IN713 C Inconel 713 Ni Cr Mo Alloy Wire/Rod for Aerospace & Gas Turbines
In713C refers to Inco713C, In713LC, belongs to nickel based alloys, usually delivered as cast. It is a γ' phase precipitation hardening cast superalloy having good creep strength, thermal fatigue properties and oxidation resistance below 900℃(1652℉).
In713C| Inconel 713 Alloy Chemical Composition
| C | Cr | Ni | Mo | Al | Ti | Fe | Nb | B | Zr | Mn | Si | P | S | Pb | Bi | |
| Min | 0.08 | 11.5 | Balance | 3.8 | 5.5 | 0.5 | 1.8 | 0.008 | 0.06 | |||||||
| Max | 0.16 | 13.5 | 4.8 | 6.4 | 1.0 | 1.0 | 2.5 | 0.020 | 0.15 | 0.5 | 0.5 | 0.015 | 0.01 | 0.001 | 0.0001 |
In713C| Inconel 713 Material Properties
| Grade | Density | Melting Point | Mechanical Properties | Stress Rupture | |||||||
| θ | Tensile strength | Yield Strength | Elongation | Reduction of area | Temperature | Stress | Min Hours | Elongation | |||
| In713C Inconel 713 | 8.0 |
1295-1345℃ 2363-2453℉ |
20℃ 68℉ |
755Mpa | 635 | 3.0 | / |
750℃ 1382℉ |
605Mpa | 40 | 3.0 |
|
800℃ 1472℉ |
755Mpa | / | 4.0 | 6.0 |
800℃ 1472℉ |
490Mpa | 45 | 3.0 | |||
In713C| Inconel 713 Applications
Aerospace Gas Turbine below 900℃(1652℉)
Ground-based Gas Turbine below 900℃(1652℉)
Offshore Gas Turbine below 900℃(1652℉)
In713C| Inconel 713 corrosion resistance to marine gas
| Sample condition and size/mm | Test Condition | θ | T/h | Corrosion weight loss(mg/(cm3.h)) |
| As cast, d20*3 |
NO.10 diesel oil Oil gas ratio:1:30 Salt spray concerntration:0.075% |
900℃(1652℉) | 25 | 3.33 |
In713C| Inconel 713 corrosion resistance to vulcanization
| Test Condition | θ | T/h | Weight gain/(mg/cm2) |
|
The sample was placed in a specific position of the gas turbine, and the specific component of the gas was mainly CH, and the concentration of H2S fluctuated from 0.1% to 0.4%. |
700-840℃ 1292-1544 |
2408 | 3.33 |
| 5365 | 15.50 | ||
| 13089 | 15.25 |
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