Get in Touch with TiAlloy Company
Inconel 718 Supplier Bar, Plate, Sheet, Tube, Pipe & Forgings
TiAlloy supplies Alloy 718 / UNS N07718 in plate, sheet, bar, rod, tube, pipe and forging forms. Quotations are reviewed against the requested product form, specification, dimensions, condition, quantity and inspection or documentation requirements.
Alloy 718 at a Glance
Alloy 718 / UNS N07718 / W.Nr. 2.4668 is an age-hardenable nickel-chromium alloy. Product form, material condition and the applicable specification should be confirmed together before material is quoted or ordered.
Inconel 718 ASTM & AMS Standards
Inconel 718 / Alloy 718 / UNS N07718 specifications vary by product form and material condition. Common Inconel 718 plate, sheet, strip, bar, forging, seamless tube and pipe standards include ASTM B670, ASTM B637, ASTM B983 and the applicable SAE AMS specifications shown below.
| Product Form | Inconel 718 Specification | Scope / Order Check |
|---|---|---|
| Inconel 718 Plate · Sheet · Strip | ASTM B670 AMS 5596 AMS 5597 | ASTM B670 applies to rolled precipitation-hardenable Alloy 718 flat products. AMS 5596 and AMS 5597 cover aerospace Inconel 718 sheet, strip and plate using different solution-treatment routes. Confirm thickness, dimensions, material condition and specification revision. |
| Inconel 718 Bar · Rod · Forgings · Rings | ASTM B637 AMS 5662 AMS 5663 | ASTM B637 covers precipitation-hardenable nickel-alloy rod, bar, forgings and forging stock. AMS 5662 and AMS 5663 are commonly specified for Alloy 718 bar and forgings with different heat-treatment conditions. Confirm section size, heat treatment, mechanical properties and inspection requirements. |
| Inconel 718 Seamless Tube · Pipe | ASTM B983 AMS 5589 AMS 5590 | ASTM B983 covers high-strength seamless nickel-alloy pipe and tube including UNS N07718. AMS 5589 and AMS 5590 cover Inconel 718 seamless tubing using different solution-treatment routes. Confirm OD, wall thickness, length, material condition, tolerance and testing requirements. |
Use the ASTM or SAE AMS specification stated on the drawing or purchase order. The applicable revision, product form, heat-treatment condition and supplementary testing requirements should be confirmed before quotation and production.
Check Standard & SizeInconel 718 Properties & Material Data
Inconel 718 / Alloy 718 is an age-hardenable nickel-chromium alloy designated UNS N07718. Its chemical composition, mechanical properties and physical properties should be reviewed together with the required material condition and applicable product specification.
Limiting composition for Inconel 718 / Alloy 718, expressed as weight percent.
| Weight % | Ni Nickel + Cobalt | Cr Chromium | Fe Iron | Nb + Ta Niobium + Tantalum | Mo Molybdenum | Ti Titanium | Al Aluminum |
|---|---|---|---|---|---|---|---|
| Alloy 718 | 50.00–55.00 | 17.00–21.00 | Balance | 4.75–5.50 | 2.80–3.30 | 0.65–1.15 | 0.20–0.80 |
Inconel 718 Mechanical Properties
Typical · 20°C · solution annealed + age hardened| 0.2% Yield Strength | Tensile Strength | Elongation | Reduction of Area |
|---|---|---|---|
| 1,030 MPa | 1,280 MPa | 12% | 15% |
Inconel 718 Physical Properties
Typical valuesTypical property data are provided for material comparison and preliminary engineering review. Final requirements should be confirmed against the applicable specification, revision, dimensions and required delivery condition.
Inconel 718 Product Forms & Machining Considerations
Inconel 718 plate, sheet, tube, pipe and bar are not interchangeable purchase forms even when the material designation is the same UNS N07718. Product form, specification, dimensions, material condition and machining allowance should be confirmed before quotation, especially when the material will be cut, turned, ground or machined after delivery.
Start with the required geometry, then confirm the applicable Alloy 718 specification, dimensions, condition and downstream processing requirements.
Plate & Sheet Blanks
Seamless Tube & Pipe
Round Bar & Rod Stock
Drawing-Based Structural Parts
Cut-to-Size Machining Blanks
Machining Allowance
Specify finished dimensions or provide the drawing so suitable oversize stock can be reviewed.
Supply Condition
Confirm solution-treated, aged or other specification-defined condition before machining.
Tolerance & Finish
Define cut tolerance, straightness, flatness, surface finish or other dimensional requirements.
Identification & Inspection
Heat-number traceability, inspection and packing requirements should be included when required.
