Page 456 - Wind Energy Handbook
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430                                                     COMPONENT DESIGN

               10 BS 436 (Appendix A) T–N curve   for case hardened gear tooth contact

           Torque/Endurance limit torque (BS436) or Torque/Torque at 10 7  cycles (ANSI/AGMA)  1  ANSI/AGMA T–N curve   (heavy dashed line)   for gear tooth contact stress
                  for case hardened gear tooth
                    bending (heavy line)
                                                 BS 436 (Appendix A) T–N curve
                                                   stress with no pitting allowed

                   for gear tooth bending
                       (light line)



                                                                   ANSI/AGMA T–N curve
                                                                     (light dashed line)







               0.1
                 1      10    100    1000   10000  100000  1000000  10000000  100000000 1000000000
                                           Endurance, N (cycles)
          Figure 7.27 Specimen Torque-endurance Curves for Gear Tooth Design under Variable
          Amplitude Loading
                                         "             # 1=m
                                           X    N i
                                    T 1 ¼         T m                          (7:49)
                                                    i
                                               N 1
                                            i
          where N i is the number of cycles at torque level T i , and torques less than T 1 are
          omitted from the summation. The number of cycles at the lower knee of the
                                                      6
          torque–endurance curve, N 1 , is always 3 3 10 cycles for tooth bending but is
          generally higher for contact stress, varying according to the material. Note that the
          slope index, m, of the torque–endurance curve for contact stress is half that of the
          contact stress–endurance curve because contact stress only increases as the square
          root of torque (Equation 7.46).
            Leaving braking loads out of consideration to begin with, the design infinite life
          torque will be equal to the rated torque if there are no power fluctuations above
          rated, because the number of gear tooth loading cycles at rated torque will be well
          above N 1 . For example, in the case of the 500 kW stall-regulated machine featured
          in Figure 7.24, the teeth on the critical pinion driven by the 30 r.p.m. low-speed
          shaft will experience 3 3 30 3 60 3 1050 3 20 ¼ 1:13 3 10 8  load cycles at rated
          torque over 20 years, assuming a first stage gear ratio of 3. On the other hand, for
          the 500 kW, two-bladed pitch-regulated machine, the power fluctuations above
          rated detailed in the Figure 7.24 load–duration curve result in a design infinite life
          torque for the first stage pinion tooth bending stress of 1.36 times the rated torque,
          with most of the damage coming from torques just above this value. (The first stage
          gear ratio is assumed to be three as before and the turbine rotational speed is taken
          as 40.4 r.p.m.) The design infinite life torque for tooth contact stress is only 1:17 3
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