Composite Tube Assembly Tapered Fitting Thermal Stress

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Solution Overview

Problem

Carbon composite tube assemblies connected to metallic end fittings experience stress and weakening due to differing thermal expansion rates, leading to a fragile connection over time.

Innovation Solution

A composite tube assembly design featuring a fitting with a tapered outer surface and a bolstering structure, including a reduced diameter portion for adhesive bonding and a wrap or collar for mechanical reinforcement, to create a robust connection between the composite tube and the fitting.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a metallic end fitting is directly connected to a carbon composite tube, then the connection is simple and lightweight, but the connection strength deteriorates over time due to thermal expansion differences

Engineering Contradiction:
Improveconnection strengthVSAvoidconnection reliability
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

A fitting with a tapered outer surface section is introduced as an intermediary component between the metallic end fitting and the carbon composite tube. This fitting accommodates thermal expansion differences through its geometric design and material selection, preventing direct stress transmission between the metallic end fitting and the tube while maintaining connection integrity over time.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The solution employs a composite structure combining metallic materials (end fitting), polymer materials (fitting with tapered section), and carbon composite materials (tube). This multi-material approach allows each component to be optimized for its specific function while collectively resolving the thermal expansion incompatibility between metal and carbon composite.

Inventive Principle:
Principle #40Composite materials

2Reliability

If the fitting has a complex structure with tapered sections and bolstering, then the connection robustness is improved, but the manufacturing complexity increases

Engineering Contradiction:
Improveconnection robustnessVSAvoidfitting structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The fitting incorporates a tapered outer surface section with continuous curvature that transitions smoothly between different diameter portions. This curved geometry accommodates thermal expansion through elastic deformation while maintaining structural integrity, and can be manufactured using standard forming processes for polymer components.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The fitting features localized structural variations including a reduced diameter portion for adhesive bonding and a tapered outer surface section for mechanical reinforcement. These local modifications are concentrated only where needed to achieve connection robustness, rather than requiring complex structures throughout the entire fitting.

Inventive Principle:
Principle #3Local quality

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The solution enhances the mechanical strength and durability of the connection by accommodating thermal expansion differences and preventing separation between the composite tube and the fitting, ensuring a stable and long-lasting assembly.

Implementation Method 1

a groove to accommodate an adhesive or a resin bonding the composite tube to said fitting

Methodology Applied
Scientific EffectAdhesive bonding: Adhesive

Implementation Method 2

carbon composite may have a rate of thermal expansion and/or negative thermal expansion (i.e. contraction) substantially different from that of the metallic end fitting

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentEP2320099B1Composite tube assembly
Publication Date: 2015.09.23 TYEE AIRCRAFT
  • EP2320099B1 patent drawingFigure 1~5
  • EP2320099B1 patent drawingFigure 2~3
  • EP2320099B1 patent drawingFigure 6~7

AI summary

The inventions provides for a composite tube assembly comprising: a composite tube (10') comprising an end; a fitting (12') comprising a first end (122') opposite a second end (127), said fitting second end (127) comprising a first outer diameter, wherein said fitting (12') comprises a tapered outer surface section (128') between said first and second ends (122', 127), said tapered outer surface section (128') tapering radially inward to a smaller diameter in a direction toward the first end (122'), wherein said fitting (12') penetrates a portion of said tube (10') through said tube end, wherein said second end (127) and said tapered outer surface section (128') are interior of the tube (10'), wherein said tube portion penetrated by said fitting (12') comprises a section mated to the tapered outer surface section (128') of the fitting (12'), wherein the fitting (12') comprises a constant diameter outer surface section (124') extending from the second end (127) to the tapered outer surface section (128'); and a bolstering structure (19', 21') surrounding and engaging said composite tube section.