Titanium alloys are widely used in aerospace, medical, automotive, marine, chemical processing, energy, defense and high-performance engineering applications because of their high strength-to-weight ratio, excellent corrosion resistance, high-temperature performance and biocompatibility.

However, titanium is also one of the more challenging engineering materials to manufacture.

Compared with aluminum and many steels, titanium has relatively low thermal conductivity, high chemical reactivity at elevated cutting temperatures, strong elastic recovery and a tendency to generate heat at the cutting zone. These characteristics can result in rapid tool wear, poor surface finish, chatter, dimensional problems and reduced tool life during CNC machining.

Selecting the correct titanium grade therefore requires consideration of more than tensile strength.

The alloy grade, metallurgical condition, operating temperature, corrosion environment, loading condition, manufacturing process, heat treatment and part geometry should all be considered during material selection and product design.

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1. Titanium Alloy Grades Overview

Titanium alloys can broadly be divided into:

• Commercially Pure Titanium
• Alpha Titanium Alloys
• Near-Alpha Titanium Alloys
• Alpha-Beta Titanium Alloys
• Beta Titanium Alloys

Commercially pure titanium grades generally prioritize corrosion resistance and formability, while alloyed grades provide higher strength and improved performance for demanding structural applications.

ASTM B265, for example, covers titanium and titanium alloy sheet, strip and plate and includes commercially pure grades as well as alloys such as Grade 5 Ti-6Al-4V, Grade 9 Ti-3Al-2.5V and Grade 23 Ti-6Al-4V ELI.

Major Titanium Grades

Grade	Common Designation	Alloy Type	Relative Strength	Corrosion Resistance	Machinability	Typical Applications
Grade 1	CP Ti Grade 1	Commercially Pure	Low	Excellent	Good	Chemical, medical, marine
Grade 2	CP Ti Grade 2 / TA2	Commercially Pure	Low-Medium	Excellent	Good	Chemical equipment, marine, medical
Grade 3	CP Ti Grade 3	Commercially Pure	Medium	Excellent	Fair-Good	Chemical and industrial equipment
Grade 4	CP Ti Grade 4	Commercially Pure	Highest CP Ti	Excellent	Fair	Aerospace, medical, industrial
Grade 5	Ti-6Al-4V / TC4	Alpha-Beta	Very High	Excellent	Difficult	Aerospace, medical, automotive
Grade 23	Ti-6Al-4V ELI / TC4 ELI	Alpha-Beta	High	Excellent	Difficult	Medical implants, aerospace
Grade 6	Ti-5Al-2.5Sn	Near-Alpha	High	Excellent	Difficult	Aerospace, elevated temperature
Grade 9	Ti-3Al-2.5V / TA18	Alpha-Beta	High	Excellent	Difficult	Tubes, aerospace, bicycle
Grade 12	Ti-0.3Mo-0.8Ni	Alpha	Medium	Excellent	Fair	Chemical processing
Grade 7	Ti-Pd	CP + Palladium	Low-Medium	Outstanding	Good	Chemical processing
Grade 11	Ti-Pd	CP + Palladium	Low	Outstanding	Good	Chemical processing
Grade 19	Ti-3Al-8V-6Cr-4Zr-4Mo	Beta	Very High	Good	Difficult	Aerospace
Grade 20	Ti-3Al-8V-6Cr-4Zr-4Mo-Pd	Beta	Very High	Excellent	Difficult	Chemical/aerospace
Grade 21	Ti-15Mo-3Al-2.7Nb-0.25Si	Beta	Very High	Good	Difficult	Aerospace
Grade 29	Ti-6Al-4V ELI-Ru	Alpha-Beta	High	Excellent	Difficult	Medical/aerospace
Ti-6242	Ti-6Al-2Sn-4Zr-2Mo	Near-Alpha	Very High	Excellent	Difficult	Aerospace, engines
Ti-6246	Ti-6Al-2Sn-4Zr-6Mo	Alpha-Beta/Near-Alpha	Very High	Good	Very Difficult	Aerospace
Ti-5553	Ti-5Al-5V-5Mo-3Cr	Beta	Extremely High	Good	Very Difficult	Landing gear, aerospace
Ti-10-2-3	Ti-10V-2Fe-3Al	Beta	Extremely High	Good	Very Difficult	Aerospace structures

The ASTM designation system confirms, for example, Grade 5 as Ti-6Al-4V, Grade 23 as Ti-6Al-4V ELI, Grade 9 as Ti-3Al-2.5V and Grade 6 as Ti-5Al-2.5Sn.

