CNC Machining
SOMI Capability
SOMI CNC Machining Capability

3,4,5 Axis CNC Milling
We have different types of CNC milling centers, including 3-axis, 4-axis and 5-axis milling centers. Custom parts from simple to complex structures, metal or plastic materials, can be solved.

CNC Turning
SOMI uses CNC lathes and turning centers (including local brand or imported brand machines) to process metal parts, mainly focusing on cylindrical parts. Ensure components achieve consistent size and finish.
CNC Machining
Show Custom Parts Machined by SOMI
CNC Machining
CNC Machining Materials
We offer a wide selection of materials for custom parts to complete prototypes and production runs of custom parts. The materials we process are very broad and include metals, plastics, and some composites.
Metal


- Aluminum
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Brass
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Stainless steel
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Copper
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Mild Steel
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Beryllium bronze
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Alloy steel
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Titanium
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050

- Tool steel
Aluminum has a good strength-to-weight ratio, high thermal and electrical conductivity, low density and natural corrosion resistance. It is a highly malleable metal, making it easy to machining, can be anodized.
Type:1050,1060,2011,2024,5052,5051, 6061, 6063, 7075,7050
Plastic


- ABS
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- PVC
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- POM
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- Polypropylene(PP)
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- Nylon
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- PET
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- PTFE(Teflon)
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- FR-4
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- Polycarbonate(PC)
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- PMMA
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- Polyethylene(PE)
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.

- PEEK
It is a thermoplastic polymer material with high strength, good toughness, corrosion resistance, high temperature resistance.
CNC Machining
CNC Machining Surface Finishes

As-machined
The standard finish of our parts, the "machined" finish, has a surface roughness of 3.2 μm (126 μin), which removes sharp edges and cleanly removes burrs from the part.
Machining Texture:There are slight scratches on the visible surface.

Smooth machining
A finishing CNC machining operation can be applied to the part to reduce its surface roughness. The standard smoothing surface roughness is Ra 1.6 μm (64 μin). Light surface scratches are visible.
Machining Texture:Visible, light surface scratches.

Fine machining
Refers to the process of precision treatment of raw materials or semi-finished products. The standard smoothing surface roughness is Ra 0.8 μm (32 μin).
Machining Texture:Slightly visible.

Bead blasting
Bead blasting refers to the use of round spherical media that, when impacted against the surface of a part, will leave a more uniform finish caused by the sphere “dimpling” the surface.
Machining Texture:Frosted grain.

Brushing
Brushing is a surface treatment process that uses abrasive belts to draw traces on the surface of a material, usually for aesthetic purposes.

Polishing
From Ra 0.8 to Ra0.1, the polishing process uses abrasive materials to rub the surface of the part, making the surface of the part more shiny, depending on your requirements.
Machining Texture:Smooth, glossy finish

Anodizing
Aluminum and its alloy in the corresponding electrolyte and specific process conditions, due to the action of external current, the process of forming an oxide film on the aluminum product.
Machining Texture:Smooth, matte finish.

Electroplating
Electroplated coating preserves the surface of parts and resists rusts and other defects from causing decay by applying electric currents to reduce metal cations.
Machining Texture:Smooth, glossy finish.

Electroless nickel plating
Electroless nickel plating is a process that deposits an alloy of nickel-phosphorus onto the surface of a metal. This process is chemical only, so does not involve the use of electricity.
Machining Texture:Reduced but visible.

Black oxide
Black oxide is a conversion coating similar to Alodine that is used for steel and stainless steel. It is used mainly for appearance and for mild corrosion resistance..
Machining Texture:Smooth, matte.

Powder coating
Using corona discharge, we make the powder coating adsorbed to the part, creating a more wear-resistant layer with a typical thickness ranging from 50 μm up to 150 μm.
Machining Texture:Glossy.

Chromate conversion coating
Chromate conversion coating is a type of conversion coating, used on aluminum as a corrosion inhibitor, as a primer for paint due to increased adherence or to preserve electrical conductivity.
Machining Texture:Visible.

