Aircraft Monument Floor Mounting for Reconfigurable Load Strength

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Solution Overview

Problem

Existing monument systems in commercial aircraft cabins face challenges in being both releasably mounted for reconfiguration and rigidly secured to meet industry load requirements, particularly under static and dynamic conditions as dictated by federal regulations.

Innovation Solution

A mounting system comprising a monument partition with a mounting structure and securement apparatus, including a threaded fastener and bridging washer, that secures the monument to the aircraft floor through a floor track, allowing for adjustment and sealing while ensuring structural integrity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If monument structures are releasably mounted for reconfiguration, then adaptability is improved, but structural strength deteriorates

Engineering Contradiction:
Improvereconfiguration capabilityVSAvoidstructural strength
Core Design Contradiction:
Adaptability or versatilityVSStrength

Solution Approach 1:

The mounting system employs a dynamic securement mechanism where monument structures can be selectively secured or released. The securement apparatus includes movable securing elements that can transition between locked and unlocked positions, allowing the structure to adapt between fixed and reconfigurable states based on operational requirements.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The mounting system divides the securement function into separate modular components: mounting structures attached to monument partitions, floor tracks embedded in the aircraft floor, and securement apparatus with independent securing elements. This segmentation allows individual components to be adjusted or replaced without affecting the entire system, enabling reconfiguration while maintaining overall structural integrity.

Inventive Principle:
Principle #1Segmentation

2Strength

If monument structures are rigidly secured to meet load requirements, then strength is improved, but adaptability deteriorates

Engineering Contradiction:
Improvestructural strengthVSAvoidreconfiguration capability
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The system provides dynamic securement where the mounting structures and securement apparatus can transition between rigidly locked positions (for meeting load requirements) and released positions (for reconfiguration). The securement elements are designed to provide full structural support when engaged, then can be cleanly released when reconfiguration is needed.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The floor track acts as an intermediary element between the monument structures and the aircraft floor. It provides a guided pathway that maintains structural integrity during secured operation while allowing controlled movement and repositioning when the securement apparatus is released, mediating between the conflicting requirements of strength and adaptability.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Area of stationary object

If multiple structures are spaced within one inch of one another, then space utilization is improved, but load sharing complexity increases

Engineering Contradiction:
Improvespace utilizationVSAvoidload sharing complexity
Core Design Contradiction:
Area of stationary objectVSDevice complexity

Solution Approach 1:

The floor track system merges the support function for multiple closely-spaced monument structures into a single integrated floor-mounted component. The floor track is designed to distribute and share loads from multiple adjacent structures simultaneously, eliminating the need for separate complex mounting systems for each structure and simplifying the load-sharing mechanism.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS10696403B2Aircraft monument floor mounting system
Publication Date: 2020.06.30 BE AEROSPACE INC
  • US10696403B2 patent drawing
  • US10696403B2 patent drawing
  • US10696403B2 patent drawing

AI summary

A system for mounting an aircraft monument partition to an aircraft cabin surface such as a floor may include a mounting structure fitted within and attached to a floor-abutting edge of the monument partition, the mounting structure including a mounting opening. A securement apparatus for securing the monument partition to cabin surface via the mounting structure may include a threaded fastener for extending through the mounting opening of the mounting structure and through a corresponding opening in a track mounted to the cabin surface, and a bridging washer for mating with the mounting opening; where, to secure the monument partition to the floor of the cabin area, the threaded fastener is provided through the mounting opening of the mounting structure and threaded to a mating fixture on a bottom side of the track.