Product Description
CISRI has engaged in superalloy industry over 50years. Now, we supply casting superalloys and deforming superalloyss in different shape, such as bar, rod, wire, ingot, strip, plate, tube, etc.
We provide casting master alloys to our customers including K417(IN100), K403, K4169(Inconel718C), K418(INCO713C), K640(X40), DZ40M(DSX40) etc., and deforming superalloys including Inconel601, Inconel800, Inconel800H, Inconel718, Rene41, Waspalloy, C263, A286, HA188, GH95 etc.
Product type: Fe-based superalloy, Ni-based superalloy, Co-based superalloy.
Shape type: Bar, rod, wire, ingot, strip, plate, tube, etc.
Introduction about superalloy:
Superalloys are important metal materials used for hot end parts like modern aerospace turbines, high temperature parts of rocket turbines and equipment in field of energy, metallurgy and chemistry. They can be used under conditions of high stress, high temperature (600-1100) oxidization atmosphere, and combustion and corrosion conditions. According to different base element contains, Superalloys are divided into Fe-base, Ni-base and Co-base alloys. According to different formation processing, superalloys are divided into deformation alloy, precision casting alloy and powder metallurgical alloy. The main requirements of superalloy are focus on the properties of heat-stability, heat-strength and texture stability.
Generally, superalloys are widely used in combustion chamber, force-added combustion chamber, directional blade, turbine blade and turbine disc. The typical materials used in combustion chamber and force-added combustion chamber are GH3030, GH3039, GH1140, GH333, GH2018, GH42, GH3044, GH3218, GH170, GH163 etc. Directional blade material is mainly used casting alloys; The typical alloys are K32, K14, K38, K3, K5, K17, K19, K002, K20 etc. Turbine blade material is mainly age-hardening deforming alloys and casting alloys. The typical working blade material is GH4033, GH2302, GH143, GH4049, GH151, GH118, GH220, K417, K419 etc.
Product of CISRI for example:
| 718 |
Nickel alloy precipitation hardened by gamma prime and double prime. Readily fabricated, weldable even in the hardened condition. Used for gas turbine components to 1200°F, as well as for cryogenic equipment. |
| |
Composition |
Inventory |
| |
Cr |
Ni |
Mo |
Co |
Al |
Ti |
Other |
Plate |
Sheet |
Bar |
Welding Product |
|
| |
19 |
52 |
3 |
- |
0.5 |
0.9 |
Cb: 5 |
X |
X |
X |
X |
|
| |
|
| |
Product Form |
ASME |
ASTM |
AMS |
UNS |
|
| |
Sheet, Plate |
|
B 670 |
5596 |
|
|
| |
Bar |
SB-637 |
B 637 |
5662 |
|
|
| |
Wire |
|
|
5832 |
|
|
|
FAQ
| Q1: Are you a manufacturer? |
| A1: Yes, we have large-scale, modern factory located in Kunshan City, Jiangsu Province, China. We can provide OEM/OOM services for customers around the world. |
| Q2: What about the quality of your products? |
| A2: Our production process is in conformity with ISO 9001. All products we supplied are strictly tested before shipment. |
| O3: Can you offer samples to test before the formal order? |
| A3: Yes, we can provide the existing item's sample. If there is any special feature requirement, please contact us for more details. |
| O4: How long is usually your delivery time? |
| A4: Our delivery time is usually within 14 days after we receive your order. |
| O5: What is your Shipping Methods? |
| A5: By Sea; By air; or by UPS/DHL/FedEx/TNT etc. |
Company Profile
More details please contact us.
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