Nickel-Based Alloy CNC Machining
Nickel Alloy
Prelucrare CNC
Inconel 625
Inconel 718
Hastelloy C-276
Monel 400
Aerospace · Chemical · Marine
Precision CNC machining of nickel-based superalloys for aerospace, chemical processing, oil & gas, and marine applications demanding extreme temperature resistance, corrosion resistance, and high-strength performance where stainless steel is insufficient.
Temperatura maximă de serviciu
982 °C
Inconel 625 ✦
Inconel 718 Aerospace ✦
Hastelloy C-276 Chemical ✦
Monel 400 Marine ✦
High-Pressure Coolant Machining ✦
Ceramic & PCBN Tooling ✦
Turbine Components ✦
Subsea & Offshore Parts ✦
Valve Seats · Nozzles · Flanges ✦
Inconel 625 ✦
Inconel 718 Aerospace ✦
Hastelloy C-276 Chemical ✦
Monel 400 Marine ✦
High-Pressure Coolant Machining ✦
Ceramic & PCBN Tooling ✦
Turbine Components ✦
Subsea & Offshore Parts ✦
Valve Seats · Nozzles · Flanges ✦
Grade de materiale
Four Nickel Alloys, Four Different Demands
IN625
UNS N06625 · ASTM B446 / B564 · AMS 5666
Solution-Strengthened Nickel-Chromium-Molybdenum Alloy
The industry-standard nickel alloy for seawater, chemical, and cryogenic service. Niobium additions provide solid-solution strengthening and outstanding corrosion resistance across a wide temperature range — from cryogenic (-196 °C) to 982 °C. Excellent weldability and resistance to stress corrosion cracking in chloride environments. The most widely specified nickel alloy for subsea, marine, and chemical processing components.
930 MPa
Rezistență la tracțiune
414 MPa
Yield Strength
−196–982°C
Service Range
HRB 98
Duritate
Subsea ConnectorsChemical ValvesCryogenic PartsMarine FlangesHeat Exchanger Tubes
View Inconel 625 Details
Compoziție chimică
| Nickel (Ni) | 58% min (bal.) |
| Crom (Cr) | 20.0–23.0% |
| Molybdenum (Mo) | 8.0–10.0% |
| Niobium + Ta | 3.15–4.15% |
| Iron (Fe) max | 5.0% |
| Carbon (C) max | 0.10% |
Proprietăți cheie
Exceptional resistance to seawater, chloride pitting, and crevice corrosion
Excellent weldability — retains corrosion resistance in the weld HAZ
Cryogenic toughness — suitable down to −196 °C
Not precipitation-hardenable — strength fixed by composition
More machinable than IN718 — carbide tooling standard
IN718
UNS N07718 · AMS 5662 / 5664 · ASTM B637
Precipitation-Hardened Nickel-Chromium-Molybdenum-Niobium Alloy
The most widely used aerospace superalloy — accounting for over 50% of all jet engine superalloy usage. Age-hardened by gamma-prime and gamma-double-prime precipitates, Inconel 718 achieves tensile strength up to 1380 MPa with outstanding fatigue resistance. Maintains mechanical integrity at temperatures up to 650 °C (700 °C for short durations). The most challenging of the four alloys to machine — work-hardening rate is high and ceramic tooling is required for roughing.
1380 MPa
Rezistență la tracțiune
1172 MPa
Yield Strength
to 700°C
Temperatura de serviciu
HRC 36–46
Hardness (aged)
Turbine DiscsJet Engine PartsAerospace FastenersRocket ComponentsDownhole Tools
View Inconel 718 Details
Compoziție chimică
| Nickel + Cobalt | 50.0–55.0% |
| Crom (Cr) | 17.0–21.0% |
| Niobium + Ta | 4.75–5.50% |
| Molybdenum (Mo) | 2.8–3.3% |
| Titanium (Ti) | 0.65–1.15% |
| Aluminiu (Al) | 0.20–0.80% |
Proprietăți cheie
Highest strength of the four alloys — precipitation-hardened
Outstanding fatigue and creep resistance at elevated temperature
Usually machined in annealed or solution-treated condition, then aged
Ceramic inserts + PCBN for finishing — most difficult nickel alloy to machine
Work-hardening is the primary machining challenge — no dwell at any stage
C-276
UNS N10276 · ASTM B574 / B575 · AMS 5750
Nickel-Molybdenum-Chromium Alloy — Maximum Chemical Resistance
Hastelloy C-276 is engineered for one purpose: superior corrosion resistance in the most aggressive chemical environments on earth. Its high molybdenum content (15–17%) provides exceptional resistance to pitting, crevice corrosion, and stress corrosion cracking in oxidizing and reducing acids simultaneously — a capability no stainless steel or standard Inconel grade can match. The material of choice for chemical reactor internals, scrubbers, and FGD systems where mixed acid and chloride exposure is unavoidable.
