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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Calculate the amounts of solid phases of ferrite and cementite present in pearlite.
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.
9. Typical microscopic images of spheroidite, lower bainite and tempered martensite of an iron-carbon alloy are represented in the following images; 9.a) Briefly describe the microstructural difference between spheroidite and tempered martensite. 9.b) Explain why tempered martensite is much harder and stronger. 9.c) Briefly describe the microstructural difference between lower bainite and tempered martensite. Ferrite Cementite Do 05 μη lower bainite - carbides 0.5 μm tempred martensite - carbides in multiple directions 60 μη oriented in the same direction

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