Abstract: Protective coatings on an aerospace component are provided. An aerospace component includes a surface containing nickel, nickel superalloy, aluminum, chromium, iron, titanium, hafnium, alloys thereof, or any combination thereof, and a coating disposed on the surface, where the coating contains a nanolaminate film stack having two or more pairs of a first deposited layer and a second deposited layer. The first deposited layer contains chromium oxide, chromium nitride, aluminum oxide, aluminum nitride, or any combination thereof, the second deposited layer contains aluminum oxide, aluminum nitride, silicon oxide, silicon nitride, silicon carbide, yttrium oxide, yttrium nitride, yttrium silicon nitride, hafnium oxide, hafnium nitride, hafnium silicide, hafnium silicate, titanium oxide, titanium nitride, titanium silicide, titanium silicate, or any combination thereof, and the first deposited layer and the second deposited layer have different compositions from each other.

Abstract: Susceptor assemblies comprising a susceptor base and a plurality of pie-shaped skins thereon are described. A pie anchor can be positioned in the center of the susceptor base to hold the pie-shaped skins in place during processing.

Abstract: Protective coatings on an aerospace component and methods for depositing the protective coatings are provided. A method for depositing a coating on an aerospace component includes exposing an aerospace component to a first precursor and a first reactant to form a first deposited layer on a surface of the aerospace component by a chemical vapor deposition (CVD) process or a first atomic layer deposition (ALD) process and exposing the aerospace component to a second precursor and a second reactant to form a second deposited layer on the first deposited layer by a second ALD process, where the first deposited layer and the second deposited layer have different compositions from each other.

Abstract: Pedestal assemblies with a thermal barrier plate, a torque plate and at least one kinematic mount to change a plane formed by the thermal barrier plate are described. Susceptor assemblies and processing chambers incorporating the pedestal assemblies are also described. Methods of leveling a susceptor to form parallel planes between the susceptor surface and a gas distribution assembly surface are also described.

Abstract: A reactor for coating particles includes a vacuum chamber configured to hold particles to be coated, a vacuum port to exhaust gas from the vacuum chamber via the outlet of the vacuum chamber, a chemical delivery system configured to flow a process gas into the particles via a gas inlet on the vacuum chamber, one or more vibrational actuators located on a first mounting surface of the vacuum chamber, and a controller configured to cause the one or more vibrational actuators to generate a vibrational motion in the vacuum chamber sufficient to induce a vibrational motion in the particles held within the vacuum chamber.

Abstract: A reactor for coating particles includes one or more motors, a rotary vacuum chamber configured to hold particles to be coated and coupled to the motors, a controller configured to cause the motors to rotate the chamber in a first direction about an axial axis at a rotation speed sufficient to force the particles to be centrifuged against an inner diameter of the chamber, a vacuum port to exhaust gas from the rotary vacuum chamber, a paddle assembly including a rotatable drive shaft extending through the chamber and coupled to the motors and at least one paddle extending radially from the drive shaft, such that rotation of the drive shaft by the motors orbits the paddle about the drive shaft in a second direction, and a chemical delivery system including a gas outlet on the paddle configured inject process gas into the particles.

Abstract: A reactor for coating particles includes one or more motors, a rotary vacuum chamber configured to hold particles to be coated, wherein the rotary vacuum chamber is coupled to the motors, a controller configured to cause the motors to rotate the rotary vacuum chamber about an axial axis of the rotary vacuum chamber such that the particles undergo tumbling agitation, a vacuum port to exhaust gas from the rotary vacuum chamber, a paddle assembly including a rotatable drive shaft extending through the rotary vacuum chamber and coupled to the motors and at least one paddle extending radially from the drive shaft, such that rotation of the drive shaft by the motors orbits the paddle about the drive shaft in a second direction, and a chemical delivery system including a gas outlet on the paddle configured inject process gas into the particles.

Abstract: Pedestal assemblies with a thermal barrier plate, a torque plate and at least one kinematic mount to change a plane formed by the thermal barrier plate are described. Susceptor assemblies and processing chambers incorporating the pedestal assemblies are also described. Methods of leveling a susceptor to form parallel planes between the susceptor surface and a gas distribution assembly surface are also described.

Abstract: A gas distribution assembly for applying a coating on an interior of a plurality of components includes a support with a plurality of component cavities formed within the support. Each component cavity corresponds to a respective component to fluidly couple with an interior of the respective component. A first gas source flow line is fluidly coupled with each of the component cavities to provide a first gas from a first gas source to each of the component cavities, and a second gas source flow line is fluidly coupled with each of the component cavities to provide a second gas from a second gas source to each of the component cavities.

