OEM/ODM China Nickel Alloy Incoloy 901 UNS N09901 Factory for Manchester
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HY 901 Material grades and equivalents
Incoloy 901/ Alloy 901/USN N09901/W.Nr.2.466 NS/BS Nimonic901
HY 901 (UNS N09901/Din 1.4898)
HY 901 Chemical composition:
Alloy |
% |
Ni |
Cu |
Al |
Fe |
Ti |
Co |
Mn |
S |
C |
Si |
P |
Cr |
Mo |
B |
HY 901 |
Min. |
40.0 |
2.35 |
11.0 |
5.0 |
0.01 |
|||||||||
Max. |
45.0 |
0.50 |
0.35 |
Balance |
3.10 |
1.0 |
1.0 |
0.03 |
0.10 |
0.60 |
0.03 |
14.0 |
7.0 |
0.02 |
HY 901 Physical properties:
Density |
8.14 g/cm3 |
Melting point |
1280-1345℃ |
HY 901 minimum mechanical properties in the room temperature:
Status |
Tensile strength |
Yield strength |
Elongation |
HY 901 |
1034 |
689 |
12 |
Description
A nickel-iron-chromium alloy containing titanium and aluminum for precipitation hardening and molybdenum for solid-solution strengthening. The alloy has high yield strength and creep resistance at temperatures to about 1110°F (600°C). A subtantial iron content enables the alloy to combine high strength with good forging characteristics. Used in gas turbines for discs and shafts. Standard products form is round.
Corrosion Resistance
Alloy 901 has good corrosion resistance to the atmospheres normally found in jet engine operations. It has slightly lower scaling resistance than such alloy as Types 309 and 310 stainless steel.
Workability
Hot Working
Alloy 901 is forged between 2050°F (1121°C) and 1850°F (1010°C), metal temperature. Light hot work may be continued down to 1600°F (871°C) but not below. Metal temperature should not exceed 2050°F (1121°C) during rapid working. Billets should be charged into a hot furnace and heated rapidly through the precipitation hardening range.
Weldability
Alloy 901 can be welded by the inert-gas-arc method. It is difficult to weld. All welding should be done in the solution treated condition. Cold worked parts should be re-solution treated before welding. A re-solution treatment is recommended after welding before stabilizing and aging.
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 |
High successful HRSA turbine blade roughing on Starrag LX 051
- Materials technical specs: Nimonic 80A, NiCr20TiAl (2.4952)
- MMR: sixteen.nine cm3/min
Riporto(placcatura)con filo Nimonic 80 dia. one.2 eseguito con inverter multiprocesso Weldtronic Synertech 8004 Digit in pulsato sinergico.
NB .Il lampeggio dell’arco è presente solo nella ripresa effettuata dalla fotocamera digitale usata probabilmente a causa di interferenza con l’intenso arco luminoso.
Details: belda1@tiscali.it