Inconel 718 Processing, Heat Treatment & Inspection Workflow
For Alloy 718 / Inconel 718 / UNS N07718, product form, melting and remelting route, forming process, heat-treatment condition and inspection scope should be reviewed together. Depending on the applicable specification and service requirement, the production route may include VIM, VAR, ESR, forging, rolling, tube processing, solution treatment, ageing, machining and final inspection.
Final acceptance depends on the applicable specification, product form, heat-treatment condition, required tests, heat-number traceability and released documentation.
Alloy 718 Melt Route
Confirm the required melt practice
Inconel 718 Heat Treatment
Match condition to specification
Testing & Documentation
Define acceptance evidence
RFQ
Confirm Inconel 718 Process Requirements
Product Form · Specification · Size · Melt Route · Heat Treatment · Testing · Quantity
Inconel 718 Supply, Documentation & Export
Alloy 718 / Inconel 718 / UNS N07718 orders can be reviewed for product form, specification, dimensions, material condition, testing, documentation, packing and international delivery requirements before quotation and order release.
Packing, marking and documentation are confirmed against the Alloy 718 product form, destination and purchase requirements.
Material Documentation
Export Packing Control
International Supply Review
Inconel 718 certificate, inspection and export requirements depend on the product form, governing specification, destination and purchase order. Required MTC / MTR wording, EN 10204 certification, inspection records and shipment documents should therefore be confirmed before order release.
Export
Request Inconel 718 Supply & Export Details
Grade · Product Form · Standard · Size · Quantity · Testing · Destination
Inconel 718 Forms, Sizes & Stock
TiAlloy supplies Inconel 718 / Alloy 718 / UNS N07718 / 2.4668 in plate, sheet, strip and coil, round bar, tube, pipe, forgings and cut-to-size products. Select a product form to review typical sizes, stock, small-quantity supply and related components.
Inconel 718 Plate, Sheet, Strip & Coil
- Inconel 718 Plate: approx. 5–100 mm thickness · width up to about 2,000 mm.
- Inconel 718 Sheet: approx. 0.5–4.0 mm thickness · width up to about 1,500 mm.
- Inconel 718 Strip / Coil: approx. 0.05–4.0 mm thickness · slit width, coil ID / OD and coil weight to requirement.
Inconel 718 Round Bar
- Standard Round Bar: approx. Ø6–254 mm.
- Larger Diameters: can be reviewed through a forged-bar production route.
- Lengths: mill length, fixed length or cut-to-size according to requirement.
Inconel 718 Tube, Pipe & Piping Components
- Inconel 718 Seamless Tube: approx. OD 3.35–101.6 mm · wall thickness about 0.5–15 mm.
- Inconel 718 Pipe: typical commercial requirements approximately NPS 1/4–6 in.
- Length / Tolerance: straight length, cut length, OD tolerance and wall tolerance to specification.
Inconel 718 Forgings & Machining Blanks
Availability note: Not every Inconel 718 form, size or condition is held in stock. Send the required form, dimensions, quantity, specification and material condition for a current stock or production check.
Check Inconel 718 StockInconel 718 Applications & Typical Components
Alloy 718 / UNS N07718 is primarily selected where high mechanical strength, fatigue resistance and age-hardenable properties are required together with useful corrosion and oxidation resistance. Typical applications are concentrated in aerospace, gas turbines, propulsion systems, high-strength hardware and other demanding rotating or structural components.
Aerospace & Gas Turbines
Inconel 718 was developed for demanding static and rotating turbine components where strength, fatigue behavior and creep resistance are important. The applicable material condition and specification depend on the component and acceptance requirements.
Space & Propulsion
Alloy 718 is also used in rocket and spacecraft hardware where a high-strength nickel alloy is required for structurally and thermally demanding components.
Turbochargers, Fasteners & High-Strength Hardware
Age-hardened Alloy 718 is used where compact components need high strength and reliable mechanical performance. Automotive turbocharger parts, screws, springs and mounting hardware are established examples.
Industrial & Cryogenic Components
Inconel 718 has also been used for cryogenic tankage and heat-resistant tooling. Suitability should still be evaluated against the actual temperature, loading, fabrication route and governing specification rather than by alloy designation alone.
Oil & Gas Applications
Alloy 718 can also appear in demanding oil and gas equipment, including drilling and pump components, but the required 718 variant, heat treatment and qualification route must be confirmed against the governing specification and service environment. Specialized 718 CTP-type material routes are used for certain oil and gas applications; UNS N07718 alone should not be treated as evidence that a material satisfies a specific sour-service or downhole requirement.
Application does not replace specification. When requesting Inconel 718 for a turbine, propulsion, automotive, cryogenic or oil-and-gas component, define the product form, governing standard, material condition, dimensions and required inspection criteria with the RFQ.
