Question 7.7: A support beam for a conveyor system for a production line c...
A support beam for a conveyor system for a production line carries the loads shown in Figure 7–20. Support points are at points A and C. The 20 kN load at B and the 10 kN load at D are to be applied repeatedly many thousands of times as products are loaded and unloaded from the conveyor hangers. It has been proposed to use a 50 mm diameter circu- lar steel bar for the beam. Specify a suitable steel for the beam.

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Objective Specify a suitable steel. ‘
Given Loading pattern in Figure 7–20; loads are repeated.
Beam is to be circular, D = 50 mm.
Analysis Use the type B procedure given in this section.
Results Step 1. Figure 7–21 shows the completed shearing force and bending moment diagrams. The maximum bending moment is 2.00 kN · m at the support at C.
Step 2. Appendix A–1 gives the formula for S for a round bar.
S = πD³/32 = π(50 mm)³ /32 = 12 272 mm³
Step 3. Using Equation (7–5),
\sigma_{max} = \frac{M}{S} = \frac{2.0 kN·m}{12 272 mm^{3}} \times \frac{10^{3} mm}{m} \times \frac{10^{3} N}{kN}
\sigma_{max} = 163 N/mm² = 163 MPa
Step 4. We can use Table 7–1 to determine an appropriate formula for design stress. The steel selected should be highly ductile because of the repeated load. Then, we will use
TABLE 7–1 Design stress guidelines: Bending stresses. | ||
Manner of loading | Ductile material | Brittle material |
Static | \sigma_{d} = s_{y} /2 | \sigma_{d} = s_{u} /6 |
Repeated | \sigma_{d} = s_{y} /8 | \sigma_{d} = s_{u} /10 |
Impact or shock | \sigma_{d} = s_{y} /12 | \sigma_{d} = s_{u} /15 |
\sigma_{d} = s_{u} / 8
Step 5. Let \sigma_{max} = 163 MPa = \sigma_{d} = s_{u} / 8
Step 6. Solving for s_{u} gives
s_{u} = 8(\sigma_{max}) = 8(163 MPa) = 1304 MPa
Step 7. It was decided to use steel.
Step 8. Appendix A–10 lists several common steel alloys. From that table, we can select candidate materials that have good ductility and an ultimate strength of at least 1304 MPa. Four are listed as follows:
A–10 Typical properties of carbon and alloy steels .^{a} | ||||||
Ultimate | Yield | |||||
strength, s_{u} | strength, s_{y} | |||||
Material SAE no. | Condition^{b} | ksi | Mpa | ksi | Mpa | Percent elongation |
1020 | Annealed | 57 | 393 | 43 | 296 | 36 |
1020 | Hot rolled | 65 | 448 | 48 | 331 | 36 |
1020 | Cold drawn | 75 | 517 | 64 | 441 | 20 |
1040 | Annealed | 75 | 517 | 51 | 352 | 30 |
1040 | Hot rolled | 90 | 621 | 60 | 414 | 25 |
1040 | Cold drawn | 97 | 668 | 82 | 565 | 16 |
1040 | WQT 700 | 127 | 876 | 93 | 641 | 19 |
1040 | WQT 900 | 118 | 814 | 90 | 621 | 22 |
1040 | WQT 1100 | 107 | 738 | 80 | 552 | 24 |
1040 | WQT 1300 | 87 | 600 | 63 | 434 | 32 |
1080 | Annealed | 89 | 614 | 54 | 372 | 25 |
1080 | OQT 700 | 189 | 1303 | 141 | 972 | 12 |
1080 | OQT 900 | 179 | 1234 | 129 | 889 | 13 |
1080 | OQT 1100 | 145 | 1000 | 103 | 710 | 17 |
1080 | OQT 1300 | 117 | 807 | 70 | 483 | 23 |
1141 | Annealed | 87 | 600 | 51 | 352 | 26 |
1141 | Cold drawn | 112 | 772 | 95 | 655 | 14 |
1141 | OQT 700 | 193 | 1331 | 172 | 1186 | 9 |
1141 | OQT 900 | 146 | 1007 | 129 | 889 | 15 |
1141 | OQT 1100 | 116 | 800 | 97 | 669 | 20 |
1141 | OQT 1300 | 94 | 648 | 68 | 469 | 28 |
4140 | Annealed | 95 | 655 | 60 | 414 | 26 |
4140 | OQT 700 | 231 | 1593 | 212 | 1462 | 12 |
4140 | OQT 900 | 187 | 1289 | 173 | 1193 | 15 |
4140 | OQT 1100 | 147 | 1014 | 131 | 903 | 18 |
4140 | OQT 1300 | 118 | 814 | 101 | 696 | 23 |
5160 | Annealed | 105 | 724 | 40 | 276 | 17 |
5160 | OQT 700 | 263 | 1813 | 238 | 1641 | 9 |
5160 | OQT 900 | 196 | 1351 | 179 | 1234 | 12 |
5160 | OQT 1100 | 149 | 1027 | 132 | 910 | 17 |
5160 | OQT 1300 | 115 | 793 | 103 | 710 | 23 |
SAE 1080 OQT 700; s_{u} = 1303 MPa; 12% elongation
SAE 1141 OQT 700; s_{u} = 1331 MPa; 9% elongation
SAE 4140 OQT 700; s_{u} = 1593 MPa; 12% elongation
SAE 5160 OQT 900; s_{u} = 1351 MPa; 12% elongation
Step 9. For applications to beams carrying repeated loads, it is typical to use a medium carbon steel. Either the SAE 4140 or the SAE 5160 could be used. With 12% elongation, ductility should be adequate.
Comment Note in Appendix A–10 that SAE 4140 OQT 900 has an ultimate strength of 1289 MPa and 15% elongation. The strength is within 2% of the computed value. It may be suitable to specify this material to gain better ductility. A slight reduction in the design factor would result. Because the values in Table 7–1 are somewhat conservative, this would normally be justified. Alternatively, a larger diameter bar could be used resulting in a lower design stress. It may then be possible to use a lower cost steel.

