Methods and systems for selectively forming crystalline boron-doped silicon germanium on a surface of a substrate. The methods can be used to selectively form the boron-doped silicon germanium within a gap from the bottom upward. Exemplary methods can be used to, for example, form source and/or drain regions in field effect transistor devices, such as in gate-all-around field effect transistor devices.

Methods and systems for selectively forming crystalline boron-doped silicon germanium on a surface of a substrate. The methods can be used to selectively form the boron-doped silicon germanium within a gap from the bottom upward. Exemplary methods can be used to, for example, form source and/or drain regions in field effect transistor devices, such as in gate-all-around field effect transistor devices.

Methods and systems for forming structures including a superlattice of silicon-containing epitaxial layers using nanoparticles. Exemplary methods can include forming nanoparticles in situ and depositing the nanoparticles onto a substrate surface to thereby form the epitaxial layers.

Methods and systems for forming structures including a superlattice of silicon-containing epitaxial layers using nanoparticles. Exemplary methods can include forming nanoparticles in situ and depositing the nanoparticles onto a substrate surface to thereby form the epitaxial layers.

A casting method includes: forming a seed, the seed having a first end and a second end, the forming including bending a seed precursor; placing the seed second end in contact or spaced facing relation with a chill plate; contacting the first end with molten material; and cooling and solidifying the molten material so that a crystalline structure of the seed propagates into the solidifying material. The forming further included reducing a thickness of the seed proximate the first end relative to a thickness of the seed proximate the second end.

A nickel-based superalloy composition is provided that includes 6.1 wt. % to 6.6 wt. % aluminum; 5.6 wt. % to 6.6 wt. % tantalum; 9.0 wt. % to 11.0 wt. % chromium; 5.5 wt % to 6.2 wt. % tungsten; 1.1 wt. % to 1.4 wt % molybdenum; 2.0 wt. % to 2.6 wt % rhenium; 5.5 wt. % to 10.0 wt % cobalt; 0.2 wt % to 0.5 wt % hafnium; up to 0.05 wt % carbon; 0.002 wt % to 0.01 wt % boron; and a balance of nickel and incidental impurities, wherein the composition exhibits a rupture life that is greater than 40 hours at 982.2° C. and 40 ksi, and wherein the composition exhibits a corrosion resistance of less than 50.8 μm attack at 926.7° C. after a 940 hour burner rig test. Components are also provided formed from the composition.

A nickel-based superalloy composition is provided that includes 6.1 wt. % to 6.6 wt. % aluminum; 5.6 wt. % to 6.6 wt. % tantalum; 9.0 wt. % to 11.0 wt. % chromium; 5.5 wt % to 6.2 wt. % tungsten; 1.1 wt. % to 1.4 wt % molybdenum; 2.0 wt. % to 2.6 wt % rhenium; 5.5 wt. % to 10.0 wt % cobalt; 0.2 wt % to 0.5 wt % hafnium; up to 0.05 wt % carbon; 0.002 wt % to 0.01 wt % boron; and a balance of nickel and incidental impurities, wherein the composition exhibits a rupture life that is greater than 40 hours at 982.2° C. and 40 ksi, and wherein the composition exhibits a corrosion resistance of less than 50.8 μm attack at 926.7° C. after a 940 hour burner rig test. Components are also provided formed from the composition.

A nickel-based superalloy is provided, which includes: 5.6 wt % to 6.6 wt % aluminum; 6.0 wt % to 9.0 wt % tantalum; 4.0 wt % to 7.0 wt % chromium; 4.0 wt % to 7.0 wt % tungsten; 0.5 wt % to 2.5 wt % molybdenum; 1.5 wt % to 5.5 wt % rhenium; 7.0 wt % to 13.0 wt % cobalt; 0.1 wt % to 0.7 wt % hafnium; 0.001 wt % to 0.005 wt % carbon; 0.002 wt % to 0.05 wt % boron; up to 0.1 wt % yttrium; and a balance of nickel and incidental impurities, wherein the composition exhibits a rupture life that is greater than 80 hours at 1093.3° C. and 20 ksi and an oxidation resistance of less than 25.4 μm surface loss at 1176.7° C. after a 400 hour Mach I test. Components are also provided formed from such a nickel-based superalloy.

A nickel-based superalloy is provided, which includes: 5.6 wt % to 6.6 wt % aluminum; 6.0 wt % to 9.0 wt % tantalum; 4.0 wt % to 7.0 wt % chromium; 4.0 wt % to 7.0 wt % tungsten; 0.5 wt % to 2.5 wt % molybdenum; 1.5 wt % to 5.5 wt % rhenium; 7.0 wt % to 13.0 wt % cobalt; 0.1 wt % to 0.7 wt % hafnium; 0.001 wt % to 0.005 wt % carbon; 0.002 wt % to 0.05 wt % boron; up to 0.1 wt % yttrium; and a balance of nickel and incidental impurities, wherein the composition exhibits a rupture life that is greater than 80 hours at 1093.3° C. and 20 ksi and an oxidation resistance of less than 25.4 μm surface loss at 1176.7° C. after a 400 hour Mach I test. Components are also provided formed from such a nickel-based superalloy.

Some variations provide a method of making an additively manufactured single-crystal metallic component, comprising: providing a feedstock comprising a first metal or metal alloy; providing a build plate comprising a single crystal of a second metal or metal alloy; exposing the feedstock to an energy source for melting the feedstock, generating a melt layer on the build plate; and solidifying the melt layer, generating a solid layer (on the build plate) of a metal component. The solid layer is also a single crystal of the first metal or metal alloy. The method may be repeated many times to build the part. Some variations provide a single-crystal metallic component comprising a plurality of solid layers in an additive-manufacturing build direction, wherein the plurality of solid layers forms a single crystal of a metal or metal alloy with a continuous crystallographic texture. The crystal orientation may vary along the additive-manufacturing build direction.