Forgings, Fasteners, Boltings, Stud Bolts, Screws, Nuts
This specification covers forged carbon and alloy steel flanges intended primarily for petroleum and gas pipelines in areas subject to low ambient temperatures. Included are flanges to specified dimensions or to dimensional standards such as those MSS, ASME, and API specifications that are referenced in Section 2.
Supplementary requirements are provided for use when additional requirements are desired. These shall apply only when specified individually by the purchaser in the order.
Eight grades, four yield-strength classes, and three different notch toughness levels are included.
The availability of a particular size of flange of a specific grade and class is limited only by the capability of the composition to meet the specified mechanical property requirements. However, current practice normally limits the following:
Grade | Elements | |||||||||||||||||||||||
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C, max, % | Mn,% | P, max, % | S, max,% | Si, max, % | Cr,% | Ni,% | Mo,% | V,% | N, % | Cu, % | Nb, % | |||||||||||||
Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | Heat analysis | Product analysis | |
ASTM A707 L1 A | 0.20 | 0.23 | 0.60-1.50 | 0.55-1.60 | 0.030 | 0.035 | 0.030 | 0.040 | 0.35 | 0.37 | 0.30 max | 0.34 max | 0.40 max | 0.43 max | 0.12 max | 0.13 max | 0.05 max | 0.06 max | ... | ... | 0.40 max | 0.43 max | 0.02 max | 0.03 max |
ASTM A707 L2 A | 0.30 | 0.33 | 0.60-1.35 | 0.55-1.45 | 0.030 | 0.035 | 0.030 | 0.040 | 0.35 | 0.37 | 0.30 max | 0.34 max | 0.40 max | 0.43 max | 0.12 max | 0.13 max | 0.05 max | 0.06 max | ... | ... | 0.40 max | 0.43 max | 0.02 max | 0.03 max |
ASTM A707 L3 | 0.22 | 0.25 | 1.15-1.50 | 1.05-1.60 | 0.025 | 0.030 | 0.025 | 0.035 | 0.30 | 0.32 | 0.30 max | 0.34 max | 0.40 max | 0.43 max | 0.12 max | 0.13 max | 0.04-0.11 | 0.03--0.13 | 0.010-0.030 | 0.005-0.035 | 0.20 mine | 0.18 mine | 0.02 max | 0.03 max |
ASTM A707 L4 | 0.18 | 0.20 | 0.45-0.65 | 0.40-0.70 | 0.025 | 0.030 | 0.025 | 0.035 | 0.35 | 0.37 | 0.30 max | 0.34 max | 1.65-2.00 | 1.60-2.05 | 0.20-0.30 | 0.19-D.33 | 0.05 max | 0.06 max | ... | ... | 0.40 max | 0.43 max | 0.02 max | 0.03 max |
ASTM A707 L5 | 0.07 | 0.09 | 0.40-0.70 | 0.35-0.75 | 0.025 | 0.030 | 0.025 | 0.035 | 0.35 | 0.37 | 0.60-0.90 | 0.56-0.94 | 0.70-1.00 | 0.67-1.03 | 0.15-0.25 | 0.14-0.28 | 0.05 max | 0.06 max | ... | ... | 1.00-1.30 | 0.95-1.35 | 0.03 min | 0.02 min |
ASTM A707 L6 | 0.07 | 0.09 | 1.85-2.20 | 1.75-2.30 | 0.025 | 0.030 | 0.025 | 0.035 | 0.15 | 0.17 | 0.30 max | 0.34 max | 0.40 max | 0.43 max | 0.25--0.35 | 0.22--0.38 | 0.05 max | 0.06 max | ... | ... | 0.40 max | 0.43 max | 0.06-0.10 | 0.05-0.11 |
ASTM A707 L7 B | 0.20 | 0.22 | 0.90 max | 1.00 max | 0.025 | 0.030 | 0.025 | 0.035 | 0.35 | 0.37 | 0.30 max | 0.34 max | 3.2-3.7 | 3.18-3.82 | 0.12 max | 0.13 max | 0.05 max | 0.06 max | ... | ... | 0.40 max | 0.43 max | 0.02 max | 0.03 max |
ASTM A707 L8 | 0.20 | 0.22 | 0.20-0.40 | 0.15-0.45 | 0.020 | 0.025 | 0.020 | 0.025 | 0.35 | 0.37 | 1.50-2.00 | 1.44-2.06 | 2.8-3.9 | 2.68-3.97 | 0.40-0.60 | 0.35-0.65 | 0.05 max | 0.06 max | ... | ... | 0.40 max | 0.43 max | 0.02 max | 0.03 max |
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Property | Class 1 | Class 2 | Class 3 | Class 4 |
---|---|---|---|---|
Yield strengthA min, ksi [MPa] | 42 [290] | 52 [360] | 60 [415] | 75 [515] |
Tensile strength, min, ksi [MPa] | 60 [415] | 66 [455] | 75 [515] | 90 [620] |
Elongation in 2 in. or 50 mm, min, % | 22 | 22 | 20 | 20 |
Reduction of area, min, % | 40 | 40 | 40 | 40 |
Hardness, HBW | 149-207 | 149-217 | 156-235 | 179-265 |
Cv energy absorption,B,C min, avg, ft·lbf [J] | 30 [41] | 40 [54] | 50 [68] | 50 [68] |
Cv energy absorption,B,D min, ft·lbf [J] | 24 [33] | 32 [43] | 40 [54] | 40 [54] |
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After forging and before reheating for heat treatment, the forging shall be allowed to cool substantially below the transformation range. The method of cooling shall be such as to ensure against the development of cracks, flakes, etc.
All material shall be heat treated by annealing, normalizing, precipitation hardening, quenching-and-tempering, normalizing-and-tempering, normalizing-and-precipitation hardening, or quenching-and-precipitation hardening.
The procedures for the various heat treatments are as given in Specification A961/A961M except as defined in the following:
Precipitation Hardening-Consists of heating to a temperature between 1000 and 1250°F [538 and 677°C], holding at temperature for not less than 1⁄2 h, and then cooling at any convenient rate.
S1 | Ultrasonic Examination |
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S2 | Additional Tension and Impact Tests |
S3 | Carbon Equivalent |
S4 | Notch Toughness, 50 % Shear FATT Minimum |
S5 | Additional Ultrasonic Test Requirement |
S6 | Notch Toughness, Measurement, and Reporting of Percent Shear and Lateral Expansion |