790 MPa
Rezistență la tracțiune
355 MPa
Yield Strength
to 1040°C
Temperatura de serviciu
HRB 100
Duritate
Reactor InternalsScrubber ComponentsAcid Pump PartsFGD SystemsChemical Fittings
View Hastelloy C-276 Details
Compoziție chimică
| Nickel (Ni) | Balance (≥57%) |
| Molybdenum (Mo) | 15.0–17.0% |
| Crom (Cr) | 14.5–16.5% |
| Iron (Fe) | 4.0–7.0% |
| Tungsten (W) | 3.0–4.5% |
| Carbon (C) max | 0.01% |
Proprietăți cheie
Resists both oxidizing AND reducing acids — unique dual capability
Ultra-low carbon (0.01% max) — no carbide sensitization after welding
Outstanding chloride pitting and crevice corrosion resistance
Resists hydrochloric, sulfuric, nitric, hydrofluoric, and mixed acids
Harder to machine than IN625 — tungsten/Mo phases accelerate tool wear
M400
UNS N04400 · ASTM B164 / B165 · AMS 4574
Nickel-Copper Alloy — Seawater, Brine & HF Acid Resistance
The simplest and oldest commercial nickel alloy — approximately 67% Ni and 31% Cu. Monel 400 offers excellent corrosion resistance in seawater, brine, hydrofluoric acid, and alkaline environments at a lower cost and with significantly better machinability than Inconel or Hastelloy grades. It is not heat-treatable to high strength levels but is stronger than copper and significantly more corrosion resistant than stainless steel in marine environments. The standard material for marine pump shafts, impellers, propeller shafts, and HF acid handling equipment.
550 MPa
Rezistență la tracțiune
240 MPa
Yield Strength
to 480°C
Temperatura de serviciu
HRB 65–85
Duritate
Marine Pump ShaftsPropeller ShaftsHF Acid ValvesHeat Exchanger TubesBrine Fittings
View Monel 400 Details
Compoziție chimică
| Nickel + Cobalt | ≥63% (min) |
| Copper (Cu) | 28.0–34.0% |
| Iron (Fe) | 2.5% max |
| Mangan (Mn) | 2.0% max |
| Silicon (Si) max | 0.50% |
| Carbon (C) max | 0.30% |
Proprietăți cheie
Excellent seawater and brine corrosion resistance — outperforms 316 SS
Exceptional HF (hydrofluoric) acid resistance — unique capability
Best machinability of the four alloys — closer to stainless than Inconel
Lower cost than Inconel — economical for large or high-volume parts
Not suitable for high-temperature service above 480 °C
Ghid de selecție a calității
Alegerea potrivită Nickel Alloy
🌊
Choose Inconel 625 when…✓Seawater, subsea, or offshore environment
✓Cryogenic service (down to −196 °C)
✓Weldability is important (piping, overlays)
✓Chemical process equipment in chloride environments
✓Moderate temperature service up to 982 °C
✈
Choose Inconel 718 when…✓Aerospace, turbine, or jet engine application
✓Maximum strength (up to 1380 MPa) required
✓High fatigue and creep resistance at temperature
✓Downhole oil & gas tooling and wellhead components
✓Space and rocket propulsion components
⚗
Choose Hastelloy C-276 when…✓Aggressive mixed acid environments (HCl + H₂SO₄)
✓Chemical reactor internals and scrubber systems
✓Both oxidizing AND reducing acid exposure simultaneously
✓Flue gas desulfurization (FGD) components
✓When IN625 corrosion resistance is insufficient
⚓
Choose Monel 400 when…✓Marine pump shafts, impellers, and propeller shafts
✓HF (hydrofluoric) acid handling equipment
✓Seawater and brine service at moderate temperatures
✓Lower cost nickel alloy for larger or high-volume parts
✓Alkaline and caustic service environments
Compararea Materialelor
Comparare completă a proprietăților — All Four Grades
| Proprietate | Inconel 625 | Inconel 718 | Hastelloy C-276 | Monel 400 | 316L SS (ref) |
|---|---|---|---|---|---|
| Base System | Ni-Cr-Mo-Nb | Ni-Cr-Mo-Nb (aged) | Ni-Mo-Cr-W | Ni-Cu | Fe-Cr-Ni-Mo |
| Rezistență la tracțiune | 930 MPa | Up to 1380 MPa | 790 MPa | 550 MPa | ~485–690 MPa |