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2. Commercially Pure Titanium

Commercially pure titanium is not completely pure titanium. Different grades contain controlled amounts of elements such as oxygen, iron, carbon and nitrogen.

The four most commonly referenced CP titanium grades are Grade 1, Grade 2, Grade 3 and Grade 4.

As the grade number increases, strength generally increases, while ductility and formability tend to decrease.

Property	Grade 1	Grade 2	Grade 3	Grade 4
Strength	Low	Medium-Low	Medium	Highest CP Ti
Ductility	Excellent	Excellent	Good	Good
Corrosion Resistance	Excellent	Excellent	Excellent	Excellent
Formability	Excellent	Excellent	Good	Good
Weldability	Excellent	Excellent	Excellent	Excellent
Machinability	Good	Good	Fair	Fair
Typical Use	Chemical/medical	Chemical/marine	Industrial	Aerospace/industrial

Grade 2 Titanium

Grade 2 is one of the most widely used commercially pure titanium grades.

It provides an excellent balance of:

• Corrosion resistance
• Strength
• Formability
• Weldability
• Availability

Typical applications include:

• Chemical processing equipment
• Heat exchangers
• Marine components
• Medical components
• Pumps
• Valves
• Tanks
• Piping

Best choice when corrosion resistance is more important than maximum strength.

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3. Grade 5 Titanium — Ti-6Al-4V / TC4

Ti-6Al-4V, commonly known as Grade 5 titanium or TC4, is the most important titanium alloy for general engineering and CNC machining.

ASTM B265 identifies Grade 5 as an alloy containing nominally 6% aluminum and 4% vanadium.

Key Properties

• Very high strength
• Excellent strength-to-weight ratio
• Excellent corrosion resistance
• Good fatigue performance
• Good biocompatibility
• Good temperature resistance
• Heat treatable
• Difficult to machine

Typical Applications

• Aerospace components
• Aircraft structures
• Engine components
• Medical implants
• Surgical instruments
• Automotive components
• Racing components
• Robotics
• High-performance CNC parts

Typical Material Characteristics

Property	Ti-6Al-4V
Alloy Type	Alpha-Beta
Density	~4.43 g/cm³
Tensile Strength	Typically ~900 MPa or higher depending on condition
Yield Strength	Typically ~830 MPa or higher depending on condition
Elastic Modulus	~110 GPa
Corrosion Resistance	Excellent
Machinability	Difficult
Weldability	Good with proper process control

Actual mechanical properties must be specified according to the applicable material specification, product form, heat treatment and temper.

Why Is Ti-6Al-4V Difficult to Machine?

The major problems are:

1. Low thermal conductivity
2. Heat concentration at the cutting edge
3. High chemical affinity at elevated temperatures
4. High strength at machining temperatures
5. Strong elastic recovery
6. Work hardening
7. Chatter sensitivity
8. Relatively low cutting speeds

These characteristics can accelerate tool wear and make thermal control critical.

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4. Grade 23 Titanium — Ti-6Al-4V ELI

Grade 23 is the Extra Low Interstitial version of Ti-6Al-4V.

It has the same basic alloy system as Grade 5 but uses tighter limits on interstitial elements.

ASTM B265 specifically identifies Grade 23 as Ti-6Al-4V with extra-low interstitial elements.

Typical Applications

• Medical implants
• Orthopedic components
• Surgical components
• Aerospace structures
• Cryogenic applications

Why Choose Grade 23 Instead of Grade 5?

Grade 23 is generally selected when requirements for:

• Ductility
• Fracture toughness
• Fatigue performance
• Biocompatibility
• Medical applications

are more demanding.

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5. Grade 9 Titanium — Ti-3Al-2.5V

Grade 9 is commonly known as Ti-3Al-2.5V and is also widely associated with TA18.

ASTM B265 identifies Grade 9 as Ti-3Al-2.5V.

Characteristics

• Higher strength than CP titanium
• Excellent corrosion resistance
• Good ductility
• Good weldability
• Better formability than many high-strength titanium alloys
• Suitable for tubing

Typical Applications

• Aerospace tubing
• Hydraulic systems
• Bicycle frames
• Heat exchanger tubing
• Aircraft components
• Pressure tubing

Grade 9 is particularly useful when a combination of light weight, corrosion resistance, strength and tube formability is required.

