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GuidePublished 14 Aug 202623 min readBy Kevin JoginManufacturingManufacturing ProcessesCutting Metal with LasersLaser Welding — Two Modes

Engineering · Manufacturing · Manufacturing Processes

Manufacturing Process Selection from Raw Material to Finished Part: Cutting Metal with Lasers

Engineering handbook for manufacturing process selection from raw material to finished part, covering cutting metal with lasers, laser welding — two modes, laser...

Executive summary

This handbook section converts the supplied engineering material into a practical, source-controlled reference. It concentrates on the following learning outcomes.

Cutting Metal with Lasers
Laser Welding — Two Modes
Laser Drilling
Laser Heat Treatment
Laser Marking
Flame Spraying and Surface Treatments

Cutting Metal with Lasers

CO₂ and Nd:YAG Cutting Speeds for Nonferrous Metals:

Material Thickness (mm) CO₂ Speed (m/min) at 1500W Nd:YAG Speed (m/min) Nd:YAG Power (W)
Copper 1 2.25
Copper 2 0.75
Aluminum 1 8.0 2.5 1,000
Aluminum 2 4.0 1.0 1,000
Aluminum 3 1.5 0.5 1,000
Titanium 1 6.0 1.0 150
Titanium 2 3.0
Brass 1 3.0

Laser Welding — Two Modes

Conduction welding: Relies on thermal diffusivity to conduct heat into the joint. Used for spot welding and partial penetration seam welding.

Deep penetration (keyhole) welding: Beam energy creates a hole through the metal thickness. Vapor pressure holds molten metal against the hole wall. Maximum practical penetration: approximately 25 mm (1 inch).

Key advantage of laser welding: Low total heat input. Heat concentration causes conduction primarily perpendicular to motion. With the beam moving faster than thermal conduction speed, material changes occur only in the narrow path — producing welds with minimum thermal distortion.


Laser Drilling

Method Max Depth (mm) Max Diameter (mm) Aspect Ratio Recast Layer (mm) Taper
Direct (single pulse) 1.5 (metal) / 8 (nonmetal) 0.5 – 1.0 < 10:1 ~0.1 Up to 25%
Percussive (multi-pulse) 25 1.5 50:1 0.5 < 10%
Trepanning (circumferential) 10 2.5 0.025 Minimal

Laser Heat Treatment

At less than 10⁴ W/cm² power density (compared to >10⁵ for cutting), the defocused beam treats surfaces. But there's a challenge: at room temperature, over 90% of CO₂ laser power is reflected by metal surfaces (93% for steel). The surface must be prepared by:

  • Surface roughening (tiny craters trap beam energy)
  • Coating the metal surface (most common method)
  • Using absorptive paints or chemicals

Laser Marking

Two methods:

  1. Mask marking: Beam projected through a mask onto the workpiece. Minimum line width: 0.1 mm (0.004 inch). CO₂ lasers produce legible marks at speeds up to 20,000 marks/hour.

  2. Scanned-beam marking: Pulsed laser beam directed by controlled mirror oscillation — virtually unlimited pattern choice. Can produce continuous lines or dot-matrix patterns.



Flame Spraying and Surface Treatments


Flame Spraying Process

Metals, alloys, ceramics, and cermets are deposited on surfaces to build up worn parts, provide wear/corrosion resistance, or correct defective castings.

Equipment types:

  • Wire-fed spray gun: Wire fed through nozzle; combustible gas + oxygen + compressed air melt and blow atomized metal
  • Powder-fed equipment: Powders (including ceramics and cermets) fed through a flame
  • Plasma flame: Temperatures from 12,000 to 30,000+°F — materials include alumina, zirconia, tungsten, molybdenum, tantalum, copper, aluminum, carbides, and nickel-base alloys

Surface preparation is critical:

  1. Degrease / solvent clean
  2. Undercut surface to allow coating thickness
  3. Abrasive / grit blast for roughened surface
  4. Groove (flat surfaces) or rough thread (cylindrical work)
  5. Preheat base metal

Hard Facing

Adding a coating of wear/corrosion/heat/impact-resistant material to components (new or worn). Applied by oxyacetylene gas, shielded-metal arc, submerged arc, plasma arc, or inert-gas-shielded arc welding — or by spraying.

