Monel K-500 (UNS N05500) Technical Guide | High-Strength Precipitation-Hardened Nickel-Copper Alloy
Date: 2024年10月24日 Categories: All Products、Monel Views: 1474
Excerpt:
Monel K-500 (UNS N05500) technical guide from Hangbo Alloy: precipitation-hardened nickel-copper alloy combining Monel 400 corrosion resistance with age-hardened strength to ~1100 MPa. ASTM B865 bar and forgings with QQ-N-286 and AMS 4676 callouts for pump shafts, valves and fasteners.
Monel K-500 (UNS N05500) — Precipitation-Hardened Nickel-Copper Rod, Bar, Forgings, and Wire | Hangbo Alloy
High-Precision Engineering Reference for High-Strength Marine, Oilfield, and Process Hardware
Introduction
Monel K-500 — registered as UNS N05500 and listed under the German material number W.Nr. 2.4375 — is the age-hardened member of the Monel nickel-copper family. It starts from the same metallurgical base as Monel 400 (UNS N04400): roughly two-thirds nickel, one-third copper, with that alloy's famously broad corrosion resistance in seawater, caustic media, and reducing acids. What distinguishes K-500 is the deliberate addition of aluminum (2.30–3.15%) and titanium (0.35–0.85%), which allows the alloy to be precipitation-hardened after fabrication. A controlled thermal aging treatment precipitates a submicroscopic Ni₃(Al,Ti) phase throughout the matrix and roughly doubles the yield strength of the annealed material while leaving the Monel-400 corrosion envelope essentially intact.
That combination — corrosion resistance equal to the Monel family plus mechanical strength approaching low-alloy steels — is why K-500 has become the default specification for the most mechanically demanding nickel-copper hardware in service: marine pump shafts and impellers, propeller shafts, fasteners, valve trim, oil-well drill collars and surveying instruments, and springs. In high-velocity seawater, where Monel 400 components may suffer erosion or fatigue, K-500 delivers very low corrosion rates together with the strength to resist shaft deflection and impeller loading. In sour-oil and sour-gas service, age-hardened K-500 is accepted under NACE MR0175/ISO 15156 within defined hardness limits, and its low magnetic permeability — essentially non-magnetic even at cryogenic temperatures — makes it a historic standard for non-magnetic drill collars and downhole survey housings.
Shanghai Hangbo Alloy Group supplies Monel K-500 as round bar, flat and square bar, forgings, heading wire, and machined components, certified to ASTM B865 (the governing product specification for precipitation-hardening nickel-copper-aluminum alloy rod, bar, forgings, and heading wire), with EN 10204 3.1 mill certification, full heat-lot traceability, and the aging cycle documented on every certificate. This guide provides the engineering data needed to specify, procure, fabricate, and verify N05500.
1. Alloy Identity and Metallurgy
| Property | Value | Notes |
|---|---|---|
| UNS designation | N05500 | Precipitation-hardenable nickel-copper alloy |
| Common trade names | Monel K-500, K-Monel, Alloy K-500 | "K" denotes the age-hardenable branch of the Monel family |
| Werkstoff number | 2.4375 | DIN/EN designation used across Europe |
| Density | ~8.43–8.44 g/cm³ | Slightly lower than Monel 400 (~8.80) |
| Melting range | ~1315–1350 °C | Solidus–liquidus |
| Crystal structure | FCC (austenitic) + Ni₃(Al,Ti) precipitate | Age-hardening response after solution anneal |
| Strengthening system | γ′-type Ni₃(Al,Ti) precipitation | Al + Ti additions; develops on aging at ~480–620 °C |
| Magnetic behavior | Essentially non-magnetic | Permeability ~1.001–1.002 even at low temperature |
| Design service envelope | Cryogenic to ~590 °C | Above ~600 °C overaging progressively softens the alloy |
| Governing specification | ASTM B865 | Rod, bar, forgings, and heading wire |
The metallurgy of K-500 explains every practical rule a buyer or fabricator must follow:
- It is Monel 400 plus a hardening system. Aluminum and titanium are added to the Ni-Cu solid solution. In the annealed (solution-treated) condition they remain dissolved, and the alloy is soft and formable. Heating into the aging window — approximately 480–620 °C depending on product form and prior cold work — precipitates fine Ni₃(Al,Ti) particles coherent with the matrix, which block dislocation motion and raise strength dramatically.
