gearbox.standards.agma2101._strength#
Allowable stress adjustments of AGMA 2001-D04: Z_N, Y_N, C_H, K_R and K_T.
- RELIABILITY_FACTORS = {'fewer than 1 failure in 10': 0.85, 'fewer than 1 failure in 100': 1.0, 'fewer than 1 failure in 1000': 1.25, 'fewer than 1 failure in 10000': 1.5, 'fewer than 1 failure in 2': 0.7}#
Reliability factors
K_Rof table 11, by the number of failures allowed per 10^n units.
- pitting_stress_cycle_factor(gear, cycles)[source]#
Stress cycle factor
Z_Nof figure 17 (general application line).2.466 N^-0.056(nitrided:1.249 N^-0.0138) between 10^4 and 10^7 cycles, constant below 10^4, and1.4488 N^-0.023above 10^7. The lower edge of the shaded zone, used for critical service, has no formula in the standard and is not implemented.- Raises:
ValueError – If the gear is not made of steel.
- Return type:
- bending_stress_cycle_factor(gear, cycles)[source]#
Stress cycle factor
Y_Nof figure 18 (general application line).Through-hardened steels interpolate on the Brinell hardness between the 160 HB and 400 HB curves (clause 17.2): linearly in
ln Y_Nat 10^3 cycles againstln HB, then a straight line on log-log axes toY_N = 1.04at3 x 10^6cycles. Above that,1.3558 N^-0.0178.- Raises:
ValueError – If the gear is not made of steel.
- Return type:
- hardness_ratio_factors(transmission)[source]#
Hardness ratio factors
(C_H pinion, C_H wheel), AGMA 2001-D04 clause 14.C_Hof the pinion is 1. For the wheel:through-hardened pair (14.1):
1 + A (m_G - 1)withA = 0.00898 HB_P/HB_G - 0.00829for1.2 <= HB_P/HB_G <= 1.7(0 below, 0.00698 above);surface-hardened pinion against a through-hardened wheel of 180 to 400 HB (14.2):
1 + B (450 - HB_G)withB = 0.00075 exp(-0.0112 f_p),f_pbeing the roughnessRaof the pinion in microinches.Rais estimated asRz / 6(ISO 6336-2 note).