| Yield Strength | 414 MPa | Up to 1172 MPa | 355 MPa | 240 MPa | ~170–310 MPa |
| Max Service Temp. | 982 °C | 700 °C (mech.) | 1040 °C | 480 °C | ~870 °C (ox.) |
| Seawater / Chloride | Excelent | Bine | Excelent | Excelent | Moderate — pits |
| Mixed Acid Resistance | Bine | Moderată | Best in class | Moderată | Poor in HCl |
| HF Acid Resistance | Bine | Corect | Bine | Excellent — unique | Prost |
| Precipitation Hardenable | No | Yes — to 1380 MPa | No | No | No |
| Machinability (relative) | Moderate — 15–20% of 316SS | Hardest — 10–15% of 316SS | Moderate — 15–20% of 316SS | Best — 25–30% of 316SS | 100% (reference) |
| Aplicație principală | Subsea, cryogenic, chemical | Aerospace, turbine, downhole | Chemical reactors, FGD, acids | Marine, HF acid, brine | General corrosion resistance |
Note de prelucrare
Machining Nickel Alloys — Ce trebuie să știe inginerii
⚠
Challenges with Nickel Alloy Machining!
Extreme work-hardening — especially Inconel 718Nickel alloys work-harden rapidly under cutting forces. Any dwell, rubbing, or re-cutting of already machined surfaces creates a hard surface layer that damages the next cutting edge. Inconel 718 in aged condition has work-hardening rates comparable to austenitic stainless steel at its worst — requiring constant chip engagement.
!
Heat concentration at the cutting edgeLow thermal conductivity means heat generated at the tool tip cannot conduct away into the workpiece — concentrating it in the insert. This causes diffusion wear, notching, and chemical attack of the tool coating at a fraction of the cutting speeds used on steel.
!
Abrasive hard phases in C-276 and IN718Hastelloy C-276 contains tungsten-rich and molybdenum-rich intermetallic phases significantly harder than the surrounding nickel matrix. Inconel 718 contains gamma-prime and gamma-double-prime precipitates. Both cause accelerated abrasive wear — carbide tools require very conservative cutting speeds and monitored tool life limits.
!
Built-up edge and adhesion on tool rake facesNickel is chemically reactive with most tool coatings at high temperature. At elevated cutting temperatures, nickel diffuses into carbide substrates and forms a built-up edge — degrading surface finish and causing unpredictable breakout. This makes flood coolant and high-pressure coolant mandatory, not optional.
!
Springback and dimensional variation on thin wallsHigh elastic modulus combined with work-hardening causes nickel alloy parts to spring back more than stainless after each cutting pass — thin walls and complex features require confirmation passes and adjusted programs relative to stainless steel toolpaths.
✓
Cum abordăm aceste provocări✓
Grade-specific tooling strategy for each alloyIN625 and C-276: PVD AlTiN-coated carbide (positive rake, sharp edge). IN718 roughing: SiAlON ceramic inserts (aggressive material removal at controlled speed). IN718 finishing: PCBN inserts for precise dimensional control. Monel 400: uncoated carbide or TiN-coated carbide to prevent built-up edge in the copper-rich matrix.
✓
High-pressure coolant at 70–100 bar on every nickel alloy operationFlood coolant is insufficient for nickel alloys. High-pressure coolant (70–100 bar) directed precisely at the cutting zone manages temperature, breaks chips, and flushes away nickel chips that would otherwise re-cut and damage the surface. Dramatically extends tool life and improves surface integrity.
✓
Continuous cutting — no dwell or re-cutting at any stagePrograms are written with full chip engagement at all times. Tool retracts clear the machined surface before any pause. Corner radii and lead angles chosen to prevent notching at depth-of-cut line. No in-cut pauses regardless of program interruption requirements.
