Waspaloy Alloy UNS N07001

Short Introduction:

HY Waspaloy/W.NR 2.4654/UNS N07001/GH4738 is a nickel base, age hardenable super alloy with excellent high temperature strength and good corrosion resistance, notably to oxidation, at service temperatures up to 1200°F (650°C) for critical rotating applications, and up to 1600°F (870°C) for other, less demanding, applications. The alloy’s high-temperature strength is derived from its solid solution strengthening elements, molybdenum, cobalt and chromium, and its age hardening elements, aluminum and titanium. Its strength and stability ranges are higher than those typically available for alloy 718.

Category:

Description

Waspaloy Alloy UNS N07001

Waspaloy Alloy UNS N07001

HY Waspaloy Material grades and equivalents: W.NR 2.4654; UNS N07001; GH4738

Introduction:

HY Waspaloy Alloy is a nickelbase, age hardenable super alloy with excellent high temperature strength and good corrosion resistance, notably to oxidation, at service temperatures up to 1200°F (650°C) for critical rotating applications, and

up to 1600°F (870°C) for other, less demanding, applications. The alloy’s high-temperature strength is derived from its solid solution strengthening elements, molybdenum, cobalt and chromium, and its age hardening elements, aluminum and titanium. Its strength and stability ranges are higher than those typically available for alloy 718.

HY Waspaloy Chemical composition:

Alloy

%

Ni

Cu

Al

Zr

B

Cr

Mo

Fe

Co

C

Mn

Si

Ti

P

S

HY Waspaloy

Min.

Balance

1.20

0.02

0.003

18.00

3.5

12.0

0.02

2.75

Max.

0.5

1.60

0.12

0.01

21.00

5.0

2.0

15.0

0.1

1.0

0.75

3.25

0.03

0.03

HY Waspaloy Physical properties:

Density

8.19 g/cm3

Melting point

1330℃-1360 ℃

HY Waspaloy Applications Fileds:

HY Waspaloy is used for gas turbine engine components that call for considerable strengthand corrosion resistance at high operating temperatures. Current and potential applications include compressor and rotor discs, shafts, spacers, seals, rings and casings, fasteners and other miscellaneous engine hardware, airframe assemblies and missile systems.

Regular shape for all kinds of alloys

Form

Specification

Supply Form

Others

Sheet

Thickness:0.40-4.75mm,General Width:1000、1219、1500mm

Whole Coil or piece of it

Cold Annealed,Surface 2B、2E

Plate

Thickness:4.76-60mm,Width:1500、2000、2500mm,Length:3000、6000、8000、8500mm(Under 10mm plate can be coiled)

Whole Coil or piece of it

Single hot rolling,Solid solution annealed state,Surface 1D

Belt

Thickness:0.10-3.0mm,Width:50-500mm

Whole Coil or Specified size

Cold Annealed,Surface 2B、2E

Bar & Rod

Rolled barΦ5-45mm,Length≤1500mm

Polished Bar(circle、Square)

Solution annealing,descaling

Forged barΦ26-245mm,Length≤4000mm

Weld tube

Outer diameterΦ4.76-135mm,Wall Thickness0.25-4.00mm,Length:≤35000 mm

Base on your requirement

Seamless Tube

Outer diameterΦ3-114mm,Wall Thickness0.2-4.5mm

Base on your requirement

Wire

Outer diameterΦ0.1-13mm

Base on your requirement

Ni & Ni alloy, Ti & Ti alloy

Forged piece

discs,rings,squares,blocks,slabs

Base on your requirement

Steel, Alloy

Flangs

All kinds of Flangs

Base on your requirement

Steel, Alloy

Welding Material

Coil wire Φ0.025mm-1.6mm

Base on your requirement

Certificate of Origin:America, Sweden, Britain, Germany, Austria, Italy, France.

Straight WireΦ1.6mm-4.0mm

Welding rodΦ1.2mm-4.0mm

Tube

Elbow, three links, four links, different diameter size

Base on your requirement

Ni & Ni alloy, Ti & Ti alloy

Explosive bonded laminate

Raw Sheet Thickness≥2mm

Base on your requirement

Ni & Ni alloy, Ti & Ti alloy