Aircraft Headrest With Oblique Deployable Side Supports

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Solution Overview

Problem

Existing headrests lack sufficient configurability to provide effective support for the sides of the head, limiting comfort and ergonomics, especially in seats designed for safety and comfort like aircraft passenger seats.

Innovation Solution

A headrest assembly with a center portion and deployable left and right ears, where each ear is equipped with a dogleg support that rotates about an axis oblique to the center portion's plane, allowing the ears to move between stowed and deployed positions for enhanced side support.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If traditional headrest design with limited height and tilt adjustment is used, then the structure is simple and easy to manufacture, but the configurability to support the sides of the head is insufficient

Engineering Contradiction:
Improveconfigurability to support sides of headVSAvoidstructure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The headrest is divided into multiple independent segments: a center portion and two separate ear portions. Each ear can be independently positioned relative to the center portion, allowing customized configuration for head support while maintaining a relatively simple overall structure. The segmentation enables adaptability without requiring complete structural redesign.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The ear portions are designed to be movable relative to the center portion through rotatable joints with oblique axes of rotation. This dynamic capability allows the ears to rotate between stowed and deployed positions, providing configurability for side head support while keeping the mechanism simple enough for practical manufacturing and operation.

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If ears are added to provide side support, then support configurability is improved, but the number of components and structural complexity increases

Engineering Contradiction:
Improveside support capabilityVSAvoidnumber of components
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The ear portions are integrated with the center portion through shared rotational joints and common mounting structures. The oblique axis joints serve dual purposes: they connect the ears to the center while simultaneously providing the rotational movement capability. This merging reduces the total number of separate components compared to having fully independent ear assemblies.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The oblique axis rotational joints serve multiple functions: they provide the mechanical connection between ears and center portion, enable the rotational movement for deployment, and define the geometric relationship for proper ear positioning. This multi-functionality reduces the need for additional specialized components.

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

3Ease of operation

If ears are made deployable with oblique rotation, then ergonomics and comfort are improved, but the mechanism complexity increases

Engineering Contradiction:
Improveergonomics and comfortVSAvoidmechanism complexity
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The ear portions are designed with rotatable joints that have oblique axes of rotation, enabling smooth deployment and adjustment movements. This dynamic design allows users to easily position the ears for optimal head support comfort while maintaining a relatively simple mechanical implementation using basic rotational joints rather than complex actuation mechanisms.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP4541656A1Headrest with deployable oblique supports
Publication Date: 2025.04.23 BE AEROSPACE INC
  • EP4541656A1 patent drawingFigure 1
  • EP4541656A1 patent drawingFigure 2
  • EP4541656A1 patent drawingFigure 3

AI summary

A headrest assembly (100) and an aircraft passenger seat (136) including a headrest assembly. In embodiments, the headrest assembly includes a center portion (104) including left and right lateral receivers (118, 120) each defining an axis of rotation (122) oblique to a plane of the center portion, and left and right ears (106, 108) each including a dogleg support (124) rotatably received in its respective lateral receiver, wherein each ear is configured to rotate independently about its axis of rotation between a stowed position alongside the center portion and a deployed position oblique to the plane of the center portion. In use, for example, the ears may be deployed to provide a provision for sleeping in which the sides of the head are supported.