Aircraft Monument Mounting With Adjustable Multi-Point Attachment
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Solution Overview
Problem
Existing aircraft monument attachment apparatuses suffer from slippage and bolt failure due to high stress levels, leading to high replacement and repair costs and increased aircraft weight.
Innovation Solution
An aircraft monument attachment apparatus comprising an attachment structure, a bridge fitting, and a position adjustment part with adjustable coupling interfaces and multiple fastening points, allowing for selective positioning in three axes and reduced stress on individual fixings.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If conventional single-point attachment is used, then installation is simple, but bolt failure and slippage occur due to high stress
Solution Approach 1:
The attachment structure is divided into multiple separate fixings (at least two fixings distributed across different locations) rather than using a single centralized attachment point. This segmentation distributes the mechanical stress across multiple fastening points, preventing bolt failure and slippage while maintaining structural integrity of the monument attachment system.
2Manufacturing precision
If high-precision machined aluminium and stainless steel are used, then manufacturing precision is high, but manufacturing cost is high
Solution Approach 1:
The attachment system is segmented into modular components (attachment structure, bridge fitting, position adjustment part) that can be manufactured separately using standard precision machining processes. This modularity allows each component to be optimized for its specific function while using cost-effective materials and manufacturing methods, reducing overall manufacturing cost while maintaining positioning precision.
Solution Approach 2:
The position adjustment part enables dynamic positioning of the bridge fitting relative to the attachment structure along the Z-axis through adjustable coupling mechanisms. This dynamic adjustment capability allows for precise positioning during installation without requiring the entire structure to be manufactured with ultra-high precision, thereby reducing manufacturing costs while maintaining positioning accuracy.
3Reliability
If replacement is necessary after bolt failure, then reliability is restored, but replacement cost is high
Solution Approach 1:
The segmented design with multiple independent fixings means that if one bolt fails, the other fixings remain functional and can continue to support the monument attachment. This eliminates the need for complete replacement of the attachment system, significantly reducing repair costs and downtime while maintaining overall reliability.
Solution Approach 2:
The distributed multi-point attachment system provides built-in redundancy that cushions against the impact of individual bolt failure. The stress distribution across multiple fixings prevents single-point failures from compromising the entire attachment system, effectively preparing the system in advance to withstand localized failures without requiring expensive replacements.
4Weight of moving object
If weight is reduced, then fuel consumption decreases, but structural strength may be compromised
Solution Approach 1:
The attachment structure is segmented into multiple lightweight fixings distributed across different locations rather than using a single heavy attachment point. This segmentation allows for optimized material usage in each component, reducing overall weight while maintaining sufficient strength through the distributed load-bearing capability of multiple fixings.
Data Source
Figure 1A~1B
Figure 1C~1D
Figure 2
AI summary
An aircraft monument attachment apparatus (100) comprising an attachment structure (101) for attaching the monument attachment apparatus (100) to an aircraft cabin surface, a bridge fitting (103), and a position adjustment part (105) connectable between the attachment structure (101) and the bridge fitting (103). The bridge fitting (103) comprises a first set of fastening apertures (117a, 117b) for providing connection to a second set of fastening apertures (133a, 133b) of the position adjustment part (105). The attachment structure (101) comprises a first interface (123), and the position adjustment part (105) comprises a second interface (129) arranged to adjustably couple to the first interface (123) such that that the position adjustment part (105) can be selectively positioned relative to the attachment structure (101). In use, the first set of fastening apertures (117a, 117b) of the bridge fitting (103) at least partially overlaps with the second set of fastening apertures (133a, 133b) of the position adjustment part (105) and the first interface (123) and the second interface (129) are coupled with the position adjustment part (105) selectively positioned relative to the attachment structure (101).