A large electrical transformer is to be suspended from a roof truss of a building. The total weight of the transformer is 32 000 lb. Design the means of support.
A large electrical transformer is to be suspended from a roof truss of a building. The total weight of the transformer is 32 000 lb. Design the means of support.
Objective
Design the means of supporting the transformer.
Given
The total load is 32 000 lb. The transformer will be suspended below a roof truss inside a building. The load can be considered to be static. It is assumed that it will be protected from the weather and that temperatures are not expected to be severely cold or hot in the vicinity of the transformer.
Basic Design Decisions
Two straight, cylindrical rods will be used to support the transformer, connecting the top of its casing to the bottom chord of the roof truss. The ends of the rod will be threaded to allow them to be secured by nuts or by threading them into tapped holes. This design example will be concerned only with the rods. It is assumed that appropriate attachment points are available to allow the two rods to share the load equally during service. However, it is possible that only one rod will carry the entire load at some point during installation. Therefore, each rod will be designed to carry the full 32 000 lb.
We will use steel for the rods, and because neither weight nor physical size is critical in this application, a plain, medium-carbon steel will be used. We specify AISI 1040 cold-drawn steel. From Appendix 3. we find that it has a yield strength of 71 ksi and moderately high ductility as represented by its 12% elongation. The rods should be protected from corrosion by appropriate coatings.
The objective of the design analysis that follows is to determine the size of the rod.
Analysis
The rods are to be subjected to direct normal tensile stress. Assuming that the threads at the ends of the rods are cut or rolled into the nominal diameter of the rods, the critical place for stress analysis is in the threaded portion.Use the direct tensile stress formula. Equation (3_1): σ = F/A. We will first compute the design stress and then compute the required cross-sectional area to maintain the stress in service below that value. Finally, a standard thread will be specified from the data in Chapter 18 on fasteners.
Case CI from Section 5_9 applies for computing the design stress because the rod is made from a ductile steel and it carries a static load. The design stress is
\sigma _{d}=s_{y}/NWe specify a design factor of N = 3, because it is typical for general machine design and because there is some uncertainty about the actual installation procedures that may be used (see Section 5_7). Then
\sigma_{d}=s_{y} / N=(71000 \mathrm{psi}) / 3=23667 \mathrm{psi}Results
In the basic tensile stress equation, σ = F/A. we know F. and we will let \sigma =\sigma _{d}. Then the required cross-sectional area is
A=F / \sigma_{d}=(32000 \mathrm{lb}) /\left(23667 \mathrm{lb} / \mathrm{in}^{2}\right)=1.35 \mathrm{in}^{2}A standard size thread will now be specified from the data in Chapter 18 on fasteners. You should be familiar with such data from earlier courses. Table A2_2(b)
Coarse threads: UNC | Fine threads: UNF | ||||
Size | Basic major diameter, D (in) |
Threads per inch, n |
Tensile stress area (in^{2}) |
Threads per inch, n |
Tensile stress area (in^{2}) |
1/4 | 0.2500 | 20 | 0.0318 | 28 | 0.0364 |
5/16 | 0.3125 | 18 | 0.0524 | 24 | 0.0580 |
3/8 | 0.3750 | 16 | 0.0775 | 24 | 0.0878 |
7/16 | 0.4375 | 14 | 0.1063 | 20 | 0.1187 |
1/2 | 0.5000 | 13 | 0.1419 | 20 | 0.1599 |
9/16 | 0.5625 | 12 | 0.182 | 18 | 0.203 |
5/8 | 0.6250 | 11 | 0.226 | 18 | 0.256 |
3/4 | 0.7500 | 10 | 0.334 | 16 | 0.373 |
7/8 | 0.8750 | 9 | 0.462 | 14 | 0.509 |
1 | 1.000 | 8 | 0.606 | 12 | 0.663 |
1^{\frac{1}{8} } | 1.125 | 7 | 0.763 | 12 | 0.856 |
1^{\frac{1}{4} } | 1.250 | 7 | 0.969 | 12 | 1.073 |
1^{\frac{3}{8} } | 1.375 | 6 | 1.155 | 12 | 1.315 |
1^{\frac{1}{2} } | 1.500 | 6 | 1.405 | 12 | 1.581 |
1^{\frac{3}{4} } | 1.750 | 5 | 1.90 | ||
2 | 2.000 | 44 | 2.50 |
lists the tensile stress area for American Standard threads. A\mid \frac{1}{2}-6 UNC thread (\mid\frac{1}{2}-in-diameter rod with 6 threads per in) has a tensile stress area of 1.405 in^{2} which should be satisfactory for this application.
Comments
The final design specifies a \mid\frac{1}{2}-in-diameter rod made from AISI 1040 cold-drawn steel with \mid\frac{1}{2}-6 UNC threads machined on each end to allow the attachment of the rods to the transformer and to the truss.