Overhead Payload Module Stowbin Integration

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Solution Overview

Problem

Existing aircraft overhead payload modules are heavy, costly, and inefficient in terms of space utilization, with separate mounting and installation requirements that increase installation time and complexity.

Innovation Solution

The overhead payload module integrates a ceiling assembly, aisle floor assembly, and payload assemblies with structurally integrated stowbin modules and aisle support structures, using blade fittings for secure attachment to support rails, enhancing load-carrying capacity and reducing weight and manufacturing costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If the module and stowbin support assembly are separately mounted to the same support structure, then both components can be independently installed and maintained, but the support structure requires additional space and the installation time increases

Engineering Contradiction:
ImproveIndependent installation and maintenance capabilityVSAvoidInstallation complexity and time
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent combines the module and stowbin support assembly into a single integrated structure where the stowbin support assembly is mounted to the module rather than separately to the support structure. This integration eliminates the need for separate mounting operations and reduces installation time while maintaining the functional independence of both components through modular design elements that allow for easy assembly and disassembly.

Inventive Principle:
Principle #5Merging (Combining)

2Ease of manufacture

If the module and stowbin support assembly are separately mounted, then each component can be optimized independently, but excessive fasteners and components are required

Engineering Contradiction:
ImproveComponent optimization flexibilityVSAvoidNumber of fasteners and components
Core Design Contradiction:
Ease of manufactureVSQuantity of substance

Solution Approach 1:

The integration of the stowbin support assembly to the module creates a unified structure that shares common mounting interfaces and fastening points. This reduces the total number of fasteners required compared to separately mounting both components to the support structure, while still allowing independent optimization of each component's design and manufacturing.

Inventive Principle:
Principle #5Merging (Combining)

3Reliability

If separate mounting structures are used for the module and stowbin support assembly, then each can be securely attached, but the overall weight increases

Engineering Contradiction:
ImproveAttachment securityVSAvoidOverall assembly weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

By integrating the stowbin support assembly to the module, the patent eliminates redundant mounting structures and shared load paths. The unified structure uses a single set of mounting interfaces and fasteners to secure both components, reducing the overall weight while maintaining secure attachment through proper structural design and load distribution.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS11383841B2Overhead payload module with integrated stowbins
Publication Date: 2022.07.12 THE BOEING CO
  • US11383841B2 patent drawing
  • US11383841B2 patent drawing
  • US11383841B2 patent drawing

AI summary

In an example, an overhead payload module is described. The overhead payload module comprises a ceiling assembly, an aisle floor assembly, a first payload assembly attached to the ceiling assembly and the aisle floor assembly to form a first side of the overhead payload module, and a second payload assembly attached to the ceiling assembly and the aisle floor assembly to form a second side of the overhead payload module. The first payload assembly comprises a first payload module and a first overhead stowbin module structurally integrated with the first payload module and having a first stowage area configured to receive stowbins. The second payload assembly is positioned opposite the first payload assembly to form an aisle therebetween and comprises a second payload module and a second overhead stowbin module structurally integrated with the second payload module and having a second stowage area configured to receive stowbins.