Spur gears have no axial thrust in this model; helical gears add Fa = Ft*tan(beta).
Steady torque applied to the checked gear before service factor.
Operating pitch diameter of the checked gear.
Normal pressure angle. For a spur gear, this is the same as the transverse pressure angle.
Helix angle at the pitch cylinder. Hidden for spur gears.
Multiplier for shock, duty cycle and uncertainty. Forces are based on T x SF.
Rotational speed of the checked gear for pitch-line speed and power.
3.125 kN · 702.5 lbf
Tooth load from design torque and pitch diameter.
Ft = 2*Tdesign/d.
Also computed
1.178 kN · 264.7 lbf
Fr = Ft*tan(alpha_t).
0.8373 kN · 188.2 lbf
Helical thrust load from helix angle.
Fa = Ft*tan(beta). Spur gears return zero.
3.443 kN · 774 lbf
Vector sum of Ft, Fr and Fa.
3.339 kN · 750.7 lbf
sqrt(Ft^2 + Fr^2), useful for first-pass shaft bending.
Applied torque multiplied by service factor.
v = pi*d*n/60.
P = T*omega before service factor.
Higher helix angle increases thrust bearing load.
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