Adjustable Offset Mounting Assembly for Aircraft Fuel Tubes

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Solution Overview

Problem

In aircraft fuel systems, particularly in composite wing structures, there is a need for pass-through mounting assemblies that can reduce electromagnetic effects, accommodate tubing alignment, and permit tubing movement while ensuring secure retention and minimizing stress on both the tubing and the structure, due to the challenges of electromagnetic interference, structural flexibility, and harsh environments.

Innovation Solution

The solution involves a pass-through mounting assembly comprising an outer sleeve, an inner sleeve, a bushing component, and a cap, which are configured to be assembled onto a partition aperture to retain a tube, providing adjustable angular and radial positioning of the tube aperture to match the tube's position, thereby reducing electromagnetic interference and stress on the tube and partition, and including electrically insulating components to prevent arcing and dielectric breakdown.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If traditional metal mounting assemblies are used in composite wing structures, then electromagnetic shielding is improved, but induced currents and arcing risks increase due to lesser shielding in composite materials

Engineering Contradiction:
Improveelectromagnetic shieldingVSAvoidinduced currents
Core Design Contradiction:
Object-affected harmful factorsVSObject-generated harmful factors

Solution Approach 1:

The mounting assembly is divided into multiple separate components (mounting block, tube clamp, retaining cap) that can be independently positioned and adjusted. This segmentation allows each component to be optimized for electromagnetic isolation while maintaining structural function, reducing induced currents through distributed positioning rather than a single continuous metal structure

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The mounting assembly introduces intermediate non-conductive elements between the conductive tube and the composite wing structure. These intermediaries act as mediators that prevent direct electromagnetic coupling and reduce induced currents while still providing mechanical support and retention

Inventive Principle:
Principle #24Intermediary (Mediator)

2Strength

If rigid mounting assemblies are used to secure tubing, then retention strength is improved, but stress and damage risk increase due to composite wing flexibility and tubing misalignment

Engineering Contradiction:
Improveretention strengthVSAvoidstress on tubing
Core Design Contradiction:
StrengthVSObject-affected harmful factors

Solution Approach 1:

The tube clamp incorporates a resilient or adjustable mechanism that allows dynamic adaptation to tubing position variations. The clamp can flex or be positioned at different angles to accommodate composite wing flexibility and tubing misalignment, maintaining secure retention without applying excessive stress to the tubing

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The mounting assembly allows adjustment of geometric parameters such as the angular position of the tube clamp relative to the mounting block. This parameter adjustment enables optimization of both retention strength and stress distribution, accommodating variations in tubing alignment while maintaining secure retention

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If adjustable angular positioning is implemented for tube aperture, then alignment with tubing is improved, but device complexity increases

Engineering Contradiction:
Improvealignment precisionVSAvoidmounting assembly complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The adjustable angular positioning is achieved through segmentation of the mounting assembly into independently rotatable or adjustable components. The tube clamp can be positioned at different angular orientations relative to the mounting block, allowing alignment precision without requiring a completely redesigned complex mechanism

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The mounting assembly uses nested components where the tube clamp fits within or around the mounting block structure. This nesting allows for compact integration of adjustment mechanisms while maintaining alignment precision, reducing overall device complexity compared to separate adjustable components

Inventive Principle:
Principle #7Nested doll (Nesting)

4Reliability

If electrically insulating components are used to prevent arcing, then electromagnetic safety is improved, but electrical conductivity and grounding capability deteriorate

Engineering Contradiction:
Improveelectromagnetic safetyVSAvoidgrounding capability
Core Design Contradiction:
ReliabilityVSPower

Solution Approach 1:

The mounting assembly segments the electrical path into insulating and conductive portions. Non-conductive mounting block and tube clamp components prevent arcing and electromagnetic interference, while separate grounding connections can be established at appropriate locations to maintain grounding capability without compromising electromagnetic safety

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Electrically insulating materials serve as intermediaries between conductive elements (tube and grounding points). These intermediaries prevent direct electrical contact that could cause arcing, while still allowing for controlled grounding paths to be established through designated connection points, balancing electromagnetic safety with grounding requirements

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentEP3103724B1Electromagnetic effects-sensitive pass-through mounting assemblies with adjustable offset
Publication Date: 2018.05.09 THE BOEING CO
  • EP3103724B1 patent drawingFigure 1~2
  • EP3103724B1 patent drawingFigure 3
  • EP3103724B1 patent drawingFigure 4

AI summary

Pass-through mounting assemblies (20) include an outer sleeve (30), an inner sleeve (40), a bushing component (60), and a cap (80) that are configured to be assembled onto a partition aperture (12) in a partition to retain a tube (16) as the tube passes through the partition (10). The outer sleeve (30) is sized to fit into the partition aperture (12). The inner sleeve (40) is sized to nest into the outer sleeve (30) and includes a non-concentric inner rim (48). The bushing component (60) defines a tube aperture (28) configured to retain the tube and includes an outer rim (68) sized to nest into the inner rim (48) of the inner sleeve (40). The tube aperture (28) is non-concentric with the outer rim (68) of the bushing component (60). The cap includes an inner rim (48) sized to nest over the outer rim (68) of the inner sleeve (40). The tube aperture (28) position may be adjusted by changing the relative angular position of the bushing component (60), the inner sleeve (40), and the cap (80).