Sheet Metal Fabrication
SOMI Capability
SOMI Sheet Metal Fabrication Capability

Laser Cutting
Laser cutting is a technology that uses a high-powered laser beam to cut materials such as metal, wood, plastic, and more with precision and accuracy.
High precision, Fast processing speed.
Diverse selection of materials and material thickness.

Metal Bending
Metal bending is a process that involves deforming metal sheets or bars to form desired shapes and angles.
High precision and accuracy.
High flexibility in curved shape.
Enhanced metal component strength and durability.

Metal Welding
Metal welding is a process that involves joining metal pieces together by heating them to their melting point and then allowing them to cool, forming a strong and durable bond. This technique is essential for creating complex structures and components in various industries.
Versatility in Joining Techniques.
Enhanced Structural Integrity and Durability.
Sheet Metal Fabrication
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Sheet Metal Fabrication
Sheet Metal Fabrication Materials
In sheet metal fabrication, selecting the right material is crucial for ensuring the performance, durability, and cost-effectiveness of the final product. The following are some common materials used in sheet metal fabrication along with their characteristics, to help you make the best choice for your project.
Metals Suitable for Sheet Metal Processing


- 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
Sheet Metal Fabrication
Sheet Metal Fabrication 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 Sheet Metal Fabrication

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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Quality Assurance at the Heart of Our Operations
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Contact us Today for Your Sheet Metal Fabrication Requirements
Ready to elevate your manufacturing with the precision and quality of SOMI's Sheet Metal Fabrication 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.
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FAQ
Frequently Asked Questions
- How do you design sheet metal parts for manufacturability?
The short answer
Start with thickness: it sets every other limit. Keep holes at least one thickness across and 2.5 thicknesses plus the bend radius away from a bend line, keep the inside bend radius at one thickness for mild steel, and tolerance to ISO 2768-m except where a feature actually mates. That removes most avoidable cost before a quote is issued.
Thickness first, because it sets every limit
Sheet metal design for manufacturability is usually presented as a list of independent rules, which is misleading. The rules are all functions of one number. Material thickness sets the minimum hole diameter, the minimum inside bend radius, the minimum flange the press brake can grip, the distance a hole must stay clear of a bend, the tonnage needed to cut and form, and the tolerance the process can hold. Change the thickness by 50 percent and every one of those limits moves with it, which is why "make it thicker so it is stronger" is such an expensive instinct: a formed rib, a swage or a change of section will often deliver the stiffness at a fraction of the cost, without moving every constraint on the drawing.
The practical range for fabricated sheet parts is 0.5 to 3 mm for enclosures and brackets, 3 to 6 mm for structural work, and beyond 6 mm bending capability falls away quickly and machining or casting usually becomes the better route. Standardising on one or two gauges across an assembly is worth more than optimising each part individually, because it removes material changes, separate setup and separate scrap handling from the shop floor.
Holes, slots and edges
Holes smaller than the material thickness are the classic DFM error. A laser can technically cut a 0.5 mm hole in 2 mm steel, but the cut is slow, the hole tapers, and the heat-affected zone around it is larger than the hole itself; a punch needs a tool that small and will break it. The working rule is a minimum diameter equal to the thickness, with 1.2 times the thickness preferred for a clean laser cut. The same logic applies to slots: a slot narrower than the sheet thickness cuts badly and wears tooling, so keep the width at one thickness or more.
Position matters as much as size. Holes placed inside the bend deformation zone stretch into ovals as the material flows, and the distortion is not recoverable after forming. Keep holes and slots at least 2.5 times the thickness plus the inside bend radius away from the bend line, keep them 1.5 times the thickness from any edge, and leave 2 times the thickness between adjacent holes so the web between them does not distort. Where a hole must sit close to a bend for functional reasons, the usual fix is to cut it after forming, or to add a relief so the deformation has somewhere else to go.