Hard-facing material categories:

  • High-speed steels
  • Austenitic manganese steels
  • Austenitic high-chromium irons
  • Cobalt-base alloys
  • Copper-base alloys
  • Nickel-chromium-boron alloys
  • Chromium plating

Surface Treatment Methods

Treatment Application
Etching Chemical surface preparation with acid-based fluids
Conversion coatings Chemical surface modification (passivation, coloring)
Anodizing Aluminum alloys — creates hard, corrosion-resistant oxide layer
Plating Electrodeposited or hot-dipped metal coatings
Chromium plating Hard wear-resistant surface for tools and components


Powder Metallurgy and Injection Molding of Metal


Metal Injection Molding (MIM)

Combines die casting and injection molding by mixing powdered metal (5–10 µm particle size) with thermoplastic binders chosen for maximum flow. After molding:

  1. Binder removal — may take several days to avoid distortion
  2. Sintering in controlled atmosphere furnace at high temperatures
  3. Density reaches approximately 95% of wrought material
  4. Optional coining for greater accuracy

Limitations:

  • Parts restricted to approximately a 1.5-inch cube
  • Shrinkage of 10–35% after binder removal and consolidation
  • Tolerances similar to die casting


Cutting Metals — Oxy-Fuel and Plasma


The Cutting Torch

Oxy-fuel cutting uses a torch that burns a mixture of (usually) acetylene and oxygen. Metals that can be cut include carbon steel, low-alloy steels, and cast iron.

Stainless steel cutting requires special techniques — the chromium oxide that forms during cutting has a higher melting point than the base metal and acts as a barrier.


Plasma Arc Cutting

Uses a constricted arc to ionize gas into plasma — creating temperatures high enough to melt and blow away virtually any conductive material.

Precision plasma arc cutting uses a magnetic field to stabilize the arc, producing narrower kerfs without adverse effects on cutting speed. Results are comparable to laser cutting for small-batch production of blanks.

Underwater plasma cutting reduces noise and fumes; oxidation of cut surfaces is almost nonexistent.



Improvement method and result

Two years after that first disastrous shift, the practitioner stood in the same stamping room — but now he was the engineer everyone called when processes went wrong.

What changed wasn't his job title. It was his understanding of mechanics.

He could look at a ragged edge and immediately diagnose whether the clearance was too tight, too loose, or applied in the wrong direction. He could watch an EDM operation and predict surface finish from the duty cycle. He could recommend the right casting process for a component based on its geometry, material, and production volume.

The deepest lesson wasn't any single formula or specification. It was this:

Every manufacturing process is a conversation between energy and material. The engineer's job is to understand both sides of that conversation — and to control the variables that determine whether the result is a precision component or a pile of scrap.



Your Next Step

You now have a reference that covers the mechanics behind every major manufacturing process — from press work to laser treatment. But knowing isn't the same as applying.

Here's your challenge:

Pick the one process from this guide that you work with most frequently. Go back to that section and identify one variable you've been estimating rather than calculating. Run the numbers. Check your current practice against the specifications in this guide.

That single calculation might be the difference between your next 14,000 parts being perfect — or scrap.


What's the most critical manufacturing variable in your shop that doesn't get enough attention? Share your experience — because every engineer who reads this has something to teach the next one.


Context and scope

You're losing parts, wasting material, and burning through tooling — not because your team lacks skill, but because the processes you've inherited were never designed for the work you're doing today.

