Chemical CNC alloy processing services
This page explains how we machine titanium, Inconel, 17-4PH, CoCr and magnesium without the scrapped batches those alloys usually produce. It is written for design engineers and sourcing engineers who need to judge whether a shop can hold tolerance in a hard alloy before releasing a drawing set.

What chemical cnc alloy processing actually means here
A set of decisions made before the first cut, not a single machine setting.
Why alloy parts fail on an ordinary CNC program
Alloys earn their place because they resist things. Ti-6Al-4V keeps its strength at temperatures where aluminum sags. Inconel 718 holds shape in a turbine housing. 17-4PH stays corrosion-free in a surgical tray. The same properties that make the part useful also make it hard to cut: low thermal conductivity, high work-hardening rate, a tendency to gall on the tool edge.
The usual failure is not a broken cutter. It is heat. In titanium, roughly 80% of the cutting heat goes into the tool and the workpiece rather than into the chip, so the edge softens, rubs instead of shearing, and work-hardens the surface it just passed. The next pass cuts a layer that is now harder than the drawing assumed.
On a three-axis machine with flood coolant, that heat has nowhere to go. Deep pockets in 17-4PH trap chips, recutting turns them into abrasive paste, and a thin wall deflects under load. Hold the feed too low and the tool rubs. Push it too high and the insert chips. There is a narrow window, and finding it is most of the job.
Coolant chemistry, pressure and where it is aimed
Standard flood coolant is built for aluminum and mild steel. In high-pressure alloy work we use formulated fluids with additive packages chosen for the material in the vise: EP additives for titanium, chlorine-free formulations for Inconel so the fluid does not attack the cobalt binder in the insert, and lower-concentration mixes for magnesium to limit hydrogen generation at the chip interface.
Delivery matters as much as the fluid. Through-tool coolant at high pressure puts liquid at the cutting edge rather than around the part. On deep bores and long-reach five-axis work, that is the difference between a 12 mm tool surviving a 6× diameter reach and snapping at the third pass.
Fluid concentration is checked by refractometer during the run, not once a week. Tramp oil, fines and bacteria shift the mix, and a fluid that worked on Monday can leave a gummy residue on Thursday that clogs a fine internal channel. For medical and aerospace work, the fluid must also rinse clean enough for the part to pass inspection without a manual scrub that could alter a surface.
Alloy behavior and machining approach
Typical shop-floor settings for the alloys we run most. Ranges depend on feature geometry and tool reach.
| Alloy group | Main difficulty | Coolant strategy | Typical cutting speed |
|---|---|---|---|
| Ti-6Al-4V (TC4) | Heat into tool, work hardening | High-pressure through-tool, EP additive | 40–70 m/min |
| Inconel 718 / 625 | Notch wear, built-up edge | Chlorine-free, heavy flow | 20–35 m/min |
| 17-4PH (SUS630) | Galling in H900 condition | Soluble oil, 8–10% concentration | 60–90 m/min |
| CoCr (medical) | Hard inclusions, tool chipping | High pressure, filtered fluid | 30–50 m/min |
| Magnesium AZ31B / AZ91D | Chip ignition risk | Low-concentration mix, large flow | 200–400 m/min |
| 316L stainless | Tendency to smear, gum | Soluble oil, strong flushing | 80–120 m/min |
Five-axis motion as part of the process, not a separate step
Five-axis does more than reach the back of a part. Tilting the tool lets us keep a constant engagement angle through a curved surface, so the load on the insert stays flat instead of spiking at every corner. Flat load means predictable heat, and predictable heat means the dimensional result stays inside ±0.005 mm without a second setup.
On a part like an aerospace bracket or a surgical instrument body, the alternative is three or four setups. Each setup adds a re-clamp error, and each re-clamp adds a chance to scratch a finished face. One five-axis operation removes most of that risk. The trade-off is programming time and a longer cycle on the first article.
Not every feature belongs on a five-axis machine. A simple bushing with a through bore and two faces runs faster on a lathe, and we route it there. The decision is made per part, not per customer.
