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Nickel-Aluminium Bronze · Grade Specification

UNS C63000

High-strength American Nickel-Aluminium Bronze

A high-strength Nickel-Aluminium Bronze combining excellent seawater corrosion resistance, non-sparking behaviour and outstanding anti-galling performance under load, used worldwide for aerospace landing gear bushes and bearings.

Overview

An American nickel-aluminium bronze whose unique combined properties of high strength, good fatigue, excellent corrosion resistance in sea water, non-sparking and wear properties make it a popular choice across the whole spectrum of industry.

It has very high anti-galling properties under load and is used on a world basis for aerospace landing gear bushes and bearings where its strength, fatigue, wear properties, shock resistance and corrosion resistance are well proven.

Content on this page is compiled from the UNS C63000 datasheet published on copperalloys.net.

Key features

Corrosion resistance

Good resistance to corrosion.

Hydrogen embrittlement immunity

Immune to hydrogen embrittlement.

Biofouling immunity

Immune to bio-fouling.

Uniformity of properties

Uniform mechanical properties across the section.

Anti-galling

Anti-galling behaviour under load against mating components.

Chemical composition (% by weight)

Specification limits from the published standard.

ElementUNS C63000
Mn≤ 1.5
Al9–11
Ni4–5.5
Sn≤ 0.2
Si≤ 0.25
Fe2–4
Zn≤ 0.3

Mechanical property requirements

Minimum values required by the published specification.

PropertyUNS C63000
Tensile Strength Rm (MPa)≥ 620
0.2% Proof Stress Rp0.2 (MPa)≥ 235
Yield Strength at 0.5% Extension Under Load≥ 250 MPa
Elongation (%)≥ 10 (in 2 in / 50 mm)

Typical mechanical properties by condition and size

Typical values as published on copperalloys.net - indicative only.

ConditionSize (mm dia)Size (in dia)Yield 0.2% (MPa)UTS (MPa)Elong %Hardness (HB)
02075–3003–12300–350600–70012–21180–240
HR5050–802.0–3.2380–430725–80010–15180–240
TQ5080–1303.2–5.1320–400620–77015–20180–240
  • 020 - Hot forged and annealed.
  • HR50 - Drawn and stress relieved (high strength).
  • TQ50 - Quench hardened and temper annealed.

Typical physical properties

As published on copperalloys.net for UNS C63000.

Density
7580 kg/m³ @ 20 °C
Specific gravity
7.58
Specific heat
376.7 J/kg·°C @ 20 °C
Electrical conductivity
0.041 MS/cm @ 20 °C
Thermal conductivity
0.391 W/cm·°C @ 20 °C
Thermal expansion
15.5 × 10⁻⁶ per °C (20–300 °C)
Electrical resistivity
19.28 µΩ·cm @ 20 °C
Relative magnetic permeability
1.4 µ
Machining index
20 (vs free-machining brass = 100)
Modulus of rigidity
46,884 MPa
Modulus of elasticity
125,484 MPa
Melting range
1049–1071 °C
Hot working range
788–927 °C
Cold working
Limited
Cryogenic
Retains properties down to −190 °C
Elevated temperature
Retains properties to 350 °C

Applications

Typical uses

  • Marine fasteners, hardware and fittings
  • Aerospace landing gear components
  • Thrust washers
  • Gears
  • Control bushes
  • Faucet balls

Also suitable for

  • Non-sparking safety tooling
  • Valve stems and seats
  • Wear plates
  • Welding clamps
  • Valve spindles and components
  • Fasteners and bearing bushes
  • Firefighting equipment for offshore platforms
Production methods

Cast, Wrought (forged)

Product forms

Bar, Rod, Plate, Sheet, Tube, Sections, Rings

Industries served

Aerospace, Marine, Naval Defence, Petrochemical

Manufacturing ranges

With very little limitation on size, C63000 is available as standard in rod, bar, blocks, rings, tubes and discs up to a piece weight of 4,500 kg / 9,900 lbs.

Copper Alloys is also regularly making customised shaped forgings and can increase piece weight up to 20,000 kg / 44,000 lbs.

Copper Alloys Ltd also offers finished machined components in all alloys, complete project management and tailored mechanical properties beyond those of the specification to meet special requirements.

Joining & welding

Recommended welding processes.

  • Tungsten inert gas (TIG) / gas tungsten arc (GTAW)
  • Metal inert gas (MIG) / gas metal arc (GMAW)
  • Manual arc (MMA)
  • Friction welding
  • Laser welding
  • Brazing (possible with special fluxes)
  • Soldering or oxy-acetylene - not recommended

Equivalent specifications

US

ASTM B150 C63000ASTM B124 C63000ASTM B171 C63000QQ-C-465B (1) C63000AMS 4640MIL-B-16166ASM SB150 C63000

European

EN 12163 CW307GDIN 17665 CuAl10Ni5Fe4EN 12165 CW307GDIN 17672 CuAl10Ni5Fe4EN 12167 CW307GWNr 2.0966EN 12420 CW307GNF L14-705 CuAl10Ni5Fe4EN 1653 CW307GUA10NNF A 51-116 CuAl10Ni5Fe4

Frequently asked questions

What are typical applications of C63000?+

C63000 is used across marine fasteners and hardware, aerospace landing gear bushes and bearings, thrust washers, gears, control bushes and non-sparking safety tooling - exploiting its strength, wear, corrosion resistance and anti-galling behaviour.

How is C63000 typically supplied?+

As standard in rod, bar, blocks, rings, tubes and discs up to 4,500 kg piece weight, with customised shaped forgings up to 20,000 kg.

How is C63000 welded?+

TIG (GTAW), MIG (GMAW), manual arc, friction and laser welding are all recommended. Brazing is possible with special fluxes; soldering and oxy-acetylene are not recommended.

Discuss your UNS C63000 requirements

Copper Alloys Ltd manufactures Nickel-Aluminium Bronze to UNS C63000 - from stocked bar, rod and rings to fully-machined components and shaped forgings up to 20,000 kg piece weight.

Information provided is for reference only

All chemical, mechanical, production, product-form and industry figures on this page are indicative estimates compiled for general reference and to aid early-stage material selection. They are not engineering, procurement, safety, regulatory or design advice and must not be relied upon as such.

Before specifying, purchasing or using any material, confirm the requirements against the current controlled version of the relevant standard and obtain a certified material test report and written technical confirmation from Copper Alloys Ltd or another qualified foundry. Copper Alloys Ltd accepts no liability for any loss or damage arising from reliance on the information presented on this page.