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Die Casting

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SOMI Capability

SOMI Die Casting Capability

At SOMI Company, we specialize in high-quality metal die casting, offering a diverse range of services including zinc alloy and aluminum alloy die casting. Our advanced manufacturing processes ensure that we meet the unique requirements of various industries, delivering precision-engineered components tailored to your specifications.

Zinc Alloy Die Casting

Zinc alloy die-casting is a manufacturing process that involves the injection of molten zinc alloy into a steel mold, or die, to create precise and complex parts. This technique is renowned for its ability to produce high-quality components with excellent dimensional accuracy, smooth surfaces, and fine details. 

Aluminum Alloy Die Casting

Aluminum alloy die-casting is a manufacturing process that involves injecting molten aluminum into a metal mold, or die, to create high-precision components. This technique is widely used in various industries due to its ability to produce intricate shapes with excellent surface finish and dimensional accuracy.

SOMI Die Casting

Die Casting Materials

SOMI's metal die casting service materials mainly include Zinc alloy and Aluminum alloy.

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.

Die Casting

Die Casting surface finishes

SOMI offers a diverse range of surface finishes, each tailored to meet the specific needs of your projects. Here’s a closer look at some of the options.
  • 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 Die Casting

Our facilities are equipped with the latest in high-precision Die Casting equipment, capable of executing complex designs with exacting tolerances. From prototyping to full-scale production, It's comprehensive machining capabilities cater to a diverse range of industries, including aerospace, automotive, medical, and more.

Consumer Electronics

Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.

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Aerospace & Aviation

Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.

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Automotive

Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.

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Medical

Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.

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Robotics & Automation

Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.

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Industrial Machinery Parts

Our manufactured electronic components consistently meet the tight tolerances required in this ever-evolving industry.

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Test Inspection

Quality Assurance at the Heart of Our Operations

Quality is not just a buzzword at SOMI,it's the foundation upon which we build our reputation Our rigorous quality assurance process encompasses every stage of production, from initial design to final inspection. We employ advanced measurement and testing equipment to verify that each part meets our stringent standards and, more importantly, your expectations. This unwavering dedication to quality ensures that SOMI's Die Casting services are a step above the rest.

Get a Quote

Contact us Today for Your Die Casting Requirements

Ready to elevate your manufacturing with the precision and quality of SOMI's Die Casting 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 are committed to providing full-process services from prototyping to mass production. We provide rapid prototyping services to ensure that your design can be realized accurately and efficiently.

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!

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FAQ

Frequently Asked Questions

If you have any further questions, please contact us. We look forward to working with you.
  • Die casting vs injection molding: how do you choose for a housing?

    The short answer

    Choose die casting when the housing must carry load, spread heat, block electromagnetic interference or survive fire. Choose injection moulding when it must insulate, stay light and reach a low piece price. Tooling runs 15,000 to 60,000 dollars against 3,000 to 25,000, so volume decides the rest.

    Start with the material, not the process

    Die casting and injection moulding look similar on a factory floor: a steel tool, a clamp unit, a shot of molten material, a part ejected every cycle. The difference is what is being shot. Die casting runs aluminium, zinc or magnesium at 620 to 700 degrees Celsius; injection moulding runs thermoplastics at 180 to 350 degrees Celsius. That single fact fixes almost every downstream property. A die-cast housing is electrically conductive, thermally conductive, fire resistant, dimensionally stable at high temperature and roughly three times stiffer than the same wall in glass-filled nylon. A moulded housing is an insulator, weighs a third to a half as much, can be moulded in colour with a textured surface, and can integrate living hinges and snap fits that metal cannot produce in one shot.

    So the first question is not which process is cheaper; it is which set of properties the housing has to deliver. A motor housing that must sink 40 watts and survive a short circuit is a metal part, and no amount of cost engineering will make a moulded cover do that job. A consumer device cover that must be light, warm to the touch, radio-transparent and available in five colours is a moulded part, and casting it is an expensive way to make it heavier.

    Tooling, tool life and the volume where each pays

    The tooling difference is larger than the material difference. A single-cavity aluminium die casting tool typically costs 15,000 to 60,000 dollars and takes 8 to 20 weeks; a comparable single-cavity plastic mould costs 3,000 to 25,000 dollars and takes 6 to 10 weeks. Die casting tooling carries thicker plates, hot-work steel and slides that survive thermal cycling, which is where the money goes. Moulds can use pre-hardened steel and simpler cooling, because the melt is far cooler.