Every distance in the middle column is a multiple of thickness, which is why the thickness decision comes before the feature layout. Feature Rule of thumb Reason Hole diameter at least 1.0 x t, 1.2 x t preferred smaller holes burn, taper or need a second operation Hole to bend line 2.5 x t + inside radius the bend deformation zone pulls the hole out of round Hole to edge 1.5 x t thin ligaments tear during forming and handling Hole to hole 2.0 x t the web distorts and the pitch drifts Slot width 1.0 x t narrow slots cut with dross and wear the punch Internal corner radius 0.5 x t a round cutter cannot produce a sharp internal corner Minimum flange 4.0 x t + bend radius shorter flanges cannot be supported by the V-die Bend radius and flange length
The minimum inside bend radius is a material property, not a shop preference. Mild steel and soft aluminium form at about one thickness; stainless work-hardens in the bend and needs 1.5 to 2 thicknesses; 6061-T6 aluminium is the exception that catches designers out, needing 3 to 4 thicknesses because the tempered alloy has almost no ductility left and cracks on the outside of a tight bend. Bending across the rolling direction rather than along it also raises the safe radius, because the grain structure is anisotropic. When a design needs a tighter radius than the material allows, the answer is usually a softer temper or a different alloy rather than a press brake operator trying harder.
Flange length is the other half of the bend rule. A press brake grips the flange between the punch and the V-die, and a flange shorter than about four thicknesses plus the bend radius cannot be supported through the stroke; it slips, the angle drifts, and the operator ends up making a special tool. The same constraint applies to the distance between two bends: if the flat between them is shorter than the tooling needs, the part cannot be formed in the intended sequence. Both are visible on the flat pattern before any tooling is cut, which is why the flat pattern, not the 3D model, is the drawing the shop actually quotes from.
6061-T6 is the outlier that causes most cracked bends. If the design needs a tight radius, change the temper, not the tooling. Tolerances: spend them only where they matter
Over-tolerancing is the single largest avoidable cost in sheet metal. A fabricated part is a stack of processes, each with its own natural variation: laser positioning, bend angle, bend position, hole distortion after forming, and welding distortion if the part is assembled. ISO 2768-m general tolerances cover the overwhelming majority of features at no extra cost. Naming a tighter value on a feature that does not mate, seal or locate does not make the part more accurate; it adds inspection, rejection and price. The workable discipline is to tolerance by function: identify the features that locate a mating part, carry a load or seal against something, give those an informed callout, and leave everything else under general tolerance.
Characteristic Normal capability What tightening costs Laser cut feature position ±0.1 mm under 300 mm inspection time, not accuracy Bend angle ±0.5 degrees in-process adjustment, slower cycle Bend to bend dimension ±0.3 to 0.5 mm special tooling or a second hit Hole position after forming ±0.3 mm post-form drilling General tolerance ISO 2768-m nothing, it is the default Halving any of the above not a process capability 15 to 30 percent added to part price Features that quietly add operations
Several features are cheap on a drawing and expensive on a routing. A countersink or counterbore is a second operation, and on a laser-cut part it usually means a drill press and a fixture. A tapped hole is a third. A press-fit insert needs a hole sized for it and enough material around it to displace into, which sets a minimum thickness and edge distance that the design may not have. A weld seam adds fixturing, distortion and post-weld finishing, and a full-length cosmetic weld on thin sheet is one of the most expensive lines you can put on a drawing. A blanket "deburr all edges" note is also an operation, sometimes a manual one, on a part that may only need two edges dressed. Each of these is legitimate when the function requires it; the error is adding them by default.
The review order that catches cost early
Because the constraints cascade, the review has to run in order. Fix the thickness first and check that it is a stocked gauge. Place holes and slots next, against the bend lines rather than against the part outline, because the bend lines are what move during forming. Then set the bend rules: inside radius, flange length, relief at the end of every bend line, and a bend sequence the tooling can actually run. Tolerance last, general first and critical features only where they earn their cost. Finish after that, because a powder coat adds 60 to 90 microns and will close a small gap or fill a fine thread that was dimensioned before coating was considered.
Running the review in this order means each decision is made once. Running it backwards is how a part gets redesigned three times before the first cut. See sheet metal fabrication for the laser cutting, bending and assembly capability these rules are written against, custom sheet metal parts for bracket and enclosure work quoted from a flat pattern, and metal bending for press brake work where flange length and radius decide the tooling.