Electrophoresis
In the solution under the action of direct current electric field, the charged resin moves to the opposite electrode phenomenon. Strong corrosion resistance, can be on different colors.
Machining Texture:Visible.

As-machined
The standard finish of our parts, the "machined" finish, has a surface roughness of 3.2 μm (126 μin), which removes sharp edges and cleanly removes burrs from the part.
Machining Texture:There are slight scratches on the visible surface.

Smooth machining
A finishing CNC machining operation can be applied to the part to reduce its surface roughness. The standard smoothing surface roughness is Ra 1.6 μm (64 μin). Light surface scratches are visible.
Machining Texture:Visible, light surface scratches.

Fine machining
Refers to the process of precision treatment of raw materials or semi-finished products. The standard smoothing surface roughness is Ra 0.8 μm (32 μin).
Machining Texture:Slightly visible.

Bead blasting
Bead blasting refers to the use of round spherical media that, when impacted against the surface of a part, will leave a more uniform finish caused by the sphere “dimpling” the surface.
Machining Texture:Frosted grain.

Brushing
Brushing is a surface treatment process that uses abrasive belts to draw traces on the surface of a material, usually for aesthetic purposes.

Polishing
From Ra 0.8 to Ra0.1, the polishing process uses abrasive materials to rub the surface of the part, making the surface of the part more shiny, depending on your requirements.
Machining Texture:Smooth, glossy finish

Anodizing
Aluminum and its alloy in the corresponding electrolyte and specific process conditions, due to the action of external current, the process of forming an oxide film on the aluminum product.
Machining Texture:Smooth, matte finish.

Electroplating
Electroplated coating preserves the surface of parts and resists rusts and other defects from causing decay by applying electric currents to reduce metal cations.
Machining Texture:Smooth, glossy finish.

Electroless nickel plating
Electroless nickel plating is a process that deposits an alloy of nickel-phosphorus onto the surface of a metal. This process is chemical only, so does not involve the use of electricity.
Machining Texture:Reduced but visible.

Black oxide
Black oxide is a conversion coating similar to Alodine that is used for steel and stainless steel. It is used mainly for appearance and for mild corrosion resistance..
Machining Texture:Smooth, matte.

Powder coating
Using corona discharge, we make the powder coating adsorbed to the part, creating a more wear-resistant layer with a typical thickness ranging from 50 μm up to 150 μm.
Machining Texture:Glossy.

Chromate conversion coating
Chromate conversion coating is a type of conversion coating, used on aluminum as a corrosion inhibitor, as a primer for paint due to increased adherence or to preserve electrical conductivity.
Machining Texture:Visible.

Electrophoresis
In the solution under the action of direct current electric field, the charged resin moves to the opposite electrode phenomenon. Strong corrosion resistance, can be on different colors.
Machining Texture:Visible.
Industry
Application Areas of CNC Machining

