Abstract: The present disclosure relates to, inter alia, a gel formulation in a package, the package may be pressurized. The formulation comprises one or more active agents and is co-mingled with a gas propellant prior to being filled under pressure into the package. The gas propellant is added in sufficient amounts to be dispersed in the formulation; the pressurized package is under sufficient pressure suitable to maintain the first gas propellant dispersed in the formulation. The pressurized package is under sufficient pressure to expel the formulation as a whipped gel formulation upon application of external force on the formulation in the package. The present disclosure also relates to, inter alia, a method of preparing the disclosed formulation; a package comprising the disclosed formulation, and a method of using the disclosed formulation.

Abstract: An electrical propulsion system for a vertical take-off and landing (VTOL) aircraft comprises an electrical motor assembly and an inverter assembly. The inverter assembly comprises a housing, a capacitor assembly, at least one printed circuit board assembly (PCBA), and a plurality of positioning pins. The capacitor assembly comprises a center hole, at least one capacitor, a capacitor housing having at least one busbar, and a plurality of through holes in the capacitor housing. The capacitor assembly and the at least one PCBA are positioned inside the housing. The plurality of positioning pins pass through the through the plurality of through holes of the capacitor housing and the at least one PCBA and are connected to the housing.

Abstract: The present disclosure relates to, inter alia, a formulation comprising one or more active agents and one or more thermal stabilizing agents and is co-mingled with a first propellant that is a gas propellant prior to being filled under pressure into said package; the first propellant is added in sufficient amounts to be dispersed in the formulation; the package is under sufficient pressure suitable to expel the formulation as a whipped formulation upon application of external force on said formulation in said package. The present disclosure also relates to, inter alia, a method of preparing the disclosed formulation; a package comprising the disclosed formulation, and a method of using the disclosed formulation.

Abstract: The present disclosure relates to, inter alia, a formulation in a package. The formulation comprises one or more active agents and is co-mingled with a whipping agent prior to being filled under pressure into the package. The whipping agent is added in sufficient amounts to be dispersed in the formulation. The pressurized package is under sufficient pressure suitable to maintain the whipping agent dispersed in the formulation; and the pressurized package is under sufficient pressure to expel the formulation as a whipped formulation upon application of external force on the formulation in the package.

Abstract: The present disclosure relates to, inter alia, a formulation in a package, the formulation comprises one or more active agents and is co-mingled with a whipping agent prior to being filled under pressure into the package. The whipping agent is added in sufficient amounts to be dispersed in the formulation. The pressurized package is under sufficient pressure suitable to maintain the whipping agent dispersed in the formulation; and the pressurized package is under sufficient pressure to expel the formulation as a whipped formulation upon application of external force on the formulation in the package.

Abstract: The present disclosure relates to, inter alia, a formulation in a package. The formulation comprises one or more active agents and is co-mingled with a whipping agent prior to being filled under pressure into the package. The whipping agent is added in sufficient amounts to be dispersed in the formulation. The pressurized package is under sufficient pressure suitable to maintain the whipping agent dispersed in the formulation; and the pressurized package is under sufficient pressure to expel the formulation as a whipped formulation upon application of external force on the formulation in the package.

Abstract: The present disclosure relates to, inter alia, a formulation in a package, the formulation comprises one or more active agents and is co-mingled with a whipping agent prior to being filled under pressure into the package. The whipping agent is added in sufficient amounts to be dispersed in the formulation. The pressurized package is under sufficient pressure suitable to maintain the whipping agent dispersed in the formulation; and the pressurized package is under sufficient pressure to expel the formulation as a whipped formulation upon application of external force on the formulation in the package.

Abstract: An anhydrous alcohol gel formulation. The gel formulation comprises one or more film forming agents, one of which is TM-Si 5. The gel formulation comprises active agent(s), which differs based on the purpose of the gel formulation. In certain embodiments, the gel formulation comprises one or more emollients. In certain embodiments, the gel formulation comprises one or more viscosity increasing agents. In certain embodiments, the gel formulation comprises Zinc Oxide. The formulation optionally comprises other ingredients. Such optional ingredients include: a skin conditioning and/or bulking agent; a fragrance, such as, for example and without limitation, Fragrance SZ-2108 MOD 2010; etc.

Abstract: A gas turbine and nozzle system is provided that includes a radial inflow turbine rotor and a volute providing a flow path to deliver a pressurized gas to a circumference of the radial turbine rotor. The volute incorporates a shape which substantially conforms to a radial turbine shroud contour. The volute includes at least first and second parts. A mating surface between the first and second parts is substantially aligned with a direction of pressurized gas flow in the volute.

Abstract: An anhydrous alcohol gel formulation. The gel formulation comprises one or more film forming agents, one of which is TM-Si 5. The gel formulation comprises active agent(s), which differs based on the purpose of the gel formulation. In certain embodiments, the gel formulation comprises one or more emollients. In certain embodiments, the gel formulation comprises one or more viscosity increasing agents. In certain embodiments, the gel formulation comprises Zinc Oxide. The formulation optionally comprises other ingredients. Such optional ingredients include: a skin conditioning and/or bulking agent; a fragrance, such as, for example and without limitation, Fragrance SZ-2108 MOD 2010; etc.