Scope and sources. The DFM checklist of hole diameter at least one thickness, internal corner radius at least half a thickness, hole to bend line at least 2.5 thicknesses plus the inside radius, minimum flange set by the V-die, slot width at least one thickness, edge distance at least one thickness and ISO 2768-m as the default tolerance is set out in a sheet metal DFM rule set written for the shop floor. The thickness bands of 0.5 to 3 mm for enclosures, 3 to 6 mm for structural parts, the 1.0 and 1.5 thickness bend radius rules, the hole spacing figures and the ISO 2768-m reference come from a manufacturability guide for sheet metal parts. The laser tolerance of ±0.1 mm, bend angle of ±0.5 degrees, flange of ±0.5 mm, formed hole position of ±0.3 mm and the 15 to 30 percent cost of halving a tolerance are from a sheet metal fabrication design guide. The 4 times thickness plus radius flange minimum, the 2.5 times thickness plus radius hole clearance and the 3 to 4 times thickness radius for 6061-T6 are from a fabrication guide covering bend radius and hole placement, with slot orientation and tolerance-by-function advice in a sheet metal design guide. These are standard-tooling rules; the exact limits for a specific gauge, temper and tool set should be confirmed by the fabricator on your flat pattern.
- Which sheet metal finish resists outdoor corrosion best?
The short answer
For bare steel outdoors, hot-dip galvanizing lasts longest: an 85 micron coating gives roughly 20 to 40 years in a C4 coastal or industrial site, and it keeps protecting scratched edges. Where colour is needed, powder over galvanizing adds a second barrier; 316L stainless needs no coating in marine air.
Why there is no single best finish
Corrosion is a rate, not a property of a coating. The same 85 micron zinc layer will last more than a century on a heated indoor frame and somewhere between ten and twenty years on a jetty, because the atmosphere around it consumes zinc at a different speed. ISO 9223 sorts atmospheres into categories from C1, a heated interior, to CX, an offshore splash zone, and the first-year zinc loss rises from about 0.1 microns to 8.4 microns a year across that range, with uncoated steel losing between 1.3 and 200 microns in the same year. Until you know which category the part will live in, any claim that one finish is "best" is a guess.
So the honest answer has two parts. If the part can stay unpainted and the environment is C3 or worse, hot-dip galvanizing is the benchmark, because it protects by sacrificing zinc rather than by sealing the surface. If the part must be a colour, or the environment is C4 to C5, a duplex system of powder over galvanizing is the usual specification. Everything else on this page is the reasoning behind those two sentences, and the cases where neither applies.
The finishes ranked for outdoor exposure
Six finishes account for most outdoor sheet metal work, and they fail in different ways. Hot-dip galvanizing immerses the fabricated part in molten zinc, forming zinc-iron alloy layers that are metallurgically bonded to the steel; the coating is thick, abrasion resistant and cathodic, so a scratch does not become a rust site. Powder coating over bare steel is a barrier only: it is tough and UV stable while intact, but any pinhole, cut edge or scratch exposes steel that has no protection of its own, and rust creeps under the film from that point. A duplex system combines the two, with the powder giving colour and UV resistance and the zinc giving sacrificial protection at every damaged point. E-coat is a thin, uniform epoxy film that reaches recesses and edges well but degrades in sunlight unless it is topcoated. Zinc plating is electrodeposited and therefore thin, typically 5 to 15 microns, which is adequate indoors and inadequate at the coast. Anodizing works only on aluminium, where the oxide layer is grown from the metal itself and cannot chip off, but it is brittle and colour fades in strong UV. Bare 316L stainless relies on its molybdenum content for pitting resistance and needs no coating at all in marine air, at a material cost several times that of coated carbon steel.
The mechanism column matters more than the hours column. Sacrificial coatings keep working after damage; barrier coatings stop working where they are damaged. The one row that surprises buyers is powder on bare steel. A good polyester powder at 70 to 80 microns will pass 750 hours of salt spray on a test panel, which reads like a decade of protection, and on a real fabrication it often fails at the cut edges first, because those edges were never coated to the same thickness. This is why the same powder performs far better over galvanizing: the edge is protected by zinc even where the film is thin.