Somewhere right now, a shop floor supervisor is watching a flame-cut edge on stainless steel that looks like it was chewed by an animal. Down the hall, an engineer is specifying a hard-facing alloy for a valve seat without understanding the thermal limits of the deposit. In another facility, a technician is running a polishing wheel at the wrong speed, wondering why the surface finish looks worse after each pass.

These aren't rare mistakes. They're the daily reality of manufacturing operations that haven't been updated with the full depth of process knowledge available. And every one of them costs you — in scrap, rework, downtime, and lost customer confidence.

This guide is your correction. It covers the full spectrum of advanced manufacturing processes: laser operations, hard facing, flame and arc cutting, finishing with files and burs, power brush finishing, polishing and buffing, and surface treatments — with the technical depth you need to make better decisions starting today.



THE PROBLEM: "We've Always Done It This Way" Is Destroying Your Margins


You're Using the Wrong Process for the Job

Here is the uncomfortable truth: most shops select manufacturing processes based on what equipment they own, not what the job actually requires. A shop with a plasma cutter uses plasma for everything. A shop with an oxyacetylene setup burns through stainless steel at a crawl, producing slag-covered edges that require hours of secondary finishing — when a laser or flux-injection method would have cut the time by 80%.

The same pattern repeats across every category of manufacturing work:

  • Cutting — Using flame cutting on cast iron when arc cutting handles the material's reluctance to oxidize far more effectively
  • Surface hardening — Applying induction heating across an entire part when a laser could harden only the wear zone, eliminating distortion entirely
  • Hard facing — Choosing a cobalt-base alloy for a low-temperature application where a cheaper nickel-chromium-boron deposit would outperform it
  • Finishing — Running a power brush at incorrect speeds, causing the brush to peen burrs into adjacent surfaces rather than removing them
  • Surface treatment — Anodizing an aluminum alloy with more than 5% copper using the chromic process, corroding the base metal in the process

Each of these mistakes has a compounding cost. You don't just lose the part. You lose the time to remake it, the material to replace it, the inspection effort to catch it, and the credibility with your customer who wonders why delivery slipped.


The Knowledge Gap Is Wider Than You Think

Here's what makes this problem truly dangerous: the information to solve it exists, but it's buried.

The technical data on laser beam divergence, hard-facing alloy hardness ranges, cutting torch gas pressures, file coarseness specifications, and anodizing process parameters lives in engineering handbooks, supplier catalogs, and the heads of retiring machinists. It's not organized for decision-making. It's not structured for comparison. And it's certainly not written in a way that a new engineer, a shop manager, or a process planner can act on quickly.

That gap between knowing a process exists and knowing how to select, specify, and optimize it is where most manufacturing profit disappears.



THE AGITATION: What It Actually Costs When You Get This Wrong


Scenario 1: The Laser That Nobody Understood

Meet the source manufacturing plant — a mid-size contract shop that invested heavily in a 2-kW CO₂ laser system. The sales pitch was compelling: cut metal, weld, drill, mark, and heat treat — all from one machine. The purchase price was substantial. The ROI projections looked great.

Six months in, the laser sat idle 40% of the time.

The problem wasn't the machine. It was the process knowledge. Reyes's operators were trying to cut 6.25 mm mild steel with the same beam parameters they used for 1.5 mm cold-rolled stock. They didn't understand that process depth is proportional to power and inversely proportional to speed. They didn't know that the maximum economically efficient cutting range for their power level topped out at about 12.5 mm. And they certainly didn't know that their oxygen assist gas pressure, nozzle-to-surface spacing, and focus position were creating kerf widths twice as large as necessary.

The result? Surface roughness values of 50 µm on parts that needed 15 µm. Heat-affected zones three times deeper than specification allowed. And cut edges that required secondary grinding — destroying the entire economic justification for the laser in the first place.

