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                                                                                             Load and Stress Analysis  145
                                     3–128     Repeat Prob. 3–126 with a bend radius of  in.
                                                                              1
                                                                              4
                                     3–129     The cast-iron bell-crank lever depicted in the figure is acted upon by forces F 1 of 2.4 kN and F 2
                                               of 3.2 kN. The section A–A at the central pivot has a curved inner surface with a radius of
                                               r i = 25 mm. Estimate the stresses at the inner and outer surfaces of the curved portion of the lever.
                                                  F
                                                   1
                                                            200
                                                                                              Nylon bushing
                                                                        60°               87
                                                                                 25
                                                                    A
                                  Problem 3–129                                                     9
                                                           A
                                                    25 R.
                                                                    150                              31
                                                                                          28
                                                                                          47
                                                                   F 2
                                                                                        Section A–A
                                                                      Dimensions in mm
                                                                              3
                                     3–130     The crane hook depicted in Fig. 3–35 has a -in-diameter hole in the center of the critical section.
                                                                              4
                                               For a load of 6 kip, estimate the bending stresses at the inner and outer surfaces at the critical section.
                                     3–131     An offset tensile link is shaped to clear an obstruction with a geometry as shown in the figure. The
                                               cross section at the critical location is elliptical, with a major axis of 3 in and a minor axis of 1.5 in.
                                               For a load of 20 kip, estimate the stresses at the inner and outer surfaces of the critical section.
                                                                 12-in R.


                                  Problem 3–131                    9 in






                                     3–132     A cast-steel C frame as shown in the figure has a rectangular cross section of 1.25 in by 2 in, with
                                               a 0.5-in-radius semicircular notch on both sides that forms midflank fluting as shown. Estimate A,
                                               r c , r n , and e, and for a load of 2000 lbf, estimate the inner and outer surface stresses at the throat
                                               C. Note: Table 3–4 can be used to determine r n for this section. From the table, the integral

                                                dA/r can be evaluated for a rectangle and a circle by evaluating A/r n for each shape [see

                                               Eq. (3–64)]. Subtracting A/r n of the circle from that of the rectangle yields  dA/r for the C
                                               frame, and r n can then be evaluated.

                                                                          0.5-in R.

                                                       4.5 in
                                               2000 lbf                    1.25 in
                                  Problem 3–132
                                                         1.25-in R.

                                                                           0.5 in
                                                              0.5 in
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