Composite Corner Fitting Strap Load Transfer

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Solution Overview

Problem

Conventional metallic corner fittings in structural assemblies are heavy and lack energy-absorbing capability, while composite corner fittings face interlaminar tension issues when subjected to non-parallel or out-of-plane loads, necessitating additional plies that increase weight and complexity.

Innovation Solution

A composite corner fitting comprising a male and female fitting with a semi-conical shape and a strap, where the strap's planar portions are clamped between the fittings, allowing efficient tension load transfer into beam webs while avoiding interlaminar tension, formed from fiber-reinforced polymer matrix material for enhanced energy absorption.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If metallic corner fittings are used, then strength and load transfer capability are improved, but weight increases and energy-absorbing capability is reduced

Engineering Contradiction:
Improveload transfer capabilityVSAvoidweight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The corner fitting uses composite materials consisting of fiber-reinforced polymer matrix instead of metallic materials, providing both weight reduction and maintained strength characteristics suitable for structural reinforcement applications

Inventive Principle:
Principle #40Composite materials

2Weight of moving object

If composite corner fittings are used, then weight is reduced and energy-absorbing capability is improved, but interlaminar tension effects occur when subjected to non-parallel or out-of-plane loads

Engineering Contradiction:
ImproveweightVSAvoidresistance to interlaminar tension
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The composite plies are oriented at specific angles (0°, 45°, -45°, 90°) in different regions of the corner fitting to locally optimize strength characteristics, with fibers aligned to resist both in-plane and out-of-plane loads while minimizing interlaminar tension effects

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The design incorporates multiple layers (plies) of composite material with varying fiber orientations in the thickness dimension, creating a three-dimensional stress distribution that resists interlaminar tension while maintaining weight advantages

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Reliability

If additional composite plies are added to resist interlaminar tension, then reliability is improved, but weight and structural complexity increase

Engineering Contradiction:
Improveresistance to interlaminar tensionVSAvoidstructural complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The corner fitting optimizes the number, thickness, and orientation angles of composite plies to achieve the minimum required strength against interlaminar tension, avoiding excessive material usage and structural complexity while maintaining reliability

Inventive Principle:
Principle #35Parameter changes

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 provides improved load-carrying capability and energy absorption during high-strain-rate compression events, reducing weight and complexity by effectively transferring tension loads into beam webs, offering better protection in aircraft and other structural applications.

Implementation Method 1

formed from fiber-reinforced polymer matrix material for enhanced energy absorption

Methodology Applied
Scientific EffectEnergy absorption:

Implementation Method 2

the strap's planar portions are clamped between the fittings, allowing efficient tension load transfer into beam webs

Methodology Applied
Scientific EffectMechanical force transfer: Mechanical Force

Data Source

PatentEP3170740B1Corner tension fitting
Publication Date: 2020.03.04 THE BOEING CO
  • EP3170740B1 patent drawingFigure 1
  • EP3170740B1 patent drawingFigure 2
  • EP3170740B1 patent drawingFigure 3

AI summary

A corner fitting may include a male fitting having a convex portion and a female fitting having a concave portion configured complementary to the convex portion. In addition, the corner fitting may include a strap having a strap radius portion and a pair of strap planar portions extending from opposite ends of the strap radius portion. The strap planar portions may be parallel to one another when the strap radius portion is clamped between the convex portion and the concave portion and the corner fitting is viewed from a side, and non-parallel to one another when the corner fitting is viewed from an end.