    Tool life runs the other way. An aluminium die is commonly rated 100,000 to 150,000 shots before heat-check refurbishment, with premium steel and good thermal management reaching 300,000 or more; zinc dies last considerably longer because the melt is cooler. A hardened plastic mould commonly lasts several times longer than an aluminium die, and its wear parts are cheaper to replace. The practical effect is that die casting carries a higher tooling cost over a shorter tool life, which is only recovered by the per-part economics at volume: plastic housing programmes usually justify tooling from about 1,000 to 10,000 parts, die casting from about 5,000 to 50,000, depending on size and complexity.

    Volume, parts per yearMoulded housingDie-cast housingWhat decides it
    under 1,0003D print or machinemachine or fabricateneither tool amortises
    1,000 to 5,000tool pays, mould itbridge tool or machineplastic tooling is 3 to 5 times cheaper
    5,000 to 20,000competitivetool pays if the part is metalfunction decides first, then price
    20,000 to 100,000lowest piece pricecompetitive on functionmetal properties against unit cost
    above 100,000multi-cavity mouldmulti-cavity die, premium steelcavity count and tool life
    Comparison matrix of die casting and injection moulding for housings: material aluminium and zinc against thermoplastics, melt temperature 620 to 700 against 180 to 350 degrees Celsius, single cavity tooling 15,000 to 60,000 against 3,000 to 25,000 dollars, cycle time 20 to 90 against 15 to 60 seconds, wall 1 to 6 against 0.5 to 4 mm, tool life 100,000 to 150,000 shots against several times longer, and the housing role of structure and heat against insulation and appearance
    The tooling and tool-life rows are the ones that decide the business case; the material rows are the ones that decide whether there is a case at all.

    Wall thickness and the geometry each process allows

    Housing walls sit in a narrow band in both processes, for opposite reasons. Die cast aluminium is practical from about 1.0 mm to 3.0 mm, with 1.5 to 2.5 mm the comfortable middle for a structural housing; thinner sections lose fill and thicker ones create isolated mass that cannot be fed, producing shrinkage. Moulded ABS runs 1.1 to 3.6 mm, polycarbonate 1.0 to 3.8 mm and glass-filled nylon 0.8 to 2.9 mm, with the same rule that walls should be uniform: a thick section cools last, pulls material from the skin and leaves a sink mark on the far face.

    Geometry follows the material. Die casting needs draft on every vertical face, generous fillets at internal corners and ribs that are thinner than the wall they stiffen, with slides for undercuts; it can produce very fine detail, sharp logos and textured surfaces straight from the die, and it can cast in bosses and mounting pads that would otherwise be separate parts. Injection moulding allows thinner ribs, deeper draws, snap fits, living hinges, threaded inserts moulded in place and multi-shot colour, and it can hold a Class A cosmetic surface with a texture that would need secondary work on a casting.

    Range chart of housing wall thickness in millimetres: die cast aluminium 1.0 to 3.0, die cast zinc 0.5 to 1.5, moulded ABS 1.1 to 3.6, moulded polycarbonate 1.0 to 3.8 and glass-filled nylon 0.8 to 2.9
    Both processes punish a thick section more than a thin one. The design rule is uniformity, not a single minimum number.

    Cycle time, tolerance and what happens after the shot

    A housing-sized aluminium part cycles in roughly 20 to 90 seconds, a plastic housing in 15 to 60 seconds, so cycle time rarely decides between them; the difference is smaller than the difference in material cost. Tolerance does differ, but less than buyers expect, and it is governed by standards rather than by slogans: castings are toleranced under the ISO 8062 system and moulded plastics under ISO 20457, and in both cases the tolerance you get depends on the feature, the tool and the material. As a working rule, a die casting holds around plus or minus 0.1 to 0.3 mm on as-cast features and a moulded part plus or minus 0.05 to 0.2 mm, with machined or reamed features on either reaching 0.05 mm or better.

    Post-processing is where the two diverge most in cost. A casting usually needs deburring, trimming, shot blasting, and often machining on mating faces, seal grooves and threads, plus a conversion coating or powder coat; a moulded part usually needs gate trimming and nothing else, with colour and texture built into the tool. That is why a die-cast housing is rarely the cheapest part at the same wall thickness: the secondary operations are part of the process, not an option.