Here's the data they never saw:

Material Thickness (mm) Surface Finish — CW (µm) Surface Finish — Pulsed (µm)
Cold-Rolled Steel 1 8
Cold-Rolled Steel 2 10
Cold-Rolled Steel 3 15
Mild Steel 1 30
Mild Steel 2 30
Mild Steel 3 35
Stainless Steel 1 30
Stainless Steel 2 35
Stainless Steel 3 50

And here's the heat-affected zone data that would have changed their process parameters:

Material Thickness (mm) CW HAZ (mm) Pulsed HAZ (mm)
4 0.50 0.15
3 0.37 0.15
2 0.10 0.12
1 0.75 0.07

Switching to pulsed mode alone would have reduced their heat-affected zones by 60–90% on thicker sections. But nobody told them. And the handbook collecting dust on the shelf? It had the answer on page 1417.


Scenario 2: The Hard-Facing Disaster

Diallo Industrial supplied hard-faced valve trim for steam engines operating at 1,100°F. Their metallurgist specified austenitic high-chromium iron (EFeCr-A) — a material with outstanding low-stress scratch-abrasion resistance and as-welded hardness of 51 to 62 Rockwell C.

On paper, it looked perfect. In the field, the deposits cracked within 90 days.

Why? Because high-chromium iron deposits will withstand only light impact without cracking. Dynamic compression stresses above 60,000 psi must be avoided. The valve trim in question experienced repetitive impact loading from the steam flow. The material was brilliant at resisting scratching — and utterly wrong for the application.

What should they have used? Cobalt-base alloys (CoCr-A) — which are specifically designed for valve contact surfaces in engines. Their hardness ranges from 38 to 47 Rockwell C (gas-welded), they exhibit outstanding elevated-temperature strength, their deposits return to approximate original hardness after cooling, and — critically — they have far superior impact resistance at operating temperatures above 1,000°F.

The cost of the wrong specification: 47 field failures, a complete product recall, and six months of lost customer trust.

Here's the comparison table that could have prevented it:

Hard-Facing Alloy Hardness (Rc) Max Service Temp Impact Resistance Best Application
High-Speed Steels (RFe5/EFe5) 55–60 1,100°F Medium (as-deposited) Cutting tools, shear blades, dies
Austenitic Manganese (EFeMn) 170–230 Bhn (work-hardens to 450–550 Bhn) Below 500°F High Rock crushers, railway frogs
Austenitic High-Chromium Iron (EFeCr-A) 51–62 1,800°F (oxidation) Light only Agricultural equipment, sand-blasting
Cobalt-Base (CoCr-A/B/C) 38–58 1,200°F+ Good to excellent Exhaust valves, pump shafts
Copper-Base (CuAl/CuSn/CuZn) 130–390 Bhn Moderate Varies Bearings, gears, wear plates
Nickel-Chromium-Boron (NiCr-A/B/C) 35–62 1,750°F Light Seal rings, valves, cams

Scenario 3: The Finishing Bottleneck Nobody Measured

Park Precision made beautiful gear blanks. Their CNC work was tight, their heat treatment was consistent, and their inspection pass rates were excellent — right up until the finishing department.

The shop's deburring operation used radial wire brushes on gear tooth profiles. But the brushes were set up with line contact instead of full face contact. The result: non-uniform wear on the brush face, wire points flaring to the side, and burrs that were peened into adjacent surfaces rather than removed.

The fix wasn't a new machine. It wasn't a new brush. It was a setup change: positioning the brushes on the center line of the gear tooth profile, using short trim dense wire fill, and implementing brush reversal to maintain cutting efficiency at the wire points.

Total cost of the fix: zero in capital equipment. The savings: 23% reduction in finishing cycle time and a near-complete elimination of downstream rework on burred tooth edges.



THE SOLUTION: A Complete Technical Framework for Intelligent Process Selection

What follows is not theory. It's the working knowledge — organized for decision-making — across every major category in your notes. Use it as a reference, a training tool, or the foundation of your shop's process standards.