✓
Monitored tool life — inserts changed at intervals, not on failureTool life in nickel alloy machining is managed by cutting time and number of passes — not by visual wear assessment. Inserts are changed at defined intervals before built-up edge or thermal damage occurs. This prevents the batch-to-batch surface quality variation caused by running worn tools.
✓
Machine state and age before post-machining heat treatmentFor IN718 aerospace parts: we machine in solution-treated (soft) condition to tolerance, then coordinate with the customer's heat treat facility or our approved sub-contractor for precipitation hardening (aging at 720 °C + 620 °C). Post-age dimensional verification confirms that aging distortion is within tolerance.
Capacități de fabricație
Cum Prelucrăm Nickel Alloy Parts
PROCES / 01
CNC Turning — Shafts, Flanges & Nozzles
Precision CNC turning of Inconel 625/718, Hastelloy C-276, and Monel 400 shafts, flanges, nozzles, and rotational components. Grade-specific insert geometry and high-pressure coolant. Tolerances to ±0.01 mm on precision sealing diameters and bearing journals.
PROCES / 02
CNC Milling — Housings, Brackets & Valve Bodies
3-axis and 5-axis milling of complex nickel alloy housings, valve bodies, brackets, and structural components. Climb milling strategy to minimise work-hardening. Rigid setups and short tool stick-out mandatory for dimensional control.
PROCESS / 06
Prototype to Production Supply
Single-piece prototypes through repeat production orders. Nickel alloy parts are expensive — we treat every piece as a prototype. Process is documented from first article and maintained through production runs to ensure quality consistency across all deliveries.
Galerie de aplicații
Typical Nickel Alloy Parts Producem
Inconel 625
Subsea Connectors & Flanges
MaterialIN625 — ASTM B564, NACE MR0175
ProcesCNC Turning · Boring · Threading
IndustrieSubsea · Offshore · Oil & Gas
Inconel 718
Aerospace Turbine & Engine Parts
MaterialIN718 — AMS 5662/5664, aged
Proces5-Axis Milling · PCBN Finish · CMM
IndustrieAerospace · Defence · Space
Industrii deservite
Nickel Alloys for Extreme Environments
Aerospațial
Inconel 718
Oil & Gas
IN625 / IN718
Chimic
Hastelloy C-276
Marine
Monel 400 / IN625
Farmaceutic
C-276 / IN625
Power Gen.
IN625 / IN718
From Raw Billet to Finished Part
Cum producem Nickel Alloy Parts
PASUL 01
Material & Cert Verification
IN625, IN718, C-276, or Monel 400 sourced with full MTR. Heat number, chemical composition, and mechanical properties verified before release. Grade-appropriate stock form selected.
PASUL 02
Prelucrare brută
Grade-specific tooling: ceramic inserts for IN718 roughing, AlTiN carbide for IN625/C-276/Monel. High-pressure coolant (70–100 bar) from first cut. Continuous chip engagement — no dwell.
PASUL 03
Prelucrare finală
PCBN finishing on IN718, fresh carbide on IN625/C-276/Monel. Final dimensions, threads, sealing faces, and critical features completed with tool life monitoring and fresh inserts.
PASUL 04
Secondary Ops & Heat Treatment
Threading, drilling, secondary milling. IN718 aerospace parts: precipitation aging per AMS 2774. Pressure testing for fluid-service parts. Surface treatment if specified.
PASUL 05
Inspecție și Livrare
CMM dimensional verification, surface finish, hardness. MTR, inspection report, pressure test record (where applicable), and heat traceability shipped with every order.
Post-Procesare
Tratament de suprafață pentru Nickel Alloy Parts
Nickel alloy parts are most commonly supplied as-machined — the alloy's inherent corrosion resistance is the primary functional requirement. When additional surface properties are needed, the following treatments are compatible with nickel-based alloys.
Electropolizare
Electrochemical material removal producing ultra-smooth (Ra ≤ 0.2 μm), highly passivated surfaces. Used on IN625 and C-276 chemical and pharmaceutical contact parts to eliminate micro-crevices and maximise corrosion resistance at weld HAZ and machined surfaces.
Pasivare
Nitric acid or citric acid passivation to remove free iron contamination from the machined surface and restore the native oxide protective layer. Specified for IN625, C-276, and Monel 400 parts after machining to maximize corrosion resistance and meet ASTM A967 or ASTM B912 requirements.