Zinc thickness sets the service life
Once the substrate is galvanized, life becomes arithmetic: coating thickness divided by the local zinc loss rate. The rate comes from the corrosivity category, and the thickness comes from ISO 1461, which sets minimum mean coating masses by article thickness rather than one number for everything. That detail matters for sheet metal specifically, because sheet parts are thin. A 6 mm plate is guaranteed 85 microns, a 3 mm sheet 70 microns, a 1.5 mm sheet 55 microns and anything under 1.5 mm only 45 microns. The same galvanizing bath therefore produces a coating on a 1.2 mm enclosure panel that will last roughly half as long as the coating on a 10 mm base plate, and no amount of specification writing changes that.
Read this as a ranking, not a service life. Salt spray is one constant condition; a real site cycles between wet, dry, sun and frost. Corrosivity category Typical site Zinc loss, year one Life of an 85 micron coating C2 low rural, unheated buildings 0.1 to 0.7 microns over 100 years C3 medium urban, light industrial 0.7 to 2.1 microns 40 to over 100 years C4 high industrial, coastal 2.1 to 4.2 microns 20 to 40 years C5 very high high-salinity coast 4.2 to 8.4 microns 10 to 20 years CX extreme offshore, splash zone 8.4 to 25 microns 3 to 10 years Two cautions on that table. The rates are first-year figures, and zinc corrosion slows as the surface patina builds, so real life is usually longer than a straight division suggests. And the table assumes sound galvanizing at the full coating thickness; a 45 micron coating on thin sheet lands at roughly half the life shown, which is why thin-gauge outdoor parts are often specified as duplex rather than galvanized alone.
Where each finish fails outdoors
Powder on bare steel fails at edges, holes and scratches, then creeps: a rust blister lifts the film and holds water against the steel. Hot-dip galvanizing fails at welds and seams that were not sealed, in trapped water, and through white rust if parts are stacked wet in storage before installation. It also distorts thin panels in the molten bath and fills threaded holes and close-tolerance bores unless they are masked or re-tapped. Anodizing fails where the oxide is cracked by bending after coating, and its colour fades under UV even though the corrosion protection remains. Zinc plating fails simply because it is too thin for chloride exposure; 168 hours of salt spray is a few months at the coast. E-coat fails in sunlight unless a topcoat is added, and its thin film offers little abrasion resistance on handling edges. Bare 316L fails only in warm chloride environments where pitting can start, typically above 60 degrees Celsius or in stagnant seawater.
One specification trap: "stainless steel" is not a finish. A 430 or 304 part in a coastal C4 site will show tea staining within months, while 316L in the same place stays clean. If the drawing says only "stainless", the finish has not been specified at all.
Design rules that keep a coating intact
Coatings fail at geometry long before they fail at chemistry. Any closed hollow section that will be galvanized needs vent and drain holes, sized and placed so the zinc can flow in and out and no air pocket is trapped; the same holes prevent a blowout in the bath. Lap joints, hemmed edges and overlapping panels should be avoided or sealed, because they create a crevice that holds electrolyte and cannot be coated. Sharp external edges should be broken with a small radius, since a paint or powder film pulls thin over a sharp corner and that is where corrosion starts. Mixed fasteners are a similar problem: a stainless bolt in a galvanized bracket creates a galvanic couple that eats the zinc locally. Finally, do not mix finishes within one assembly unless you intend the difference, because a painted bracket bolted to a bare galvanized frame will show a colour mismatch and will also concentrate coating damage at the joint.
What to put on the drawing
A corrosion specification needs five numbers or phrases, and most drawings carry only one. State the substrate grade, the finish process and its standard, the coating thickness in microns with a minimum as well as a nominal, the test method and hours with pass and fail criteria, and the areas to be masked. "Powder coat black" is not a specification; "polyester powder, 70 to 90 microns, over hot-dip galvanized to ISO 1461, 1,000 hours neutral salt spray to ASTM B117 with no red rust and no blistering above rating 8, threads masked" is. The test method matters because ASTM B117 and ISO 9227 define the apparatus but not the acceptance criteria; the buyer has to write those, and a supplier cannot be held to a limit that was never stated.
