Factory Outlets Nickel Alloy Inconel X-750 UNS N07750 for Israel Manufacturer
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HY X-750 Material grades and equivalents
Inconel X-750 / GB GH4145 / UNS N07750/W.Nr.2.4669 NiCr15Fe7TiAl / AFNOR NC15FeT
HY X-750 Chemical composition:
Alloy |
% |
Ni |
Cr |
Fe |
Nb |
Co |
C |
Mn |
Si |
S |
Cu |
Al |
Ti |
HY X-750 |
Min. |
14 |
5 |
0.7 |
0.4 |
2.25 |
|||||||
Max. |
70 |
17 |
9 |
1.2 |
1 |
0.08 |
1 |
0.5 |
0.01 |
0.5 |
1 |
2.75 |
HY X-750 Physical properties:
Density |
8.28 g/cm3 |
Melting range |
1393-1427℃ |
HY X-750 Alloy m inimum Mechanical properties in the room temperature:
Alloy |
Tensile strength |
Yield strength RP0.2N/mm2 |
ElongationA5 % |
Brinell hardness HB |
Solution treatment |
1267 |
868 |
25 |
≤400 |
HY X-750 Characteristic as below::
HY X-750 is a precipitation-hardenable alloy which has been used in applications such as high temperature structural members for gas turbines, jet engine parts, nuclear power plant applications, heat-treating fixtures, forming tools, and extrusion dies. The alloy is highly resistant to chemical corrosion and oxidation and has high stress-rupture strength and low creep rates under high stresses at temperatures up to 1500°F (816°C) after suitable heat treatment.
HY X-750 Machinability:
Conventional machining techniques used for iron based alloys may be used. This alloy does work-harden during machining and has higher strength and “gumminess” not typical of steels. Heavy duty machining equipment and tooling should be used to minimize chatter or work-hardening of the alloy ahead of the cutting.
HY X-750 Corrosion resistance:
HY X-750 has excellent resistance to chloride ion stress-corrosion cracking. It exhibits satisfactory resistance to numerous oxidizing environments. The alloy has similar corrosion resistance to alloy 600 in many media.
HY X-750 Application range and field:
- Nuclear reactors
- Gas turbines
- Rocket engines
- Pressure vessels
Aircraft structures
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
The progress of improved metallic resources is a crucial action at the leading edge of science and know-how. Metals offer unrivalled mixtures of houses and reliability at a cost which is economical. They are adaptable mainly because subtle improvements in their microstructure can cause dramatic variations in their houses. For illustration, it is feasible to purchase business steel with a energy as lower as 50 MPa or as large as 5500 MPa. They can be built with a microstructure which is finer than that of carbon nanotubes. An understanding of the progress of microstructure in metals, rooted in thermodynamics, crystallography and kinetic phenomena is crucial for the resources scientist. The bulk of the 1.4 billion tonnes of metals made annually are the outcome of developments within just the last 10 a long time
http://www.msm.cam.ac.british isles/phase-trans/2002/creep.1.html