    The hybrid housing is often the right answer

    Many production housings are both. A die-cast aluminium chassis carries the load, spreads heat from the power stage and provides the electromagnetic shield; a moulded cover closes it, provides the visible surface, the colour and the user interface, and keeps hands away from a hot or live surface. The joint is designed once, with a gasket groove in the casting and a matching lip in the cover, and the assembly is usually cheaper and lighter than an all-metal box and more capable than an all-plastic one.

    The design rules for the hybrid are worth stating. Put the tight tolerances and the sealing groove in the metal part, because it is more dimensionally stable and can be machined. Use the plastic part for features that need to flex, clip or insulate. Keep the thermal path in the metal and the user-contact surfaces in plastic. Decide the split before either tool is cut, because the parting line between the two parts is the one interface that cannot be fixed later without changing both tools.

    One common false economy: casting a housing that will be almost entirely covered by a plastic shell. If the metal is hidden, its cosmetic surface, its texture and much of its as-cast tolerance are being paid for and never seen. In that case either expose more metal, or move the part to moulding and use metal only where the function demands it.

    A decision sequence for a new housing

    Ask whether the part must be metal: structural load, heat spreading, electromagnetic shielding, fire rating or a grounded chassis. If yes, die casting is the default at volume, and machining at low volume. If no, ask whether the annual volume clears the plastic tooling threshold, which for most consumer housings is a few thousand parts. Then ask whether the surface must be cosmetic in colour, in which case moulding wins on both cost and finish. Finally, check the tool: draft, wall uniformity, gate position, ejector marks and, for a casting, the thermal balance of the die. Most housing failures at first article are one of those five, not a material problem.

    Four stage decision flow for a housing: first ask whether it must be metal for strength, heat, EMI or fire, then whether annual volume clears five thousand parts, then whether it needs electrical insulation, and finally check the tool for shot life and draft angle
    Function first, volume second, tool third. A housing that fails the first question cannot be rescued by a cheaper tool.

    See die casting for the metal route and its alloys, injection moulding for the plastic route and its design rules, and surface finishing for the coating and anodising steps that follow either process.

    Scope and sources. The tooling ranges of 10,000 to 100,000 dollars for injection moulding and 15,000 to 150,000 for die casting, cycle times of 15 to 60 and 20 to 90 seconds, wall thickness of 0.5 to 4 mm and 1 to 6 mm, the break-even bands of 1,000 to 10,000 and 5,000 to 50,000 parts, and the note that a small plastic housing may cost 0.40 dollars against 1.50 die cast are from a process comparison of injection moulding and die casting. The melt temperatures of 600 to 720 degrees Celsius for aluminium against 200 to 300 for polymers, the die face temperature of 180 to 320 degrees Celsius, the H13 die life of 100,000 to 150,000 shots for aluminium and 500,000 or more for zinc, and the failure modes of thermal fatigue against wear are from a die casting die reference. The process sequence, the housing and enclosure applications of each route and the secondary operations that follow are from a die casting and injection moulding comparison. The ISO 8062 and ISO 20457 tolerance systems are public standards for castings and moulded plastics respectively; the tolerance figures are working values and should be confirmed for the specific feature and material.

  • What are the most common die casting defects and how are they prevented?

    The short answer

    Porosity, cold shuts, flash, shrinkage, hot cracks and die soldering cause most die casting rejects. Start with the void shape: round voids are gas from venting and shot profile, jagged voids are shrinkage from feeding and wall design. Cut a section before changing any parameter.

    The defect map

    Die casting has a short list of failure modes and a long list of causes, and the useful way to organise them is by mechanism rather than by name. Filling defects happen when metal arrives cold, slow or turbulent: cold shuts, misruns and gas porosity all come from that family. Feeding defects happen after the cavity is full, when the casting contracts and there is no liquid metal or pressure to follow it: shrinkage porosity, sinks and hot cracks. Tooling defects come from the die itself: flash from a parting line that no longer closes, soldering from a die face that is too hot, heat checking from thermal cycling. Almost every defect a buyer sees on an incoming inspection traces back to one of those three families, and the fix is different for each.