Most projects answer the first two questions quickly. The last step, writing the numbers, is the one that gets skipped. See surface finishing for the coating processes we run on fabricated parts, sheet metal fabrication for cutting, forming and assembly before coating, and custom sheet metal parts for the bracket and enclosure work these finishes are usually applied to.
Scope and sources. The ISO 9223 corrosivity categories, first-year zinc loss rates of 0.1 to 8.4 microns, the 85 micron ISO 1461 coating on steel over 6 mm and the resulting service-life estimates are set out in a galvanising, powder coating and duplex comparison, with the same category table and the steel-loss column given in a coating-life guide for high-salinity sites. The ISO 1461 minimum mean thicknesses of 45, 55, 70 and 85 microns by article thickness, and the conversion of 610 grams per square metre to 85 microns, come from a hot-dip galvanizing service-life reference. The salt spray benchmarks of 96 to 336 hours for zinc plating, 500 to 1,000 hours for powder over steel, 1,000 to 1,500 hours for powder over galvanizing, 336 to 1,000 hours for Type III anodizing and 1,000 plus hours for bare 316L are from a guide to writing corrosion specifications for outdoor fabrications, with cost and service-life context in a surface-finish cost comparison. These are planning figures for standard processes; the coating thickness and test hours for a specific part should be confirmed against the actual site category and the coater's capability.
- What is a bend relief and why does it prevent tearing?
The short answer
A bend relief is a small notch cut at the end of a bend line, where the bend meets an edge or another flange. Without it the material has nowhere to flow, so it tears or bulges. Cut it at least one material thickness wide and as deep as the bend radius plus one thickness.
Why a bend with no relief tears
When sheet metal is formed, the outside of the bend stretches and the inside compresses, so material has to move along the bend line to accommodate the change. Where that line ends at the edge of the sheet, at a notch, or at another flange that is already formed, the material has no direction left to flow in. The strain then concentrates at the very end of the bend line: the outer fibre exceeds what the sheet can take and the corner tears, or the material piles up and bulges outwards instead. The failure is created in the flat pattern, not at the press brake, which is why a design that looks perfect in a 3D model can arrive as a box with exploded corners, sharp burrs and a deformed adjacent flange. Cutting a small piece of material away before forming gives the bend somewhere to go; that cut is the relief.
The two rules that size a relief
Two dimensions matter, and both are tied to the material thickness and the inside radius rather than to a fixed number. The relief must be at least one material thickness wide, with about twice the thickness a comfortable working value. It must be at least as deep as the bend radius plus one thickness, and roughly the bend radius plus 1.2 times the thickness if you want margin. The depth rule has a physical reason: the relief has to reach past the bend line, because a cut that stops short of it leaves the flange to tear exactly as it would with no relief at all. A worked example is easier than the algebra. For a 2 mm aluminium part with a 2 mm inside radius, the minimum relief is 2 mm wide and 4 mm deep, and 4 mm wide is the value that gives the tooling room and leaves a visibly deliberate notch rather than a ragged corner.
All four numbers scale with the thickness. Change the material to 3 mm and every figure moves with it. Feature Rule For a 2 mm part, R2 Relief width, minimum 1 x material thickness 2 mm Relief width, recommended about 2 x material thickness 4 mm Relief depth, minimum bend radius + material thickness 4 mm Relief depth, recommended bend radius + 1.2 x thickness 4.4 mm Minimum flange length to form 4 x thickness + bend radius 10 mm Feature to bend distance 2.5 x thickness + bend radius 7 mm Minimum inside bend radius 1 x thickness, soft alloys 2 mm Minimum inside bend radius 1.5 to 2 x thickness, hard tempers 3 to 4 mm Three relief shapes and when to use each
A rectangular notch is the standard choice for laser-cut and punched work: it removes material cleanly, produces no burr, is trivial to program, and the only cost is a visible gap in the corner of the finished part. A tear relief removes nothing at all, simply slitting the corner so the metal tears along the slit as it bends; it gives the tightest corner with no visible gap, which suits a punched part where the corner will be hidden or welded, but the torn edge is jagged and sharp and can cut fingers or wire harnesses. An obround or rounded slot is the choice for parts that will see vibration or repeated load, because the rounded end spreads the stress concentration instead of leaving a sharp inside corner for a crack to start from; it is slightly slower to cut in thick material and needs the flat pattern checked. Whichever you choose, generate reliefs with the sheet-metal tool in the CAD system rather than drawing them by hand, so the geometry stays consistent with the thickness and radius actually in use.