Abstract: Embodiments of the present disclosure generally relate to protective coatings on an aerospace component and methods for depositing the protective coatings. In one or more embodiments, a method for depositing a coating on an aerospace component includes exposing an aerospace component to a first precursor and a first reactant to form a first deposited layer on a surface of the aerospace component by a chemical vapor deposition (CVD) process or a first atomic layer deposition (ALD) process and exposing the aerospace component to a second precursor and a second reactant to form a second deposited layer on the first deposited layer by a second ALD process, where the first deposited layer and the second deposited layer have different compositions from each other.

Abstract: Apparatus and methods of measuring and controlling the gap between a susceptor assembly and a gas distribution assembly are described. Apparatus and methods for positional control and temperature control for wafer transfer purposes are also described.

Abstract: Apparatus and methods for processing a semiconductor wafer including a two-axis lift-rotation motor center pedestal with vacuum capabilities. Wafers are subjected to a pressure differential between the top surface and bottom surface so that sufficient force prevents the wafer from moving during processing, the pressure differential generated by applying a decreased pressure to the back side of the wafer through interface with the motor assembly.

Abstract: Apparatus and method for processing a plurality of substrates in a batch processing chamber are described. The apparatus comprises a susceptor assembly, a lift assembly and a rotation assembly. The susceptor assembly has a top surface and a bottom surface with a plurality of recesses in the top surface. Each of the recesses has a lift pocket in the recess bottom. The lift assembly including a lift plate having a top surface to contact the substrate. The lift plate is connected to a lift shaft that extends through the susceptor assembly and connects to a lift friction pad. The rotation assembly has a rotation friction pad that contacts the lift friction pad. The rotation friction pad is connected to a rotation shaft and can be vertically aligned with the lift friction pad.

Abstract: An anti-wetting coating including a ceramic material and a second material that may include, but not be limited to, pure amorphous silicon, hydrogenated silicon, silicon hydride, polytetrafluoroethylene (PTFE), perfluoroalkoxy alkanes (PFA), fluorinated ethylene propylene (FEP), polyvinylidene fluoride (PVDF), low density polyethylene (PELD), polyamide, polyimide, polyimide-amide, polyurea, polyurethane, polythiurea, polyester, polyimine, and combinations thereof.

Abstract: Apparatus and methods of measuring and controlling the gap between a susceptor assembly and a gas distribution assembly are described. Apparatus and methods for positional control and temperature control for wafer transfer purposes are also described.

Abstract: Methods comprise performing two or more thermal cycles on an article comprising a body and a ceramic coating. Each thermal cycle of the two or more thermal cycles comprise heating the ceramic article to a target temperature at a first ramping rate. Each thermal cycle further comprises maintaining the article at the target temperature for a first duration of time and then cooling the article to a second target temperature at a second ramping rate. The method further comprises submerging the article in a bath for a second duration of time to remove the particles from the ceramic coating.

Abstract: Apparatus and method for processing a plurality of substrates in a batch processing chamber are described. The apparatus comprises a susceptor assembly, a lift assembly and a rotation assembly. The susceptor assembly has a top surface and a bottom surface with a plurality of recesses in the top surface. Each of the recesses has a lift pocket in the recess bottom. The lift assembly including a lift plate having a top surface to contact the substrate. The lift plate is connected to a lift shaft that extends through the susceptor assembly and connects to a lift friction pad. The rotation assembly has a rotation friction pad that contacts the lift friction pad. The rotation friction pad is connected to a rotation shaft and can be vertically aligned with the lift friction pad.

Abstract: Apparatus and methods for processing a semiconductor wafer including a two-axis lift-rotation motor center pedestal with vacuum capabilities. Wafers are subjected to a pressure differential between the top surface and bottom surface so that sufficient force prevents the wafer from moving during processing, the pressure differential generated by applying a decreased pressure to the back side of the wafer through interface with the motor assembly.

Abstract: Methods comprise loading an article comprising a ceramic coating into an induction heating system or a microwave heating system and heat treating the ceramic coating using the microwave heating system or the induction heating system within a temperature range for a duration of about 1-15 minutes.

Abstract: Plasma source assemblies comprising a housing with an RF hot electrode and a return electrode are described. The housing includes a gas inlet and a front face defining a flow path. The RF hot electrode includes a first surface oriented substantially parallel to the flow path. The return electrode includes a first surface oriented substantially parallel to the flow path and spaced from the first surface of the RF hot electrode to form a gap. Processing chambers incorporating the plasma source assemblies and methods of using the plasma source assemblies are also described.