22-Mec-A4 Design and Manufacture of Machine Elements · May 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Paper format. National Examinations, May 2017 — 16-Mec-A4, Design and Manufacture of Machine Elements. Three hours, open book, any non-communicating calculator. Six questions in two parts: Part A (Q1–Q3) is manufacturing-process theory, Part B (Q4–Q6) is machine-element analysis. The rubric asks for two questions from Part A and two from Part B, all of equal value (25 % each). All six are solved here, because this set is a study resource rather than an examination script.
Reference texts.
Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.
Given. Figure ex1 shows three sections of equal area: (a) an I-section with thin flanges and a thin web, (b) a channel whose two legs turn inward at the bottom into re-entrant lips, and (c) a thin split ring. Figure ex2 shows a heavy, unbalanced section carrying two small hollow holes and a labelled sharp inside corner. Figure Ro1 shows a rolled strip with wavy edges; Figure Ro2 shows a rolled strip cracked at both edges.
Find. (a) The section requiring the greatest extrusion force, with justification; (b) the consequence of leaving the ex2 section unbalanced, plus its other extrusion problems; (c) the mechanism behind each rolling defect.
Approach. Extrusion pressure is not a function of area alone. For a given reduction, the pressure is written p = Yavg (a + b ln R) and is then multiplied by a shape factor that grows with the ratio of the section perimeter to the perimeter of a circle of equal area. The reason is physical: the perimeter is the length of the die land, so it sets the sliding-friction area, and a long, convoluted perimeter also forces the metal to undergo redundant (non-useful) shear as it turns into the thin outlying features.
Scaling the three outlines off the printed figure and normalising every one to the same area gives the complexity factor Kc = P/Pcircle:
| Figure ex1 section | Perimeter / √Area | Kc = P / Pcircle |
|---|---|---|
| (a) I-section, thin flanges and web | 10.1 | 2.86 |
| (b) Channel with re-entrant lips | 10.1 | 2.84 |
| (c) Split ring, uniform thin wall | 8.7 | 2.45 |
| (reference) solid round bar | 3.54 | 1.00 |
Answer: section (b), the channel with the inward-turned lips, requires the greatest force, with the I-section (a) an extremely close second and the split ring (c) clearly the easiest of the three.
The numbers put (a) and (b) within 1 % of each other — far inside the accuracy of dimensions scaled off a sketch — so the perimeter argument alone cannot separate them, and the tie is broken on a feature the perimeter does not capture. Section (b) is the only one of the three with a re-entrant profile: the lips turn back inward, so metal must flow into a deep, narrow pocket whose mouth is narrower than the space behind it, and the die must carry an unsupported tongue between the two lips. Filling a re-entrant pocket demands additional redundant shear and a higher local pressure, and the cantilevered die tongue deflects under that pressure, which the operator compensates for with still more pressure. Section (a) has the same thin walls but every feature opens outward, so metal reaches it by a direct radial flow.
The split ring (c) is the counter-intuitive result worth stating explicitly: it looks the most delicate, but a uniform thin annulus has a comparatively modest perimeter for its area, no re-entrant features and no sharp corners, so it is the least demanding of the three. Thinness by itself does not raise the extrusion force — convolution and re-entrancy do.
An unbalanced section is one whose thick and thin regions are distributed asymmetrically about the extrusion axis. Metal leaves a die land at a velocity that depends on the local channel thickness and friction, so a thick region wants to run faster than a thin one.
If the imbalance is not addressed, the extrudate leaves the die distorted rather than straight. The faster-flowing heavy side elongates more than the light side, and because the two are joined they cannot separate — the profile therefore curves, bows and twists as it emerges, and it develops longitudinal residual stress even where it looks straight. The consequences on the run-out table are a product that will not stay within straightness tolerance, that whips against the puller and the die, that distorts again during subsequent ageing or heat treatment as the residual stresses relax, and that may tear along the thick/thin junction where the velocity mismatch is greatest. The extrudate can also drag against one side of the die and score its surface. The cure is to balance the flow rather than the geometry: lengthen the die land on the thick regions and shorten it on the thin ones (choke and relief), feed the thin sections preferentially with feeder plates or a pocket die, and where possible redesign the section toward uniform wall thickness.
The other extrusion problems visible in this design are:
(i) Figure Ro1 — wavy edges. Under the separating force the work rolls bend elastically, deflecting away from each other at mid-span, so the roll gap is thicker at the centre than at the edges. The strip edges are therefore reduced more than the centre, and greater reduction means greater elongation. The edges cannot elongate freely because they are attached to the shorter centre, so they are held in longitudinal compression — and a thin plate in longitudinal compression buckles. The waves are that buckle, frozen into the strip. The remedies all attack the roll-gap profile: grind a positive camber onto the rolls, use backup rolls or roll-bending jacks to counteract the deflection, run with roll crown control, or simply take a lighter pass so the separating force and hence the deflection are smaller.
(ii) Figure Ro2 — edge cracking. This is the mirror-image fault. When the roll gap is thicker at the edges than at the centre — over-cambered rolls, or barrelled rolls, or a strip that has been over-crowned upstream — the centre of the strip is reduced more and elongates more, and it drags the under-reduced edges along with it. The edges are then in longitudinal tension, and since a rolled edge is also the coldest, most work-hardened and least ductile part of the strip (and often carries pre-existing edge damage from an earlier pass or from the slab), that tension opens transverse cracks in from each edge, exactly as drawn. Edge cracking is aggravated by low rolling temperature, by rolling material with poor edge ductility, and by the free-surface bulging (barrelling) of the edges, which superimposes a secondary tensile hoop stress on the edge surface. The remedies are to correct the roll-gap profile, to keep the edges hot (edge heaters), to edge-roll or trim the strip before the heavy passes, and to reduce the pass reduction.
| Sub-part | Result |
|---|---|
| (a) Highest extrusion force | Section (b), the re-entrant lipped channel (Kc = 2.84, tied with (a) at 2.86 on perimeter; the re-entrant pocket and cantilevered die tongue break the tie). Section (c) is the easiest at Kc = 2.45. |
| (b) Unbalanced section, if unaddressed | Differential exit velocity → bowing, twisting, camber, residual stress, possible tearing; fix by balancing die-land lengths (choke/relief) and feeder pockets |
| (b) Other issues | Sharp inside corner (die cracking, surface defect); enclosed holes need a porthole/bridge die and leave weld seams; very unequal walls; off-centre centroid |
| (c)(i) Figure Ro1 | Wavy edges — roll bending thickens the gap at mid-span; edges over-reduced, elongate more, are held in compression and buckle |
| (c)(ii) Figure Ro2 | Edge cracking — gap thicker at the edges; centre over-reduced and elongates more, putting the colder, less ductile edges in tension |