    Matrix of eight die casting defects with mechanism and first fix: gas porosity from air trapped during fill fixed by venting and vacuum, shrink porosity from missing feed fixed by intensification, cold shut from cold metal fronts, misrun from early freezing, flash from clamp and die wear, hot cracks from uneven contraction, soldering above 400 degrees Celsius and blisters from gas under the skin
    Read the middle column first. Two defects that look alike on the surface often have opposite causes, which is why parameter changes made without a diagnosis usually make things worse.
    DefectWhat it looks likeUsual causeWhat to change
    Gas porosityround internal voids, blisters after heat treatmentair or gas trapped during fillventing, vacuum, slower slow-shot, less lubricant
    Shrink porosityjagged voids, sinks on thick sectionsno feed during solidificationhigher intensification, longer hold, uniform walls
    Cold shutvisible seam or line where fronts metmetal too cold, fill too slow, long flow pathpour temperature, gate velocity, die preheat
    Misrunincomplete corner or thin ribmetal freezes before the cavity fillspour temperature, fill speed, venting
    Flashthin fin at the parting line or slidesclamp too low, die worn, pressure spikeclamp tonnage, die recondition, shot profile
    Hot crackcrack at a sharp transitionuneven contraction, poor ductilityradii, wall uniformity, alloy choice
    Solderingrough torn patch, die damagedie face above about 400 Ccooling, spray coverage, surface treatment
    Blistersurface bubble after T6 or service heatgas just below the skindegas the melt, vent, use T5 instead

    Porosity: gas or shrinkage, and how to tell

    Porosity is the defect that consumes the most meeting time, and most of that time is wasted because nobody has looked at the void. Cut the part through the suspect section and examine the cavity at magnification. A round void with smooth walls is gas: air or vapour was trapped during filling and could not escape before the metal froze. A jagged, irregular void with dendritic edges is shrinkage: the metal contracted as it solidified and there was no liquid metal or pressure available to fill the space it left. The two need opposite corrections, and a parameter change made without that one check has roughly a fifty percent chance of being wrong.

    For gas, the chain is venting, vacuum and shot profile. Vents and overflows belong at the last-filled areas, and the total vent area should be a meaningful fraction of the casting's projected area rather than a token slot; a common target is above 0.5 percent. Where the part is pressure-tight or the wall is thin, vacuum assistance removes the air before the metal arrives. The slow-shot stage should advance the metal without folding air into it, typically 0.1 to 0.3 metres per second, and the fast stage then fills the cavity before the front freezes, typically 35 to 60 metres per second. Lubricant is part of the same system: an over-sprayed die releases gas that has nowhere to go, so a fine atomised spray that leaves the surface slightly damp, not wet, is the target.

    For shrinkage, the chain is intensification, hold time and wall design. Intensification pressure of roughly 40 to 70 MPa, applied before the gate freezes, keeps feeding the casting as it contracts; hold time should cover most of the solidification time of the thickest wall, commonly 2 to 6 seconds. Neither will rescue a part designed with a 6 mm boss beside a 2 mm wall, because the thick section solidifies last and isolated. Coring the boss, adding cooling at the heavy section and keeping walls within about 2 to 1 is the design-side fix, and it is always cheaper than process compensation.

    Range chart of die casting temperature windows in degrees Celsius: aluminium pour at 670 to 700, aluminium die face at 180 to 250, zinc pour at 390 to 430, zinc die face at 180 to 230, magnesium pour at 640 to 680 and the 400 degree onset of aluminium soldering on steel
    Most defects start at the edge of a window rather than in the middle. A die running at 150 C has cold-shut risk; one running at 320 C has soldering and heat-check risk.

    Thermal balance is the root cause most people skip

    Die temperature decides fill, solidification and die life at the same time, which is why it is the first thing an experienced die caster checks and the last thing a buyer hears about. Aluminium dies normally run with a face temperature of 180 to 250 degrees Celsius at steady state. Below that range, metal freezes on contact, cold shuts and misruns appear, and intensification cannot reach the cavity. Above it, the release agent breaks down, aluminium starts to react with the steel, and soldering begins; the reaction becomes aggressive above roughly 400 degrees Celsius at the die surface, which is why local hot spots do the most damage.

    Thermal balance is also a geometric problem. A die with a thick steel mass on one side and a thin core on the other will run hot on the heavy side and cold on the thin side, no matter what the controller says, because the heat input and the cooling capacity are not matched. The fixes are cooling lines placed by thermal simulation rather than by convenience, baffles or bubblers in deep cores, and a spray pattern that actually covers the hot zones instead of the whole face evenly. Where a die is chronically out of balance, a die coat or a local insert of high-conductivity material is often more effective than another round of parameter tuning.