When Inconel 718 Is the Right Choice
Alloy 718 / UNS N07718 is usually considered when mechanical strength is a primary material-selection requirement. Its precipitation-hardening response allows high tensile, yield, fatigue and creep capability to be developed through the specified heat-treatment route.
Choose Alloy 718 when the requirement is driven by
- High tensile and yield strength in a precipitation-hardened nickel alloy
- Fatigue resistance for highly loaded rotating or structural components
- Creep and stress-rupture performance at elevated temperature
- A specification-controlled aerospace, turbine, propulsion or high-strength industrial component
- A material condition that can be developed through solution treatment and ageing
Strength alone does not decide the alloy
Inconel 718 should not automatically replace another nickel alloy simply because higher strength is required. Corrosion environment, operating temperature, fabrication route, weldability, heat treatment, product form and governing specification can change the appropriate material choice.
718 vs 625
Strength vs corrosion / fabrication
When 718 may be more appropriate
Alloy 718 is precipitation hardenable and is commonly selected where high mechanical strength, fatigue performance and specification-controlled heat treatment are central to the component design.
When 625 may deserve more attention
Alloy 625 is commonly considered where corrosion resistance, weldability and fabrication without a required precipitation-hardening cycle are more important than obtaining the higher strength levels associated with aged Alloy 718.
718 vs X-750
Different strengthening routes
Both are age-hardenable nickel alloys, but they are not interchangeable
Alloy 718 and X-750 can both appear in high-temperature hardware, springs, fasteners and turbine-related applications. Their chemistry, heat-treatment schedules, mechanical-property requirements and applicable product specifications differ.
The correct choice should therefore follow the required service condition and governing material specification, rather than the general description “high-temperature nickel alloy.”
718 vs 725
High strength and service environment
Oil & gas requirements need separate review
Alloy 725 is another age-hardenable nickel alloy used for high-strength applications where corrosion resistance is also important. Certain oil-and-gas applications may therefore lead to a comparison between Alloy 718 variants and Alloy 725.
Material selection should consider the actual corrosive environment, heat-treatment condition, sour-service requirements and customer specification. The UNS designation alone does not establish application qualification.
Selection note
Do not select Inconel 718 from alloy name alone. Confirm the required product form, specification, heat-treatment condition, operating temperature, mechanical loading, corrosion environment and inspection criteria before treating Alloy 718 as an approved substitution for another nickel alloy.
Inconel 718 Price & Lead Time
Inconel 718 / Alloy 718 / UNS N07718 pricing is based on the actual purchase requirement. There is no single Inconel 718 price per kg that applies equally to plate, bar, tube, pipe and forgings.
Product form, dimensions, specification, material condition, quantity, testing, processing and destination are reviewed before a commercial quotation and lead time are confirmed.
What affects Inconel 718 pricing?
Product form and size
Inconel 718 plate, sheet, round bar, tube, pipe and forgings follow different material and processing routes. Thickness, diameter, OD, wall thickness, length and cut size affect the quotation.
Specification and material condition
ASTM, SAE AMS or customer specifications may require different supply conditions, heat treatment, mechanical properties and acceptance criteria.
Testing and additional processing
PMI, mechanical testing, NDT, cutting, grinding, turning or machining should be included in the RFQ when required.
Quantity and delivery requirement
Order quantity, packing, documentation, destination and agreed Incoterms are reviewed with the material requirement.
Price references
Nickel market
Nickel market pricing can indicate changes in raw-material value but does not represent the finished price of an Alloy 718 product.
Alloy surcharge
Published alloy surcharges can indicate market movement. Final pricing still depends on form, size, condition, processing, testing and quantity.
Inconel 718 lead time is order-specific
A standard-size Alloy 718 bar does not necessarily follow the same delivery route as a special-size plate, seamless tube or finished forging. Lead time is reviewed against the product form, size availability, material condition, processing, inspection scope and quantity.
- Standard or special dimensions
- Solution treatment or ageing condition
- Mechanical testing, PMI or NDT
- Cutting, grinding or machining
- Quantity, packing and shipment requirements
Request Inconel 718 Price
Send the actual requirement so price and lead time can be reviewed against the correct material form, specification and delivery scope.
Standard · Condition · Testing · Destination
Inconel 718 Service & Engineering Notes
Alloy 718 / UNS N07718 does not have one set of mechanical or service properties that applies independently of material condition. Heat treatment, operating temperature, loading, environment, product form and governing specification all matter when the material is evaluated for an engineering application.
Where service data needs context
Strength depends on material condition
Inconel 718 develops its characteristic high strength through a controlled solution-treatment and precipitation-hardening route. Solution-treated material and fully aged material should not be assumed to have the same mechanical properties. The required condition must therefore be linked to the governing specification and purchase order.
