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Low-cost single-crystal turbine blades, volume 1The exothermic casting process was successfully developed into a low cost nonproprietary method for producing single crystal (SC) castings. Casting yields were lower than expected, on the order of 20 percent, but it is felt that the casting yield could be significantly improved with minor modifications to the process. Single crystal Mar-M 247 and two derivative SC alloys were developed. NASAIR 100 and SC Alloy 3 were fully characterized through mechanical property testing. SC Mar-M 247 shows no significant improvement in strength over directionally solidified (DS) Mar-M 247, but the derivative alloys, NASAIR 100 and Alloy 3, show significant tensile and fatigue improvements. The 1000 hr/238 MPa (20 ksi) stress rupture capability compared to DS Mar-M 247 was improved over 28 C. Firtree testing, holography, and strain gauge rig testing were used to evaluate the effects of the anisotropic characteristics of single crystal materials. In general, the single crystal material behaved similarly to DS Mar-M 247. Two complete engine sets of SC HP turbine blades were cast using the exothermic casting process and fully machined.
Document ID
19840007179
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Strangman, T. E.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Heath, B.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Fujii, M.
(Garrett Turbine Engine Co. Phoenix, AZ, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1983
Subject Category
Metallic Materials
Report/Patent Number
GARRETT-21-4314-1
NAS 1.26:168218
NASA-CR-168218
Report Number: GARRETT-21-4314-1
Report Number: NAS 1.26:168218
Report Number: NASA-CR-168218
Accession Number
84N15247
Funding Number(s)
CONTRACT_GRANT: NAS3-20073
PROJECT: RTOP 510-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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