Fluid Cell Cushion for Aircraft Seat Comfort

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Solution Overview

Problem

Commercial aircraft seats provide limited adjustability and comfort due to their constrained design, leading to reduced passenger comfort during long flights.

Innovation Solution

A shape-adapting system for cushion assemblies, comprising a support base with fluid-retaining cells connected by a fluid exchange sub-system and valves, allowing fluid migration to change the shape of the support base, which can be controlled to enhance comfort and support.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If a conventional fixed design is used for aircraft seats, then the device complexity is reduced, but passenger comfort and adjustability deteriorate

Engineering Contradiction:
Improveseat adjustabilityVSAvoidseat structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The seat cushion is divided into multiple independent cells that can be individually inflated or deflated. Each cell acts as an independent unit, allowing localized adjustment of support and pressure distribution without affecting the entire seat structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The seat transitions from a static fixed structure to a dynamic adjustable structure using inflatable cells that can change volume and shape in response to control signals, enabling real-time adaptation to passenger needs.

Inventive Principle:
Principle #15Dynamics

2Weight of moving object

If lightweight materials and structures are used, then fuel consumption is reduced, but structural strength and support capability deteriorate

Engineering Contradiction:
Improveseat weightVSAvoidsupport capability
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

Inflatable cells use pneumatic pressure to generate structural support and load-bearing capability. The pressurized air or gas within the cells provides the necessary strength and rigidity to support passenger weight while maintaining a lightweight structure when deflated or partially inflated.

Inventive Principle:
Principle #29Pneumatics and hydraulics

Solution Approach 2:

The cells are constructed from flexible materials that can deform and adapt to applied loads. These thin-walled structures provide sufficient strength through their geometric configuration and internal pressure rather than through heavy material construction.

Inventive Principle:
Principle #30Flexible shells and thin films

3Ease of operation

If fixed shape cushion assemblies are used, then manufacturing simplicity is maintained, but passenger comfort during long flights deteriorates

Engineering Contradiction:
Improvecomfort adjustmentVSAvoidfluid exchange system
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The fluid exchange subsystem automatically redistributes fluid between cells in response to pressure changes and passenger movement, providing self-adjusting comfort features without requiring complex active control systems for each individual cell.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The fluid exchange subsystem serves multiple functions: it enables shape adjustment, provides pressure redistribution, and allows connectivity between cells for balanced fluid distribution, replacing the need for multiple independent control systems.

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 system increases passenger comfort by allowing adjustable support and pressure points, reducing weight and fuel consumption, making it suitable for aircraft use.

Implementation Method 1

the valve(s) is configured to move between an open position in which the fluid is able to migrate among the cells to change a shape of the support base

Methodology Applied
Scientific EffectFluid migration:

Implementation Method 2

At least one of the cells may be formed of an elastomeric material

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Implementation Method 3

A pump may be in fluid communication with the fluid exchange sub-system. The pump is configured to be operated to selectively inflate and deflate the cells

Methodology Applied
Scientific EffectHydraulic pressure control: Hydraulic Press

Data Source

PatentUS10850655B2Shape adapting system and method for a cushion assembly
Publication Date: 2020.12.01 THE BOEING CO
  • US10850655B2 patent drawing
  • US10850655B2 patent drawing
  • US10850655B2 patent drawing

AI summary

A shape adapting system of a cushion assembly and method of forming a shape adapting system of a cushion assembly include an array of cells that retain a fluid, a fluid exchange sub-system coupled to the cells, wherein the fluid exchange sub-system fluidly connects the cells together, and at least one valve coupled to the fluid exchange sub-system. The valve(s) is configured to move between an open position in which the fluid is able to migrate among the cells to change a shape of the support base, and a closed position in which the shape of the support base is maintained.