Titanium Spline Reinforced with Silicon Carbide Fibers

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Solution Overview

Problem

Aircraft brake spline structures face challenges in achieving the necessary strength and reliability at high temperatures while minimizing weight, as conventional high-strength materials like steel and nickel alloys are dense and heavy, and titanium, although lighter, requires larger dimensions to provide strength, reducing the volume available for friction discs.

Innovation Solution

The use of internally reinforced metal splines with composite blocks of silicon carbide fibers in a diffusion-bonded matrix, preferably titanium alloy, to enhance the structural integrity and reduce weight, allowing for efficient torque transmission and heat conduction.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If high-strength materials like steel and nickel alloys are used for spline structures, then strength and reliability at high temperatures are improved, but weight increases significantly

Engineering Contradiction:
ImprovestrengthVSAvoidweight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent applies composite materials by combining metal matrix (titanium alloy) with silicon carbide fibers and boron carbide particles. This composite structure provides high-temperature strength comparable to steel and nickel alloys while maintaining the weight advantages of titanium, thereby resolving the contradiction between strength and weight

Inventive Principle:
Principle #40Composite materials

2Weight of moving object

If titanium is used for drive bars, then weight is reduced, but transverse dimensions must be increased to provide requisite strength, reducing volume for friction discs

Engineering Contradiction:
ImproveweightVSAvoidvolume
Core Design Contradiction:
Weight of moving objectVSVolume of moving object

Solution Approach 1:

The silicon carbide fiber-reinforced titanium alloy composite enables the drive bar to maintain small transverse dimensions while providing the required strength, thus preserving the volume available for friction discs while keeping the weight reduction benefit of titanium

Inventive Principle:
Principle #40Composite materials

3Strength

If spline structures are made larger to compensate for lower strength density, then strength is improved, but the volume available for friction discs is reduced

Engineering Contradiction:
ImprovestrengthVSAvoidvolume
Core Design Contradiction:
StrengthVSVolume of stationary object

Solution Approach 1:

The composite material provides high strength-to-volume ratio, allowing the spline structure to maintain compact dimensions while achieving the necessary strength levels, thereby preserving the volume required for friction discs

Inventive Principle:
Principle #40Composite materials

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 reinforced spline structures provide improved strength and durability at high temperatures with reduced weight, maintaining the volume for friction discs and enhancing the braking performance of aircraft by distributing forces effectively.

Implementation Method 1

a composite block comprising a bundle of silicon carbide fibres that are contained in a matrix that is diffusion bonded to the spline

Methodology Applied
Scientific EffectDiffusion bonding: Diffusion Welding

Data Source

PatentUS8562242B2Reinforced splines and their manufacture
Publication Date: 2013.10.22 TISICS
  • US8562242B2 patent drawing
  • US8562242B2 patent drawing
  • US8562242B2 patent drawing

AI summary

A spline structure, in the form of an aeronautical brake drive bar, has wheel attachment points at its ends for engaging a wheel rim. Each wheel carries a regularly spaced series of these drive bars for engaging friction discs carried by the wheel hub. The main body of each brake drive bar is formed from titanium internally reinforced by composite blocks each comprising a bundle of silicon carbide fibers contained in a matrix that is diffusion bonded within the main body. Other spline structures can be formed in a similar manner.