AMS 6930 Titanium Forging

AMS 6930 Titanium Forging

Alloy Name: Beta-C (or Beta C) Chemical Composition: Ti-5Al-5Mo-5V-1Cr-1Fe (nominal composition) Type: This is a high-strength near-β type titanium alloy (strictly speaking, it is an α-β alloy with rich β-stabilizing elements) Main Characteristics: It has excellent hardenability, good plasticity, weldability, and heat treatment strengthening ability. Under the solution aging condition, it can achieve very high strength (>1100 MPa). Component Equivalence is Key: Beta-C (AMS 6930/6931) and TC18 are basically the same in nominal chemical composition (Ti-5Al-5Mo-5V-1Cr-1Fe) and main properties. Applications: This alloy is mainly used for critical structural components in aerospace, such as landing gear parts, large forgings, fuselage structural components, joints, etc., which require extremely high strength and good toughness.
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Description

AMS 6930 Titanium Forging is specification-controlled forged titanium stock for aerospace and other high-integrity machined components whose design calls for AMS 6930. Forging shapes the starting material before final machining, allowing the blank envelope and material flow to follow a three-dimensional part more closely than rectangular stock. The form can support rings, hubs, structural fittings, and other loaded geometries when the approved drawing, specification revision, delivery condition, and forging route are treated as one controlled package.

The deliverable is more specific than a titanium piece with enough outside stock. A final component model may omit die split, draft, flash-removal regions, sacrificial extensions, flow orientation, and surfaces reserved for process control. A dedicated forging drawing makes those features visible and defines where machining allowance begins. It also allows testing, nondestructive examination, traceability, and rough-machining scope to be quoted consistently. AMS 6930 provides the named material basis, while the buyer's drawings and purchase documents establish configuration, revision, quantity, inspection stages, and the record set needed to release each forging into downstream production.

AMS 6930 titanium forging blank for aerospace component machining
An AMS 6930 forging is supplied against coordinated material, shape, condition, and inspection documents.

Align the Revision Set Before Pricing Tooling

The enquiry should identify the AMS 6930 revision and the current forging and finished-part drawings. Add the delivery condition and any purchaser-controlled processing notes that apply to the supplied stage. When documents conflict, the hierarchy or resolution needs to be clear before tooling and test material are committed. A model filename alone is not a durable revision-control system.

Substitution decisions remain separate from the base quotation. Bar, plate, another titanium grade, or a different condition may look commercially attractive, but they can carry different process history, section response, and specification requirements. An alternative can be described with its technical and commercial effects so the design authority can evaluate it without losing the AMS 6930 baseline.

Controlled inputContentOffer decision
Material documentAMS 6930 and required revisionFixes the ordered specification basis
Forging definitionEnvelope, orientation, datums, and part identitySupports route and tooling review
Delivered stageAs-forged, cleaned, proof-machined, or rough-machinedSeparates included work from later operations
Test planLot basis, specimen locations, methods, and reportsEstablishes release evidence and sacrificial stock
Commercial controlsQuantity, tooling ownership, first-off scope, and recordsMakes quotations comparable beyond unit price

Build a Forging Envelope Around Stable Machining

The forging drawing can show minimum stock, datum targets, no-blend regions, die parting, draft, test extensions, and any face allowed to remain as forged. Allowance should be sufficient to remove expected surface and establish finished geometry, yet restrained enough to avoid unnecessary material and machining. Workholding needs also influence local stock, particularly where the component becomes thin after roughing.

Sharp section changes, narrow webs, and abrupt radii deserve early process review because they affect die fill and manufacturability. Grain-flow requirements need a drawing reference and an agreed evaluation method. Broad requests for ideal flow cannot be inspected consistently. If macro examination or sacrificial sectioning is part of first-off approval, identify the cut location, evaluation basis, and disposition of the tested piece.

Select the Supplied Stage Deliberately

An as-forged piece leaves maximum conversion work with the machining organization. Cleaning and proof machining can reveal surfaces and establish preliminary datums. Rough machining reduces freight mass and may expose conditions sooner, but it also transfers more responsibility for stock distribution, identity transfer, and intermediate inspection into the forging order. Finished-to-drawing scope adds a much broader feature and surface acceptance package.

