Aircraft Seat Backrest Locking Mechanism With Reduced Mass

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Solution Overview

Problem

Existing aircraft seat mechanisms require high-mass components to lock the backrest, which is disadvantageous for aircraft applications due to weight constraints.

Innovation Solution

A seat design featuring a pivot connection and a rack-type locking mechanism with a ring and indexer system, utilizing asymmetrical toothing profiles and elastic return means to reduce the mass of the blocking member, allowing for adjustable backrest inclination while minimizing weight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a traditional locking mechanism is used to lock the backrest, then the backrest can be securely locked at the desired inclination, but the mass of the locking member increases

Engineering Contradiction:
Improvelocking reliabilityVSAvoidmass of locking member
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The locking mechanism is divided into two independent functional components: a rack-type locking member that engages with the arm, and a separate indexer that locks the ring in rotation. This segmentation allows each component to be optimized for its specific function, reducing the overall mass while maintaining reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The arm acts as an intermediary element between the backrest and the locking member. It transmits forces from the backrest to the locking member, reducing the forces to which the locking member is directly subjected. This force reduction allows for a lighter locking member design while maintaining adequate locking strength.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Strength

If the locking member is designed to withstand high forces, then it can securely lock the backrest, but its mass increases

Engineering Contradiction:
Improvelocking strengthVSAvoidmass of locking member
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The arm serves as a force-distributing intermediary that reduces the peak forces transmitted to the locking member. By distributing forces more efficiently through the arm, the locking member can be designed with lower strength requirements, directly reducing its mass.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The locking mechanism utilizes rotational locking of the ring around the front transverse beam, adding a dimensional aspect to the force distribution. This rotational constraint distributes forces across different directions, reducing the burden on any single component and allowing for lighter design.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

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 reduces the mass of the blocking member by distributing forces more efficiently, enabling adjustable backrest inclination without increasing the overall seat mass, and allows for easy locking and unlocking of the backrest position.

Implementation Method 1

the teeth of the slider teeth and the teeth of the toothed sector have asymmetrical tooth profiles sized to ensure locking of the ring when the indexer is engaged and a thrust is exerted on the backrest to increase its inclination, and to cause disengagement of the indexer when sufficient thrust is exerted on the backrest to reduce its inclination

Methodology Applied
Scientific EffectAsymmetrical tooth profiling:

Implementation Method 2

comprising elastic return means returning the slide to its disengaged position

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 3

a pivot connection carried by a rear transverse beam of the lower frame and by which the upper frame is connected to the lower frame

Methodology Applied
Scientific EffectPivot connection: Hinge

Implementation Method 4

a rack-type locking member carried at least in part by a front transverse beam of the lower frame, and capable of being in an engaged state to lock the front end in its current position

Methodology Applied
Scientific EffectRack and pinion engagement: Rack and Pinion

Data Source

PatentEP4101766B1Aircraft seat comprising an adjustable backrest
Publication Date: 2024.04.03 EXPLISEAT
  • EP4101766B1 patent drawingFigure 1~2
  • EP4101766B1 patent drawingFigure 3~4
  • EP4101766B1 patent drawingFigure 5~6

AI summary

The invention relates to a seat (1) intended to be fixed to the floor of a vehicle, comprising a seat (2) incorporating a lower frame (6), and a backrest (4) incorporating an upper frame (11) linked to the lower frame (6), the inclination of this backrest (4) being adjustable between a minimum inclination and a maximum inclination, this seat (1) comprising: - a pivot joint (P1) carried by a rear transverse beam (14) of the lower frame (6) and by which the upper frame (11) is linked to the lower frame (6); - an arm (23) rigidly attached to the upper frame (11) and comprising a front end (24); - a locking member (25) carried at least in part by a front transverse beam (13) of the lower frame (6), and being able to be in an engaged state to lock the front end (24) in its current position or in a disengaged state to release the front end (24).