The surface is where parts live or die. Every finishing process here stays in-house.
Vacuum hardening, carburizing, nitriding, induction hardening, hard chrome, electroless nickel, shot peening, laser cladding — every one in-house. No subcontractor queues, no coating roulette, no drawings leaving the plant. Surface engineering is not an add-on here — it is where this company began.

A machined part is a promise; the surface is where it is kept:
Hardness and case depth decide whether a shaft survives its first thousand hours or its first hundred
A plating pinhole in a marine or downhole environment is a countdown timer
Shot peening and surface integrity decide cyclic life; a beautiful ground finish with the wrong residual stress fails early
A seal face’s flatness and texture decide whether thousand-bar pressure stays contained
Send a process out, and someone else’s process can change your part’s dimensions — or worse, its structural integrity. The part leaves the machinist’s control, sits in someone else’s queue, comes back with a coating nobody specified the adhesion test for — and when it fails, the machinist blames the coater, the coater blames the substrate, and your program pays for the argument. We eliminated the argument by eliminating the hand-off.

| Process | Purpose |
|---|---|
| Vacuum hardening (≤1,250°C) | Distortion-controlled hardening for precision parts |
| Carburizing | Deep case hardening — wear surface + tough core |
| Nitriding | Low-distortion case hardening; fatigue & wear |
| Plasma nitriding | Ion-assisted case hardening — uniform, deep case with a controllable compound layer; suited to stainless and non-magnetic grades |
| Induction hardening | Localized hardening: journals, wear bands |
| Stress-relief annealing | Dimensional stability before/after machining |
| Carbonitriding | Case hardening for thin cases — wear + fatigue |
| QPQ salt-bath oxynitrocarburizing | Oxynitrocarburizing in a salt bath (QPQ) — combined wear and corrosion resistance; low distortion |
| Process | Purpose |
|---|---|
| Hard chrome plating | Wear + corrosion for shafts, plungers, seal areas |
| Electroless nickel | Uniform corrosion-resistant coating, complex geometries |
| Copper plating (incl. thread plating) | Conductive / underlayer; anti-galling copper on threads and sealing faces |
| PTFE (Teflon) powder coating | Low-friction, anti-galling surfaces |
| Anodizing | Hard and decorative anodic oxide on aluminium alloys — wear and corrosion protection |
| HVOF thermal spray (tungsten carbide) | High-velocity oxy-fuel sprayed WC coatings — dense, low-porosity wear surfaces on shafts and seal areas |
| Process | Purpose |
|---|---|
| Shot peening | Compressive residual stress — fatigue life extension — to SAE AMS 2430; 200% coverage; compressive layer depth > 600 μm; multiple peening programs (high/low intensity, glass bead) by part requirement |
| Laser cladding | Wear-surface rebuilding on shafts — nickel-based wear bands with 60% tungsten carbide content; cladding layer smooth, free of visible cracks and porosity; substrate hardness ≥ 40 HRC, embedded particles > 2,000 HV, wear-band working hardness > 50 HRC |
| Narrow-gap butt welding | Non-magnetic steels & superalloys — groove angle within 2°, weld depth up to 60 mm |
| PTA plasma overlay welding | Hardfacing (HF 3000) and Stellite alloy overlays |
| Flame spray welding | Hardfacing (HF 3000) |
| Bore TIG welding | Internal bore repair — from Ø40 mm ID, up to 2,000 mm deep |
| TIG & laser welding of difficult alloys | P550, 15-15HS MAX, Inconel 718, 17-4 PH — downhole-grade joints |
| Post-weld test suite | Tensile, Charpy impact, side bend, sensitization, macro analysis, hardness, NDT (visual / penetrant / ultrasonic), magnetic hot-spot testing for non-magnetic grades |
| Vacuum potting (encapsulation) | In-house-developed vacuum potting system; assemblies qualified at 150 °C / 140 MPa with 30-min hold — protection for downhole electronics |



Proven on real parts, not test coupons: among our showroom reference parts, one HF 3000 hardfaced component runs a 16-process, 30-day route where the overlay is applied while safeguarding the base metal’s mechanical properties; one antenna component combines 8 groups of 16 sealed angle holes, in-house vacuum potting, and laser-clad tungsten-carbide wear bands over 5 mm thick — all on one part.
Most machine shops bolt on finishing as an afterthought. Zhongnan grew out of it.
Our founder spent 1983–1991 at the Wuhan Research Institute of Materials Protection — China’s national institute for surface engineering — where he led the plasma surfacing research that won a national first prize, then spent four years taking surface technology to over 600 factories across the country. In 1993, the first company he founded was a surface-strengthening plant.
So the in-house finishing department is not a convenience we added. It is the discipline this company was founded on — four decades of surface science, from the national institute to your part.

Coating thickness is planned when the machining program is written, not discovered when the part comes back. Dimensions on your print are final-after-coating, because the machinist and the coater read the same drawing in the same plant
Substrate to surface, one engineering team owns the result. No three-way arguments between machinist, heat treater, and plater
No transport queues between vendors; a part can move from final grind to plating to inspection in the same shift
Finishing is the most outsourced link in this industry, and every hand-off is an IP exposure. Our chain has none
Yes — that is the point of in-house finishing. Coating allowance is engineered into the machining program; your print dimensions are met after coating, verified by our metrology before shipment.
It depends on the part and the service condition — different duty calls for different thicknesses. Send the drawing with its coating callout, and we will confirm the thickness range we hold for that process.
Yes — adhesion and porosity are checked by cross-cut, bend, and thermal-shock tests.
Programs we have executed include work to AMS 2750 (heat-treatment pyrometry), SAE AMS 2430 (shot peening), ASTM F1586 (surgical-grade stainless steel), and NACE MR0175 (sour-service materials). Tell us the specification your drawing calls out, and we will confirm our execution route.
Yes — send the part drawing with the coating callout and its current condition, and we will confirm the process route and quote.
Upload your drawing with the coating callout — or just tell us the working environment, and our surface engineers will propose the finishing stack. Within 24 hours, an engineer responds.
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