Timed Gaseous Alloying for Titanium Matrix Composites

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Solution Overview

Problem

Conventional metal alloy production methods are inefficient, generating significant waste, requiring multiple steps, and struggling to achieve optimal properties like high strength and wear resistance, particularly in titanium alloys, due to limitations in solute levels and processing techniques.

Innovation Solution

A method using direct manufacturing and timed gaseous alloying for forming metallic matrix composite structures, allowing controlled introduction of alloying agents during deposition to create high-strength, wear-resistant alloys with domains of varying nitrogen content, reducing cracking and processing issues.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If conventional subtractive machining methods are used to produce metal parts, then complex shapes can be achieved, but large portions of starting material are reduced to waste and cutting fluids must be disposed of

Engineering Contradiction:
Improvecomplex shapeVSAvoidmaterial waste
Core Design Contradiction:
ShapeVSLoss of substance

Solution Approach 1:

The patent replaces conventional mechanical subtractive machining with a chemical deposition process. Gas-phase alloying agents are deposited onto a substrate to form the desired part shape directly, eliminating the need for mechanical cutting tools and the associated material waste and cutting fluid disposal problems.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the fundamental processing parameter from mechanical removal to chemical deposition. By controlling deposition conditions such as gas flow rates, temperature, and deposition time, the desired complex shapes are formed additively rather than subtractively, dramatically reducing material waste.

Inventive Principle:
Principle #35Parameter changes

2Shape

If conventional machining operations are used to produce articles with unusual shapes or internal features, then the desired geometry can be achieved, but a significant capital investment and large amount of space are required

Engineering Contradiction:
Improveunusual shape with internal featuresVSAvoidmachine tool complexity
Core Design Contradiction:
ShapeVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical machine tools with a chemical vapor deposition system. The gas-phase alloying process can access internal features and create unusual shapes without requiring sophisticated multi-axis machining centers, significantly reducing equipment complexity and space requirements.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Shape

If multiple parts are produced and joined together to create an article, then complex assemblies can be formed, but close-tolerance machining and joining operations increase production time and cost

Engineering Contradiction:
Improvecomplex assemblyVSAvoidproduction time
Core Design Contradiction:
ShapeVSLoss of time

Solution Approach 1:

The patent merges multiple separate machining and joining operations into a single deposition process. The gas-phase alloying can create complex assembled geometries in one continuous operation, eliminating the need for separate close-tolerance machining and joining steps, thereby dramatically reducing production time.

Inventive Principle:
Principle #5Merging (Combining)

4Strength

If nitrogen is added to titanium alloys above 500 ppm to increase tensile strength, then strength is improved, but tensile ductility drops and solidification cracking occurs

Engineering Contradiction:
Improvetensile strengthVSAvoidductility and cracking resistance
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent applies local quality by creating a non-uniform nitrogen distribution within the titanium alloy. The gas-phase deposition process allows nitrogen to be concentrated in specific regions or surface layers while maintaining lower nitrogen content in other areas, thereby achieving high strength where needed while preserving ductility and preventing cracking in critical zones.

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

This approach enables the production of high-strength, wear-resistant alloys in a single operation, minimizing waste and processing problems, while maintaining hardness and strength benefits, suitable for applications like ballistic armor and aerospace components.

Implementation Method 1

alloys with the gaseous alloying element to form a metallic matrix composite structure

Methodology Applied
Scientific EffectDiffusion: Diffusion

Implementation Method 2

melting the metallic feedstock with the heat source to form a molten pool

Methodology Applied
Scientific EffectMelting: Melting

Implementation Method 3

cooling and solidifying the molten pool to form a metallic matrix composite structure

Methodology Applied
Scientific EffectSolidification: Freezing

Data Source

PatentUS8685501B2Co-continuous metal-metal matrix composite material using timed deposition processing
Publication Date: 2014.04.01 LOCKHEED MARTIN CORP
  • US8685501B2 patent drawing
  • US8685501B2 patent drawing
  • US8685501B2 patent drawing

AI summary

A direct manufacturing technique involving rapid solidification processing uses a reaction between a metallic molten pool and a reactant gas in an inert atmosphere to form alloys with improved desired properties. By utilizing rapid solidification techniques, solubility levels are increased resulting in alloys with unique mechanical and physical properties. Laser deposition of alloys in atmospheres of varying reactant content produce compositions with intermingled and significantly improved overall properties.