Low MOQ for Titanium alloy 6Al-2Sn-4Zr-2Mo UNS R54620 for United Arab emirates Factory
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HY Titanium 6-2-4-2 Material grades and equivalents
6Al-2Sn-4Zr-2Mo, 6-2-4-2 Titanium, 6-2-4-2, UNS R54620
Introduction
A near-alpha alloy, primarily used for high strength and toughness, with good creep resistance up to 1000°F. Forging and machining characteristics similar to those of Ti 6Al-4V. Applications include compressor components, hot airframe skin, and engine afterburner structures. The weld ability of Ti 6-2-4-2 is fair, using AMS 4952 weld wire. Several different treatments are available.
Chemistry Composition
|
|
Al |
Sn |
Zr |
Mo |
C |
N |
H |
O |
Si |
Fe |
Y |
Others, |
Others, |
Ti |
|
MIN |
5.5 |
1.8 |
3.6 |
1.8 |
- |
- |
- |
- |
0.06 |
- |
- |
- |
- |
- |
|
MAX |
6.5 |
2.2 |
4.4 |
2.2 |
0.05 |
0.05 |
0.015 |
0.12 |
0.1 |
0.25 |
0.005 |
0.1 |
0.3 |
Balance |
Features
- Machinability similar to austenitic stainless steels
- Easily welded if proper precautions are taken to prevent oxygen, nitrogen and hydrogen contaminations
- Long term stability for temperatures up to 800°F
Applications
- Compressor discs, blades
- Airframe structure, skin
- Engine afterburner components
- Hush kits
Physical Properties
Density: 0.160 lb/in3
Beta Transus: 1825±25°F
Thermal Conductivity: 4.00 Btu • hr/ft2 • hr°F
Coefficient of Thermal Expansion: 32-212°F 4.3 x10-6 in/in°F
Modulus of Elasticity: 16.5×106 psi
Mechanical Properties
Minimum Tensile Properties, AMS 4919, Duplex Annealed
|
Thickness, in |
0.025 ≤ 0.062 |
> 0.062 ≤ 1.000 |
> 1.000 ≤ 3.000 |
|
Tensile Strength, ksi |
135,000 |
135,000 |
135,000 |
|
0.2% offset Yield Strength, ksi |
125,000 |
125,000 |
125,000 |
|
Elongation, % |
8 |
10 |
10 |
| 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 |
Inconel 718, The Severe Metal Alloy. http://www.techsteel.web/alloy/nickel/inconel-718
Turbine Blades have revolutionized air vacation and electricity era.
Hundreds of slim precision blades spinning at a hundred,000 RPM have to have a materials that can stand up to excessive disorders.
Inconel 718 is a distinctive metal alloy that can stand up to excessive temperatures from -423° to 1300°F
This alloy is aged hardened, making it possible for it to be welded without having hardening for the duration of heating and cooling.
The improvement of Inconel began in the fifties for use in vital steam line plants. Originally used for armed service programs it was later on adopted by the professional sector.
Inconel 718‘s tolerance for excessive temperature make it specially perfectly suited for programs such as
turbine blades
nuclear electricity plants, and
aerospace programs. It was used in the space shuttles high force pump.
AMS 5589 | AMS 5596 | AMS 5597 | AMS 5663 | AMS 5664
For extra inconel 718 details take a look at techsteel.web
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http://www.msm.cam.ac.british isles/phase-trans/2002/creep.1.html
