Products/ASTM A193/A193M-26

MATERIAL DATA · COLD FORMING

B8MLCuN / B8MLCuNA Bolting Material

Standard-reference composition and finished-component requirements for B8MLCuN / B8MLCuNA Bolting Material. Product form, Class, heat treatment and acceptance conditions require separate confirmation; this reference does not establish actual supply or measured heat results.

Supply and technical review · Creation Group accepts supply and technical review enquiries for this product. Dimensions, delivery condition, quantity and inspection documents are confirmed in the order technical agreement after review.

01Applicable standardASTM A193/A193M-26
02Material gradeB8MLCuN / B8MLCuNA
03Product formhigh-temperature and high-pressure bolting material
04Delivery informationTo be confirmed against the order technical requirements

Material technical data

Only data directly related to this material is shown here. Inspection, equipment, process and packaging information is linked separately.

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ASTM A193/A193M-26 composition requirements and conditions

Standard reference requirements compiled from ASTM A193/A193M-26. Raw-material composition and the Class, heat treatment and performance conditions of finished components require separate confirmation; these are not actual supply or measured heat results.

Composition: Table 1, physical page 4; mass fraction wt%. Values are upper limits unless ranges, minimum values or conditional requirements are stated separately.

ElementRequirement
C≤ 0.020
Mn≤ 1.00
P≤ 0.030
S≤ 0.010
Si≤ 0.80
Cr19.5—20.5
Ni17.5—18.5
Mo6.0—6.5
Cu0.50—1.00
NbNot specified (must not be assumed 0)
TiNot specified (must not be assumed 0)
VNot specified (must not be assumed 0)
AlNot specified (must not be assumed 0)
N0.18—0.25

Product-analysis tolerances are separate from the base composition ranges; intentional additions of Bi, Se, Te and Pb are prohibited.

Product-analysis tolerances (wt%, Table 1; must not be added directly to the base composition ranges)
ElementDeviation
C0.005
Mn0.03
P0.005
S0.002
Si0.05
Cr0.20
Ni0.15
Mo0.10
CuNot listed in the original table (do not enter 0)
NbNot listed in the original table (do not enter 0)
TiNot listed in the original table (do not enter 0)
VNot listed in the original table (do not enter 0)
AlNot listed in the original table (do not enter 0)
N0.02

Product-analysis tolerances are separate from the tabulated requirements. For the same element in the same heat, deviations must not occur both above and below the range. Unless otherwise stated, maximum values allow upward deviations only, ranges allow upward or downward deviations, and minimum values allow downward deviations only. Tolerances must not be added to the tabulated ranges in advance.

Customary-unit properties (Table 2)

Under 1.6, customary units apply unless the order or contract specifies the metric M edition. Under 1.7, the two unit systems are used independently and must not be mixed or combined through conversion. Properties are room-temperature requirements after the corresponding heat treatment; the specific Class, product form, specimen and order require separate confirmation.

GradeClassDiameter conditionHeat treatment / minimum tempering temperatureRm≥ ksiRp0.2≥ ksiA4D≥ %Z≥ %Maximum hardnessFootnotePhysical page
B8MLCuNA1AAll diametersCarbide solution treatment in the finished condition75303050192 HBW or 90 HRB6
B8MLCuN1B/1DAll diametersCarbide solution treatment80353040223 HBW or 96 HRBC6
B8MLCuN2Up to ¾ inCarbide solution treatment and strain hardening110951545321 HBW or 35 HRCB,D7
B8MLCuN2Over ¾ up to and including 1 inCarbide solution treatment and strain hardening100802045321 HBW or 35 HRCB,D7
B8MLCuN2Over 1 up to and including 1¼ inCarbide solution treatment and strain hardening95652545321 HBW or 35 HRCB,D7
B8MLCuN2Over 1¼ up to and including 1½ inCarbide solution treatment and strain hardening90503045321 HBW or 35 HRCB,D7
  • B: Class1 is solution treated; 1A is solution treated in the finished condition; 2 is solution treated and strain hardened. Strain-hardened austenitic steel over ¾ in may have nonuniform properties across the section.
  • C: A maximum hardness of 241 HBW (100 HRB) is permitted for diameters up to ¾ in, only for rows marked C.
  • D: For diameters of 1½ in and above, core properties may be lower than the reported test values measured at 1/2 of the radius.

Metric properties (Table 3)

Under 1.6, customary units apply unless the order or contract specifies the metric M edition. Under 1.7, the two unit systems are used independently and must not be mixed or combined through conversion. Properties are room-temperature requirements after the corresponding heat treatment; the specific Class, product form, specimen and order require separate confirmation.

