Co-Bonded Composite Strut Reinforcement for Compression Loads

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Solution Overview

Problem

Composite tubular struts used in applications like aerospace often require over-sizing to handle compression loads, leading to increased cost and weight, as their compressive strength is generally lower than tensile strength.

Innovation Solution

A composite columnar structure with a sleeve-like reinforcement around a laminated core, which includes a metal, precured fiber reinforced composite, or ceramic sleeve, enhancing compressive strength while maintaining a lightweight design by controlling wrinkling during consolidation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If composite tubular struts are over-sized to handle compression loads, then compressive strength is improved, but weight and cost increase

Engineering Contradiction:
Improvecompressive strengthVSAvoidstrut weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent applies composite materials by combining a fiber-reinforced resin laminate core with a metal reinforcement layer (titanium, aluminum, or steel). This hybrid composite structure leverages the high specific strength of composites for tensile loads while the metal layer provides enhanced compressive strength, resolving the contradiction between compressive strength and weight by creating a material system that excels in both compression and tension without requiring overall size increase

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The reinforcement layer is applied locally only where compressive strength enhancement is needed - specifically as an intermediate layer between the laminate core and the outer skin. This localized application of metal reinforcement provides compressive load-bearing capacity exactly where required, while maintaining the lightweight composite structure in regions where it suffices, thus improving compressive strength without proportionally increasing overall weight

Inventive Principle:
Principle #3Local quality

2Strength

If composite tubular struts are over-sized to handle compression loads, then compressive strength is improved, but cost increases

Engineering Contradiction:
Improvecompressive strengthVSAvoidmanufacturing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The hybrid composite construction allows optimization of material usage - employing cost-effective resin laminates for the core structure and applying expensive metal reinforcement only as a thin intermediate layer where structurally necessary. This composite approach achieves required compressive strength without the prohibitive cost of entirely metal or oversized composite construction

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The reinforcement layer is applied locally only where compressive strength enhancement is needed - specifically as an intermediate layer between the laminate core and the outer skin. This localized application of metal reinforcement provides compressive load-bearing capacity exactly where required, while maintaining the lightweight composite structure in regions where it suffices, thus improving compressive strength without proportionally increasing overall weight

Inventive Principle:
Principle #3Local quality

3Strength

If a reinforcement layer is added to enhance compressive strength, then compression load capability is improved, but structural complexity increases

Engineering Contradiction:
Improvecompression load capabilityVSAvoidstructural complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The reinforcement layer serves multiple functions simultaneously: it enhances compressive strength, acts as a bonding interface between the laminate core and outer skin, and provides a substrate for outer skin attachment. By merging these functions into a single intermediate layer, the design achieves enhanced compression capability without proportionally increasing structural complexity

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The metal reinforcement layer performs multiple roles: structural reinforcement for compression, bonding substrate for the outer skin, and potential attachment surface for fittings. This multi-functionality means that adding the reinforcement layer does not simply add one function but delivers several benefits simultaneously, offsetting the increase in structural complexity with increased functional efficiency

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 structure effectively resists axial compression loads without significant weight addition, allowing for 'right-sizing' to meet both compression and tension load specifications, thereby reducing costs and weight.

Implementation Method 1

the reinforcement may include corrugations on the inside wall thereof which may control wrinkling of underlying laminate plies of the laminate core during consolidation and curing of the laminate core

Methodology Applied
Scientific EffectMechanical constraint:

Implementation Method 2

The reinforcement allows composite tubular struts and similar columnar structures to be designed that are 'right-sized' to meet both compression and tension load carrying specifications

Methodology Applied
Scientific EffectCompressive strength:

Data Source

PatentUS9486965B2Composite columnar structure having co-bonded reinforcement and fabrication method
Publication Date: 2016.11.08 THE BOEING CO
  • US9486965B2 patent drawing
  • US9486965B2 patent drawing
  • US9486965B2 patent drawing

AI summary

A columnar structure comprises a generally hollow laminate core, an outer composite skin, and a sleeve-like reinforcement. The sleeve-like reinforcement surrounds the laminate core and is sandwiched between the laminate core and the outer composite skin for reacting compressive loads imposed on the columnar structure.