    Defects that process settings cannot fix

    Some defects are designed in. Sharp internal corners concentrate stress and start hot cracks; generous radii at every transition are the cheapest fix in the whole process. Abrupt wall changes create isolated heavy sections that cannot be fed, so a gradual transition over at least three times the thickness difference is better than a step. Deep, narrow pockets need long thin cores that bend and run hot, so they should be widened or split. Undercuts add slides, and every slide adds a parting line that can flash and a surface that can solder.

    Heat treatment belongs in the same category. A T6 treatment on a casting with uncontrolled porosity turns trapped gas into blisters, because the gas expands at solution temperature and pushes the skin out. Where porosity cannot be eliminated, T5 ageing gives most of the dimensional stability with much less blister risk, and vacuum impregnation can seal micro-porosity in non-structural, pressure-tight parts such as housings and valve bodies. Neither is a substitute for a sound casting, but both are legitimate routes for a part that is otherwise correct.

    What to specify and what to inspect

    A die casting purchase order that says "no porosity" is unenforceable, because no process delivers it. What works is a specification by zone and function: structural sections and pressure boundaries get a defined porosity level verified by X-ray or sectioning, cosmetic faces get a surface acceptance standard, and non-critical sections get the general level. State the inspection method and the sampling frequency, because a visual check and a radiograph answer different questions. For pressure-tight parts, state the leak test pressure and the acceptance criterion, and decide in advance whether impregnation is permitted.

    On the process side, ask for the shot profile, the die temperature record and the die maintenance interval, and ask how the supplier verifies that intensification is reaching the cavity. A supplier who can show those three things is controlling the causes; one who can only show final inspection is controlling the symptoms, and the symptoms will move to the next order.

    Four step porosity diagnosis flow: cut a section and read the void shape, round voids mean gas so check vents and the shot profile, jagged voids mean shrinkage so raise intensification and even the walls, then X-ray the next thirty shots to verify the correction
    The loop is deliberately short. One sectioned part and thirty verified shots resolve most porosity arguments faster than a week of parameter changes.

    See die casting for the process and the alloys behind these defects, aluminium die casting for housing and bracket work, and surface finishing for the coating steps that follow casting and can hide or reveal a surface defect.

    Scope and sources. The distinction between round gas voids and jagged shrinkage voids, the troubleshooting order that starts with a sectioned part, the effect of venting and overflow design, the 400 degree Celsius onset of aluminium soldering on steel and the use of vacuum impregnation are set out in a die casting defect and prevention guide. The slow-shot range of 0.1 to 0.3 metres per second, fast shot of 35 to 60 metres per second, pour temperature of 670 to 700 degrees Celsius, die temperature of 180 to 250 degrees Celsius, intensification of 40 to 70 MPa, hold time of 2 to 6 seconds, clamping of 40 to 70 kilonewtons per square centimetre of projected area and vent area above 0.5 percent of projected area are from a review of aluminium die casting parameters. The H13 die life of 100,000 to 300,000 shots for aluminium, the T5 against T6 blister risk, the 0.5 to 1.0 mm machining allowance and the cavity-count guidance are from a die casting design and defect prevention guide. These are typical windows; the correct settings for a specific die are established on its own trial shots.

  • How does zinc alloy die casting compare to aluminum in strength and cost?

    The short answer

    Zinc wins on strength per unit volume and on thin walls; aluminium wins on strength per kilogram. Zamak 3 reaches 215 to 283 MPa tensile with about 10 percent elongation, against about 320 MPa with 1.5 to 3.5 percent for A380. Zinc is 2.4 times denser, so aluminium wins any weight-driven programme.

    Strength: the same headline number, two different meanings

    Zinc and aluminium are quoted with tensile strengths in the same range, and that is where the confusion starts. The headline figure says nothing about how much of that strength is available per kilogram, and nothing about how the material behaves when it is overloaded. Both matter more than the tensile number itself, so the comparison has to be read column by column rather than row by row.

