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A comparison of forming technologies for ceramic gas-turbine engine componentsFor over ten years, injection molding and slip casting have been actively developed as forming techniques for ceramic gas turbine components. Co-development of these two processes has continued within the U.S. DOE-sponsored Advanced Turbine Technology Application Project (ATTAP). Progress within ATTAP with respect to these two techniques is summarized. A critique and comparison of the two processes are given. Critical aspects of both processes with respect to size, dimensional control, material properties, quality, cost, and potential for manufacturing scale-up are discussed.
Document ID
19910059984
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hengst, R. R.
(Norton Co. Northboro, MA, United States)
Heichel, D. N.
(Norton Co. Northboro, MA, United States)
Holowczak, J. E.
(Norton Co. Northboro, MA, United States)
Taglialavore, A. P.
(Norton Co. Northboro, MA, United States)
Mcentire, B. J.
(Norton/TRW Ceramics Northboro, MA, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1990
Subject Category
Mechanical Engineering
Report/Patent Number
ASME PAPER 90-GT-184
Accession Number
91A44607
Distribution Limits
Public
Copyright
Other

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