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6. Grade 6 Titanium — Ti-5Al-2.5Sn

Grade 6 is a near-alpha titanium alloy containing aluminum and tin.

It is mainly used when elevated-temperature performance and structural stability are important.

Typical Applications

• Aircraft components
• Aerospace structures
• Engine components
• High-temperature applications

Compared with Grade 5, Grade 6 is generally considered more specialized for elevated-temperature aerospace applications.

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7. Grade 7 and Grade 11 Titanium

Grade 7 and Grade 11 are commercially pure titanium modified with palladium.

The addition of palladium improves corrosion resistance, particularly in reducing acidic environments.

ASTM B265 identifies Grade 7 and Grade 11 as unalloyed titanium with controlled palladium additions.

Typical Applications

• Chemical processing
• Heat exchangers
• Chemical tanks
• Piping
• Pumps
• Process equipment

These grades are much more about corrosion resistance than maximum mechanical strength.

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8. Grade 12 Titanium

Grade 12 contains molybdenum and nickel additions.

It is designed for applications requiring improved corrosion resistance and somewhat higher strength than commercially pure titanium.

Typical Applications

• Chemical processing
• Heat exchangers
• Process piping
• Industrial equipment
• Corrosive environments

ASTM B265 specifies Grade 12 as a titanium alloy containing approximately 0.3% molybdenum and 0.8% nickel.

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9. High-Strength Titanium Alloys

For demanding aerospace applications, several titanium alloys offer substantially higher strength than conventional Grade 5.

Important examples include:

• Ti-6Al-2Sn-4Zr-2Mo
• Ti-6Al-2Sn-4Zr-6Mo
• Ti-5Al-5V-5Mo-3Cr
• Ti-10V-2Fe-3Al
• Ti-3Al-8V-6Cr-4Zr-4Mo

These alloys can offer extremely high strength but often introduce additional challenges in machining, heat treatment and dimensional control.

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10. Ti-5Al-5V-5Mo-3Cr — Ti-5553

Ti-5553 is a high-strength beta titanium alloy.

It is particularly important in aerospace applications such as landing gear and structural components.

MSC’s machining guidance notes that Ti-5553 can be substantially more difficult to machine than Ti-6Al-4V and recommends significantly lower cutting speeds, sharp tooling, light cutter engagement, dynamic or trochoidal toolpaths and high-pressure coolant.

Typical Applications

• Aircraft landing gear
• Aerospace structural components
• High-load components
• Heavy-duty aerospace hardware

Machining Characteristics

Ti-5553 requires:

• Low cutting speed
• Sharp cutting edges
• Rigid workholding
• Controlled cutter engagement
• High-pressure coolant
• Careful tool wear monitoring

A practical starting point may be around 60–80 SFM, or approximately 18–24 m/min, depending on tooling and machining conditions. This should be treated as a starting range rather than a universal production specification.

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11. Titanium CNC Machining Parameters

This section is especially valuable for your website because it targets commercial searches such as:

• titanium CNC machining parameters
• Ti-6Al-4V cutting speed
• titanium milling parameters
• titanium turning parameters
• titanium machining speed
• titanium feed rate
• titanium carbide tooling

Ti-6Al-4V CNC Machining Starting Parameters

The following values should be presented as engineering starting points, not guaranteed production parameters.

Actual parameters depend on:

• Machine rigidity
• Tool diameter
• Tool material
• Tool coating
• Number of flutes
• Workpiece geometry
• Radial engagement
• Axial engagement
• Coolant pressure
• Machine spindle power
• Holder rigidity
• Part fixturing

Milling

Parameter	Roughing Starting Range	Finishing Starting Range
Cutting Speed Vc	30–60 m/min	50–90 m/min
Feed per Tooth fz	0.05–0.15 mm/tooth	0.03–0.10 mm/tooth
Axial DOC ap	1–2.5 mm	0.2–0.8 mm
Radial DOC ae	5–20% D	5–15% D
Coolant	Flood / HPC	Flood / HPC
Tool	Carbide	Carbide
Tool Coating	Application-dependent	Application-dependent

Published machining guidance for Ti-6Al-4V gives similar conservative cutting-speed ranges and emphasizes high-pressure coolant and avoiding excessively light cuts that encourage rubbing and work hardening.

