Boze Titanium Manufacturing Center | Grade 21 Ti-15Mo-3Nb-3Al | AMS 4915 / Beta Alloy

Grade 21 Titanium CNC Machining Services — Ti-15Mo-3Nb-3Al-0.2Si (UNS R58210)

Precision Grade 21 metastable beta titanium (Ti-15Mo-3Nb-3Al-0.2Si, UNS R58210) components for high-strength aerospace structural and fastener applications. AMS 4915 / 4917 / 4928 controlled process with MTR-supported traceability and coordinated solution-treat + age sequence.

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1100+ MPa UTS
Beta Heat-Treat
1 piece MOQ
5–7 d Prototype
Ti-15Mo-3Nb-3Al UNS R58210 AMS 4915 AMS 4928 Aerospace Beta

AS9100D

Aerospace Quality Management System

ISO 9001:2015

Certified Quality Management System

Medical Device Quality Standard

MTR Traceability

Material Test Reports with Every Shipment

Engineering Compliance

High-Strength Beta-Alloy Material Compliance Starts with the Correct Specification

For aerospace structural components, fasteners, and high-strength assemblies where Grade 5 strength (~895 MPa UTS) is insufficient but cold-formability and weldability are still required, Grade 21 (Ti-15Mo-3Nb-3Al) is the specified alloy. The manufacturing process must preserve the agreed heat-treatment sequence and the material identity, and document the solution-treat / age parameters applied.

Standard / SpecificationMaterial or Quality ScopeApplication in Procurement
AMS 4915

Titanium alloy sheet, strip, and plate (Ti-15Mo-3Nb-3Al-0.2Si)

Verify specification applicability for plate and sheet stock.

AMS 4917

Titanium alloy plate (Ti-15Mo-3Nb-3Al-0.2Si)

Confirm specification applicability for plate applications.

AMS 4928

Titanium alloy bars and billets (Ti-15Mo-3Nb-3Al-0.2Si)

Verify specification for bar / billet stock.

ASTM B348

Titanium and titanium alloy bars and billets (general, applicable to beta alloys)

General bar / billet reference where AMS not specified.

ASTM B600

Surface preparation of titanium and titanium alloy surfaces

Pickling / passivation reference for fatigue-loaded components.

Technical Capabilities

Three Critical Controls for Grade 21 Beta-Alloy Machining

01

Beta-Phase Stability and Over-Aging Avoidance

Engineering Challenge

Grade 21 strength is developed by aging the metastable beta matrix. Excessive heat input during machining — high cutting temperatures, slow traverse, or interrupted cuts that re-heat the same zone — can locally over-age the surface and produce inconsistent hardness, dimensional drift, and reduced fatigue life.

Our Machining Approach

We select cutting parameters and tool geometries to keep the cutting-zone temperature well below the aging range. Sharp tools, high-pressure coolant, and conservative engagement keep the bulk material cool. Material is supplied in the solution-treated condition for machining; aging is performed as a separate post-machining step per the customer specification.

Engineering Outcome

Mechanical properties consistent with the agreed specification at the machined surface and in the bulk. Final tolerance and property targets are confirmed after CAD, drawing, material condition, and inspection method review.

02

Cold-Form + Age-Hardening Sequence Coordination

Engineering Challenge

The advantage of Grade 21 is its cold-formability in the solution-treated condition followed by age-hardening to 1100+ MPa UTS. Machining a part that has already been age-hardened is significantly harder and risks tool breakage; machining a part that has been cold-formed but not aged can produce springback and shape drift.

Our Machining Approach

We confirm the sequence with the customer at the RFQ stage: machine in the solution-treated condition, then age. We use a stress-relief step between heavy roughing and finishing to minimize distortion during aging. Inspection intervals are scheduled to catch any movement between machining and aging.

Engineering Outcome

Final geometry held within drawing tolerance after aging, with documented cutting parameters and the agreed heat-treatment sequence.

03

Heat-Treatment Parameter Control and Documentation

Engineering Challenge

Grade 21 mechanical properties are highly sensitive to solution-treatment temperature, quench rate, and aging parameters. A 10 °C shift in aging temperature or a missed quench step can move the yield strength by 100 MPa or more, and the result is not visible at the machined surface — only in subsequent mechanical testing.

