Modified eutectic alloys for high temperature service Final report, Jul. 1967 - Apr. 1969
Eutectic modified cobalt tungsten chromium alloy for chill casting
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Eutectic modified cobalt tungsten chromium alloy for chill casting
Fatigue characteristics of unidirectionally solidified Al-intermetallic aluminum nickel eutectic alloy consisting of discontinuous Al-Ni intermettalic whiskers in Al matrix
Microstructure and crystallography of lamellar eutectic alloy of Ni and intermetallic Ni-Ti compound
Crystal microstructure and mechanical properties of unidirectionally solidified Ni-Ni-Nb intermetallic eutectic alloy at high temperature, examining deformation and fracture modes
Temperature effects on mechanical properties and fracture behavior of lamellar Ni-nickel titanide intermetallic eutectic alloy showing dependence on intermetallic constituent
Contact preparation at low temperatures is possible with the use of a copper-titanium eutectic alloy. Contacts formed with this alloy are ohmic on p-type silicon carbide and rectifying on n-type.
Solidification, structure, and properties of nickel and niobium eutectic alloys
Monotonic and cyclic mechanical response of nickel-nickel niobium eutectic alloy to tensile, compressive and fatigue testing
High temperature friction and wear characteristics of self lubricating composite disks of sintered tungsten, molybdenum, and cobalt molybdenum, impregnated with fluoride eutectic
Solidification, structure, and properties of eutectic alloys including consideration of properties control
Ni-Ni Nb eutectic composite, investigating monotonic mechanical response, deformation and fracture mechanisms
Banding observed in unidirectional solidification of eutectic alloys is shown to be due to melting back of the freezing interface because of oscillations in the temperature of the furnace. General theoretical criteria as to the amplitude and frequency of the permissible temperature oscillations are given to ensure that banding will not occur.
Eutectic mixture of aluminum oxide and zirconium oxide provides new bonding technique for sapphires and rubies. Technique effectively reduces possibility of contamination. Bonding material is aluminum oxide and zirconium oxide mixture that matches coefficient of thermal expansion of sapphire.
The suitability of the eutectics for high temperature fasteners was investigated. Material properties were determined as a function of temperature, and included shear parallel and perpendicular to the growth direction and torsion parallel to it. Techniques for fabricating typical fastener shapes included grinding, creep forming, and direct casting. Both lamellar Ni3Al-Ni3Nb and fibrous (Co,Cr,Al)-(Cr,Co)7C3 alloys showed promise as candidate materials for high temperature fastener applications. A brief evaluation of the performance of the best fabricated fastener design was made.
Thermotransport (or thermal diffusion, Soret effect) is shown to cause significant amount of segregation during the directional solidification of aluminum-copper eutectic. The concentration changes are predicted quantitatively and they are a function of temperature gradient, rate of melting and solidification and the time of soaking. There is a fair agreement between the experiments and calculations. A process is suggested where these concentration changes may be minimized.
Continuous and discontinuous NaF fibers, embedded in a NaCl matrix, have been produced in space and on earth, respectively. The production of continuous fibers in a eutectic mixture was attributed to the absence of convection current in the liquid during solidification in space. Image transmission and optical transmittance measurements of transverse sections of the space-grown and earth-grown ingots were made with a light microscope and a spectrometer. It was found that better optical properties were obtained from samples grown in space. This was attributed to a better alignment of NaF fibers along the ingot axis.
A program was performed to scale up the edge-defined, film-fed growth (EFG) method for the gamma/gamma prime-beta eutectic alloy of the nominal composition Ni-19.7 Cb - 6 Cr-2.5 Al. Procedures and problem areas are described. Flat bars approximately 12 x 1.7 x 200 mm were grown, mostly at speeds of 38 mm/hr, and tensile tests on these bars at 25 and 1000 C showed lower strength than expected. The feasibility of growing hollow airfoils was also demonstrated by growing bars over 200 mm long with a teardrop shaped cross-section, having a major dimension of 12 mm and a maximum width of 5 mm.
The lamellar directionally solidified nickel-base eutectic alloy gamma/gamma prime-delta has potential as an advanced turbine blade material. The microstructural stability of this alloy was investigated. Specimens were plastically deformed by uniform compression or Brinell indentation, then annealed between 705 and 1120 C. Microstructural changes observed after annealing included gamma prime coarsening, pinch-off and spheroidization of delta lamellae, and the appearance of an unidentified blocky phase in surface layers. All but the first of these was localized in severely deformed regions, suggesting that microstructural instability is not a serious problem in the use of this alloy.