Turning

Parameter	Starting Range
Cutting Speed Vc	40–60 m/min
Feed fn Roughing	0.15–0.30 mm/rev
Feed fn Finishing	0.05–0.15 mm/rev
DOC Roughing	0.5–2.5 mm
DOC Finishing	0.25–1.0 mm
Coolant	High-pressure flood
Tool	Sharp carbide

These values are consistent with published Ti-6Al-4V turning guidance using carbide tooling and flood/HPC coolant.

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12. Titanium Machining: Important Rule

A common mistake is to think:

“Titanium is hard, so simply use a very hard cutting tool and high cutting speed.”

This is not the correct approach.

Titanium’s machining difficulty is strongly related to heat generation and heat evacuation, not simply hardness.

Titanium has relatively poor thermal conductivity, meaning a large proportion of cutting heat remains concentrated near the tool-workpiece interface instead of being rapidly carried away by the chips.

Therefore:

Control heat rather than simply increasing cutting speed.

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13. Major Titanium Machining Difficulties

13.1 Low Thermal Conductivity

Titanium does not conduct heat away from the cutting zone efficiently.

Consequences include:

• High cutting-edge temperature
• Rapid tool wear
• Edge chipping
• Built-up edge
• Surface damage

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13.2 High Chemical Reactivity

At elevated temperatures, titanium can react with tool materials.

This can lead to:

• Adhesive wear
• Crater wear
• Tool welding
• Edge breakdown

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13.3 Work Hardening

If the cutting tool rubs rather than cuts, the surface can become harder.

This creates a dangerous cycle:

Rubbing → Heat → Work Hardening → More Tool Wear → More Heat

Therefore, avoid dwelling and avoid excessively light cutting passes that simply rub the material.

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13.4 Elastic Recovery

Titanium has significant elastic recovery.

During machining, the material can spring back against the tool, causing:

• Tool deflection
• Dimensional errors
• Chatter
• Poor surface finish

This becomes particularly important when machining thin walls.

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13.5 Chatter

Titanium components often require:

• Rigid workholding
• Short tool overhang
• Rigid tool holders
• Optimized toolpaths
• Controlled radial engagement

Dynamic milling or trochoidal strategies can be useful for difficult titanium alloys such as Ti-5553.

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14. Titanium Tooling Recommendations

For CNC machining titanium, carbide tooling is generally preferred.

Recommended Principles

• Use sharp cutting edges
• Use rigid tool holders
• Minimize tool overhang
• Maintain consistent chip load
• Avoid rubbing
• Use appropriate carbide grades
• Use suitable coatings where validated
• Use high-pressure coolant where available
• Monitor tool wear closely

For difficult beta titanium alloys, published industrial guidance specifically recommends sharp uncoated or PVD-coated tools, light cutter engagement and high-pressure coolant.

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15. Titanium Coolant Requirements

Coolant is an important part of titanium machining.

Recommended strategies include:

• High-pressure flood coolant
• Through-tool coolant
• Continuous coolant delivery
• Good chip evacuation

The most important principle is:

Do not allow the cutting zone to repeatedly heat up and cool down unnecessarily.

For high-performance titanium machining, high-pressure coolant can substantially improve heat control and chip evacuation. Published machining guidance for Ti-6Al-4V recommends HPC/flood coolant, while some shop guidance specifies pressures of approximately 70 bar or higher for aggressive machining setups.

The actual coolant pressure should be selected according to the machine, toolholder, tooling and process.

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16. Titanium Product Design Guidelines

Titanium parts should be designed differently from aluminum parts.

16.1 Avoid Excessively Thin Walls

Thin titanium walls are susceptible to:

• Deflection
• Chatter
• Thermal deformation
• Dimensional variation
• Tool pressure

Whenever possible, increase wall thickness or add ribs.

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16.2 Use Generous Internal Radii

Sharp internal corners increase:

• Stress concentration
• Cutting forces
• Tool wear
• Machining time

Use a radius compatible with the cutting tool.

For CNC machining:

Larger internal radii generally improve both manufacturability and tool life.

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16.3 Avoid Deep Narrow Cavities

Deep cavities create:

• Long tool overhang
• Poor rigidity
• Difficult chip evacuation
• Increased vibration
• Poor coolant access

A wider and shallower cavity is usually easier to machine than a deep narrow cavity.

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16.4 Minimize Extreme Tool Reach

A long end mill may deflect significantly when machining titanium.