Laser Operations — Cutting, Welding, Drilling, Heat Treatment, and Marking


How Lasers Actually Work

A laser produces optical-frequency radiation in intense, controllable quantities of energy. When directed against a material surface, this energy causes a localized effect — heating, melting, or vaporizing — with minimal distortion to the surrounding part.

The four basic components:

  • An amplifying medium (solid crystal or gas mixture)
  • A means to excite this medium (flashlamp or electric discharge)
  • Mirrors forming an optical resonator
  • An output transmission device to direct beam energy to the workpiece

The two dominant industrial laser types are:

Nd:YAG (Solid-State) Lasers — Use a crystal of yttrium aluminum garnet doped with neodymium. Emit radiation at 1.06 µm (near infrared). Excited by flashlamp bursts. Beams can be transmitted through flexible optical fibers for multiaxis work.

CO₂ Lasers — Use a gaseous mixture of helium, nitrogen, and carbon dioxide. Emit at 10.6 µm wavelength. Excited by electric discharge. Produce higher power levels (up to 25,000 W continuous) but cannot use fiber optic delivery.


The Science of Beam Quality

Beam quality determines everything downstream. The key metric is — the ratio between the spot diameter of a given laser and that of a theoretically perfect beam. This value is always greater than 1.

  • CO₂ lasers at 1 kW: M² ≈ 1.5
  • YAG lasers at 500 W: M² ≈ 12.0

A lower M² means a tighter focused spot, higher power density, and better performance in cutting, welding, and drilling. The beam mode (TEM₀₀ for Gaussian, TEM₀₁* for donut-shaped) directly affects how energy is distributed across the work surface.

The critical relationship: A CO₂ laser operating at 10.6 µm wavelength will produce a focused spot ten times larger than an Nd:YAG laser at 1.06 µm using the same focal length lens. This is why wavelength matters for precision work.


Cutting Metal with Lasers

The laser beam heats the material surface to the melting or vaporization point. A concentric gas jet expels the molten metal and vapor. Moving the resulting molten-walled hole along a path produces the cut.

The governing relationship:

Process depth ∝ Power / Speed

Doubling power doubles penetration depth. The maximum practical thickness for steel alloys is approximately 25 mm (1 in.), but the most economically efficient range is up to 12.5 mm (0.49 in.).

Beam assistance is essential for ferrous alloys. A jet of oxygen concentric with the laser beam combines with the heated steel in an exothermic reaction — the oxygen literally burns through the material, adding energy to the cut. Control of gas pressure, gas stream shape, and nozzle positioning is critical.

Typical kerf widths in CO₂ laser cutting:

Material Thickness (mm) Kerf Width (mm)
Carbon Steel 1.5 0.05
Carbon Steel 2.25 0.12
Carbon Steel 3.12 0.20
Carbon Steel 6.25 0.30
Aluminum 2.25 0.25
Plastics < 4.0 2 × beam diameter

Cutting Nonmetals with Lasers

CO₂ laser light at 10.6 µm is fully absorbed by most organic and inorganic nonmetals at room temperature. This makes CO₂ lasers extraordinarily effective for nonmetal cutting, where moderate power levels can achieve clean cuts in a wide range of materials.

Material Thickness (mm) Speed (m/min) Power (W)
Polythene 1 11 500
Polypropylene 1 17 500
Polystyrene 1 19 500
Nylon 1 20 500
ABS 1 21 500
Polycarbonate 1 21 500
PVC 1 28 500
Fiberglass 1.6 5.2 450
Glass 1 1.5 500
Alumina 1 1.4 500
Hardwood 10 2.6 500
Plywood 12 4.8 1,000
Cardboard 4.6 9.0 350

Important consideration: Thermosetting plastics are sensitive to reheating and may produce a gummy or charred residue. Many plastics compositions, when vaporized, produce potentially harmful fumes — workstation exhaust systems are essential.


