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Aerospace Spot Weld Shear Strength: titanium alloy

titan ftu below100 t0040 to titan ftu below100 t0160

Design-allowable shear load per spot (lbs) for resistance spot welds per MIL-HDBK-5J Section 8.2.2.3 and MIL-W-6858. Indexed by material family (aluminum alloy, steel/nickel/cobalt alloy, magnesium alloy, titanium alloy), parent metal Ftu range (ksi), and sheet thickness (in). Tensile allowable is 25% of shear strength. Covers thicknesses 0.020–0.160 in. No filler metal — allowable is empirical load-per-spot based on sheet thickness and parent metal ultimate tensile strength.

Aerospace Engineeringmaterial family: titanium alloy7 rowsPage 3 of 3
material familyrecord iddesign shear strength lbs (lbf)material ftu range ksisheet thickness in (in)standardtensile allowable lbs (lbf)tensile allowable noteweld spec
titanium alloytitan ftu below100 t0040388below 1000.04MIL-HDBK-5J Section 8.2.2.39725% of shear strengthMIL-W-6858
titanium alloytitan ftu below100 t0050520below 1000.05MIL-HDBK-5J Section 8.2.2.313025% of shear strengthMIL-W-6858
titanium alloytitan ftu below100 t0063700below 1000.063MIL-HDBK-5J Section 8.2.2.317525% of shear strengthMIL-W-6858
titanium alloytitan ftu below100 t0080920below 1000.08MIL-HDBK-5J Section 8.2.2.323025% of shear strengthMIL-W-6858
titanium alloytitan ftu below100 t01001,200below 1000.1MIL-HDBK-5J Section 8.2.2.330025% of shear strengthMIL-W-6858
titanium alloytitan ftu below100 t01251,540below 1000.125MIL-HDBK-5J Section 8.2.2.338525% of shear strengthMIL-W-6858
titanium alloytitan ftu below100 t01602,000below 1000.16MIL-HDBK-5J Section 8.2.2.350025% of shear strengthMIL-W-6858

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