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Investment castings
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280079
EISBN: 978-1-62708-267-9
... Abstract This chapter discusses the application of investment casting to nickel- and cobalt-base superalloys. It describes the production of polycrystalline and single crystal castings, the materials normally used, and the part dimensions and tolerances typically achieved. It explains how...
Abstract
This chapter discusses the application of investment casting to nickel- and cobalt-base superalloys. It describes the production of polycrystalline and single crystal castings, the materials normally used, and the part dimensions and tolerances typically achieved. It explains how patterns, molds, and shells are produced, discusses the practice of directional solidification, and examines an assortment of turbine components cast from nickel- and cobalt-base alloys. The chapter also addresses casting problems such as inclusions, porosity, distortion, core shift, and leaching and explains how to avoid them.
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Published: 01 October 2012
Fig. 1.12 Titanium alloy investment castings. (a) Investment-cast titanium components for use in corrosive environments. (b) Titanium knee and hip implant prostheses manufactured by the investment casting process. Source: Ref 1.6
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Published: 01 December 1995
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Published: 01 October 2011
Fig. 5.25 Schematic of investment cast parts. (a) Shell mold investment casting. (b) Solid mold investment casting
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Published: 01 December 2018
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Published: 01 March 2002
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Published: 01 December 2018
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Published: 01 December 2018
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Published: 01 December 2018
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Published: 01 November 2013
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Published: 01 November 2013
Fig. 24 Investment cast turbine blade with convex wall removed showing complex core. Source: Ref 6
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Published: 01 October 2012
Fig. 5.29 Complex investment-cast titanium components used for gas turbine applications. Source: Ref 5.14
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Published: 01 October 2012
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Published: 01 April 2013
Fig. 10 Digital radiography images of an investment cast jet engine turbine blade showing detail through a wide range in material thickness. The trailing edge of the blade (along the top of the image) is 2 mm (0.080 in.) thick, the root section of the blade (to the far left in the image) is 19
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Published: 01 March 2002
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Published: 01 March 2002
Fig. 5.2 Investment-cast turbine blade with convex wall removed showing complex internal arrangement produced by the core standing alongside the blade
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Published: 01 March 2002
Fig. 5.3 (a) Automated dipping of investment casting molds, (b) cutaway view of shell mold for an air-cooled gas turbine blade
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Published: 01 March 2002
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Published: 01 March 2002
Fig. 5.11 Investment-cast gas turbine engine. (a) Polycrystalline integral nozzles, and (b) integral rotors
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Published: 01 June 2008
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