Aircraft Ceiling Decoration Panel Installation via Flexible Insertion

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Solution Overview

Problem

Existing methods for installing and removing decoration panels in aircraft ceiling assemblies are complex and time-consuming, often requiring the removal of multiple aircraft structures and the use of visible fasteners that detract from aesthetics.

Innovation Solution

A method and system for installing decoration panels in aircraft ceiling assemblies involve removing a generic panel to create an opening, inserting the decoration panel, and coupling it to the ceiling assembly using a plurality of fasteners, including hooks and clamp hooks, which are concealed by a generic panel upon reinstallation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If existing fasteners are used to install decoration panels, then the panels can be securely fastened to the ceiling assembly, but the fasteners are visible and detract from the aesthetics of the decoration panels

Engineering Contradiction:
Improveaesthetic qualityVSAvoidfastener visibility
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

A valence panel is introduced as an intermediary component that covers the fasteners. The valence panel is installed around the perimeter of the decoration panel, concealing the visible fasteners while maintaining secure attachment. This mediator element resolves the aesthetic conflict by hiding the functional fasteners from view.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The ceiling assembly is segmented into multiple components: ceiling panels, decoration panels, and valence panels. This segmentation allows the valence panel to be positioned specifically to cover fasteners without interfering with the structural integrity or aesthetic presentation of the decoration panel.

Inventive Principle:
Principle #1Segmentation

2Ease of manufacture

If the ceiling assembly is removed and disassembled outside the aircraft to install rigid decoration panels, then the panels can be installed, but the process becomes more complex and time consuming

Engineering Contradiction:
Improveinstallation feasibilityVSAvoidinstallation time
Core Design Contradiction:
Ease of manufactureVSLoss of time

Solution Approach 1:

The decoration panel is designed with flexible properties, allowing it to be bent and manipulated during installation. This flexibility enables the panel to be inserted through the service volume opening in the ceiling assembly without requiring complete removal of the ceiling assembly, significantly reducing installation time and complexity.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The decoration panel utilizes a flexible shell structure that can deform during insertion and then return to its original shape. This flexible design allows the panel to pass through the limited opening in the ceiling assembly and be properly positioned without requiring the ceiling assembly to be completely disassembled.

Inventive Principle:
Principle #30Flexible shells and thin films

3Stability of the object's composition

If rigid decoration panels are used, then the panels provide structural stability, but they cannot fit through the service volume of the ceiling assembly

Engineering Contradiction:
Improvepanel stabilityVSAvoidinsertability
Core Design Contradiction:
Stability of the object's compositionVSEase of operation

Solution Approach 1:

The decoration panel transitions from a rigid state during final installation to a flexible state during insertion. The panel is designed to be manipulated into a curved or bent configuration that allows it to pass through the service volume opening, after which it returns to its stable, flat configuration to provide the required structural stability.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The physical parameters of the decoration panel, specifically its rigidity and flexibility, are dynamically changed during the installation process. The panel is temporarily deformed to reduce its rigidity for insertion, then restored to its original rigid state to provide structural stability once installed.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS12221203B2System for installing decoration panels to an aircraft ceiling assembly
Publication Date: 2025.02.11 THE BOEING CO
  • US12221203B2 patent drawing
  • US12221203B2 patent drawing
  • US12221203B2 patent drawing

AI summary

In an example, a method for installing a decoration panel in a ceiling assembly in an aircraft is disclosed. The method comprises removing a generic panel from the ceiling assembly to produce an opening in the ceiling assembly. The method also comprises inserting the decoration panel through the opening in the ceiling assembly. The method also comprises coupling the decoration panel to the ceiling assembly using a plurality of fasteners such that the decoration panel extends across the opening in the ceiling assembly. The plurality of fasteners includes a first type of fastener and a second type of fastener.