Abstract: A turbomachine includes an annular casing, a fan disposed inside the annular casing and mounted for rotation about an axial centerline, and an airfoil. The fan includes fan blades that extend radially outwardly toward the annular casing. The airfoil includes a first side and a second side coupled together at a leading edge and a trailing edge, a plurality of first chord sections defining at least one first chord length, and a plurality of second chord sections defining at least one second chord length. The plurality of first chord sections and second chord sections define a waveform along a leading edge of the airfoil. The fan has an average chord fan width according to a first performance factor. The fan has a quantity of fan blades according to a second performance factor.

Abstract: A gas turbine engine is provided. The gas turbine engine includes a turbomachine defining an engine inlet to an inlet duct, a fan duct inlet to a fan duct, and a core inlet to a core duct; a primary fan driven by the turbomachine; and a secondary fan located downstream of the primary fan within the inlet duct. The gas turbine engine defines a thrust to power airflow ratio between 3.5 and 100 and a core bypass ratio between 0.1 and 10, wherein the thrust to power airflow ratio is a ratio of an airflow through a bypass passage over the turbomachine plus an airflow through the fan duct to an airflow through the core duct, and wherein the core bypass ratio is a ratio of the airflow through the fan duct to the airflow through the core duct.

Abstract: A personal signaling device including an electronics package with a circuit board, an emitter, and an activation switch. The device may include a translucent body with a lens section, an extended seal, and/or an attachment through hole. The device may include a base with an inner well configured to at least partially enclose the electronics package, an outer well configured to at least partially surround the sealing ring, and an attachment through hole configured to join with that of the translucent body.

Abstract: A device includes a substrate having a first side and a second side, a first transistor that includes a first gate over a first protrusion and a first source region and a first drain region interposing the first protrusion, a first buried contact disposed adjacent to the first protrusion and having at least a portion extending into the substrate, a first contact plug disposed over the first drain region, first conductive lines disposed over the first contact plug and electrically connecting to the first drain region by the first contact plug, first via penetrating through the substrate and connecting the first buried contact; and second conductive lines disposed over the second side of the substrate and electrically connecting to the first via. The first buried contact is electrically connecting to the first source region or the first gate.

Abstract: A wheat variety designated 6PRUL80B, the plants and seeds of wheat variety 6PRUL80B, methods for producing a wheat plant produced by crossing the variety 6PRUL80B with another wheat plant, and hybrid wheat seeds and plants produced by crossing the variety 6PRUL80B with another wheat line or plant, and the creation of variants by backcrossing, mutagenesis or transformation of variety 6PRUL80B are disclosed. Methods for producing other wheat varieties or breeding lines derived from wheat variety 6PRUL80B and to wheat varieties or breeding lines produced by those methods are also provided.

Abstract: A tool for assisting a billiards player to easily and accurately aim and direct the cue ball to strike a target ball an propel the target ball towards a target such as a pool table pocket. An aiming ring is placed on the billiards table adjacent to the target ball that allows the billiards player to automatically aim the cue ball and propel the target ball into a pocket or other desired location. A billiards goniometer tool is described to assist with bumper shots.

Abstract: A protective carrier for a microcavity vessel is provided. The protective carrier comprises a substantially flat rigid plate comprising a top surface and a bottom surface. A flange disposed around at least a portion of a perimeter of the rigid plate, the flange extending from the top surface of the rigid plate. One or more ribs disposed on the bottom surface of the rigid plate. A protective microcavity vessel carrier system is provided that comprises a microcavity vessel comprising a microcavity substrate on a bottom surface; and a protective carrier. The microcavity vessel may be a microcavity flask, microcavity plate such as an open well reservoir plate, microcavity bioreactor, or a stacked 3D microcavity culture vessel.

Abstract: An irradiation device for additively manufacturing a three-dimensional object includes two beam generation devices emitting energy beams that are characteristically different than one another. An optical modulator includes a micromirror array disposed downstream from the first and second beam generation devices. A focusing lens assembly is disposed downstream from the optical modulator. The micromirror array includes a plurality of micromirror elements to reflect beam segments corresponding to the first and second energy beams incident upon the focusing lens assembly. The focusing lens assembly focuses a first portion of the beam segments corresponding to the first energy beam to at least partially overlap with one another at a first one of a plurality of combination zones and focuses a second portion of the beam segments corresponding to the second energy beam to at least partially overlap with each other at a second one of a plurality of combination zones.

