Manufacturing Engineering & Technology
Manufacturing Engineering & Technology
7th Edition
ISBN: 9780133128741
Author: Serope Kalpakjian, Steven Schmid
Publisher: Prentice Hall
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Chapter 4, Problem 22QLP

Describe the characteristics of (a) an alloy, (b) pearlite, (c) austenite, (d) martensite, and (e) cementite.

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Nickel-based alloys are used for gas turbine blades in aerospace engines. Briefly discuss the characteristics that make these alloys the choice for this application. Single-crystal technology is applied to nickel alloys that are used as gas turbine blades in aerospace engines. With the aid of sketches describe how a single-crystal casting can be manufactured and explain why a single-crystal casting is likely to have superior creep resistance than a directly-solidified one. Demonstrate the application of the Ten-percent Rule by calculating the approximate tensile strength and elastic modulus in the 0° direction of a carbon-fibre reinforced polymer composite if the strength and elastic moduluş in the 0° single ply are 3620 MPa and 143 GPa respectively. The lay-up sequence of the composite is [02/+45/-45/902]s.
6. Describe each of the following crystal structure imperfections: a) substitutional atom; b) interstitial atom; c) vacancy. 7. At equilibrium, what is the maximum amount of carbon that can dissolve in pure iron at 600°C (by wt%). If the carbon content exceeds this maximum value, briefly describe the microstructure of the resulting alloy. 8. Give an example of a stress concentration in a metal part. 9. How would you expect the mechanical properties of a metal with an FCC structure to differ from one with a BCC structure? Why? 10. What is a slip system and how is it different than a slip plane?
wWucostuons ¢ 1. Differentiate between the following transformations Pearlite, (b) Bainitic (c) Martensitic, based on Diffusion, Temperature range, Nuclei, Kinetics of reaction, Crystallography, Density of dislocation, Surface relief, and Growth rate.

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