The chosen stage should match available process control and commercial risk. Test extensions, setup lugs, and sacrificial material may still be required even when the shipped part is near net shape. Quotations should state whether those items, first-off work, tooling, and inspection fixtures are included so a low unit price is not compared against a technically fuller offer.

Forged titanium ring blank illustrating annular machining allowance and flow direction
An annular blank demonstrates how orientation and radial machining stock become part of a forging definition.

Put Test Locations on the Same Drawing as the Part

Mechanical testing is meaningful when lot basis, specimen type, orientation, extraction location, heat-treatment state, method, and acceptance criterion agree with the controlled documents. Separate test stock may not represent every section of a complex forging. Extensions or sacrificial areas can be designed into the envelope where the applicable plan requires representative material.

Nondestructive examination needs similar precision. State the technique, stage, coverage, applicable reference or class, acceptance rules, and report content. Geometry can limit access in hubs, webs, and tight transitions, so examination feasibility belongs in route review rather than appearing as an undefined full-inspection note after forging.

Carry Identity Through Cleaning and Roughing

Heat, lot, and individual-piece references need a controlled path from source material through forging, heat treatment, cleaning, and machining. Agree where a durable mark may be applied and how identity moves when that area is removed. Travelers, piece maps, and packing lists can retain the link without placing intrusive marks on critical finished zones.

Records can be indexed by forging identity so receiving teams can match material documentation, process state, ordered tests, examination reports, dimensions, and deviations to the physical piece. Witness or third-party points should be scheduled before the relevant operation. Document review after completion cannot recreate an observation that was meant to occur during production.

Protect Datums and Mass in Transit

Forgings may be heavy, irregular, and vulnerable at machined targets or thin extensions. A shipping case should block movement, separate finished faces, protect test lugs and identification, and permit planned handling. Lifting provisions or marked lift locations are useful when the component geometry creates a handling risk. Straps and blocks should bear on robust regions rather than on datums or narrow edges.

For an annular Grade 5 requirement, Grade 5 Titanium Ring represents a different material and product route. Projects still evaluating broader thermal-duty categories can review High Temperature Titanium Alloy. These related forms can sharpen the selection discussion, but only AMS 6930 applies when that designation is released on the current forging order.

Questions Asked Before Forging Release

Why is a finished-part model insufficient for a forging quotation?

It may not show allowance, draft, die split, flow orientation, process lugs, test extensions, or as-forged surfaces. A forging envelope adds the features needed to design the route and price the supplied stage.

Can proof machining be included before shipment?

Yes, when the drawing defines datums, stock remaining, inspected features, identity transfer, and acceptance after proof machining. The offer should state whether the operation includes only cleanup or a controlled rough-machined geometry.

What defines an ultrasonic examination quotation?

The order needs the governing method, examination stage, required coverage, applicable sensitivity or class, acceptance criteria, difficult-to-scan regions, and report level. The word ultrasonic by itself leaves the scope open.

How are tooling and first-off costs compared?

Ask each quotation to identify tooling ownership, expected life or reuse assumptions where applicable, first-off quantity, sacrificial material, sectioning, fixtures, tests, and approval records. This separates recurring piece price from qualification work.

May bar stock replace the forging when machining allowance is available?

Only through the project's deviation process. Sufficient size does not demonstrate the same specification compliance, material flow, section behavior, test basis, or approved component route.

Release One Coherent Forging Package

Request AMS 6930 Titanium Forging with the applicable revision, approved forging drawing, finished-part reference, quantity, delivery condition, required date, and supplied stage. Include orientation, machining stock, datums, tooling ownership, first-off activities, heat-treatment boundary, mechanical test locations, nondestructive examination, dimensional checks, traceability, marking, record index, witness points, and packaging constraints. State annual or follow-on demand where it affects tooling and lot planning. A coordinated package allows the forging source, machine shop, quality team, and buyer to work from the same configuration before material is converted into a high-value component.

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