Consumer Electronics
Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.
Learn More
Aerospace & Aviation
Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.
Learn More
Automotive
Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.
Learn More
Medical
Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.
Learn More
Robotics & Automation
Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.
Learn More
Industrial Machinery Parts
Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.
Learn MoreTest Inspection
Quality Assurance at the Heart of Our Operations
Get a Quote
Contact us Today for Your CNC Machining Requirements
Ready to elevate your manufacturing with the precision and quality of SOMI's CNC machining services? Contact us today to discuss your project and discover how we can help you achieve unparalleled results. With SOMI, you're not just choosing a service provider, you're choosing a partner dedicated to your success.
We hope to discuss potential cooperation opportunities with you and ask you to provide quotation information for your project. Looking forward to your reply and working with you to promote the success of your project!
- *Name
- *Phone
- *Title
- *Content
FAQ
Frequently Asked Questions
- Where does heat treatment fit in a CNC machining sequence?
The short answer
Plan the sequence as rough machine, heat treat, finish machine. Roughing removes bulk while the metal is soft, the treatment releases stress and moves the part, and finishing cuts the movement away. Finish before hardening and you inherit distortion: a quenched 4140 plate can move 0.1 to 0.3 mm over 300 mm.
The default route: rough, treat, finish
Heat treatment is a stage inside the machining sequence, not a service bolted onto the end of it. Roughing removes most of the material while it is cheapest to cut and leaves stock on the faces that have to end up accurate; the treatment then hardens the part, or relieves the stress that roughing put into it, and moves the geometry a little; finish machining or grinding then brings the part to its final size, so the movement is removed rather than inherited. A 4140 plate finish-milled at 30 HRC and then quenched to 45 HRC will typically move 0.1 to 0.3 mm across a 300 mm length, which is far outside any fine tolerance. Where the part is thin-walled, long, wide or asymmetric, an intermediate stress relief between roughing and semi-finishing is often added, because it stabilises the part before the final cuts are taken. The whole plan, including allowance, fixturing and inspection, should be agreed before the first cut, not after the first out-of-tolerance report.
The order is the whole point. Move the treatment to the end and the part arrives at inspection already distorted. Six treatments and where each one sits
Annealing and normalising are done on the stock, before any cutting, because they soften the material and make it machinable; if the mill already supplies the grade in an annealed, normalised or pre-hardened condition that matches the drawing, the step can be skipped and the lead time with it. Stress relief goes after roughing and before finishing, holds the part at roughly 550 to 650 degrees Celsius to let the internal stresses redistribute, and is the cheapest insurance there is against a part that creeps out of flatness after delivery. Through hardening, quench and temper, is placed after roughing and before finishing so the quench distortion can be machined away; carburising follows the same logic and ends with a grinding or hard-turning operation to clean up the case. Nitriding and induction hardening are shallow and move a part much less, but they still belong before the final finishing pass, because the case itself cannot be cut back afterwards without losing the property you paid for. For aluminium, solution treatment with artificial aging is the equivalent step, and 2xxx, 6xxx and 7xxx grades all respond to it.
Two of these are done to make the part cuttable, three are done to give it strength, and one exists purely to stop it moving. How much metal moves, and how much stock to leave
Distortion cannot be eliminated, because hardening involves a phase change and a release of residual stress, so the practical aim is to budget for it. On a small, well-supported part the movement after treatment is commonly held within about 0.05 mm. On a long or asymmetric part it is much larger, which is why a calculated allowance of roughly 0.2 to 0.5 mm is left on the critical surfaces before hardening and removed afterwards by grinding or hard turning. The allowance has to be large enough to clean up the post-treatment shape and small enough not to waste cutting time, and it is worth telling the heat treater how the part will be supported and quenched, because the racking position and the quench direction move the result as much as the furnace does. If a part repeatedly fails on flatness, the fix is usually a stress relief cycle and a support change rather than a tighter tolerance.