Design the component so that:

• Shorter tools can be used
• Tool access is straightforward
• Deep pockets are avoided
• Internal corners are accessible

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17. Titanium Design for CNC Machining

Design Factor	Recommended Approach
Wall Thickness	Avoid unnecessarily thin walls
Internal Corner	Use generous radius
Pocket Depth	Avoid excessive depth-to-width ratio
Tool Reach	Minimize tool overhang
Holes	Avoid unnecessary deep small holes
Threads	Provide adequate engagement length
Sharp Corners	Avoid where possible
Thin Ribs	Increase thickness where possible
Large Flat Areas	Consider distortion and stress relief
Fixturing	Provide stable clamping surfaces
Datum Features	Include accessible datum surfaces
Surface Finish	Specify only what is functionally necessary

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18. Titanium Thread Design

Threading titanium requires particular attention because of its tendency toward:

• Galling
• Adhesive wear
• Heat generation
• Tool damage

For threaded titanium components:

• Avoid unnecessarily tight tolerances
• Use appropriate thread geometry
• Consider surface treatment
• Provide adequate engagement
• Avoid excessive preload
• Consider galvanic compatibility with mating fasteners

For frequently assembled components, the mating material and lubrication strategy should also be considered.

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19. Titanium Hole Design

Deep holes are among the more difficult features to machine in titanium.

Potential problems include:

• Heat accumulation
• Chip evacuation
• Drill wear
• Hole size variation
• Tool breakage

For deep holes:

• Use appropriate pecking strategy
• Maintain coolant flow
• Control cutting speed
• Avoid excessive feed
• Use suitable carbide drills where appropriate
• Consider gun drilling or specialized processes for extreme depth

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20. Titanium Surface Treatment

Titanium can be used without coating because of its naturally protective oxide film, but surface treatment can be beneficial depending on the application.

Potential treatments include:

• Anodizing
• Micro-arc oxidation
• PVD coatings
• Passivation/cleaning
• Polishing
• Shot peening
• Specialized wear-resistant coatings

The correct treatment depends on whether the primary requirement is:

• Corrosion resistance
• Wear resistance
• Appearance
• Biocompatibility
• Fatigue performance
• Friction reduction

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21. Titanium Alloy Selection by Application

Application	Recommended Grades	Main Reason
General corrosion-resistant components	Grade 2	Excellent corrosion resistance
Chemical equipment	Grade 2 / 7 / 12	Corrosion resistance
Marine applications	Grade 2 / 5	Excellent seawater resistance
CNC machining	Grade 5	Strength + availability
Aerospace structures	Grade 5 / 23 / 6 / 6242	Strength-to-weight ratio
Medical implants	Grade 23	ELI + biocompatibility
Tubing	Grade 9	Strength + formability
Aircraft landing gear	Ti-5553	Very high strength
High-temperature aerospace	Ti-6242	High-temperature capability
High-strength aerospace	Ti-5553 / Ti-10-2-3	Very high strength
Chemical processing	Grade 7 / 12	Corrosion resistance
Bicycle components	Grade 9 / 5	Lightweight + strength
Racing components	Grade 5	High specific strength
Hydraulic tubing	Grade 9	Strength + formability

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22. Titanium Alloy Selection by Environment

Operating Environment	Recommended Considerations
Seawater	Grade 2 / Grade 5
Chloride Environment	Grade 2 / Grade 7 / Grade 12
Acidic Chemical Environment	Grade 7 / Grade 12
High Temperature	Ti-6242 / specialized near-alpha alloys
Aerospace Structural	Grade 5 / Grade 23 / beta alloys
Medical	Grade 23
Cyclic Loading	Grade 5 / Grade 23 depending on specification
High Strength	Grade 5 / Ti-5553 / Ti-10-2-3
Lightweight Structure	Grade 5
Welded Structure	Grade 2 / Grade 5 / Grade 9

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23. Titanium Alloy Failure Factors

Titanium is highly corrosion resistant, but this does not mean titanium components cannot fail.

Common failure mechanisms include:

Mechanical Failure

• Tensile overload
• Fatigue
• Buckling
• Fracture
• Stress concentration

Manufacturing-Related Failure

• Tool marks
• Surface damage
• Residual stress
• Dimensional distortion
• Poor heat treatment
• Incorrect machining parameters

Environmental Failure

• Galvanic corrosion
• Hydrogen-related effects
• High-temperature oxidation
• Fretting
• Corrosion-fatigue

Design-Related Failure

• Sharp corners
• Thin walls
• Excessive stress concentration
• Poor load paths
• Insufficient thread engagement
• Poor joint design

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24. Titanium Galvanic Corrosion

Titanium itself has excellent corrosion resistance, but galvanic corrosion can occur when titanium is electrically connected to another metal in an electrolyte.

