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Comparison of Compressive Stress-Strain Responses at High Temperatures for Representative Single Crystal and Polycrystal Superalloys Polycrystalline disk superalloys and single crystal blade superalloys have divergent grain and precipitate microstructures but can each display reduced strength and increasing deformation for certain test conditions at high temperatures. To allow thermo-mechanical processes such as forging and rolling to be applied, favorable temperatures and strain rates must first be identified using compression testing. The objective of this study was to perform compression tests at high temperatures on a polycrystalline disk superalloy and a single crystal blade superalloy in order to compare their stress-strain responses for given test conditions and determine preferred conditions. It was determined that the conditions required for stable flow differed significantly between the polycrystalline and single crystal superalloys. The conditions leading to unstable flow were also identified for each alloy. The microstructural deformation modes for both stable and unstable flow are discussed.
Document ID
20205001972
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
T P Gabb
(Glenn Research Center Cleveland, Ohio, United States)
J Telesman
(Glenn Research Center Cleveland, Ohio, United States)
A J Ring
(Glenn Research Center Cleveland, Ohio, United States)
I E Locci
(University of Toledo Toledo, Ohio, United States)
C A Kantzos
(Glenn Research Center Cleveland, Ohio, United States)
T M Smith
(Glenn Research Center Cleveland, Ohio, United States)
R J Pawlik
(HX5 Sierra )
L J Evans
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
May 8, 2020
Publication Date
June 7, 2020
Publication Information
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-19835
Funding Number(s)
WBS: 081876.02.03.04.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
compression, superalloy, turbine engine
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