Welding with Lasers

Laser welding converts absorbed energy into heat, causing a phase change from solid to liquid and back. Two distinct modes exist:

Conduction Welding — Relies on thermal diffusivity to conduct heat into the joint. Used for spot welding and partial penetration seam welding. Heat is concentrated into the focused beam diameter for short time periods.

Deep Penetration (Keyhole) Welding — Beam energy creates a hole through the full material thickness. Vapor pressure of evaporated metal holds a layer of molten metal against the hole wall. As the beam moves, molten metal flows around the hole and solidifies behind the interaction point. Maximum practical penetration: approximately 25 mm.

The greatest advantage of laser welding: low total heat input. The beam moves faster than the speed of thermal conduction, so heat flows only perpendicular to the direction of motion. The result is minimum thermal distortion — only enough heat to fuse the joint is applied.

Joint tolerances are critical:

  • Corner, tee, and lap joints: gaps ≤ 25% of the thinnest section thickness
  • Butt and edge joints: gaps ≤ 10% of the thinnest section thickness

Processing gas matters. Helium is ideal. CO₂ and argon can be used but don't produce a perfectly clean weld. At energy intensities of 10⁶ W/cm² or higher, easily ionized gases will form plasma that blocks beam transmission — so gas selection is a performance-critical decision.


Drilling with Lasers

Three methods, in order of increasing hole quality:

Direct Drilling — Single-pulse, single-hole. Fastest method but lowest quality. Maximum depth: 1.5 mm in metals, 8 mm in nonmetals. Hole taper can be as much as 25%. Recast layer depth: approximately 0.1 mm.

Percussive Drilling — Rapid sequence of pulses. Higher quality than direct drilling in metals up to 25 mm thick. Aspect ratio up to 50:1. Taper under 10%. Recast layer: 0.5 mm. Hole diameter tolerance: ±5%.

Trepanning — The focused beam moves around the hole circumference via a rotating mirror assembly. Best quality. Maximum hole depth: 10 mm. Maximum diameter: 2.5 mm. Recast layer: only 25 µm.


Heat Treatment with Lasers

The defocused beam from a CO₂ laser at power densities below 10⁴ W/cm² is used for surface hardening. At this power level, over 90% of beam energy is reflected by metals at room temperature — so surface preparation is required. Options include surface roughening or coating (black enamel paint is a common expedient that vaporizes during processing, leaving a clean surface).

Materials applicability for laser heat treatment:

  • Good candidates: Medium- and high-carbon steels, tool steels, low-alloy steels, cast irons, steels with fine-carbide dispersion
  • Marginally hardenable: Annealed carbon steels, spheroidized carbon steels, mild-carbon steels (0.2% C), ferritic nodular cast irons
  • Not hardenable: Low-carbon steels (< 0.1% C), austenitic stainless steels, nonferrous alloys

Typical hardening rate: 130 cm²/min for a 1 mm case depth in 4140 steel. While laser hardening is typically slower than induction heating, it eliminates residual heat effects that cause part distortion — making it cost-effective when the hardened area is limited.


Laser Marking

Two principal methods:

Mask Marking — The beam projects through a mask and is reimaged onto the workpiece surface. CO₂ lasers can produce legible marks at line speeds of 20,000 marks/h with energy densities of 1–20 J/cm². Minimum individual line width: 0.1 mm.

Scanned-Beam Marking — A pulsed laser beam is directed onto the surface by controlled mirror oscillation in a preprogrammed pattern. Provides virtually unlimited choice of patterns. Not all applications remove base metal — some produce discoloration that serves as the mark. For highly reflective metals like aluminum, pretreating the surface (anodizing) produces better results.