Abstract: The present disclosure relates to, inter alia, a method of making a whipped formulation and the formulation. The method comprises: selecting an amount of a gas propellant co-mingled with one or more active agents. The gas propellant is dispersed in the formulation, and the formulation is filled under pressure into a package, which may be pressurized. The package has a selected amount of pressure (“pre-gas or cut-bag pressure”). The pressure maintains the gas propellant dispersed in the formulation and the pressurized package is under sufficient pressure such that the formulation may be expelled as a whipped formulation upon application of external force on said formulation in said package. The whipped formulation is characterized by providing a desired sensory impact to a user.

Abstract: The present disclosure relates to, inter alia, a formulation in a package, the formulation comprises one or more active agents and is co-mingled with a whipping agent prior to being filled under pressure into the package. The whipping agent is added in sufficient amounts to be dispersed in the formulation. The pressurized package is under sufficient pressure suitable to maintain the whipping agent dispersed in the formulation; and the pressurized package is under sufficient pressure to expel the formulation as a whipped formulation upon application of external force on the formulation in the package.

Abstract: The present disclosure relates to, inter alia, a formulation in a package. The formulation comprises one or more active agents and is co-mingled with a whipping agent prior to being filled under pressure into the package. The whipping agent is added in sufficient amounts to be dispersed in the formulation. The pressurized package is under sufficient pressure suitable to maintain the whipping agent dispersed in the formulation; and the pressurized package is under sufficient pressure to expel the formulation as a whipped formulation upon application of external force on the formulation in the package.

Abstract: A gas turbine and nozzle system is provided that includes a radial inflow turbine rotor and a volute providing a flow path to deliver a pressurized gas to a circumference of the radial turbine rotor. The volute incorporates a shape which substantially conforms to a radial turbine shroud contour. The volute includes at least first and second parts. A mating surface between the first and second parts is substantially aligned with a direction of pressurized gas flow in the volute.

Abstract: The present disclosure relates to, inter alia, a formulation comprising one or more active agents and one or more thermal stabilizing agents and is co-mingled with a first propellant that is a gas propellant prior to being filled under pressure into said package; the first propellant is added in sufficient amounts to be dispersed in the formulation; the package is under sufficient pressure suitable to expel the formulation as a whipped formulation upon application of external force on said formulation in said package. The present disclosure also relates to, inter alia, a method of preparing the disclosed formulation; a package comprising the disclosed formulation, and a method of using the disclosed formulation.

Abstract: The present disclosure relates to, inter alia, a gel formulation in a package, the package may be pressurized. The formulation comprises one or more active agents and is co-mingled with a gas propellant prior to being filled under pressure into the package. The gas propellant is added in sufficient amounts to be dispersed in the formulation; the pressurized package is under sufficient pressure suitable to maintain the first gas propellant dispersed in the formulation. The pressurized package is under sufficient pressure to expel the formulation as a whipped gel formulation upon application of external force on the formulation in the package. The present disclosure also relates to, inter alia, a method of preparing the disclosed formulation; a package comprising the disclosed formulation, and a method of using the disclosed formulation.

Abstract: A means of attachment applicable to mating parts which have substantially different coefficients of thermal expansion is disclosed. The means of attachment substantially reduces the friction between the mating surfaces while still keeping the mating parts centered with respect to one another. The approach is based on radial recessed faces wherein the radial faces slide relative to each other. There may be three or more recessed/raised faces on each mating component, which when mated, maintain the alignment between the mating parts while allowing differential growth of the mating parts. This approach also the provides a much larger bearing surface for the attachment than a radial pin/slot approach, for example, and substantially eliminates areas of high stress concentration. It is thus a more robust design for components that undergo many thousands of thermal cycles.

Abstract: A gas turbine and nozzle system is provided that includes a radial inflow turbine rotor and a volute providing a flow path to deliver a pressurized gas to a circumference of the radial turbine rotor. The volute incorporates a shape which substantially conforms to a radial turbine shroud contour. The volute includes at least first and second parts. A mating surface between the first and second parts is substantially aligned with a direction of pressurized gas flow in the volute.

Abstract: A method and apparatus are disclosed for a gas turbine spool design combining metallic and ceramic components in a way that controls clearances between critical components over a range of engine operating temperatures and pressures. In a first embodiment, a ceramic turbine rotor rotates just inside a ceramic shroud and separated by a small clearance gap. The ceramic rotor is connected to a metallic volute. In order to accommodate the differential rates of thermal expansion between the ceramic rotor and metallic volute, an active clearance control system is used to maintain the desired axial clearance between ceramic rotor and the ceramic shroud over the range of engine operating temperatures. In a second embodiment, a ceramic turbine rotor rotates just inside a ceramic shroud which is part of a single piece ceramic volute/shroud assembly.

Abstract: A computer-implemented method of dynamic range control is disclosed. The method includes at a device with a display, displaying a volume (relative loudness level) control to control the volume level of an output audio signal of the device, the volume control including a dynamic resizable window control for controlling the dynamic range of the output audio signal. A method for adjusting dynamic range of an audio signal is also disclosed. The method includes providing an input audio signal with a first dynamic range, mapping the first dynamic range to a second dynamic range using a transfer function with a linear portion aligned to an average level of the input audio signal, and generating an output audio signal with the second dynamic range from the input audio signal.