Distortion is not a defect to be avoided, it is a quantity to be planned. The allowance is the number that decides whether it turns into scrap. Hardness decides whether you can still cut it
The hardness a treatment produces sets what happens next. Below about 35 HRC, carbide runs at normal parameters and the process is straightforward. Between 35 and 45 HRC, cutting speeds come down and the depth of cut per pass gets smaller, so the cycle lengthens and the tooling bill rises. Above roughly 50 HRC the part is in hard milling or grinding territory, which needs a very stiff setup to avoid chatter and is often better handled by grinding for a simple flat or cylindrical face. Surface finish follows the same ladder: Ra 1.6 to 3.2 micrometres is a normal as-machined steel surface, 0.8 to 1.6 micrometres comes from a controlled finish-milling pass, and 0.2 to 0.8 micrometres generally means a ground surface. If a drawing asks for a hardness figure that pushes the part past the point where the critical features can still be machined, the treatment and the tolerance have to be reconciled before the order is placed.
Hardness after treatment What still cuts it Cost to the cycle Below 35 HRC carbide at normal speeds and feeds baseline, no premium 35 to 45 HRC reduced speeds, lighter passes longer cycle, more tool changes 45 to 55 HRC hard milling with a very stiff setup specialist machine time, smaller depths Above 55 HRC grinding or EDM on the critical faces an added operation and an added check Nitrided case the geometry, finished before treatment the case cannot be cut back afterwards Surface finish target Ra 1.6 to 3.2 as-machined, 0.8 to 1.6 finish-milled 0.2 to 0.8 needs a ground surface What to ask for, and what to check on arrival
Give the heat treater the alloy grade and starting condition, the target hardness range rather than a single figure, the case depth and treated area where those apply, and the heat-treatment standard your own contract invokes; those four lines decide whether the result is repeatable between batches. On arrival, check the property and the geometry separately, because a part that hits the hardness figure can still be outside tolerance and a part that measures perfectly can have missed its target hardness. Hardness is normally verified by Rockwell, Brinell or Vickers, with a microhardness traverse to confirm case depth on carburised or nitrided parts; geometry needs the same instruments used for the final datum, and a CMM where position or form is critical. Hardness reports and treatment records should be part of the inspection pack, and the measurement method should be agreed before the job starts, because a CMM result and a micrometer result can differ by more than a fine tolerance.
See CNC machining services for parts routed through roughing, treatment and finishing in one sequence, surface finishing for the nitriding, plating and coating options that follow machining, and die casting for cast housings and dies whose tooling steel is heat treated on the same logic.
Scope and sources. The observation that a 4140 plate quenched from 30 to 45 HRC moves 0.1 to 0.3 mm across 300 mm, the hardness bands below 35 HRC, 35 to 45 HRC and above 50 HRC with the corresponding cutting strategy, the route of rough machine, heat treat, finish machine, and the surface finish ladder of Ra 1.6 to 3.2, 0.8 to 1.6 and 0.2 to 0.8 micrometres come from a guide to steel grade and heat treatment in CNC work. The grinding allowance of 0.2 to 0.5 mm on critical surfaces and the stress relief window of roughly 550 to 650 degrees Celsius come from a study of heat treatment distortion control. The three standard routes including the note that small fixtured parts are normally held within 0.05 mm, the advice that treatments causing little movement go before final finishing while quenching and carburising go after roughing, and the hardness and dimension verification practice come from a CNC heat treatment process page, with the intermediate stress relief rationale for thin walls, long shafts and large plates set out in a sequencing and distortion note. All figures are planning values; the allowance and sequence for a specific part should be agreed with the machinist and the heat treater before cutting.
- CNC drilling vs reaming vs boring: what is the difference?
The short answer
Drilling makes the hole, boring corrects its axis and size, and reaming finishes a drilled hole to a precise diameter. Expect IT12 to IT14 from drilling, IT7 to IT9 from boring, and IT6 to IT8 from reaming, with surface finish improving from Ra 12.5 down to 0.4 micrometres.
Three jobs, three tools
