Deployable Floor Panel With Foldable Seat For Aircraft Cabin

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Solution Overview

Problem

Current methods for changing the cargo-to-passenger ratio in aircraft cabin areas are time-consuming and inefficient, requiring complete removal of seat arrangements, which occupy valuable space and are exposed to weather conditions during reconfiguration.

Innovation Solution

A deployable floor panel arrangement with a foldable seat configuration that reduces dimensions by pivoting the backrest and leg arrangement, allowing for quick conversion between passenger and cargo transport modes without removing the seat arrangements from the aircraft.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If seat arrangements are completely removed from the aircraft cabin area for cargo transport, then cargo transport capacity is improved, but reconfiguration time increases and seat arrangements are exposed to weather conditions

Engineering Contradiction:
Improvecargo transport capacityVSAvoidreconfiguration time
Core Design Contradiction:
Adaptability or versatilityVSLoss of time

Solution Approach 1:

The seat arrangement is designed with movable components that can dynamically change configuration. The backrest can pivot between a deployed position (extending at an angle of approximately 80° to 180° to the floor panel) for passenger transport and a stowed position (extending at an angle of approximately 0° to 40° to the floor panel) for cargo transport, eliminating the need for complete removal and reducing reconfiguration time

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If seat arrangements are completely removed from the aircraft cabin area, then cargo transport capacity is improved, but seat arrangements must be stored at airports and handled manually

Engineering Contradiction:
Improvecargo transport capacityVSAvoidreconfiguration operation
Core Design Contradiction:
Adaptability or versatilityVSEase of operation

Solution Approach 1:

The seat arrangement incorporates a movable backrest that can be pivoted between deployed and stowed positions. This dynamic design allows the seat to remain permanently mounted on the floor panel while adapting its configuration, eliminating manual detachment and transportation of seats to and from the aircraft

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The seat arrangement is designed to perform multiple functions: it can accommodate passengers when the backrest is in the deployed position and can be converted to a cargo-friendly configuration when the backrest is stowed. This multi-functionality allows a single permanently-mounted structure to serve both passenger and cargo transport needs

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

3Adaptability or versatility

If seat arrangements are completely removed from the aircraft cabin area, then cargo transport capacity is improved, but the process requires manual detachment and transporting of seats

Engineering Contradiction:
Improvecargo transport capacityVSAvoidseat arrangement structure
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The seat arrangement uses a pivoting backrest mechanism that allows the structure to dynamically reconfigure between passenger and cargo modes. This dynamic design replaces the complexity of complete removal and reinstallation with a simpler in-situ transformation mechanism

Inventive Principle:
Principle #15Dynamics

4Ease of operation

If the backrest is kept in deployed position, then passenger comfort is improved, but space occupancy increases and limits cargo dimensions

Engineering Contradiction:
Improvepassenger comfortVSAvoidspace occupancy
Core Design Contradiction:
Ease of operationVSVolume of moving object

Solution Approach 1:

The backrest is designed as a movable component that can pivot between deployed and stowed positions. When deployed, it provides passenger comfort at an angle of approximately 80° to 180° to the floor panel. When stowed, it reduces space occupancy by extending at an angle of approximately 0° to 40° to the floor panel, allowing larger cargo dimensions

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP2939920B1Deployable floor panel arrangement for aircraft cabin area
Publication Date: 2021.10.13 AIRBUS OPERATIONS GMBH
  • EP2939920B1 patent drawingFigure 1a~1f
  • EP2939920B1 patent drawingFigure 2~2-7
  • EP2939920B1 patent drawingFigure 3~3-3

AI summary

The invention relates to a deployable floor panel (10) arrangement for an aircraft cabin area (50) comprising a substantially planar floor panel (12) with at least one foldable seat arrangement (14) mounted thereto. The seat arrangement (14) comprises at least one backrest (16) which is configured to be moveable between a stowed position in which it extends at an angle (α) of approximately 0° to 40° to the plane of the floor panel (12) and a deployed position in which it extends at an angle (α) of approximately 80° to 180° to the plane of the floor panel (12).