We run 16 simultaneous five-axis machining centers, 12 four-axis mills and 16 mill-turn centers across three plants. The largest travel is 4,000 × 400 × 150 mm, with a Ø400 mm rotary table when the part needs rotation rather than tilting.
Simulation, probing and what gets checked
Every alloy job is simulated against the actual stock model before it runs. The simulation catches tool-holder collisions at tilt angles and flags any segment where the chip load exceeds what the insert was rated for. On a first article, we also verify the post-processor output against the CAM file so the coordinates on the machine match the ones on the screen.
In-process probing checks the workpiece position after roughing and again before finishing. If thermal growth has moved the part, the finishing pass is re-zeroed rather than cut to the original offset. This is what keeps a long titanium part from drifting out of tolerance between the first and last feature.
Final inspection is done on the finished part, with reports available on request. We record raw material certificates, in-process measurements and the final dimensional report against the job number. Qualification rate across alloy work is 99.99%, and parts ship in 3–5 days once production starts.
Surface finishing and the steps that follow machining
Machined alloy surfaces usually need something after the cut. Anodizing in clear, color or hardcoat suits aluminum 6061, 7075 and 6082. Electroless nickel covers 17-4PH and 316L where wear resistance matters more than appearance. Passivation removes free iron from stainless after the chips are gone.
Bead blasting hides tool marks and gives an even matte surface, but it also rounds edges. If a drawing calls for a sharp edge, blasting has to be masked or skipped. Brushing produces a directional finish that reads well on a visible housing but not on a sealing face.
Laser marking handles part numbers and traceability marks; the minimum character height we can hold is 1.5 mm. Below that, the mark fills in and becomes unreadable after anodizing. If the mark matters for traceability, put it on a flat surface, not a curved one.
Questions engineers ask before releasing a hard-alloy job
Which alloys can you actually machine?
Titanium TA1, TA2 and TC4 (Ti-6Al-4V); Inconel 718 and 625; stainless 303, 304, 316L, 17-4PH, 440C; steel 4130, 4140, 4340; copper and brass grades including beryllium copper; magnesium AZ31B and AZ91D; and engineering plastics such as PEEK and POM.
If your alloy is not on the list, send the material spec. We will check tooling and coolant compatibility before quoting rather than after.
How does chemical cnc alloy processing differ from normal CNC work?
The mechanical motion is similar. The difference sits in fluid chemistry, pressure delivery, tool grade and cutting parameters chosen per alloy rather than per part shape.
It also changes inspection. Alloy parts move more after cutting, so probing and re-zeroing between roughing and finishing becomes routine.
What tolerance can you hold on a five-axis titanium part?
We work to ±0.005 mm (±0.0002 in) on critical features where the geometry allows it. Long, thin walls and deep bores are harder, and we will tell you which features are realistic at that tolerance before the job starts.
Surface finish ranges from Ra 0.2–0.8 μm on a fine finish to Ra 1.6–3.2 μm as machined.
Do you handle small quantities of expensive alloy?
Yes. There is no minimum order quantity. We run from one prototype to 10,000+ part runs, which matters when a single Inconel blank costs more than the machining time.
For first articles we quote and return a free DFM analysis within 12 hours, and production can start within 24 hours of approval.
How do you keep my design data confidential?
Uploads are secure and confidential. We sign an NDA on request before any file exchange, and we hold ISO 27001:2022 for information security.
Drawings are stored against the job number and are not shared outside the team working on that part.
Can you inspect and certify the finished parts?
Every part is inspected before shipment, with raw material checks, in-process monitoring and a final dimensional inspection. Reports are available on request.
We hold ISO 9001:2015, IATF 16949:2016 and ISO 13485:2016, so the documentation format can match what your quality system expects.
Send a drawing and get a real machining answer
Upload your alloy part files and we will return a quote with a free DFM analysis within 12 hours.
12-hour quote±0.005 mm100% inspectionNDA on request