(GAPmax) Maximum Gap: | 0.750 | | in. | (GAPmin) Minimum Gap: | 0.437 | | in. | (Pg) Theoretical Thrust Load Capacity - Groove Yield: Notes: Yield Strength of Groove Material (Ys): 45,000 psi. Calculated using a safety factor (K) of 4
Equation: Pg = [ B * d * Ys * pi ] / K = [ (2.000 in.) * (0.045 in.) * (45,000 psi) * 3.14 ] / 4 | 3,179 | | lbs. | | (Pr) Theoretical Thrust Load Capacity - Ring Shear: Notes: Ring Material: Carbon Spring Steel (SAE 1060-1095). Shear Strength of Ring Material (Ss): 138,000 psi. Calculated using a safety factor (K) of 3
Equation: Pr = [ B * t * Ss * pi ] / K = [ (2.000 in.) * (0.042 in.) * (138,000 psi) * 3.14 ] / 3 | 12,132 | | lbs. | | Industry Equivalent Part Number(s): ND-200 | | |
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