Solution Overview

Problem

Existing in-flight evacuation systems are complex, time-consuming, and require manual procedures, making them unreliable in emergency situations, and lack the ability to eject passenger seats sequentially for quick and safe passenger egress from an aircraft in case of an emergency.

Innovation Solution

An in-flight emergency evacuation system featuring a seating area with movable passenger seats on rails, automatic doors, and heavy-duty Kevlar domed parachutes, allowing for sequential ejection of passenger seats into emergency rooms, which can accommodate each row of seats independently and facilitate safe exit with minimal manual intervention, along with portable oxygen devices, protective shields, and airbags for shock absorption and flotation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If existing in-flight evacuation systems are used, then passengers can be evacuated from the aircraft, but the systems are complex and time-consuming requiring manual procedures

Engineering Contradiction:
Improveevacuation speedVSAvoidsystem complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The aircraft seating area is divided into multiple evacuation zones, each with its own emergency room and parachute system. Passenger seats are grouped in sets of three that can be independently ejected, allowing parallel evacuation operations that reduce overall time while maintaining manageable system complexity through modular design

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The evacuation system operates automatically without requiring manual procedures. The system self-activates upon detection of emergency conditions, automatically ejecting passenger seat sets sequentially through motorized mechanisms, thereby eliminating the need for complex manual operations while maintaining high evacuation speed

Inventive Principle:
Principle #25Self-service

2Reliability

If existing in-flight evacuation systems are used, then passengers can be evacuated, but they require manual procedures which are unreliable in emergency situations

Engineering Contradiction:
Improveevacuation reliabilityVSAvoidmanual operation requirement
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The system is designed to operate autonomously without manual intervention. Sensors detect emergency conditions and automatically trigger the evacuation sequence, making the system reliable in panic situations where manual operations would fail. The automatic door mechanisms and motorized seat ejection systems eliminate the need for human operation

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The system incorporates automatic detection and control mechanisms that monitor emergency conditions and regulate the evacuation process. Feedback loops ensure that each seat set is properly ejected and that the system responds appropriately to various emergency scenarios, enhancing reliability without requiring manual procedures

Inventive Principle:
Principle #23Feedback

3Speed

If sequential ejection of passenger seats is implemented, then quick and safe egress of passengers is achieved, but aircraft structural modifications are required

Engineering Contradiction:
Improveegress speedVSAvoidaircraft structural modification
Core Design Contradiction:
SpeedVSEase of manufacture

Solution Approach 1:

The aircraft structure is divided into modular evacuation zones with dedicated emergency rooms and ejection mechanisms. This segmentation allows for localized structural modifications rather than requiring complete aircraft redesign, enabling quick egress through targeted changes to specific sections while maintaining overall aircraft integrity

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The emergency rooms are positioned within the aircraft structure in a nested configuration, with each emergency room containing the necessary ejection mechanisms and parachutes. This nesting approach minimizes structural modifications by integrating evacuation systems within existing aircraft compartments rather than requiring extensive external modifications

Inventive Principle:
Principle #7Nested doll (Nesting)

4Reliability

If complex evacuation systems are used, then evacuation capability is provided, but the systems are time-consuming

Engineering Contradiction:
Improveevacuation capabilityVSAvoidevacuation time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The aircraft is divided into multiple independent evacuation zones that can operate simultaneously. Each zone has its own emergency room, motorized ejection system, and parachute deployment mechanism, allowing parallel evacuation operations that reduce total evacuation time while maintaining reliable evacuation capability through redundant systems

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Parachutes are pre-positioned and pre-checked within each emergency room before evacuation is needed. The motorized ejection systems are pre-configured and tested to ensure immediate operation. This preliminary preparation eliminates time-consuming setup procedures during actual evacuation while maintaining system reliability

Inventive Principle:
Principle #10Preliminary 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

Enables quick, safe, and efficient evacuation of passengers with reduced aircraft structural modifications, minimizing manual intervention and ensuring timely egress, even in panic situations, while providing necessary safety features for safe landing and location assistance post-emergency.

Implementation Method 1

at least one heavy-duty Kevlar domed parachute positioned underneath a middle seat of each row of the passenger seats configured to open during the ejection of the passenger seats outside the aircraft

Methodology Applied
Scientific EffectParachute: Parachute

Implementation Method 2

airbags for shock absorption and flotation

Methodology Applied
Scientific EffectAirbag:

Data Source

PatentUS20230142872A1In-flight emergency evacuation system
Publication Date: 2023.05.11 ALFADIL AYMEN
  • US20230142872A1 patent drawing
  • US20230142872A1 patent drawing
  • US20230142872A1 patent drawing

AI summary

The invention provides an in-flight emergency evacuation system in an aircraft which has a seating area comprising of plurality of rows of passenger seats which are positioned on plurality of rails. The passenger seats are slidably movable on the rails. The system further discloses at least one emergency room which is configured to accommodate the passenger seats inside it during an emergency condition for safely ejecting the passengers outside of the emergency rooms. During an emergency condition, the crew members of the aircraft can hit the evacuation button which automatically starts the evacuation process. Once the evacuation button is pressed, the slidably movable motorized passenger seats which are positioned on the rails starts moving in a sequential manner into the emergency room which is capable of accommodating one row of passenger seats at a time and ejecting it outside the aircraft.