- Cold work and aging interact. Cold work before aging raises the dislocation density and accelerates precipitation, so spring temper and heavily drawn product age at lower temperatures (about 480–540 °C) and shorter times than soft annealed stock (which typically ages near 590–610 °C for up to 16 hours). The certificate should always state the prior condition and the exact aging cycle.
- Aging causes a slight, predictable contraction on the order of 0.0002 mm/mm (0.0002 in/in). Shafts and precision parts are therefore routinely machined slightly oversize in the annealed or soft condition, age-hardened, then finish-machined to final tolerance — the recommended sequence for the tightest results.
- Corrosion resistance is inherited, with one caveat. In the age-hardened condition K-500 shows a greater tendency toward stress-corrosion cracking in some specific environments than annealed Monel 400, and high-strength product must be protected from hydrogen charging in cathodically protected seawater systems. Both points are covered in Section 5 and in the FAQ.
2. Governing Specifications — ASTM B865 and Related Callouts
| Product Form | Governing Specification | ASME / Related Equivalents | Typical Supply by Hangbo Alloy |
|---|---|---|---|
| Rod and bar (round, flat, square, hex) | ASTM B865 | ASME SB-865 | Round bar Ø 6–350 mm; flat/square/hex in stock sizes |
| Forgings (blocks, discs, rings, shafts) | ASTM B865 | ASME SB-865 | Custom forged and rolled shapes on qualified route |
| Heading wire and fastener stock | ASTM B865 | AMS 4676-type practice | Coil and straight-length wire for cold heading |
| Aerospace bar and forging stock | AMS 4676 | AMS 4677 (as applicable) | Certified aerospace-grade lots on request |
| Oil and gas (sour service) | NACE MR0175 / ISO 15156 | Hardness-limited acceptance | Age-hardened to ≤35 HRC where required |
| Former federal procurement | QQ-N-286 (historic) | Superseded by B865 in commercial practice | — |
| European reference | DIN 17743 / W.Nr. 2.4375 | NiCu30Al | Chemical and mechanical per order |
When writing the purchase order, Hangbo Alloy recommends the full callout: "Monel K-500 (UNS N05500) round bar per ASTM B865, annealed condition, to be age-hardened after machining," or "…annealed and age-hardened, final hardness verified," and confirmation that the mill certificate states the UNS number, the ASTM standard, the heat number, the actual aluminum and titanium values, and the aging cycle used.
3. Chemical Composition (Specified Ranges)
The limits below follow the UNS N05500 registration and the product requirements applied by Hangbo Alloy; copper is the balance element.
| Element | Specified Range (wt %) | Typical Hangbo Alloy Heat | Role-in-Alloy / Watch-Point |
|---|---|---|---|
| Nickel + Cobalt (Ni+Co) | 63.0 – 70.0 | ~65 | Base; matrix corrosion resistance and strength |
| Copper (Cu) | 27.0 – 33.0 (balance) | ~30 | Principal alloying element; seawater and acid resistance |
| Aluminum (Al) | 2.30 – 3.15 | ~2.9 | Primary γ′-type precipitate former — the hardening engine |
| Titanium (Ti) | 0.35 – 0.85 | ~0.6 | Co-precipitates with Al; controls aging response |
| Iron (Fe) | 2.0 max | ~0.8 | Solid-solution contribution; residual control |
| Manganese (Mn) | 1.5 max | ~0.6 | Deoxidation and hot workability |
| Carbon (C) | 0.25 max | ~0.10 | Residual; kept moderate for toughness |
| Silicon (Si) | 0.50 max | ~0.20 | Deoxidizer |
| Sulfur (S) | 0.010 max | ≤0.005 | Held low for hot workability and corrosion uniformity |
| Phosphorus (P) | 0.020 max (typical control) | ≤0.010 | Residual |
The two numbers to verify on every K-500 certificate are aluminum (2.30–3.15%) and titanium (0.35–0.85%). A heat mislabeled from the Monel 400 family — which contains neither element in meaningful quantity — cannot be age-hardened and will fail a hardness verification after aging, so an inexpensive hardness test after a trial age is a decisive grade-authenticity check. Hangbo Alloy reports Al and Ti on every N05500 certificate and can supply third-party verification testing.