GradeClassDiameter conditionHeat treatment / minimum tempering temperatureRm≥ MPaRp0.2≥ MPaA4D≥ %Z≥ %Maximum hardnessFootnotePhysical page
B8MLCuNA1AAll diametersCarbide solution treatment in the finished condition5152053050192 HBW or 90 HRB8
B8MLCuN1B/1DAll diametersCarbide solution treatment5502403040223 HBW or 96 HRBC8
B8MLCuN2Up to M20Carbide solution treatment and strain hardening7606551545321 HBW or 35 HRCB,D8
B8MLCuN2Over M20 up to and including M24Carbide solution treatment and strain hardening6905502045321 HBW or 35 HRCB,D8
B8MLCuN2Over M24 up to and including M30Carbide solution treatment and strain hardening6554502545321 HBW or 35 HRCB,D8
B8MLCuN2Over M30 up to and including M36Carbide solution treatment and strain hardening6203453045321 HBW or 35 HRCB,D8
  • B: Class 1 is solution treated; 1A is solution treated in the finished condition; 2 is solution treated and strain hardened. Strain-hardened austenitic steel over M20 may have nonuniform properties across the section.
  • C: A maximum hardness of 241 HBW (100 HRB) is permitted for diameters up to M20, only for rows marked C.
  • D: For diameters of M38 and above, core properties may be lower than the reported test values measured at 1/2 of the radius.

Product form, heat treatment and inspection limitations

  • 6.2.1: Class 1, 1B, 1C (B8R/B8S only), and 2, 2B, 2C may apply to bar, wire and finished bolting components. Class 1A (all grades) and 1C (B8RA/B8SA only) apply only to finished bolting components. A finished-component Class must not be directly assigned as a raw-material wire Class.
  • 6.2.1, 6.2.3: Class 1D applies to bar, wire and finished components machined directly from them without further hot or cold working. Hot-rolled/forged bars of the specified grades must be rapidly cooled immediately while above 954°C, and Class 1D service temperature must be below 454°C (the 454°C endpoint is excluded). This process description does not establish that arbitrary cold-drawn wire meets 1D.
  • 6.2.4: Class 1A and the B8RA/B8SA grades of 1C require carbide solution treatment of finished components after all rolling, forging, heading and thread cutting/rolling have been completed. This does not apply to initial raw material such as bar.
  • 6.2.5: Class 2, 2B, 2C require carbide solution treatment followed by strain hardening to achieve the corresponding properties. Grade or composition alone cannot establish compliance with these Classes.
  • 9.1.1: Table 2/3 tensile requirements apply at room temperature after heat treatment. Strain-hardened stainless steel components (Class 2/2B/2C) are tested full-size after strain hardening. Where equipment capacity is insufficient, components over 1.500 in. in diameter may be tested using machined specimens. If full-size and specimen results conflict, the full-size results govern. The original dimensional condition is stated only in customary units; no metric endpoint is invented.
  • 9.1.2, 12.1.3: Applicable headed components also require full-size wedge-load testing. The minimum wedge tensile load is calculated from the specified tensile strength and thread stress area. Units: ksi×in² gives kip (×1000 gives lbf); MPa×mm² gives N (÷1000 gives kN). Unnormalized products must not be labelled directly as lbf or kN. Verify the stress area under A962/A962M. Material-specimen properties do not replace applicable finished-component testing; confirm the applicable head type, size and length under 12.1.3.
  • 9.2.1: Hardness requirements follow Table 2/3, with testing under A962/A962M or F606/F606M. A tabulated maximum hardness does not establish that finished-product hardness testing has been completed.

Contact: website@chqwire.net. This information is for technical material-selection reference only; it is not a quotation, contractual guarantee or heat-specific quality certificate. The applicable standard, order and material certificate govern.

Application and ordering note

Chemical composition, mechanical properties, delivery condition and other technical requirements are subject to the currently applicable standard edition, customer drawings and the order technical agreement. Website information does not replace formal quality certification documents.

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Carbon equivalent calculator — B8MLCuN / B8MLCuNA Bolting Material

Basis: ASTM A193/A193M-26

Composition used for calculation and applicability: Carbon-equivalent calculation has not yet been fully verified

Carbon-equivalent calculation has not yet been fully verified

A stated upper limit means 0 to that limit. A lower limit alone does not define an upper bound. Missing elements are unknown, not zero. Standard-limit combinations are not measured heat results.

Carbon equivalent supports weldability assessment; it does not approve cold heading, fastener strength or a welding procedure. These formulas do not directly apply to stainless steels, cast irons or non-ferrous metals.

Method reference: TWI

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Material reference data

Same-grade reference does not establish standard equivalence, supply or substitution approval.

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