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Torque parameter analysis of fasteners

The data focuses on recommended tightening torque for a standard ¼-20 UNC Grade 5 equivalent bolt (or similar high-strength condition) to provide a consistent baseline. Actual values depend on specific alloy condition, heat treatment, lubrication, and application standards (e.g., NASM, ASME).

Key Factors Influencing Torque:

  • Ultimate Tensile Strength (UTS): Primary driver for torque capacity.

  • Yield Strength: Determines clamp load before permanent deformation.

  • Material Ductility & Galling Tendency: Affects assembly behavior and may require lubricants or plating.

  • Modulus of Elasticity: Influences stiffness and load distribution.

  • Torque Formula (Simplified):T = K * d * F where T = Torque (lb-in or Nm), K = Torque coefficient (friction factor), d = Nominal diameter, F = Desired preload (clamp force). F is typically ~75% of proof load for critical joints.


Torque Data Comparison Table (Baseline: ¼-20 UNC Fastener)

Material (Common Name)Typical UTS (MPa)Typical Yield (MPa)Approx. Dry Torque (lbf-in)Approx. Dry Torque (N·m)Notes (Condition, Galling Risk, etc.)
Aluminum 7075-T657250395 - 10510.7 - 11.9High-strength Al; susceptible to stress corrosion.
PH 13-8 Mo (H1000)14801310240 - 26027.1 - 29.4Precipitation-hardening stainless; high strength.
17-4 PH (H900)13101170210 - 23023.7 - 26.0Common PH stainless; good strength.
A-286 (AMS 5731)1000690160 - 18018.1 - 20.3Austenitic superalloy; age-hardened.
Duplex Steel (2205)795550130 - 15014.7 - 17.0High strength & corrosion resistance.
Alloy 20 (Carpenter 20)620450100 - 12011.3 - 13.6Austenitic; good corrosion resistance.
310SS65531090 - 11010.2 - 12.4High-temperature austenitic stainless.
Nitronic 60 (Alloy 218)69038095 - 11510.7 - 13.0High galling resistance; work-hardens.
254 SMO750430115 - 13513.0 - 15.3Super-austenitic; high corrosion resistance.
AL-6XN745415115 - 13513.0 - 15.3Similar to 254 SMO.
Alloy 926 (UNS N08926)720420110 - 13012.4 - 14.7High Mo super-austenitic.
Inconel 71813801170220 - 24024.9 - 27.1Nickel superalloy; age-hardened.
Incoloy 9251050585170 - 19019.2 - 21.5Age-hardenable Ni-Fe alloy.
Monel K-5001100790175 - 19519.8 - 22.0Age-hardenable Ni-Cu alloy.
Hastelloy C-276790415120 - 14013.6 - 15.8Solution-strengthened; excellent corrosion resistance.
Nickel 20055024085 - 1009.6 - 11.3Commercially pure nickel; soft & ductile.
Nimonic 901250800200 - 22022.6 - 24.9Age-hardenable Ni-Cr-Co alloy.
Waspaloy1310810210 - 23023.7 - 26.0High-strength Ni superalloy.
MP35N (AMS 5844)15851170255 - 27528.8 - 31.1Ultra-high strength Co-Ni alloy.
MP15917901655290 - 31032.8 - 35.0Very high strength Co-Ni alloy.
Titanium Ti-6Al-4V (Grade 5)11701100190 - 21021.5 - 23.7High strength-to-weight ratio; galling risk.
Zirconium (R60702)53031085 - 1059.6 - 11.9Used in nuclear/chemical; low strength.
Tantalum (R05200)34517255 - 706.2 - 7.9Very ductile; low strength; corrosion resistant.
Molybdenum (Mo-1)965760155 - 17517.5 - 19.8Brittle at room temperature; high temp use.
Tungsten (W-1)1100965175 - 19519.8 - 22.0Extremely dense & hard; brittle.
Alloy 33062031090 - 11010.2 - 12.4High-temperature austenitic alloy.

Critical Considerations & Analysis

  1. Strength vs. Torque: There is a direct correlation between material yield strength and achievable clamp load/torque. MP159, MP35N, and high-strength Ni/Co superalloys (Waspaloy, Inconel 718) allow the highest torque values, followed by PH steels (17-4, PH 13-8) and Titanium. Pure/soft metals (Nickel 200, Tantalum, Zirconium) have the lowest torque ratings.

  2. Galling & Seizing (Critical for Assembly):

    • High Risk: Austenitic stainless steels (especially 300 series), Titanium, Aluminum, Nickel alloys, and Zirconium. These materials often require anti-gallant lubricants/coatings (e.g., molybdenum disulfide, copper-based, or proprietary dry films).

    • Lower Risk: Nitronic 60 is specifically designed for high galling resistance.

  3. Lubrication (Factor K): The torque values above assume a "dry" (unlubricated) condition with a torque coefficient K ~ 0.20. Using lubricant (e.g., oil, Molykote) can reduce K to ~0.14-0.16, reducing required torque by ~20-30% to achieve the same clamp load. Always follow specific fastener specifications.

  4. Temperature & Corrosion:

    • High-Temp Applications: Inconel, Incoloy, Nimonic, Waspaloy, Alloy 330, 310SS, and Molybdenum retain strength at elevated temperatures. Torque values drop at high temperature.

    • Corrosion Resistance: Hastelloy, Alloy 20, 254 SMO, AL-6XN, Tantalum, Zirconium are chosen for aggressive environments, not primarily for strength.

  5. Practical Recommendation: For critical applications (aerospace, nuclear, subsea), do not rely solely on generic torque tables. Use:

    • Engineering Standards: Refer to specific material/fastener specs (e.g., SAE AS8879 for Ti, MIL-HDBK-60).

    • Torque-Tension Testing: Empirical testing for the exact fastener system (material, plating, lubricant, hole condition) is ideal.

    • Direct Tension Indicating Methods: Use load washers, ultrasonic measurement, or turn-of-nut method for precision.

Torque parameter analysis of fasteners

Disclaimer: This data is for comparative and estimation purposes only. Always consult material certification data, RAYCHIN fastener manufacturer specifications, and applicable design codes for final torque values.

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