Rectangular for appearance, tear for a hidden punched corner, obround wherever the part will be cyclically loaded. Relief against the other rules near a bend
A bend relief is not a substitute for the rest of the sheet-metal spacing rules, and it is often confused with them. Holes and slots must sit clear of the bend line, generally at least 2.5 times the material thickness plus the bend radius away, with about 3 times the thickness as a safer figure for critical features; too close and the hole distorts into an oval as the material flows. Flanges have to be long enough for the press brake to grip them: about four thicknesses plus the bend radius is the minimum that forms consistently, and anything shorter needs special tooling or a secondary operation. The inside bend radius itself should be at least one thickness for mild steel and one and a half to two thicknesses for stainless and hard tempers, or the outer fibre cracks regardless of how good the relief is. In other words, a relief protects the end of a bend line; it does nothing for a hole placed too near the middle of one.
What a missing relief costs downstream
The immediate symptom is a torn corner and a burr that has to be dressed by hand, which is a cost in labour and a visible quality defect on any enclosure that a customer will handle. The second symptom is quieter and worse: material bulging outwards at the bend radius means the flange face is no longer flat. A lid or a mating panel then rocks on the corner bulges instead of seating, fasteners pull the joint down and distort the panel, and what looked like an assembly problem turns out to be a forming problem. The third symptom appears later, when a sharp unrelieved inside corner acts as a stress raiser and a crack begins under vibration or thermal cycling; a rounded relief changes that corner into a smooth transition and removes the initiation site. All three are avoided by a cut that takes less than a second on a laser.
The failure and the fix are one operation apart. The relief is cut in the flat pattern, before the material is ever formed. How to specify it on the drawing
Show the relief on the flat pattern rather than describing it in a note, because that is the drawing the laser or punch actually runs from, and give its width and depth as dimensions rather than leaving them to the shop. State the material thickness and the inside bend radius for every bend, since both rules above are derived from them and neither can be assumed from the sheet gauge. Note the bend direction and, where crack risk is high, ask for bends across the grain rather than along it. Keep the bend radius consistent across the part so a single tool set can form it, and flag any flange that falls below the four-thickness minimum early, because that is a tooling decision rather than a drawing one. Finally, mention any surface finish that follows, since a powder coat or paint film will be thinner or missing on the inside of a narrow notch and the gap will be more visible after coating than before it.
See sheet metal fabrication for the laser cutting and forming route we run, metal bending for press brake work quoted from your flat pattern, and metal stamping for tooled parts where a tear relief or a punched notch is built into the die.
Scope and sources. The rule that a relief width of at least 1 x material thickness and a depth of at least the bend radius plus the thickness prevent tearing, the worked example of a 2 mm part with a 2 mm radius needing a relief 2 mm wide and 4 mm deep, the three relief types with their trade-offs, and the bulge that makes a lid rock on the corner are set out in a corner relief design guide. The bend relief rules of width at least 1T and depth at least the bend radius plus 1T, the minimum flange length of about 4T plus the radius, the feature-to-bend distance of 2.5T plus the radius and the minimum inside bend radii of 1T for soft alloys and 1.5T to 2T for hard tempers come from a sheet metal design for manufacturability guide, with the same relief and minimum radius rules stated independently in a note on sheet metal bending technique. The relief width and depth rules expressed against material thickness, the recommended values of twice the thickness and the radius plus 1.2 times the thickness, and the advice to work from the bend line itself come from a sheet metal design practice guide. These are planning rules for standard tooling; the relief that a specific die and material need should be confirmed by the fabricator on your flat pattern.










