Nickel-chromium-molybdenum-columbium alloy rod and bar
Standard specification for precipitation-hardening nickel alloy rod and bar for high-temperature service.
Nickel Alloy — Industrial Product
Inconel 718 nickel alloy bars and rods supplied to ASTM B637 / AMS 5662 / AMS 5663 for high-temperature fasteners, aerospace and gas turbine components.
概述
Inconel 718 Bars & Rods combine a nickel-chromium matrix with substantial niobium, molybdenum and titanium additions to deliver high strength through precipitation (age) hardening. In the solution-annealed-plus-aged condition, the alloy achieves tensile strength above 1275 MPa while retaining useful creep resistance up to approximately 700 °C. It is supplied in round, square and hex bar form per ASTM B637 / ASME SB637 and the corresponding aerospace specifications AMS 5662, AMS 5663 and AMS 5664. The combination of high strength, fatigue resistance and thermal stability makes the bar suited to high-temperature fasteners, gas turbine and aerospace components, rocket and missile parts, high-strength shafts, valve and wellhead components for oil & gas, and tooling where sustained mechanical loading at elevated temperature is required. Each delivery is supported by mill test certification per EN 10204 3.1 and full traceability of heat number, chemical analysis and heat-treatment lot.
核心特性
典型应用
技术规格
本节数据对应所适用产品标准的相关参数,可直接用于询价与审批文件。
Final supply is confirmed against the project drawing, purchase agreement and the mill test certificate.
Reference: Per ASTM B637 / AMS 5662 / AMS 5663 for Inconel 718 (UNS N07718).
Reference: Room-temperature values per AMS 5662 (annealed) and AMS 5663 (annealed + aged). Elevated-temperature and stress-rupture values are typical and provided for design reference only.
Reference: Typical material values for Inconel 718 nickel alloy.
参考体系
适用的产品、尺寸与检验标准应在采购技术规范中一并确认。
Standard specification for precipitation-hardening nickel alloy rod and bar for high-temperature service.
ASME counterpart of ASTM B637 for pressure vessel and high-temperature applications.
Aerospace Material Specification for Inconel 718 corrosion and heat-resistant steel bar and forging stock in the annealed condition.
Aerospace Material Specification for Inconel 718 precipitation-hardened bar in the annealed + aged condition (Rm >= 1275 MPa).
Aerospace Material Specification for Inconel 718 bar and forging stock produced by vacuum induction melting plus consumable electrode remelting for premium-grade applications.
European reference for high-temperature steel and nickel alloy bar stock used for bolting and fastener manufacture.
Industry reference for Inconel 718 bar used in wellhead and Christmas tree equipment, including sour-service environments per NACE MR0175.
Defines inspection document types such as 3.1 and 3.2 for metallic product delivery.
供应能力
从定制尺寸、精密规格到热处理、表面精加工及产品专用工艺,Wayland 根据您的具体需求协调定制化供应解决方案。
按订单要求提供定尺切割和定制切割。
在产品和轧机能力允许的范围内,提供非标尺寸、公差和尺寸组合。
针对更严格的公差要求进行精密定径和尺寸控制。
按需进行冷拔、冷定径及其他冷加工工艺。
依据材料、规格及适用标准进行热处理。
依据产品、规格及应用要求进行表面处理与精整。
依据产品与应用要求进行涂层、电镀及其他表面防护处理。
依据图纸或订单要求进行弯曲、成形及其他形状加工。
热锻与冷锻,适用于大截面棒材和定制形状。
按需进行车削、钻孔、铣削及其他机加工。
精密无心磨削,提供严格的直径公差和改善的表面光洁度。
按适用标准和客户规范进行力学、化学及无损检测。
定制服务
可根据项目规格提供定制尺寸、长度、表面状态、管端处理及检验要求。最终供应能力将依据牌号、规格范围和适用标准,在每次询价时确认。
质量
检验与文档流程依据适用产品标准及项目规范要求执行。
文档
文档
文档
文档
选型
一份准备充分的规格书,是抵御反复澄清沟通最有效的防线。
根据使用工况、性能要求和适用标准选择材料牌号。
明确所需尺寸、表面状态、热处理状态及交货要求。
注明适用的产品标准、尺寸标准及适用的项目规范。
下单前确认检验、试验、认证及文件提交要求。
采购规范示例
A complete specification suitable for enquiry, covering product, technical requirements, certification and delivery terms.
物流
从工厂发运到目的港的每个环节均由指定货代协调配合,并按采购规范提供完整单据。
适用于出口的包装方案,并提供表面与边角防护。
根据产品形态与运输方式,捆扎、包覆或装箱。外表面使用耐候材料保护,端部与边角加装防护以避免运输损伤。
标准尺寸采用整箱装载;超大件货物安排散货出运。
通过指定货代进行集装箱装载。LCL 拼箱及超出集装箱尺寸的货物,依据工厂发运计划协调安排。
商业发票、装箱单与原产地证书。
工厂单据随货物同行。按采购规范提供 EN 10204 3.1 / 3.2 证书及第三方检验报告。
默认采用海运;可应要求安排其他运输方式。
可采用 FCL / LCL 集装箱运输,或针对超大尺寸货物安排散货出运。物流通过指定货代协调。
可提供 FOB · CFR · CIF · FCA · EXW 多种贸易条款。
适用《2020 年国际贸易术语解释通则》。装货港:上海 / 宁波 / 深圳。最终目的地与贸易条款按询盘确认。
常见问题
大多数询价最终归结为一组反复出现的技术问题。
Inconel 718 (UNS N07718 / NiCr19Fe19Nb5Mo3 / 2.4668) is a precipitation-hardening nickel-chromium alloy containing substantial niobium, molybdenum and titanium. In the aged condition it achieves tensile strength above 1275 MPa and retains useful creep resistance up to approximately 700 °C.
Both are nickel-chromium alloys. Inconel 625 is solid-solution strengthened (not age-hardenable) and is selected primarily for corrosion resistance in chemical, marine and offshore service. Inconel 718 is precipitation hardened and is selected for high strength at elevated temperature in aerospace, gas turbine and high-temperature fastener applications.
Industrial reference is ASTM B637 / ASME SB637. Aerospace references include AMS 5662 (annealed), AMS 5663 (annealed + aged) and AMS 5664 (premium grade). EN 10269 is the European reference for high-temperature fastener stock. API 6A covers Inconel 718 for oil & gas wellhead equipment.
Standard delivery is solution annealed (AMS 5662) for components that will be machined before final aging, or solution annealed plus precipitation aged (AMS 5663) for finished parts requiring full high-temperature strength. Aging is typically 720 °C / 8 h + furnace cool to 620 °C / 8 h, per AMS 2774.
Round bar is supplied from approximately 6 mm up to 350 mm. Smaller sizes are typically cold drawn or centerless ground, larger sizes are hot rolled or forged. Square, hex and flat sections are available on request.
Inconel 718 is suitable for continuous service up to approximately 700 °C. Above this temperature, microstructural coarsening reduces long-term strength. For sustained service above approximately 700 °C, Waspaloy, Rene 41 or Inconel 740H are typical alternatives.