N07718 Seamless Pipe Alloy 718 Chemical Composition,UT Passed Seamless Pipes
N07718 Seamless Pipes Alloy 718 Chemical Composition,UT Passed Seamless Pipes
N07718, commonly known as Alloy 718, is a precipitation-hardening nickel-chromium superalloy renowned for its exceptional strength, corrosion resistance, and thermal stability—making it a cornerstone material in high-performance industrial applications. Below is a detailed overview of its chemical composition and the significance of ultrasonic testing (UT) qualification for seamless pipes crafted from this alloy.
Chemical Composition of N07718 (Alloy 718)
The chemical makeup of N07718 is meticulously engineered to deliver its signature properties, with key elements and their typical ranges as follows:
Nickel (Ni): 50.0-55.0% – Serves as the base element, providing the alloy with a stable austenitic matrix and resistance to oxidation and corrosion in aggressive environments.
Chromium (Cr): 17.0-21.0% – Enhances corrosion resistance, particularly against pitting and crevice corrosion, while contributing to high-temperature oxidation resistance.
Iron (Fe): Balance – Acts as a secondary matrix element, aiding in workability and reducing material cost without compromising performance.
Niobium + Tantalum (Nb + Ta): 4.75-5.50% – Critical for precipitation hardening; forms intermetallic compounds (e.g., γ” phase) that strengthen the alloy at elevated temperatures (up to 650°C/1200°F).
Molybdenum (Mo): 2.80-3.30% – Boosts strength and creep resistance, especially in high-temperature service, while improving resistance to localized corrosion.
Titanium (Ti): 0.65-1.15% – Assists in precipitation hardening and grain refinement, enhancing mechanical properties.
Aluminum (Al): 0.20-0.80% – Works with titanium to promote the formation of strengthening phases (γ’ and γ”) and supports oxidation resistance.
Carbon (C): ≤0.08% – Controlled to minimize carbide formation, which can reduce ductility and toughness.
Manganese (Mn): ≤0.35%, Silicon (Si): ≤0.35% – Trace elements limited to avoid detrimental phase formations.
Phosphorus (P): ≤0.015%, Sulfur (S): ≤0.015% – Strictly controlled to prevent grain boundary embrittlement and maintain weldability.
This precise composition ensures N07718 seamless pipes excel in extreme conditions, including high-pressure systems, chemical processing, and aerospace applications.
UT-Passed Seamless Pipes: Quality and Reliability Assurance
Ultrasonic Testing (UT) is a non-destructive evaluation (NDE) method critical for verifying the integrity of N07718 seamless pipes. A "UT-passed" certification confirms the following:
- Internal Defect Detection: UT uses high-frequency sound waves to identify subsurface flaws such as cracks, inclusions, porosity, or laminations—defects that could compromise structural integrity under load or pressure. For N07718 pipes, which often operate in safety-critical environments (e.g., oil and gas downhole tools, jet engine fuel lines), eliminating such flaws is paramount.
- Compliance with Standards: UT procedures for N07718 pipes align with industry standards such as ASTM B637 (for seamless nickel-alloy pipe) or ASME Section V (NDE requirements). The testing ensures pipes meet strict acceptance criteria for defect size, distribution, and density—typically adhering to grades like AMS 2630 (aerospace) or customer-specific specifications.
- Consistency in Manufacturing: Seamless pipes undergo rigorous hot working (e.g., extrusion, piercing) and heat treatment. UT validation confirms that these processes have not introduced internal irregularities, ensuring uniform material properties across the pipe’s length and wall thickness.
- Long-Term Performance: By confirming a defect-free structure, UT-passed N07718 pipes minimize the risk of premature failure, leakage, or degradation over time—critical for applications requiring extended service life in harsh conditions (e.g., marine, nuclear, or high-temperature industrial systems).
In summary, N07718 (Alloy 718) seamless pipes combine a tailored chemical composition for strength and corrosion resistance with UT certification to guarantee structural integrity, making them a trusted choice for demanding industrial and aerospace applications.
| Grade | UNS | Density |
Tensile Strength (MPa min) |
Yield Strength (MPa min) |
Reduction of Area min (%) | Elongation min (%) | Hardness (HRC) |
| INCONEL 718 | N07718 | 8.19 | 1275MPa min | 1034MPa min | 15% | 12% min | HRC 35-40 |
Chemical Composition(%):
| Ni | Cr | Fe | C | Mn | S | Si |
| 50.0-55.0 | 17.0-21.0 | Remainder | 0.08max | 0.35max | 0.015max | 0.35max |
| B | P | Mo | Ti | Al | Cu | Co |
| 0.006max | 0.015max | 2.8-3.3 | 0.65-1.15 | 0.2-0.8 | 0.3max | 1.0max |
| Grade | UNS | DENSITY | EN/DIN W.Nr | CONDITION |
| Nickel 200 | N02200 | 8.89 | 2.4066 | Annealed |
| Nickel 201 | N02201 | 8.89 | 2.4068 | Annealed |
| MONEL 400 | N04400 | 8.80 | 2.4360 | Annealed |
| MONEL K-500 | N05500 | 8.44 | 2.4375 | Aged |
| INCOLOY 825 | N08825 | 8.14 | 2.4858 | Annealed |
| INCOLOY 925 | N09925 | 8.08 | - | Aged |
| INCOLOY 926 | N08926 | 8.1 | 1.4529 | Sol.Annealed |
| INCOLOY A-286 | S66286 | 7.94 | - | - |
| INCOLOY 800 | N08800 | 7.94 | 1.4876 | Annealed |
| INCOLOY 800H | N08810 | 7.94 | 1.4958 | Annealed |
| INCOLOY 800HT | N08011 | 7.94 | 1.4959 | Annealed |
| ALLOY 20 | N08020 | 8.08 | 2.4660 | Annealed |
| ALLOY 28 | N08028 | 8.0 | 1.4563 | Annealed |
| NIMONIC 80A | N07080 | 8.19 | 2.4952 | Aged |
| NIMONIC 901 | N09901 | 8.14 | 2.4662 | - |
| INCONEL 625 | N06625 | 8.44 | 2.4856 | Annealed |
| INCONEL 718 | N07718 | 8.19 | 2.4668 | Aged |
| INCONEL X-750 | N07750 | 8.28 | 2.4669 | Aged |
| INCONEL 600 | N06600 | 8.47 | 2.4816 | Annealed |
| INCONEL 601 | N06601 | 8.11 | 2.4851 | - |
| HASTELLOY C-276 | N10276 | 8.87 | 2.4819 | Annealed |
| HASTELLOY C-22 | N06022 | 8.69 | 2.4602 | Sol.Annealed |
| HASTELLOY C-4 | N06455 | 8.64 | 2.4610 | Sol.Annealed |
| HASTELLOY B-2 | N10665 | 9.22 | 2.4617 | Annealed |
| HASTELLOY B-3 | N10675 | 9.22 | 2.4600 | Annealed |
| HASTELLOY X | N06002 | 8.22 | 2.4665 | Aged |
| F44 | S31254 | 8.0 | 1.4547 | Annealed |
| F51 | S31803 | 7.8 | 1.4462 | Solution |
| F53 | S32750 | 7.8 | 1.4410 | Solution |
| F55 | S32760 | 7.8 | 1.4501 | Solution |
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