The three operations are separated by what each one is allowed to change. A twist drill creates a hole in solid stock and removes the bulk of the material quickly, but it follows its own deflection: the hole it leaves is usually slightly oversize, slightly tapered and not perfectly round, and its position depends on the entry. A boring bar is a single-point tool mounted on a rigid bar, so its diameter can be adjusted on the machine and it is aligned to the intended centreline; that means boring can correct the position and straightness of a hole that drilling has already produced. A reamer is a multi-flute finishing tool of fixed diameter that removes a small, even allowance and produces a very consistent round hole; what it cannot do is change where the hole is. Understanding that one distinction, boring changes geometry and reaming only changes size, prevents most of the arguments between a designer and a machine shop.
Tolerances and surface finish side by side
Drilling alone is a clearance-grade process. It lands somewhere in the IT12 to IT14 range with surface finish around Ra 3.2 to 12.5 micrometres depending on the feed, the drill quality and whether the chips cleared; that is perfectly adequate for a fastener hole, a cable route or a drain. Boring takes the same hole to IT7 to IT9 and Ra 0.8 to 3.2 micrometres, and because the size is set by the operator rather than by the tool it also handles diameters for which no standard reamer exists. Reaming holds IT6 to IT7 with Ra 0.4 to 1.6 micrometres and is the standard answer for a dowel hole, a bearing seat or an H7 press fit. The weakest common specification is an H7 callout on a hole that only ever sees a bolt pass through it: forcing a reaming operation onto every hole on a bracket adds roughly 1.5 to 2 times the machining cost for no functional benefit at all.
Read the middle column first. Only boring is allowed to move the hole; the other two accept the position they are given. Factor Drilling Boring Reaming Starts from solid stock an existing hole a drilled or bored hole Removes the bulk of the material 0.05 to 0.10 mm to approach size 0.10 to 0.30 mm on diameter Can it fix position no, it sets it approximately yes, it follows the true axis no, it follows the existing axis Size control fixed by the drill adjustable at the machine fixed by the reamer Tolerance grade IT12 to IT14 IT7 to IT9 IT6 to IT7 Surface finish Ra 3.2 to 12.5 µm Ra 0.8 to 3.2 µm Ra 0.4 to 1.6 µm Added time seconds minutes per hole 15 to 30 seconds per hole Relative cost baseline, 1x 2 to 3x 1.5 to 2x Why boring can fix a hole and reaming cannot
A reamer has no independent way to find the centre of the hole it is entering: it follows the path the drill left behind, so if the hole is off position or tapered, the finished hole is off position and round but off position. A boring bar is set on the machine's own axis, so the first pass removes the high side of an eccentric hole and the hole moves towards the true centreline. That is why the practical sequence for a tight bore is drill, then bore to correct and roughly size, then ream or fine-bore to the final figure. It is also why reamers are a poor choice for interrupted cuts such as a cross-drilled hole, and why they must not be asked to remove a heavy allowance: reaming more than about 0.3 mm on diameter overloads the flutes and produces the bell-mouthed hole that everyone then blames on the operator.
Two routes to the same hole. Boring buys position, reaming buys size; the tightest work buys both. Stock allowance, entry and blind holes
Leave the sizing tool a predictable amount of material rather than a generous one. For reaming, 0.10 to 0.30 mm on diameter is the normal allowance, and the pre-drill should be about 0.2 to 0.3 mm under the reamer size; for boring, aim to come within 0.05 to 0.10 mm of the final diameter. A reamer needs a chamfered lead-in at the entry and either a through exit or an undercut at the bottom, so a genuinely blind precision hole is usually bored rather than reamed. Where a blind hole must be reamed, the drill depth has to be set deeper than the reamed depth to leave room for the chips and the tool nose. Standardising on the sizes your shop already stocks for drills and reamers avoids the lead time and cost of special tooling, and if a non-standard diameter has to hold a tight tolerance, boring is the cheaper route.
Deep holes change the rules
Up to about five times the diameter, a standard drill behaves acceptably. Beyond that, drill deflection grows, chips have a long way to travel and heat builds up, so the hole drifts, tapers and comes out rough; peck drilling cycles and high-pressure through-coolant flushing are the minimum counter-measures above a depth-to-diameter ratio of about four to one. Where both depth and accuracy are needed, gun drilling with a single-flute tool and internal coolant delivery holds roughly twenty times diameter or more and reaches tolerance bands well under what standard drilling can manage. Deep-hole work is also where the sequence matters most, because a defect created at the entry is amplified all the way to the bottom and no later operation can bring a curved hole back to a straight line.