Temperature capability is not one universal limit
Published Alloy 718 data often describes demanding elevated-temperature service, but a single temperature should not be treated as a universal design limit. Load, exposure time, creep requirement, fatigue cycle, environment and heat-treatment condition all affect engineering suitability.
Corrosion resistance remains environment-specific
Alloy 718 provides useful oxidation and corrosion resistance, but the alloy designation alone does not establish suitability for every corrosive service. Media chemistry, temperature, chlorides, H₂S, pH, stress level and qualification requirements should be reviewed where relevant.
UNS N07718 does not define final acceptance
The UNS designation identifies the alloy chemistry family; it does not by itself establish compliance with every ASTM, SAE AMS, API, NACE or customer specification. Product form, dimensions, heat treatment, mechanical properties, testing and documentation must be checked against the actual specification being ordered.
Before material approval
Review the service requirement and purchase specification together before approving Inconel 718 for a component. For critical aerospace, turbine, pressure, cryogenic or oil-and-gas service, the buyer’s governing engineering specification takes priority over a general alloy description.
What to Include in an Inconel 718 RFQ
Send the grade, product form, dimensions, quantity, applicable specification, required condition, inspection requirements and destination with the enquiry. Attach drawings when machining, special tolerances or finished components require review.
RFQ information
Material
Inconel 718 / Alloy 718 / UNS N07718 / 2.4668, or the buyer’s approved material designation.
Product form and size
Plate, sheet, round bar, tube, pipe or forging with actual thickness, diameter, OD, wall, length, cut size and quantity.
Specification and condition
Applicable ASTM, SAE AMS or customer specification together with the required solution-treated, aged or other specification-defined condition.
Inspection and documentation
Mechanical testing, hardness, PMI, UT or other NDT where specified, together with MTC / MTR, heat-number traceability and required certification such as EN 10204 3.1 where applicable.
Delivery
Destination country or port, required packing, Incoterms and shipment-specific documentation requirements.
For machined parts or special tolerances, include the drawing with the enquiry.
Example RFQ Format example — not an actual supply case
Inconel 718 / UNS N07718 round bar, Ø45 × 2,000 mm, quantity 800 kg, ASTM B637, solution treated and aged. MTC / MTR and specified hardness required. Delivery to [Port / Country] under [Incoterm].
For custom machining, dimensional tolerances or finished components, attach the drawing and required inspection scope with the RFQ.
Send Your Inconel 718 RFQ
Provide the actual purchasing requirement so specification, price, condition, inspection and delivery can be reviewed together.
Inconel 718 Assessment Tools
Sys. Module // 01
Price & Lead Time Estimator
Evaluate core cost drivers and delivery timelines based on material parameters.
Sys. Module // 02
RFQ Readiness Checker
Validate your inquiry details and specifications before submission.
Sys. Module // 03
Form & Standard Selector
Match physical forms with certified industry standards and revisions.
Inconel 718 FAQ
FAQ answers below are derived from supplier searches in machining forums, buyer search terms and standards review. Direct answers avoid the risk of a costly receiving, service or machining shortcut.
TiAlloy engineers use these answers to confirm against form, standard, service condition and document scope before turning a question into a quotation.
FAQ.01
Can TiAlloy supply Inconel 718 sheet, tube and bar in one order?
Yes, we can quote sheet, tubing, plate, rod, pipe and tube. However the standards for flat product, hollow product and bar/rod product will need to be segregated.
FAQ.02
Is Inconel 718 tubing the same as Inconel 718 pipe?
Not always. Buyer searches frequently mix terminology, but your request must identify OD, wall thickness, pressure basis and whether ASTM B983, AMS 5589, AMS 5590 or another standard is required.
FAQ.03
Why does TiAlloy ask for machining allowance on round bar?
Machinists may have work hardening and tool wear to contend with on Alloy 718 machining inquiries. Extra stock may be needed for cleanup, and that requirement should be set before cutting.
FAQ.04
Can TiAlloy quote finished Inconel 718 bolts?
Fastener stock or raw material can be discussed with TiAlloy. If you are looking for finished bolting in accordance with a specification such as ASTM A1014/A1014M or SAE AS4877, that request will follow a separate quote path.
FAQ.05
Is Alloy 718 safe for hydrogen or sour-service oil and gas work?
No, not without review. NASA hydrogen work and ISO 15156-1:2020 show why H2S and hydrogen service need separate evaluation. Please submit the project standard, medium chemistry, temperature, pressure, approval rule and stress level.
FAQ.06
What documents should be requested with Inconel 718 suppliers?
Request the chemical analysis, mill test certificate, standard revision, heat number, certificate of conformity, inspection requirements, mechanical properties and packing list. Please include any required customer and compliance clauses early in your RFQ, particularly if the order is for aerospace or defense projects.




