Aircraft Seat Backrest Parachute Integration

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Solution Overview

Problem

Existing sitting-type lifesaving parachutes for aircraft seats cause pilot fatigue due to shoulder pressure, can get hooked with cabin devices, and hinder rapid emergency egress due to pack placement.

Innovation Solution

An aircraft seat backrest with a quick-release mechanism and back-type lifesaving parachute integration, where the parachute pack is secured on a back plate assembly, allowing for easy detachment and reducing shoulder pressure and hooking risks.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the lifesaving parachute pack is placed in the seat pan and the lifesaving straps are worn on the pilot's body, then the pilot can be secured for parachuting, but the pilot's shoulder is pressed causing fatigue during long-time flight

Engineering Contradiction:
Improvelifesaving functionVSAvoidshoulder pressure and fatigue
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent inverts the conventional sitting-type parachute configuration by placing the parachute pack on the backrest instead of in the seat pan, and positioning the straps on the back rather than the front body. This inversion moves the pressing force from the shoulder area to the broader back area, significantly reducing shoulder pressure and fatigue while maintaining effective restraint for parachuting.

Inventive Principle:
Principle #13The other way round (Inversion)

2Ease of operation

If the lifesaving parachute pack is placed in the seat pan, then the pilot can access it, but it may hook with other devices in the cabin when the pilot moves rapidly during emergency

Engineering Contradiction:
Improveaccess to parachuteVSAvoidhooking with cabin devices
Core Design Contradiction:
Ease of operationVSObject-affected harmful factors

Solution Approach 1:

The patent extracts the parachute pack from the seat pan environment and relocates it to the backrest structure. This extraction removes the source of potential hooking problems, as the pack is now positioned on the backrest where it cannot interact with cabin devices during rapid movement, while the straps remain accessible for the pilot to don quickly.

Inventive Principle:
Principle #2Taking out (Extraction)

3Reliability

If the lifesaving parachute pack is connected to the pilot's body in the conventional position, then the pilot can be restrained, but it affects the power generated when the pilot needs to rapidly move, delaying emergency off-plane time

Engineering Contradiction:
Improverestraint functionVSAvoidemergency egress time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The patent inverts the strap positioning from front-body attachment to back attachment. This allows the pilot to don the straps more quickly by accessing them from behind the backrest, and the restraint force is applied to the back rather than the front, reducing interference with rapid forward movement during emergency egress.

Inventive Principle:
Principle #13The other way round (Inversion)

4Reliability

If the back plate is permanently fixed to the backrest body, then the parachute pack is securely held, but the seat cannot be quickly reconfigured or removed for maintenance

Engineering Contradiction:
Improvesecure attachmentVSAvoidquick reconfiguration
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The patent implements a dynamic attachment system with quick-release mechanisms that allow the back plate to transition between securely fixed and easily removable states. The locking pieces with spring-loaded locking pins provide secure attachment during normal use, while enabling rapid release when reconfiguration or maintenance is needed, adapting to different operational requirements.

Inventive Principle:
Principle #15Dynamics

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 cabin movement and emergency egress without shoulder pressure and reduces the risk of hooking, facilitating efficient use in aircraft seats for pilots and operators.

Implementation Method 1

a spring enabling the locking pin to press an end part of the lock shell

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

lifesaving parachute pack

Methodology Applied
Scientific EffectDrag: Drag

Data Source

PatentUS12030643B2Aircraft seat backrest with lifesaving function
Publication Date: 2024.07.09 AEROSPACE LIFE SUPPORT IND LTD
  • US12030643B2 patent drawing
  • US12030643B2 patent drawing
  • US12030643B2 patent drawing

AI summary

An aircraft seat backrest with a lifesaving function, including a backrest body and a back plate assembly, wherein a containing cavity is arranged in a front face of the backrest body, the back plate assembly includes a back plate covering the containing cavity and a lifesaving parachute pack that is arranged on a back face of the back plate and contained in the containing cavity, the back plate is fixedly connected with the backrest body through a quick release mechanism in a quickly separable manner, lifesaving straps of the lifesaving parachute pack pass through strap through holes in the back plate, and an occupant leans against the back plate and is connected with the back plate and the lifesaving parachute pack through the lifesaving straps when riding.