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    ASTM A1014/A1014M Bolting Specification

    Precipitation Hardening Bolting (UNS N07718) for High Temperature Service

    Scope

    ASTM A1014 / A1014M covers Precipitation Hardening Bolting (UNS N07718) for High Temperature Service. AS 7467 Bolts And Screws is also reffered for Nickel Alloy, UNS N07718 Tensile Strength 185 KSI [1275 MPa] Stress Rupture Rated Procurement Specification. Bolting material alloy shall be multiple-melted using consumable electrode practice in the remelt cycle or shall be induction melted under vacuum. If consumable electrode re-melting is not performed in vacuum, electrodes produced by vacuum induction melting shall be used. Fully heat treated bolting material shall meet the dimensional requirements of Specification B637 for UNS N07718. Headed bolting components such as bolts, studs, or screws with a body length three times the diameter of the component or longer shall be subjected to full size tensile test and shall conform to the tensile strength as per this specification. The microstructure of the bolting material shall be free of freckles, white spots, and Laves phases. Threads of bolting components may show evidence of cold working as a result of rolling. The average grain size shall be determined in accordance with Test Methods E112 and found to be ASTM No. 5 or finer. Up to 20 % of the structure may have a grain size as large as a No. 3 due to the presence of non-crystallized grains. Bolting components produced from forgings shall exhibit continuous flow lines in the threads and in any shank to head or fillet and/or bearing surface areas.

    ASTM A1014/A1014M Chemical Requirements

    Element UNS N07718 ( Formerly Grade 718)
    C, max. 0.08
    Mn, max. 0.35
    Si, max. 0.35
    P, max. 0.015
    S, max. 0.015
    Cr 17.0-21.0
    Co, max.A 1.0
    Mo 2.80-3.30
    Nb + 4.75-5.50
    Ta . . .
    Ti 0.65-1.15
    Al 0.20-0.80
    B, max. 0.006
    FeB Remainder
    Cu, max. 0.30
    NiC 50.0-55.0
    • (A) If determined.
    • (B) Determined arithmetically by difference.
    • (C) Nickel + Cobalt.

    ASTM A1014/A1014M Mechanical Properties

    Properties  Room Temperature  Elevated  Temperature
    Tensile strength, min, ksi [Mpa] 185 [1275] 1200 [650]
    Yield Strength, min, ksi, [Mpa] 0.2 % offset 150 [1035] 125 [860]
    Elongation in 2 in., or 50 mm (or 4D) min % 12 12
    Reduction of area, min, % 15 15
    Hardness, Brinell 331-444 ... 

    ASTM A1014/A1014M Supplementary Requirements

    S1: Protective Atmosphere

    Heat treatment for high-temperature fasteners must be performed under a suitable protective atmosphere, such as a vacuum or inert gas environment, to maintain surface integrity. This requirement prevents the formation of heavy oxidation scales and avoids the depletion of reactive elements like chromium, aluminum, and titanium at the fastener's surface. By eliminating "denuded zones," S1 ensures the material retains its full precipitation-hardening potential and corrosion resistance across the entire cross-section.

    S2: Cleaning

    Supplementary requirement S2 mandates advanced precision cleaning of all bolting materials to remove industrial lubricants, oils, and metallic residues prior to heat treatment. In nickel-based superalloys like Inconel 718, surface contaminants can cause liquid metal embrittlement or severe intergranular attack when exposed to solution treatment temperatures as high as 1850°F(1010°C). Implementing S2 is essential for ensuring long-term structural reliability and preventing premature stress-rupture failure in aggressive service environments.

    S3: Fillet Rolling

    S3 specifies the cold-working of the underhead fillet radius to significantly enhance the fatigue life of bolts and screws. By applying high pressure to the radius, this process induces beneficial residual compressive stresses that effectively delay the initiation and propagation of fatigue cracks. Fillet rolling is a critical quality enhancement for fasteners subjected to high-frequency vibration, cyclic thermal loading, and mechanical stress concentrations in aerospace and turbine systems.

    S4: Forged Heads

    Under supplementary requirement S4, fastener heads must be formed using a forging process rather than being machined from bar stock. Forging ensures a continuous internal grain flow that follows the geometric contour of the head-to-shank transition, providing superior shear strength and resistance to "head-popping" failures. This metallurgical reinforcement is vital for safety-critical components used in high-vibration and high-impact industrial applications.

    S5: Marking

    S5 provides stringent protocols for the permanent marking and traceability of bolting components throughout the supply chain. Fasteners must be marked with manufacturer identification and grade symbols on the head or stud ends to allow for rapid verification of material and heat lot data. Standardized marking is a fundamental safety measure that ensures high-strength superalloys are correctly identified and never interchanged with lower-grade materials in critical high-temperature service.

    S6: Thread Rolling

    Supplementary requirement S6 governs the parameters for thread rolling, requiring that threads be cold-formed specifically before the final precipitation heat treatment. Cold rolling displaces material to create a high-strength thread profile with improved grain density and superior surface finishes in the thread roots. By performing rolling prior to aging, the fastener benefits from the full strength development of the subsequent precipitation cycle while maintaining the structural advantages of the cold-formed threads.