Each step does one job. Skipping the spot drill or asking the reamer to fix position is where round, straight bores turn into scrap. What to put on the drawing
Specify the tolerance and the finish you actually need, and specify them on the hole diameter only where it matters. Give the depth with a clear reference face, because hole depth measured from a rough casting face is a different hole from one measured from a machined datum. State whether the hole must be round, straight or concentric, since reaming will satisfy the first and boring is required for the others, and name the inspection method: a plug gauge, a bore gauge and a CMM can differ by more than a fine tolerance, and the difference is discovered at goods-in rather than in the drawing office. Wall thickness and hole-to-edge distance matter too, because a hole placed within about two material thicknesses of an edge will bulge or tear the edge during machining. Finally, say how many holes are involved, because the cost of a finer process is multiplied by every hole on the part.
See CNC machining services for drilled, bored and reamed holes quoted from your drawing, metal stamping for punched holes at production volume, and die casting for holes that are cast in and then finished by machining.
Scope and sources. The tolerance grades of IT12 to IT14 for drilling, IT7 to IT9 for boring and IT6 to IT8 for reaming, together with the surface finish bands of Ra 12.5 to 50, 0.8 to 3.2 and 0.4 to 1.6 micrometres and the advice against blind reamed holes and excessive reaming allowance, come from a drilling, boring and reaming comparison. The reaming allowance of 0.1 to 0.3 mm, the starting condition of each operation and the rule that reaming cannot correct position while boring can come from a precision hole machining guide. The added time of 15 to 30 seconds per hole for reaming, the relative costs of 1.5 to 2 times for reaming and 2 to 3 times for boring, the H7 against H9 comparison, the depth-to-diameter limits of 5 to 10 times diameter for standard drilling and 20 times or more for gun drilling, and the pitfall of specifying H7 on clearance holes come from a CNC hole tolerance study. Tolerance grades are quoted against the ISO 286 system, which is a published standard; all values are standard production capability and should be confirmed on your own part.
- How do you machine copper and copper alloys without work hardening?
The short answer
Cut copper with a sharp, high-positive-rake tool, a feed and depth heavy enough to stay under the work-hardened skin, and flooded coolant. Never let the tool rub: a minimum depth of about 0.13 mm, feeds of 0.03 to 0.05 mm per tooth and 150 to 400 m/min keep the cut shearing cleanly.
Why copper hardens under the tool
Work hardening, also called strain hardening, happens when the cutting edge deforms the metal instead of shearing it. Copper has a face-centred cubic lattice with many slip systems, so dislocations move easily and pile up against each other quickly; the result is a thin layer at the surface that is harder, stronger and far less ductile than the metal underneath it in a single pass. Once that layer exists, the next pass finds a harder material, and a tool that is slightly dull simply polishes it and hardens it further. This is why copper rewards a decisive cut and punishes a timid one: the classic mistake is to slow the feed and take a light pass, which converts a cutting operation into a rubbing operation and makes the problem worse on every subsequent pass.
Alloys that machine cleanly and alloys that fight back
Pure copper C11000 is the worst offender and it is also the grade most often specified, because it has the highest electrical and thermal conductivity. Alloying is the easiest fix. Free-cutting brass C36000 contains zinc and lead that break up the lattice and stop the chips from welding, which is why it is the benchmark material for machinability. Tellurium copper C14500 keeps conductivity close to C11000 but machines far more easily because the tellurium inclusions break the chip. Beryllium copper C17200 is a different problem: it is strong and abrasive, so it needs slower speeds and a very rigid setup rather than clever chip control. If a drawing says pure copper and the part is a prototype, it is worth asking whether a free-machining grade would do the same job.
The alloy choice usually matters more than the cutting parameters. C36000 will run at nearly twice the speed of C11000 with better chips. Alloy Machinability Starting speed (carbide) Watch out for C36000 free-cutting brass best in the family 250 to 300 m/min coated tools; lead content can strip a coating C14500 tellurium copper easy 200 to 300 m/min cost and availability C10300 / TU2 copper moderate 200 to 350 m/min long stringy chips that wrap the tool C11000 ETP copper difficult, hardens fast 150 to 200 m/min built-up edge, tenacious burrs C17200 beryllium copper difficult, abrasive 100 to 150 m/min tool wear, dust control in the shop Cutting parameters that avoid the hardened skin
