Titanium Alloy Basketweave Microstructure via Controlled Cooling

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Solution Overview

Problem

The high material and processing costs of titanium alloys, particularly due to the need for tightly controlled minor elements like iron and oxygen, and the costly machining processes, limit their application in industries such as aerospace, defense, and energy, where low-weight, corrosion-resistant structures are required.

Innovation Solution

A titanium alloy composition with specific ranges of aluminum, vanadium, molybdenum, chromium, iron, oxygen, and incidental elements, processed using near-net shape casting and cooling techniques to achieve a basketweave microstructure, reducing the need for hot working and allowing for additive manufacturing without damaging the alloy's physical and structural properties.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If titanium alloys are wrought and hot worked to achieve near-net shape, then mechanical properties and strength are improved, but processing costs and material waste increase significantly

Engineering Contradiction:
Improvemechanical propertiesVSAvoidprocessing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The invention utilizes phase transition during cooling from beta phase to alpha phase to achieve basketweave microstructure directly in the as-cast state, eliminating the need for subsequent hot working operations. The controlled cooling rate (0.03°C/s to 10°C/s) from the beta transus temperature transforms the microstructure in situ, providing both strength and eliminating costly machining operations.

Inventive Principle:
Principle #36Phase transitions

Solution Approach 2:

The alloy composition is specifically designed during the melting stage to enable direct formation of the desired basketweave microstructure upon cooling, without requiring subsequent hot working or machining operations. The preliminary alloy design with controlled Fe and O content allows the material to self-organize into the strength-providing microstructure during the cooling process itself.

Inventive Principle:
Principle #10Preliminary action

2Stability of the object's composition

If iron and oxygen content are tightly controlled in the melt stock, then non-uniform mechanical properties due to segregation are eliminated, but material cost increases

Engineering Contradiction:
Improveuniformity of mechanical propertiesVSAvoidmaterial cost
Core Design Contradiction:
Stability of the object's compositionVSQuantity of substance

Solution Approach 1:

The invention changes the parameter thresholds for iron and oxygen content from the conventional ELI grade limits (Fe≤0.25%, O≤0.13%) to higher permissible limits (Fe≤0.55%, O≤0.35%). This parameter change allows the use of lower-quality, cheaper scrap materials while still achieving uniform mechanical properties through the basketweave microstructure that forms during controlled cooling, which suppresses segregation effects.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention converts what would normally be harmful impurities (iron and oxygen at higher levels) into acceptable constituents by changing the processing conditions. The controlled cooling rate and specific alloy composition transform the potential harm of higher Fe/O content into a benefit by forming a microstructure that is inherently more uniform and less susceptible to segregation, thereby allowing cheaper materials to be used.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

3Ease of manufacture

If conventional titanium alloys are used with standard cooling rates, then processing is simpler, but the resulting microstructure lacks the interlocking basketweave morphology needed for optimal strength and toughness

Engineering Contradiction:
Improvecooling process simplicityVSAvoidcombination of strength and toughness
Core Design Contradiction:
Ease of manufactureVSStrength

Solution Approach 1:

The invention identifies and applies a specific cooling rate parameter range (0.03°C/s to 10°C/s) that transforms the microstructure into the desired interlocking basketweave morphology. This parameter change in cooling rate, combined with the specific alloy composition and cooling from above the beta transus temperature, produces the optimal microstructure for strength and toughness while maintaining industrial feasibility.

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 approach results in a combination of high strength and toughness at a lower cost, enabling the use of lower-quality scrap materials and reducing manufacturing costs by eliminating the need for forging and rapid cooling, while maintaining excellent mechanical properties.

Implementation Method 1

cooling the alloy from the beta phase at a cooling rate so as to form a microstructure comprising alpha phase laths in a basketweave morphology

Methodology Applied
Scientific EffectPhase transformation: Phase Change

Implementation Method 2

cooling the alloy with a gas pressurized to about 2 atm

Methodology Applied
Scientific EffectHeat transfer: Convection

Data Source

PatentEP3822007A1Method for manufacturing a titanium alloy article
Publication Date: 2021.05.19 QUESTEK INNOVATIONS LLC
  • EP3822007A1 patent drawingFigure 1
  • EP3822007A1 patent drawingFigure 2
  • EP3822007A1 patent drawingFigure 3

AI summary

Provided herein are titanium alloys that can achieve a combination of high strength and high toughness or elongation, and a method to produce the alloys. By tolerating iron, oxygen, and other incidental elements and impurities, the alloys enable the use of lower quality scrap as raw materials. The alloys are castable and can form α-phase laths in a basketweave morphology by a commercially feasible heat treatment that does not require hot-working or rapid cooling rates. The alloys comprise, by weight, about 3.0% to about 6.0% aluminum, 0% to about 1.5% tin, about 2.0% to about 4.0% vanadium, about 0.5% to about 4.5% molybdenum, about 1.0% to about 2.5% chromium, about 0.20% to about 0.55% iron, 0% to about 0.35% oxygen, 0% to about 0.007% boron, and 0% to about 0.60% other incidental elements and impurities, the balance of weight percent comprising titanium. There exists an unmet need to produce titanium alloys for use in aerospace applications which have a refined equiaxed grain structure. This can be beneficial for fatigue critical applications. The technology developed by QuesTek describes a titanium alloy and manufacturing methods thereof to obtain equiaxed grains on the order of 300 microns and corresponding UTS of approximately 170 ksi. In addition, various forms of the alloys are disclosed including ingots, billets, powders and wire in accord with the described microstructure and physical characteristics.