Laser Safety — Non-Negotiable

Safety is governed by ANSI Z136.1: Safe Use of Lasers. The critical points:

  • Eye hazard is the most serious risk. Direct viewing of the beam must be restricted. Safety eyewear matched to the specific laser wavelength is required.
  • 1.06 µm solid-state lasers require workers to be shielded from direct and indirect radiation.
  • 10.6 µm CO₂ lasers operated without shielding must meet maximum permissible exposure standards.
  • Fumes from vaporized plastics are potentially harmful — exhaust systems are mandatory.
  • Electrical hazards from high-voltage, high-amperage power supplies require proper shielding.


Hard Facing — Rebuilding Parts to Outperform the Original

Hard facing adds a coating, edge, or point of wear-resistant material to a metal component. It applies equally to new parts and worn parts — making it one of the most economically powerful processes in manufacturing when properly specified.


Application Methods

  • Oxyacetylene gas welding
  • Shielded-metal arc welding
  • Submerged arc welding
  • Plasma arc welding
  • Inert-gas-shielded arc welding (consumable and non-consumable electrode)
  • Spraying (wire or powder form)

The Selection Framework

The first consideration is the type of service the part will undergo. Then: machinability, cost, porosity, appearance, and ease of application. A general principle applies: the greater the hardness, the greater the resistance to abrasion — but this often comes at the expense of impact resistance.


Alloy-by-Alloy Guide


High-Speed Steels (RFe5 / EFe5)

  • Hardness: 55–60 Rc as-welded; 30 Rc annealed
  • Service temperature: Up to 1,100°F (maintains 47 Rc at this temperature)
  • Impact resistance: Medium as-deposited; improved when tempered
  • Special properties: Retains hardness at elevated temperatures. Takes a high polish. Well suited for metal-to-metal wear. Oxidizes readily due to high molybdenum content.
  • Typical applications: Cutting tools, shear blades, reamers, forming dies, shearing dies, guides, ingot tongs, broaches
  • Machining note: Must be annealed first. Full hardness can be regained by subsequent heat treatment.

Austenitic Manganese Steels (EFeMn)

  • Hardness: 170–230 Bhn as-deposited; work-hardens to 450–550 Bhn
  • Service temperature: Becomes brittle above 500–600°F — essentially no hot hardness
  • Impact resistance: High — the standout property of this alloy
  • Special properties: Low yield strength in compression, but compressive deformation rapidly raises it until plastic flow ceases. This is an asset in impact wear situations.
  • Typical applications: Rock-crushing equipment, railway frogs and crossings
  • Machining note: Difficult with ordinary tools. Finished surfaces are usually ground.

Austenitic High-Chromium Irons (RFeCr-A / EFeCr-A)

  • Hardness: 51–62 Rc as-welded
  • Service temperature: Good oxidation resistance up to 1,800°F
  • Impact resistance: Light only — deposits work-harden under impact but also crack. Dynamic compression stresses above 60,000 psi must be avoided.
  • Special properties: Outstanding low-stress scratch-abrasion resistance. Mediocre under high-stress grinding abrasion. Considered commercially unmachinable — finished by grinding only.
  • Typical applications: Agricultural machinery, coke chutes, steel mill guides, sand-blasting equipment, brick-making machinery

Cobalt-Base Alloys (RCoCr / ECoCr)

  • Hardness: CoCr-A: 38–47 Rc; CoCr-B: 45–49 Rc; CoCr-C: 48–58 Rc (gas-welded)
  • Service temperature: Use at 1,200°F and above is advantageous. Between 1,000–1,200°F, advantages are not definitely established. Below 1,000°F, other alloys may be better.
  • Impact resistance: Excellent creep resistance at 1,000–1,200°F. Return to approximate original hardness after cooling — they are not permanently softened by high temperatures.
  • Special properties: High polish capability. Low coefficient of friction. Excellent metal-to-metal wear resistance. Chromium promotes formation of a thin, adherent scale resistant to combustion products.
  • Typical applications: Exhaust valve contact surfaces (aircraft, truck, bus engines), steam engine valve trim, pump shafts
  • Machining note: Difficulty increases with carbon content. CoCr-A: use sintered carbide tools. CoCr-C: finish by grinding.