4. Mechanical Properties — Annealed vs. Age-Hardened
K-500 is procured and used in two principal conditions. Annealed product (designated Condition A in ASTM B865 practice) is soft, formable, and intended for fabrication followed by aging. Age-hardened product (Condition AH) is supplied at full strength for direct assembly. Typical room-temperature envelopes for bar supplied by Hangbo Alloy:
| Condition | Tensile Strength | Yield Strength (0.2% offset) | Elongation | Hardness (typical) |
|---|---|---|---|---|
| Annealed (Condition A), typical | 585–720 MPa (85–105 ksi) | 275–450 MPa (40–65 ksi) | 25–45% | 75–85 HRB (~140–165 HB) |
| Annealed + aged (Condition AH), typical | 965–1240 MPa (140–180 ksi) | 690–930 MPa (100–135 ksi) | 20–30% | 27–37 HRC |
| Cold-drawn + aged (small bars and wire) | Up to ~1370 MPa (200 ksi) | Up to ~1000 MPa (145 ksi) | 10–20% | Up to ~40 HRC |
ASTM B865 establishes the governing minimums by product form, size, and condition — for annealed-and-aged rod and bar these are on the order of 965 MPa (140 ksi) minimum tensile and 690–760 MPa (100–110 ksi) minimum 0.2% yield depending on section, with minimum elongation of about 20%. Hangbo Alloy certifies the actual minimums applicable to each ordered dimension and condition.
Because age-hardened K-500 is used in shafts, fasteners, and pressure-boundary components where dimensional stability matters, two service behaviors deserve emphasis:
| Behavior | Value | Design Consequence |
|---|---|---|
| Aging contraction | ~0.0002 mm/mm | Machine oversize before aging, finish after |
| Maximum useful service temperature | ~590 °C | Above ~600 °C overaging lowers strength permanently |
| Low-temperature toughness | Retained to cryogenic service | Used in LNG and low-temperature valve trim |
| Resistance to relaxation at temperature | Good to ~300–400 °C | Springs and fasteners hold preload |
| Modulus of elasticity | ~179 GPa (26 × 10³ ksi) | Comparable to steel stiffness per area |
5. Corrosion Resistance — The Monel Envelope at High Strength
The corrosion resistance of K-500 is substantially equivalent to that of Monel 400 across the environments that define the family, which is precisely why the alloy exists: to put Monel-grade corrosion performance into load-bearing components.
| Environment | K-500 Performance | Engineering Comment |
|---|---|---|
| High-velocity seawater | Excellent; very low corrosion rates | Pump shafts and impellers; the alloy's signature service |
| Stagnant or slow seawater | Initial fouling and pitting possible | Attack slows after initial period; avoid crevice traps |
| Caustic alkalis (NaOH, KOH) | Resistant at most concentrations | Suitable for strong alkaline service |
| Hydrofluoric acid (deaerated) | Good resistance | Standard Ni-Cu behavior; aerated acid is more aggressive |
| Dilute hydrochloric and sulfuric (deaerated) | Good at low concentration | Oxidizing contaminants accelerate attack |
| Sour gas / brine (H₂S service) | Resistant; accepted per NACE MR0175 | Age-hardened hardness must be controlled (≤35 HRC typical) |
| Neutral and alkaline salt solutions | Resistant | Broad chemical-process utility |
| Oxidizing acids (nitric, chromic) | Not recommended | Nickel-copper alloys corrode rapidly |
Two cautions are mandatory reading for design engineers. First, in the age-hardened condition K-500 has a greater tendency toward stress-corrosion cracking than annealed Monel 400 in certain environments, so highly stressed fasteners and springs should be reviewed for SCC risk against the specific medium. Second, in seawater systems where K-500 is cathodically protected by coupling to carbon steel or by impressed current, the high-strength condition can absorb hydrogen and suffer embrittlement; overprotection should be avoided, and hardness-limited (e.g., ≤35 HRC) product is frequently specified for such duty. Both considerations are standard material-selection questions that Hangbo Alloy's application engineers address on inquiry.
