Aircraft Seat Berthing Platform Reinforcement for Self-Supporting Loads

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Solution Overview

Problem

Aircraft seat berthing platforms often fail to meet load requirements set by aviation guidelines without external support, leading to potential damage and complexities in integration and certification.

Innovation Solution

A self-supporting berthing platform system with articulated panels, a hinge reinforcement assembly, and a panel reinforcement assembly that includes pivotable and rotatable components, allowing the platform to pivot between upright and berth positions while distributing loads internally.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a berthing platform is designed without external support structures, then device complexity and integration requirements are reduced, but the platform fails to meet aviation load requirements

Engineering Contradiction:
Improveintegration complexityVSAvoidload bearing capacity
Core Design Contradiction:
Device complexityVSStrength

Solution Approach 1:

The berthing platform is divided into multiple articulated panels that can independently support and distribute loads. Each panel is reinforced with internal reinforcement members that segment the load path, allowing the platform to meet load requirements without external support structures.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The platform uses an articulated mechanism with hinges that allow dynamic movement between upright and berth positions. The hinge reinforcement assembly and panel reinforcement members provide dynamic load distribution that adapts to different positions, enabling the platform to self-support while meeting aviation load requirements.

Inventive Principle:
Principle #15Dynamics

2Strength

If reinforcement structures are added to meet load requirements, then strength is improved, but device complexity increases

Engineering Contradiction:
Improveload bearing capacityVSAvoidstructural complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The reinforcement members are integrated directly into the panel structures rather than being separate external components. The hinge reinforcement assembly is merged with the hinge mechanism itself, and panel reinforcement members are embedded within the panel framework, reducing overall structural complexity while maintaining strength.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The platform's own structural components serve dual purposes: the panels provide both the berthing surface and the load-bearing structure through integrated reinforcement members. The articulated mechanism itself provides structural support without requiring separate external reinforcement structures.

Inventive Principle:
Principle #25Self-service

Data Source

PatentEP4306412A1Self supporting berthing platform system for aircraft seats
Publication Date: 2024.01.17 BE AEROSPACE INC
  • EP4306412A1 patent drawingFigure 1A
  • EP4306412A1 patent drawingFigure 1B
  • EP4306412A1 patent drawingFigure 2

AI summary

A self-supporting berthing platform system (200) is disclosed. The system may include a plurality of articulated panels (202) including a first panel coupled to a second panel via at least one hinge assembly (204). The plurality of articulated panels may be configured to pivot between at least one of an upright position and a berth position. The system may include a hinge reinforcement assembly (206) including a first reinforcement member and a second reinforcement member. The hinge reinforcement assembly may further include a flange. The system may include a panel reinforcement assembly (208) including a first panel reinforcement member coupled to the first panel and a portion of at least one seatback frame and a second panel reinforcement member sub-assembly coupled to the second panel. The second panel reinforcement member sub-assembly may include at least one panel leg and at least one support block.