    Comparison table of A380 aluminium against Zamak 3 and Zamak 5 zinc die casting alloys on tensile strength, yield strength, elongation, hardness, density, melting point, minimum wall thickness, thermal conductivity, die life and material cost
    The tensile row looks like a tie. The yield row, the elongation row and the density row do not.
    Property, as castA380 aluminiumZamak 3 zincZamak 5 zinc
    Tensile strengthAbout 320 to 325 MPa215 to 283 MPa270 to 331 MPa
    Yield strengthAbout 160 MPa140 to 221 MPaAbout 210 MPa
    Elongation at break1.5 to 3.5 percentAbout 10 percentAbout 7 percent
    Brinell hardness75 to 80 HB82 HB89 to 91 HB
    Density2.71 to 2.76 g/cm36.60 g/cm36.60 g/cm3
    Melting point540 to 660 °C381 to 387 °C380 to 386 °C
    Minimum wall thickness2.3 to 2.5 mm0.5 to 1.0 mm0.5 to 1.0 mm
    Thermal conductivity96 W/m-K113 W/m-K109 W/m-K
    Die life, typical shots100,000 to 300,000500,000 to 1,000,000500,000 to 1,000,000
    Raw material cost index1.00 baseline0.70 to 0.850.75 to 0.90
    Casting processCold chamberHot chamberHot chamber

    Two readings matter. First, Zamak 3 has a lower tensile figure than A380 in most tables and a higher yield figure, which means it reaches its working stress with less permanent deformation. Second, the elongation column is the one that predicts failure in service: zinc stretches about three times as far before it cracks, so a zinc part absorbs impact and tolerates assembly bending that would break a comparable aluminium part.

    The density penalty is the real dividing line

    Density is the single most decisive figure in the comparison. Zinc is 6.60 g/cm3 against 2.71 to 2.76 g/cm3 for A380, so it is 2.4 times heavier for the same geometry. A zinc part weighing 100 grams weighs about 41 grams in aluminium. Normalising strength by density makes the trade explicit: A380 lands near 116 to 120 MPa per unit of specific gravity, while Zamak 3 lands near 43 and Zamak 5 near 50.

    Bar chart of specific strength for die casting metals: A380 aluminium at about 118 MPa per unit density, Zamak 5 zinc at about 50 and Zamak 3 zinc at about 43
    Per kilogram, aluminium is about 2.4 to 2.8 times stronger. Per cubic centimetre, zinc is the more efficient material.

    That is why the two alloys end up in different product families rather than competing for the same one. Wherever weight drives a functional or economic outcome — vehicle fuel economy, shipping cost, a handheld product, a structural housing — aluminium wins and the density row settles the argument before any property table is consulted. Wherever the part is small and heavy use is not a concern, the density penalty is irrelevant and the zinc advantages become decisive.

    Elongation and impact: where zinc wins outright

    Zinc has roughly 10 percent elongation as cast and aluminium about 3.5 percent, and the gap is not a rounding difference. A material that stretches 10 percent before it breaks absorbs energy that a material stretching 3.5 percent does not, so zinc parts survive drop tests, crimping, staking, press fits and assembly torques that crack the same geometry in aluminium. Zinc also delivers higher hardness, 82 to 91 HB against 75 to 80 HB, which translates into better wear behaviour in mechanisms that rub.

    Bar chart of elongation at break for die casting alloys: Zamak 3 zinc at about 10 percent, Zamak 5 zinc at about 7 percent, A380 aluminium at 1.5 to 3.5 percent and AZ91D magnesium at about 3 percent
    Published elongation for the same alloy varies with section thickness and casting quality, so read the chart as a ranking rather than a specification.

    The exception is temperature. Zinc creeps under sustained load above about 100 °C, and intergranular corrosion is a real risk if the alloy is made from contaminated scrap rather than from specified high-grade ingot. Where a part runs hot or has to be welded, aluminium takes over regardless of the elongation advantage.

    Cost: what actually drives the per-part figure

    The zinc alloy itself is cheaper per kilogram than A380 — the material index sits at roughly 0.70 to 0.85 against an aluminium baseline of 1.00 — but the density penalty reverses that on a per-part basis for anything large, because 2.4 times the density means about 2.4 times the metal in the same geometry. Per-part cost therefore comes down to four things that have nothing to do with the price of the ingot.

    Cost driverZinc (hot chamber)Aluminium (cold chamber)Effect on unit cost
    Die life500,000 to 1,000,000 shots100,000 to 300,000 shotsTooling amortised over 3 to 5 times as many parts
    Cycle time300 to 500 shots per hour on small parts5 to 15 seconds longer per shotLower machine cost per part for zinc
    Melting temperature381 to 387 °C540 to 660 °CLess energy per kilogram melted
    Material mass per part2.4 times the aluminium massBaselineReverses the price advantage on large parts
    Tooling investmentSimple dies from about USD 15,000Large structural dies above USD 300,000Lower entry cost and lower change cost for zinc

    Put together, zinc is usually the cheaper route for small, intricate parts, where thin walls, long die life and a fast hot-chamber cycle outweigh the metal mass. Aluminium is usually the cheaper route for large parts, where its lower density means less metal, less weight and a smaller machine. The crossover is not a single quantity: it depends on part size, wall thickness, cavity count, annual volume and how much secondary machining the casting needs.