Shot Peening (IN718)
Controlled shot peening introduces compressive residual stress into Inconel 718 aerospace and fatigue-critical parts — increasing fatigue life in cyclic loading applications. Specified per AMS 2430 or AMS 2432 for jet engine and aerospace structural components where fatigue life improvement is required.
Bead Blasting & Polishing
Controlled glass bead blasting for uniform matte finish and stress relief on machined surfaces. Mechanical polishing (Ra ≤ 0.4 μm) for sealing faces, bearing surfaces, and flow-critical internal bores where surface finish directly affects sealing performance or fluid flow.
4
Nickel Alloy Grades
1380 MPa
IN718 Tensile Strength
±0.01mm
Toleranță de precizie
24hr
Timp de răspuns pentru ofertă
De ce să lucrați cu noi
De ce să ne alegeți pentru Nickel Alloy Machining
NKL
Four-Grade Nickel Alloy Capability — Not Just One
IN625, IN718, Hastelloy C-276, and Monel 400 all machined in-house with grade-specific tooling strategies. We advise on grade selection before quoting — preventing costly material mistakes on expensive billet.
HPQ
High-Pressure Coolant on Every Nickel Alloy Operation
70–100 bar directed coolant is standard on all nickel alloy jobs — not an upgrade. This is the single most important factor in managing tool life, surface integrity, and dimensional consistency in superalloy machining.
718
Inconel 718 Post-Age Dimensional Verification
We machine IN718 in solution-treated condition, coordinate age hardening, and verify post-age dimensions by CMM — confirming that aging distortion does not push features out of tolerance before shipment.
MTR
Full Material Traceability — MTR, CMM Report, Heat Numbers
Every nickel alloy order ships with complete material test report, heat number traceability, CMM dimensional inspection report, and pressure test records where applicable. No document chasing after delivery.
Întrebări frecvente
Întrebări frecvente Întrebări
Common questions about Inconel 625, Inconel 718, Hastelloy C-276, and Monel 400 — grade selection, machining challenges, tolerances, tooling, and material certification.
Superaliajele pe bază de nichel (inclusiv Inconel 625, Inconel 718, Hastelloy C-276 și Monel 400) sunt aliaje de înaltă performanță bazate pe nichel ca element principal, proiectate pentru rezistență extremă la temperaturi ridicate, rezistență la coroziune și rezistență mecanică la temperaturi înalte. Acestea sunt semnificativ mai dificil de prelucrat decât oțelul inoxidabil sau titanul deoarece: se întăresc rapid sub forțele de tăiere (necesitând angajament continuu al așchiilor), au o conductivitate termică foarte scăzută care concentrează căldura la vârful sculei, și conțin faze dure de carburi și intermetalice care cauzează uzură rapidă a sculei abrazive. Vitezele de tăiere pentru aliajele de nichel sunt de obicei de 10–30 ori mai mici decât cele utilizate pentru oțelul inoxidabil.
Both are nickel-chromium superalloys but with different strengthening mechanisms and applications. Inconel 625 (UNS N06625) is solution-strengthened with niobium and molybdenum — it has outstanding corrosion resistance, excellent weldability, and good strength at high temperatures, but is not age-hardenable. Inconel 718 (UNS N07718) is precipitation-hardened by niobium and aluminum additions — it has significantly higher tensile strength (up to 1380 MPa in aged condition) and fatigue resistance, making it the dominant aerospace and turbine superalloy. Inconel 718 is harder to machine than 625 due to its higher strength and work-hardening tendency.
Hastelloy C-276 (UNS N10276) este un aliaj de nichel-molibden-chromiu proiectat special pentru rezistență maximă la coroziune în medii chimice agresive. Oferă o rezistență superioară la acizi oxidanți (azotic, cromic), acizi reducători (clorhidric, sulfuric) și condiții de acid mixte — depășind atât Inconel 625, cât și oțelul inoxidabil în multe medii de serviciu chimic. Specificați Hastelloy C-276 atunci când cerința principală este rezistența chimică la coroziune (în special în medii acide conținând cloruri sau mixte oxidante/reducătoare), mai degrabă decât rezistența la temperaturi înalte. Pentru aplicații în aviație sau turbine la temperaturi înalte, Inconel 718 este alegerea corectă.