6. Applications — Where K-500 Earns Its Keep
| Application | Service Condition | Why K-500 Is Selected |
|---|---|---|
| Marine pump shafts and impellers | High-velocity seawater, cyclic loading | High strength + very low seawater corrosion rates |
| Propeller shafts and rudder stock | Seawater, torsion and bending | Fatigue strength beyond Monel 400 |
| Oil-well drill collars and stabilizers | Downhole, sour brine | Non-magnetic, strong, H₂S-tolerant |
| MWD/LWD survey housings and instruments | Downhole pressure and temperature | Low permeability preserves survey accuracy |
| Fasteners, studs, nuts, valve trim | Chemical and marine service | Strength with corrosion resistance; NACE-compliant routes |
| Pump and valve stems, doctor blades, scrapers | Abrasive and corrosive media | Hardness resists wear and galling |
| Springs and spring washers | Corrosive, moderate temperature | Age-hardened elasticity retained in seawater media |
| Electronic and cryogenic components | Low temperature, dimensional stability | Non-magnetic, tough, stable to ~590 °C |
The economic logic is consistent: K-500 costs more per kilogram than Monel 400, but it replaces lower-strength alloys in sections that would otherwise need to be oversized, replaced for wear, or withdrawn for fatigue — which is why it is specified wherever a shaft, fastener, or downhole tool must survive both the chemistry and the mechanics of the service.
7. Fabrication, Heat Treatment, and Machining
- Heat treatment sequence. Solution annealing at approximately 980–1040 °C followed by water quenching restores the soft condition and re-dissolves the hardening phase; this is mandatory before re-aging any material that has been overheated or improperly aged. Aging is then performed per the route below. Material heated above ~590 °C after hardening is overaged and cannot be re-strengthened without full re-solution and re-age.
- Aging cycles (guide). Soft annealed stock: hold 16 h at ~595–605 °C, then cool slowly (about 8–14 °C/h) to ~480 °C, then air cool. Moderately cold-worked stock: 8–16 h at ~595 °C with controlled cooling. Fully cold-worked (spring temper) stock: 6–10 h at ~525–540 °C with controlled cooling. Hangbo Alloy documents the actual cycle on each aged lot.
- Machining. Heavy machining is best performed in the annealed condition; the recommended sequence is machine slightly oversize → age-harden → finish to size. Age-hardened K-500 machines with carbide tooling to excellent finishes and close tolerances.
- Welding. K-500 can be welded using matching nickel-copper filler practice (ERNiCu-7-type consumables are commonly referenced) with procedures similar to those used for Monel 400. Because the as-welded and heat-affected zones do not receive the parent-metal aging response, welded assemblies are normally solution-annealed and re-aged where full strength is required; for maximum SCC resistance in severe media, the annealed condition may be preferred for weldments. Weld procedure qualification is recommended for pressure or critical structural service.
- Cold forming and heading. The annealed condition provides the ductility needed for cold heading, bending, and forming; the work-hardening rate is moderate and is actually exploited when spring temper is required.
- Surface condition. A magnetic nickel-rich surface film can develop during heating in air (selective oxidation of copper and aluminum); it is cosmetic and is removed by pickling or bright dipping where low-permeability surfaces are specified.
8. Why Buyers Select Hangbo Alloy for Monel K-500
- Full EN 10204 3.1 certification with heat-lot traceability, including the two grade-defining elements — aluminum and titanium — and the documented aging cycle;
- Both supply conditions — annealed (Condition A) for in-house fabrication and fully age-hardened (Condition AH) with verified hardness — from one source;
- NACE MR0175 / ISO 15156-compliant age-hardening routes with hardness verification for sour-service fasteners and downhole hardware;
- Bar, forging, and heading-wire program with cutting, rough machining, and surface-finishing services;
- Application engineering support for shaft, fastener, oilfield, and valve specifications, including the machining-oversize/age/finish sequence and welding-filler recommendations.