The single most important number is not speed but depth of cut. To cut below any layer that has already been hardened, the tool needs a minimum depth of about 0.13 mm per pass, and 0.2 to 0.4 mm is a comfortable working range for copper in a rigid setup. Feed should also be generous for the material, in the region of 0.03 to 0.05 mm per tooth on a cutter, or roughly 0.1 to 0.3 mm per revolution when turning, because thin chips bend the edge and rub instead of shearing. Cutting speed is then set to control heat rather than to control the cut: as a first cut, around 150 to 200 m/min works for C11000, 200 to 350 m/min for the tellurium grades and C10300, and 250 to 300 m/min for free-cutting brass on uncoated carbide. Tool life improves markedly if the speed is pulled back rather than pushed up when the edge starts to wear.
Speed is a heat control, not a productivity control. On copper, running slower than the band is more damaging than running faster. Tool geometry, coating and coolant
Use a tool with a sharp, high positive rake and a polished flute surface so the chip slides away rather than welding to the edge. Uncoated carbide and PVD-coated carbide both work; on copper, thick coatings are counter-productive because the soft workpiece pulls coating particles off the edge, and polycrystalline diamond is reserved for high-volume work where its hardness justifies the price. A fine edge hone of about 0.005 to 0.01 mm keeps the edge sharp without leaving it fragile. Coolant is not optional: flood the cutting zone generously, and for copper a chilled water-based fluid delivered through the spindle at around 16 to 18 degrees Celsius keeps the edge temperature stable and stops heat-driven hardening. Oil-based fluids can stain copper and encourage chip adhesion, so a water-soluble or a minimum-quantity vegetable-based lubricant is the safer choice.
- Take a decisive depth of cut so the edge bites below the surface layer instead of riding on it.
- Feed generously enough for a chip that curls and breaks rather than one that smears.
- Keep the tool sharp; a dull edge is the fastest way to raise the local hardness.
- Flood the cut, and keep the fluid cold on the grade that hardens fastest.
- Use climb milling on profiles so the cutter shears from the thick part of the chip, and keep overhang short.
- Grip with soft jaws; copper marks and deforms easily and a crushed surface is a hardened surface.
Four habits, in this order. The first two prevent hardening; the last two stop it from becoming a dimension problem. Deburring, and when copper needs a stress relief
Copper produces tough, tenacious burrs that survive a light brush and smear if you attack them mechanically. Thermal energy deburring or cryogenic tumbling handles complex parts without smearing the edges, and on simple parts a controlled handheld or abrasive-flow operation is enough; the point is to finish the edge without cold-working the faces around it. Dimensional stability is the other end of the same problem: heavy material removal leaves residual stress in the part, and a thin-walled copper busbar can creep out of flatness weeks after delivery. Where stability matters more than cycle time, a low-temperature stress relief at roughly 205 degrees Celsius before final finishing puts the part back into a predictable state.
See CNC machining services for the turning and milling work we quote on copper grades, surface finishing for the plating, tinning and passivation routes that follow machining, and metal stamping for copper busbars and contacts that are formed rather than cut.
Scope and sources. The mechanism of work hardening in copper, the role of the face-centred cubic lattice, the minimum depth of cut of 0.005 to 0.015 inch (0.13 to 0.38 mm) that keeps the edge below a hardened layer, the need for generous feed and a polished flute, and the stress relief at about 205 degrees Celsius come from a C11000 copper machining guide. The distinction between C11000 pure copper, C14500 tellurium copper and C36000 brass, the starting speeds of 100 to 200 m/min for high-speed steel and 200 to 400 m/min for carbide, and the feeds and depths for each tool material come from a copper turning guide, with the six preventive habits including climb milling, short overhang and stress relief annealing set out in a note on preventing copper work hardening. The per-alloy speeds of 250 to 300 m/min for C36000 brass and 150 to 200 m/min for copper, the feeds of 0.03 to 0.05 mm per tooth for copper, the rake angles, the 0.005 to 0.01 mm edge hone and the chilled coolant at 16 to 18 degrees Celsius come from a brass and copper tool-wear study; the roughing and finishing bands of 200 to 280 and 280 to 350 m/min for C103 copper come from a copper C103 machining page. These are starting points for a rigid machine; the parameters that suit your own part should be settled on a test cut.










