High strength
High tensile, fatigue, creep and rupture capability after the specified aging treatment.
Age-hardenable nickel-chromium superalloy
A precipitation-hardenable nickel alloy widely specified for high strength, fatigue resistance, creep performance and weldability in aerospace and energy components.
Representative product-form image. Confirm actual surface, dimensions and condition with the quotation.Material overview
Alloy 718 develops strength through controlled solution treatment and aging. Niobium, titanium and aluminum form strengthening precipitates, while chromium, nickel and molybdenum contribute corrosion resistance and elevated-temperature performance.
High tensile, fatigue, creep and rupture capability after the specified aging treatment.
Noted for resistance to post-weld cracking compared with many other precipitation-hardened superalloys.
Mechanical properties depend strongly on solution and aging practice, section size and product specification.
Technical reference
Values below are published reference limits. The purchase order, applicable specification and mill test certificate control the supplied material.
| Element | Published limit |
|---|---|
| Nickel + cobalt | 50.00-55.00 |
| Chromium | 17.00-21.00 |
| Iron | Balance |
| Niobium + tantalum | 4.75-5.50 |
| Molybdenum | 2.80-3.30 |
| Titanium | 0.65-1.15 |
| Aluminum | 0.20-0.80 |
| Cobalt | 1.00 max |
| Carbon | 0.08 max |
| Manganese | 0.35 max |
| Silicon | 0.35 max |
| Copper | 0.30 max |
Technical reference: manufacturer technical bulletin. Typical data is for material selection only and is not a design guarantee.
Common specifications
Specification editions and permitted product forms change. Send the exact standard, revision and condition shown on your drawing or material list.
| Product or requirement | Common reference |
|---|---|
| Bar and forgings | ASTM B637 |
| Plate, sheet and strip | ASTM B670 |
| Sheet, strip and plate | AMS 5596 |
| Bar and forgings | AMS 5662 / AMS 5663 |
Availability is subject to grade, size, quantity, condition, certification and mill route. No standard listed here confirms stock.
Coordinated stock or mill production is checked against the exact grade, form, size and condition in the RFQ.
MOQ varies by product form, size and source route and is stated in the order-specific quotation.
MTC scope, EN 10204 type when applicable, inspection records and third-party witnessing must be agreed before order placement.
Lead time, Incoterm, loading port and packing are confirmed after specification, quantity and destination review.
Application areas
Final material selection belongs to the buyer's qualified engineer and must consider temperature, stress, fabrication, corrosion medium and governing code.
Turbine disks, rings, casings and formed sheet-metal components.
Liquid-fueled rocket components and high-strength structures.
High-load bolts, fasteners and instrumentation components.
Rotating and pressure components requiring strength plus corrosion resistance.
RFQ checklist
Clear specifications shorten material matching and reduce repeated email clarification. Review our MTC and inspection process when defining your order documentation.
Inconel 718, UNS N07718, ASTM/AMS/EN standard and required revision.
Round bar, forged bar, plate, sheet, strip and cut blanks. Include thickness, width, length, diameter and tolerances.
Mill annealed, solution treated or solution treated and aged to the cited specification
Pieces, kilograms or total project quantity, plus any trial-order requirement.
MTC type, chemistry, mechanical tests, NDT, dimensional report and third-party inspection.
Destination country or port, required date, packing and Incoterm preference.
Fast alloy inquiry
We will review product form, specification, condition, certification and delivery requirements before preparing a targeted quotation.
Buyer questions
Quick answers for initial sourcing. Confirm critical engineering requirements against the governing specification.
Yes for full precipitation-hardened strength. Buyers should specify the required solution and aging condition or the exact AMS/ASTM requirement.
It is commonly purchased as bar or cut blanks. Machining allowance, condition, ultrasonic testing and grain-flow requirements should be stated.
Product form, melt route, heat treatment, testing, aerospace approvals, dimensions and certification requirements can materially change cost and lead time.
Related grades
Review our Alloy 625 vs 718 buyer comparison, then confirm the specified alloy and condition with your engineer. Related grades are not automatically interchangeable.
Related sourcing
Use the related product and technical pages below to match the correct product form, specification and purchase condition.
Specify condition, dimensions, inspection, documents and packing.
Specify the flat-product standard, tolerances, condition, inspection and packing.
Specifications, product-form guidance and RFQ details.
Grade identity, specifications and product-form guidance.
Compare two nickel alloy families before material selection.
Product-specific quotation
Include the product form, dimensions, quantity, standard, condition and destination. Attach a drawing or RFQ when needed. Availability, documents and lead time are confirmed after review.
Technical resources
Review UNS guides, alloy comparisons and RFQ checklists before finalizing the purchase specification.
Browse Technical ResourcesINCONEL, INCOLOY and MONEL are trademarks of the Special Metals Corporation group of companies. Laixi Special Steel is not presented as the trademark owner. Material data is informational; final supply is governed by the confirmed purchase specification and MTC.