Our Machining Approach

We do not perform the solution / aging treatment in-house unless explicitly contracted; we typically ship the machined part to the customer or to a qualified heat-treater with documented material condition and recommended parameters. When we do coordinate heat treatment, we use qualified vendors with calibrated furnaces and full cycle traceability.

Engineering Outcome

Heat-treatment cycle is traceable to the specific part, the agreed parameters are within the specification window, and the customer receives documented evidence of the cycle applied.

Applications

Titanium Parts That Perform Where It Matters

From aircraft structures to surgical implants, precision titanium machining delivers the strength, bio-compatibility, and corrosion resistance that demanding industries rely on.

[Aerospace Structural Element] AERO

Aerospace Structural Elements

Brackets, fittings & frames machined from Grade 5 Ti-6Al-4V under AS9100D-controlled processes.

[Orthopedic Bone Screw] MED

Orthopedic Bone Screws

Implant-grade Grade 23 ELI (Ti-6Al-4V ELI) parts machined in cleanroom-controlled environments.

[Marine Valve Components] MAR

Marine Valve Components

Corrosion-resistant titanium valves, shafts & housings engineered for extreme offshore service.

[Motorsport Fasteners] MTR

Motorsport Fasteners

High-strength titanium bolts, studs & hardware for racing and high-performance vehicles.

Submit Your Engineering Package

Have a Grade 21 Ti-15Mo-3Nb-3Al Component Ready for Manufacturing?

Send your drawing to initiate a technical review. Accepted file formats: STEP, STP, DXF. Target response: initial RFQ acknowledgment within 24 hours on working days. Mutual NDA available before technical file exchange.

Frequently Asked Questions

Grade 21 Ti-15Mo-3Nb-3Al CNC Machining — Engineering FAQ

Q1 What is Grade 21 titanium and what makes it different?
Grade 21 is a metastable beta titanium alloy (UNS R58210) with nominal 15% Mo, 3% Nb, 3% Al, 0.2% Si. In the solution-treated condition the beta-phase matrix is ductile and cold-formable; subsequent aging precipitates fine alpha phase and raises tensile strength to 1100+ MPa UTS. The trade-off vs Grade 5 is higher strength and better formability before aging, at the cost of higher density and more complex heat treatment.
Q2 What is the typical heat treatment for Grade 21?
Solution treatment in the beta field (typically 800–850 °C, water quench) to retain the metastable beta phase, followed by aging (typically 480–595 °C, 4–24 h) to precipitate fine alpha. The exact parameters depend on the customer specification and the strength / ductility target. Machining in the solution-treated condition is easier; aging is done after final machining.
Q3 Is Grade 21 weldable?
Yes, but the welds are typically left in the solution-treated condition and the assembly is age-hardened afterward. Beta-stabilizing elements (Mo, Nb) reduce weld-pool fluidity; the WPS / WPQ should be qualified against the actual customer specification, and post-weld stress relief is usually required.
Q4 What surface finish does Grade 21 require?
The same contamination-controlled workflow used for alloyed titanium grades: no iron embedment, no free-cutting-fluid residue, ASTM B600 alkaline cleaning + acid pickling for parts that go into fatigue-loaded service.
Q5 What is the minimum order quantity for a Grade 21 prototype?
A 1-piece minimum order quantity is supported. Indicative prototype lead time is 5–7 working days for the machined component, plus any subsequent solution / aging cycle.
About Boze Titanium Manufacturing Center

One Metal. One Focus. Infinite Precision.

Founded in 2011 in Baoji's Titanium Valley, BOZE Metal is dedicated exclusively to titanium — from raw material to precision engineering. AS9100D, & ISO 9001 certified with 500+ clients across Aerospace, Medical & Motorsport industries, we deliver end-to-end precision titanium CNC machining with full material traceability from source to component.

Boze Titanium Manufacturing Center is operated by Baoji Boze Metal Products Co., Ltd.

Certifications verified by ASTM International titanium material specifications (B265, B348, B381, F136, F2924) with full EN 10204 3.1 mill test certification. Our quality system is operated under AS9100D by Baoji Boze Metal Products Co., Ltd.

AS9100D ISO 9001 500+ Clients 15+ Years OEM/ODM