Technical FAQ — Monel K-500 (UNS N05500)
1. What is the difference between Monel 400 and Monel K-500? Monel 400 is a solid-solution nickel-copper alloy that cannot be strengthened by heat treatment; its strength comes only from cold work. K-500 is the same base with aluminum (2.30–3.15%) and titanium (0.35–0.85%) added so that a precipitation-hardening (aging) treatment can approximately double the yield strength — typically from roughly 275–450 MPa annealed to 690–930 MPa aged — while retaining the Monel corrosion envelope.
2. How is Monel K-500 hardened? By solution annealing (about 980–1040 °C, water quench) followed by aging at approximately 480–620 °C for 6–16 hours depending on prior condition and section, with controlled slow cooling through the aging window. This precipitates fine Ni₃(Al,Ti) particles that block dislocation movement. The exact cycle depends on whether the material was annealed, moderately cold-worked, or fully cold-worked before aging.
3. What is the maximum service temperature of Monel K-500? The benefits of age hardening are retained up to approximately 590 °C. Above roughly 600 °C the precipitate overages, strength falls permanently, and only re-solution annealing plus re-aging can restore it. For corrosion-dominated applications at lower stress, the practical ceiling is usually set by the medium rather than the metal.
4. Is Monel K-500 magnetic? Essentially no. Its magnetic permeability is approximately 1.001–1.002, even at cryogenic temperatures, which is why it is used for non-magnetic drill collars, stabilizers, and downhole survey housings where magnetic interference would corrupt readings. A slightly magnetic surface film can form during air heating but is removed by pickling.
5. Which ASTM specification covers Monel K-500? ASTM B865 covers rod, bar, forgings, and heading wire of UNS N05500, with ASME SB-865 as the pressure-vessel equivalent. Aerospace procurement commonly references AMS 4676; oil and gas service references NACE MR0175 / ISO 15156; the historic federal specification QQ-N-286 has been superseded by B865 in commercial practice.
6. Can Monel K-500 be welded? Yes, using nickel-copper filler practice (ERNiCu-7-type consumables are commonly cited) with procedures similar to Monel 400. Since the weld and heat-affected zones will not match the parent metal's aged strength, full-strength assemblies are solution-annealed and re-aged after welding; where maximum resistance to stress-corrosion cracking is required, the annealed condition is often preferred for weldments.
7. Why must K-500 fasteners in seawater be handled with care? Age-hardened K-500 is strong but, like all high-strength alloys, can suffer hydrogen embrittlement if it is over-protected in cathodically protected seawater systems. Designers limit hardness (commonly ≤35 HRC), avoid excessive cathodic protection potentials, and review highly stressed parts for stress-corrosion cracking in the specific medium.
8. What is the recommended machining sequence for K-500 shafts? Machine slightly oversize in the annealed condition, age-harden to full strength, then finish-machine to final tolerance. Aging produces a small, predictable contraction of about 0.0002 mm/mm, so the oversize allowance must account for it; finish machining after aging also removes any surface film and achieves the best dimensional control.
9. What product forms and sizes does Hangbo Alloy supply in K-500? Hangbo Alloy supplies round bar from 6 to 350 mm diameter, flat, square, and hexagonal bar, forgings (blocks, discs, rings, and custom shapes), heading wire, and machined components, in annealed or annealed-and-aged condition, with EN 10204 3.1 certification and full traceability. Cutting, rough machining, and surface finishing are available on request.
10. How should a purchaser verify that K-500 stock is genuine? Check the mill certificate for UNS N05500 and the two signature elements — aluminum 2.30–3.15% and titanium 0.35–0.85% — plus the documented aging cycle. A decisive shop-floor check is to age a small sample and confirm hardness rises into the 27–37 HRC range: material without aluminum and titanium cannot harden and is not K-500.
This technical guide is provided by Hangbo Alloy (Shanghai Hangbo Alloy Group Co., Ltd., nickel-alloy.com) for material-selection and engineering-reference purposes. Data presented are typical engineering values compiled from recognized industry sources and are not a substitute for the governing ASTM/ASME specifications, code approvals, or the certified mill test report applicable to each heat. Contact Hangbo Alloy at sales@hangboalloy.com or +86 136 1165 6360 for current stock, certificates, and application engineering support.