    Choosing between them

    • Choose zinc when the part is small, weight is not critical, walls thinner than 1 to 1.5 mm are needed, the as-cast tolerance has to hold within about plus or minus 0.05 to 0.1 mm, the surface has to plate directly, or ductility is needed for staking, crimping or assembly.
    • Choose aluminium when weight drives the design, the part is large, service temperature exceeds about 100 to 120 °C, the part has to be anodised, or the programme needs pressure tightness and the option of impregnation.
    • Choose zinc for the tool, aluminium for the part, when volumes are high. A zinc hot-chamber die lasts three to five times as long, so a programme that can use zinc tooling and aluminium parts is unusual but not impossible, and the two materials are not interchangeable within one die.
    • Check the finishing route before the alloy is fixed. Zinc plates directly and takes a mirror polish; aluminium needs pretreatment before plating but can be anodised in colour. The finish often decides the alloy rather than the other way round.

    Limits and open questions

    • Published property tables disagree. Tensile strength for Zamak 3 is quoted from 215 to 283 MPa and elongation for the same alloy from 7 to 13 percent depending on source, section thickness and casting quality. Treat any single number as an indicative value and test a coupon in the real section thickness.
    • Die life depends on the die, not only the alloy. The 500,000 to 1,000,000 shot figure for zinc assumes good thermal management and correct maintenance; some foundries publish a more conservative 200,000 to 500,000, especially on dies with long cores and slides.
    • Zinc creeps when it is hot. Sustained loads above roughly 100 °C cause dimensional change, so zinc is the wrong choice for engine-adjacent, lighting or heat-soak components.
    • Corrosion protection is not optional outdoors. Zinc develops a stable oxide layer in clean air, but outdoor and marine service still needs plating, powder coating or a conversion coating, and plated parts need the plating specified rather than assumed.
    • Aluminium is not pressure tight without help. A380 can be impregnated to seal porosity, which is an extra operation; casting quality and process control decide whether it holds.
    • No certification is implied here. Which quality system applies to a given programme is confirmed per programme and per factory in writing before production.

    What to send for a material recommendation

    Send the 3D model, the toleranced 2D drawing, the annual volume, the load path, the service temperature and the finish required. Those six items settle the alloy before price is quoted: a weight-critical or hot-running part points to aluminium, a small thin-wall or impact-loaded part points to zinc, and a part that needs a mirror-plated surface points to zinc for reasons that have nothing to do with strength. See aluminium die casting for large structural and thermal parts, surface finishing for the plating and coating routes, and send a drawing for a free design review that compares both alloys on your part.

    Scope and sources. Property ranges and cost drivers were compiled in 2026 from an aluminium and zinc die casting comparison (A380 at 325 MPa and 160 MPa yield, Zamak 3 at 215 to 250 MPa, Zamak 5 at 270 to 310 MPa, density 2.71 against 6.60 g/cm3, melting 540 to 660 °C against 381 to 387 °C, Brinell 80 against 82 and 91 HB, minimum wall 2.3 to 2.5 mm against 0.8 to 1.0 mm, die life 100,000 to 300,000 shots against 500,000 to 1,000,000, raw material index 0.70 to 0.90) and from a zinc die casting alloy reference (Zamak 3 at 283 MPa and 10 percent elongation, Zamak 5 at 328 MPa, A380 at 317 MPa, density 6.60 against 2.74 g/cm3, calculated specific strength of 43 against 116 MPa per unit density, and the intergranular corrosion risk from contaminated scrap). Alloy and application data were checked against a die casting materials guide and a zinc alloy property table. Cycle rate, machine economics and tooling price bands come from a die casting process and lead-time review (small zinc parts at 300 to 500 shots per hour in a hot chamber, cold chamber adding 5 to 15 seconds per shot, a simple zinc die from about USD 15,000, a large structural aluminium die above USD 300,000). These are typical published as-cast values; section thickness, casting parameters, alloy lot and finishing route all move them, and none of the figures is a specification for a particular part. Nothing on this page states or implies a certification held by any supplier.