NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Eutectic superalloys strengthened by sigma, Ni3CB lamellae and gamma prime, Ni3Al precipitatesBy means of a screening and solidification optimization study of certain alloys located on the gamma-sigma liquidus surface within the Ni-Cb-Cr-Al system, alloys with high temperature properties superior to those of all known superalloys were defined. One alloy, Ni - 19.7w/o Cb - 6.0w/o Cr - 2.5w/o Al, directionally solidified at 3 cm/hr met or exceeded each program goal. A second alloy, Ni-21.75 w/o Cb-2.55 w/o Al, although deficient in its inherent oxidation resistance, met the other program goals and combined a remarkable insensitivity of composite microstructure to solidification parameters with excellent low temperature toughness. This investigation demonstrated that useful properties for gas turbine airfoil application have been achieved by reinforcing a strong and tough gamma solid solution matrix containing precipitated gamma prime by a lamellar intermetallic compound Ni3 Cb having greater strength at elevated temperature.
Document ID
19740006075
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lemkey, F. D.
(United Aircraft Corp. East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1973
Publication Information
Publisher: NASA
Subject Category
Materials, Metallic
Report/Patent Number
M911213-5
NASA-CR-2278
Report Number: M911213-5
Report Number: NASA-CR-2278
Accession Number
74N14188
Funding Number(s)
CONTRACT_GRANT: NAS3-15562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available