Aircraft Stowable Seat Backrest Release Mechanism

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Solution Overview

Problem

Aircraft cabin stowable seats with exposed backrest latches pose safety risks due to potential tampering and compromise aesthetics with additional features needed to hide the latches.

Innovation Solution

A stowable seat design featuring a backrest support structure with integrated locking mechanisms, where a releasing member, such as a strap or wire, is hidden beneath a cushion, allowing the backrest to be rotated and locked without visible latches, ensuring security and simplicity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If exposed latches are used for the locking mechanism, then the backrest can be locked securely, but the safety is compromised due to potential tampering by unintended persons

Engineering Contradiction:
Improvelocking securityVSAvoidtampering risk
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The releasing member (pull strap) is extracted from the visible latch mechanism and relocated to a concealed position behind the seat cushion. The latch itself remains exposed but is rendered inoperable without accessing the concealed releasing member, thereby extracting the critical release function from public view while maintaining the visible locking indicator.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The pull strap acts as an intermediary element between the user and the latch mechanism. Instead of directly manipulating the latch, the user must first access and pull the concealed strap, which then actuates the latch release. This intermediary step prevents unintended operation while maintaining secure locking.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Ease of operation

If exposed latches are used for the locking mechanism, then the locking function is accessible, but the appearance is compromised due to extra parts and features needed to shroud the latches

Engineering Contradiction:
Improvelatch accessibilityVSAvoidbackrest appearance
Core Design Contradiction:
Ease of operationVSShape

Solution Approach 1:

The releasing function is extracted from the visible latch area and placed behind the cushion. The latch remains visible as a design element while the operational component (pull strap) is concealed, eliminating the need for cosmetic shrouding and maintaining clean lines.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The visible latch serves as a cosmetic copy or indicator of the locking state without being the actual operational element. The functional release mechanism is duplicated in a concealed location behind the cushion, allowing the visible latch to serve aesthetic purposes while the hidden strap provides the actual release function.

Inventive Principle:
Principle #26Copying

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 design enhances safety by concealing the locking mechanism, preventing unintended access and maintaining a clean aesthetic, while allowing easy operation of the backrest for flight attendants.

Implementation Method 1

a spring coupled to the first latch

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

A pin may be located in an aperture defined by the first latch. The pin and aperture may be configured to limit a rotation of the first latch

Methodology Applied
Scientific EffectMechanical constraint: Mechanical Force

Implementation Method 3

The releasing member may be located in the channel. Applying a load to the releasing member rotates a latch of the locking mechanism

Methodology Applied
Scientific EffectMechanical force transmission: Mechanical Force

Implementation Method 4

A cushion may be located over the backrest support and the releasing member

Methodology Applied
Scientific EffectFriction reduction: Lubrication

Data Source

PatentEP3473543B1Stowable seat with backrest release
Publication Date: 2022.02.23 AMI IND INC
  • EP3473543B1 patent drawingFigure 1
  • EP3473543B1 patent drawingFigure 2A
  • EP3473543B1 patent drawingFigure 2B

AI summary

A stowable seat (100) for an aircraft may comprise a housing (101) and a backrest support (160) configured to rotate relative to the housing (101). A locking mechanism (200a) comprising a first latch (202) may be coupled to the backrest support (160). A releasing member (170) may be in operable communication with the first latch (202). The releasing member (170) may be configured to rotate the first latch (202) relative to the backrest support (160). The releasing member (170) may be located behind a cushion (122) coupled to the backrest support (160).