Monel 400 (UNS N04400) este un aliaj de nichel-cupru (aproximativ 67% Ni, 31% Cu) — cel mai simplu și cel mai vechi aliaj comercial de nichel. Spre deosebire de Inconel (nichel-chrom) și Hastelloy (nichel-molibden-chrom), Monel 400 își derivă rezistența la coroziune în principal din sistemul nichel-cupru. Are o rezistență excepțională la apă de mare și soluții saline, acid fluorhidric și medii alcaline. De asemenea, este cel mai ușor de prelucrat dintre cele patru aliaje discutate aici. Monel 400 este specificat pentru hardware marin, axe și impelere de pompe în serviciu cu apă de mare, țevi pentru schimbătoare de căldură și echipamente pentru manipularea substanțelor chimice — în special acolo unde este necesară rezistența la acid fluorhidric.
Standard tolerance for nickel alloy CNC turning and milling is ±0.02 mm. For precision features (bores, shaft diameters, sealing faces), we hold ±0.010–0.015 mm. Note that nickel alloys spring back more than steel after cutting — particularly Inconel 718 — so final tolerances on tight-fit features require careful process control. CMM inspection reports are provided for all precision nickel alloy components. Tighter tolerances (±0.005 mm) are achievable on selected features with process confirmation — please specify in your drawing.
Nickel alloys require premium cutting tools not used on standard steel or aluminum jobs. We use coated carbide inserts (PVD TiAlN and AlTiN coatings) for general turning and milling, ceramic inserts (SiAlON and whisker-reinforced alumina) for high-speed roughing of Inconel 718, and PCBN (polycrystalline cubic boron nitride) for finishing cuts on hardened Inconel 718. High-pressure coolant (70–100 bar) is directed at the cutting zone on all nickel alloy operations. Tool life is monitored and inserts are changed at defined intervals regardless of visible wear.
Folosiți Inconel 625 pentru aplicații cu apă de mare, chimice și criogenice, unde rezistența la coroziune și sudabilitatea sunt cerințe principale. Folosiți Inconel 718 pentru aplicații aerospațiale, turbine și structuri la temperaturi înalte, unde este necesată rezistența maximă și rezistența la oboseală. Folosiți Hastelloy C-276 pentru cele mai agresive medii chimice — acizi amestecați, soluții de clorură și reactoare chimice, unde Inconel 625 s-ar coroda. Folosiți Monel 400 pentru echipamente marine, servicii cu acid HF și aplicații unde un aliaj de nichel mai ieftin și mai ușor de prelucrat este acceptabil. Dacă nu sunteți sigur, împărtășiți temperatura de funcționare, expunerea la fluide/chimicale și sarcina mecanică — vom recomanda gradul corect înainte de ofertare.
Yes. All nickel alloy orders are supplied with material test reports (MTR) including chemical composition and mechanical properties per the relevant standard: ASTM B446 for Inconel 625, AMS 5662/5664 or ASTM B637 for Inconel 718, ASTM B574 for Hastelloy C-276, and ASTM B164 for Monel 400. Heat number traceability is maintained throughout production. For aerospace and safety-critical applications, full first article inspection (FAI) reports and dimensional CMM reports are available on request.
Solicită o ofertă
Trimite-ți desenul.
Obține o ofertă.
Fiecare solicitare include o revizuire DFM — fezabilitatea toleranței, confirmarea materialului și abordarea procesului înainte de începerea producției. MOQ 1 piesă.
24hr
Răspuns la ofertă
MOQ 1
Prototipuri OK
ISO
9001:2015
📐
Revizuire DFM pentru fiecare solicitare
Fezabilitatea toleranței, strategia de fixare și confirmarea materialului. Feedback specific și acționabil — nu respingeri generice.
🎯
Inspecția primului articol — Standard
Raport FAI pentru fiecare lot nou. Certificări de material și tratament de suprafață incluse cu fiecare livrare.
🔄
Același proces: prototipare până în producție
Planul de proces din prototipul dumneavoastră se aplică loturilor de producție. Fără re-qualificare atunci când scalați.
⚙
Frezare CNC 3 / 4 / 5-Axis + Strunjire
Piese structurale complexe, arbori, carcase și componente de transmisie. Metale și plastice de inginerie.
ISO 9001:2015
Frezare 3/4/5-Axis
Frezare în strung CNC
Inspecție CMM
Livrare globală