Potential mating materials include:

• Aluminum
• Carbon steel
• Stainless steel
• Copper alloys

For assemblies exposed to:

• Seawater
• Salt spray
• High humidity
• Chemical environments

consider:

• Electrical isolation
• Appropriate coatings
• Washers
• Bushings
• Sealants
• Compatible fasteners

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25. Titanium vs Aluminum vs Stainless Steel

This is another excellent SEO comparison topic.

Property	Titanium	Aluminum	Stainless Steel
Density	Low	Very Low	High
Strength-to-Weight	Excellent	Good	Good
Corrosion Resistance	Excellent	Good	Excellent
Heat Resistance	Excellent	Fair	Excellent
Machinability	Difficult	Easy	Moderate-Difficult
Cost	High	Low	Medium
Medical Applications	Excellent	Limited	Excellent
Aerospace	Excellent	Excellent	Good
Marine	Excellent	Good	Excellent
CNC Cost	High	Low	Medium-High

The primary reason to choose titanium is usually not simply “high strength.”

It is the combination of:

Low density + high strength + corrosion resistance + temperature capability + specialized biological compatibility

that makes titanium attractive for demanding applications.

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26. Quick Titanium Grade Selection Guide

If You Need…	Consider…
Best general-purpose titanium	Grade 5 / Ti-6Al-4V
Excellent corrosion resistance	Grade 2
Medical implant material	Grade 23
Titanium tubing	Grade 9
Chemical processing	Grade 2 / 7 / 12
Maximum CP titanium strength	Grade 4
High-strength aerospace	Grade 5 / 705-type beta alloys
Very high strength	Ti-5553 / Ti-10-2-3
High-temperature aerospace	Ti-6242
Good formability + strength	Grade 9
High strength CNC machining	Grade 5
Seawater applications	Grade 2 / Grade 5
Aerospace landing gear	Ti-5553

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27. Titanium CNC Machining Design Checklist

Before sending a titanium component for CNC machining, engineers should review:

Material

• Correct titanium grade
• Correct temper / heat treatment
• Required material certification
• Applicable ASTM / AMS / EN specification

Design

• Wall thickness is sufficient
• Internal radii are adequate
• Deep cavities are minimized
• Tool access is adequate
• Sharp corners are avoided
• Stress concentrations are minimized

Manufacturing

• Appropriate carbide tooling
• Rigid workholding
• Short tool overhang
• Controlled cutting speed
• Adequate feed rate
• Sufficient coolant
• Chip evacuation strategy

Quality

• Critical dimensions identified
• Surface finish requirements defined
• Heat treatment specified
• Surface treatment specified
• Inspection requirements defined

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28. Final Titanium Alloy Selection Guide

There is no single “best” titanium alloy for every application.

The correct grade depends on the balance between:

Strength

• Weight
• Corrosion Resistance
• Temperature
• Fatigue
• Manufacturability
• Cost
• Application Requirements

For general high-strength applications, Ti-6Al-4V Grade 5 is often the starting point.

For corrosion-focused applications, Grade 2 is a common choice.

For medical applications requiring extra-low interstitial titanium, Grade 23 Ti-6Al-4V ELI is an important option.

For titanium tubing, Grade 9 Ti-3Al-2.5V offers a useful combination of strength, corrosion resistance and formability.

For extreme aerospace strength requirements, alloys such as Ti-5553 and Ti-10V-2Fe-3Al may be considered.

The final material should always be selected according to the applicable material specification, product form, heat treatment, operating environment and engineering requirements.

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Titanium CNC Machining: What Engineers Should Know

Titanium offers exceptional engineering performance, but it requires a different manufacturing approach from aluminum and conventional steels.

The key principles are:

Control heat.

Maintain a consistent chip load.

Avoid rubbing.

Use rigid tooling and workholding.

Keep tool engagement controlled.

Use appropriate coolant delivery.

Design the component for manufacturability.

Select the alloy according to the actual operating environment rather than strength alone.

For custom titanium components, the combination of material selection, DFM design, CNC process planning, tooling strategy, coolant control and inspection is critical to achieving repeatable dimensional accuracy and surface quality.