Copper-Base Alloys

A large family of alloys for bearing, corrosion-resistant, and wear-resistant surfaces:

Designation Hardness Range (Bhn) Primary Application
CuAl-A2 130–190 Bearing surfaces, corrosion-resistant surfaces
CuAl-B / CuAl-C 140–290 Bearing surfaces
CuAl-D / CuAl-E 230–390 Gears, cams, wear plates, dies
CuSn (copper-tin) Lower ranges Corrosion-resistant surfaces

All copper-base alloy deposits can be machined. Slight porosity is generally acceptable in bearing service, as porous deposits retain oil for lubrication.


Nickel-Chromium-Boron Alloys (RNiCr / ENiCr)

Three formulations — NiCr-A, NiCr-B, and NiCr-C — with escalating hardness:

Formulation Rod Hardness (Rc) Electrode Hardness (Rc)
NiCr-A 35–40 24–35
NiCr-B 45–50 30–45
NiCr-C 56–62 35–56

Lower electrode hardness values result from dilution of deposit and base metals.

  • Service temperature: Oxidation-resistant up to 1,800°F. Do not use above 1,750°F — fusion may begin.
  • Corrosion resistance: Completely resistant to atmospheric, steam, salt water, and salt spray corrosion, and to milder acids.
  • Special properties: NiCr-C has the best metal-to-metal wear resistance and is particularly resistant to galling. Can be machined with tungsten carbide tools (slow speeds, light feeds, heavy tool shanks) or ground with soft-to-medium vitrified silicon carbide wheels.
  • Typical applications: Seal rings, cement pump screws, valves, screw conveyors, cams

Chromium Plating as a Hard-Facing Method

Chromium plating is an electrolytic process that deposits chromium on metals for corrosion protection or surface wear improvement. Its most proven application is on plug and ring gages — chromium-plated gages wear longer, and when worn, can be stripped, replated, and reground to size.

Chromium's friction advantage is remarkable:

Surface Combination Static Coefficient Sliding Coefficient
Steel on Steel 0.30 0.20
Steel on Chromium-Plated Steel 0.17 0.16
Steel on Babbitt 0.25 0.20
Chromium-Plated Steel on Babbitt 0.15 0.13

Plating thickness ranges from 0.0001 to 0.002 inch, with thicker deposits used for rebuilding undersized tools. Chromium resists attack by almost all organic and inorganic compounds except muriatic and sulfuric acids. Its melting point is 2,930°F, and it remains bright up to 1,200°F.

Standard chromium plating procedure:

  1. Degrease with solvent
  2. Mount tools on racks
  3. Clean in anodic alkali bath at 82°C for 3–5 minutes
  4. Rinse in boiling water
  5. Immerse in 20% hydrochloric acid for 2–3 seconds
  6. Rinse in cold water
  7. Rinse in hot water
  8. Etch in reverse-current chromic acid bath for 2–5 minutes
  9. Place immediately in chromium plating bath
  10. Remove hydrogen embrittlement (if necessary) by immersing for 2 hours in oil bath at 177°C

Engineering use and verification

Choose and control a process from the required function, material, geometry, tolerance, surface condition, volume, safety and inspection plan. Confirm the process window with representative trials, identify the variables that move quality, and connect each critical characteristic to an observable control and reaction plan. Do not convert a successful source example into a universal limit; validate capability using the actual machine, tooling, material batch and operating conditions.

  • Confirm scope, assumptions, interfaces and required outcome.
  • Use one controlled unit system and show every conversion.
  • Identify current project, customer and regulatory requirements.
  • Separate source examples from mandatory acceptance criteria.
  • Check calculations, tables and selections by an independent method.
  • Verify safety, maintainability and credible failure modes.
  • Record evidence, revisions, approvals and unresolved limitations.
  • Validate the result under representative operating conditions.

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