Abstract: A stimulation device for stimulating multiple stimulation sites on the face simultaneously. A device frame holds protruding posts into contact with the stimulation sites and a normal force is applied to all the stimulation sites. The protruding posts can have magnets attached to contact the stimulation site and provide stimulation alone or with normal forces. The protruding posts are adjustable to fit all facial configurations.

Abstract: A turbomachine includes an annular casing, a fan disposed inside the annular casing and mounted for rotation about an axial centerline, and an airfoil. The fan includes fan blades that extend radially outwardly toward the annular casing. The airfoil includes a composite core having a pressure sidewall and a suction sidewall extending between a core leading edge and a core trailing edge and a leading edge protective wrap. The fan has an average chord fan width according to a first performance factor. The fan has a quantity of fan blades according to a second performance factor.

Abstract: A system for a laminated buswork with flexible conductors for an electric aircraft is presented. The system includes a plurality of electrical devices and an electrical bridging device electrically connected to each electrical device of the plurality of devices. The electrical bridging device includes a laminated busbar and a plurality of flexible contactors, wherein each flexible contactor is configured to attach the laminated busbar to each electrical device of the plurality of electrical devices, apply pressure to each electrical device as a function of at least a spring, and provide electrical connection to the electric aircraft as a function of the tension of the at least a spring.

Abstract: A method, system, and computer program product for predicting future transactions may obtain merchant data associated with a merchant; determine a geographic location associated with the merchant based on the merchant data; determine one or more other merchants within a first threshold distance of the geographic location; obtain transaction data associated with the one or more other merchants and the merchant; and predict, based on the transaction data, at least one of a future number of transactions for the merchant in a future time period and a future transaction amount for the merchant in the future time period.

Abstract: A turbomachine includes an annular casing and a fan disposed inside the annular casing and mounted for rotation about an axial centerline. The fan includes fan blades that extend radially outwardly toward the annular casing. The fan blades include a composite blade including a composite airfoil section having an airfoil leading edge and an airfoil trailing edge, a root attached to the composite airfoil section, and a blade shank therebetween. A metallic leading edge shield covers an axially extending portion of the composite airfoil section including at least a portion of the airfoil leading edge and covers a radially and chordwise extending portion of the airfoil leading edge of the blade shank. The fan has an average chord fan width according to a first performance factor. The fan has a quantity of fan blades according to a second performance factor.

Abstract: A turbomachine includes an annular casing and a fan disposed inside the annular casing and mounted for rotation about an axial centerline. The annular casing is formed at least partially of a composite material. The fan includes fan blades that extend radially outwardly toward the annular casing. The fan has an average chord fan width according to a first performance factor. The fan has a quantity of fan blades according to a second performance factor.

Abstract: A turbomachine includes an annular casing and a fan disposed inside the annular casing and mounted for rotation about an axial centerline. The fan includes fan blades that extend radially outwardly toward the annular casing. The fan blades include a first fan blade having a fan blade airfoil body and a metal edge. The fan blade airfoil body has a leading edge. The metal edge is located at the leading edge and has a plurality of fail-fuse elements. The fan has an average chord fan width according to a first performance factor. The fan has a quantity of fan blades according to a second performance factor.

Abstract: A wheat variety designated 6PQTB00B, the plants and seeds of wheat variety 6PQTB00B, methods for producing a wheat plant produced by crossing the variety 6PQTB00B with another wheat plant, and hybrid wheat seeds and plants produced by crossing the variety 6PQTB00B with another wheat line or plant, and the creation of variants by backcrossing, mutagenesis or transformation of variety 6PQTB00B are disclosed. Methods for producing other wheat varieties or breeding lines derived from wheat variety 6PQTB00B and to wheat varieties or breeding lines produced by those methods are also provided.

Abstract: Embodiments described herein are directed to simultaneously displaying proxy windows for application windows and/or tabs included in such application windows via a graphical user interface of an operating system. For instance, an application programming interface (API) associated with an application that supports a tabbed document interface (TDI) provides information associated with each tab opened within an application window associated with the application. An API of the operating system receives and utilizes such information to generate and display a proxy window for each tab. The proxy windows for the tabs may be displayed alongside proxy windows of application windows for other applications. The proxy windows may be generated and displayed in response to user invocation of various features of the operating system graphical user interface, including, but not limited to, a task switcher feature, a taskbar feature, or a window snap feature.

Abstract: An engine includes a fan section having an open fan defining an axial centerline and a rotor. The rotor includes a plurality of fan blades mounted to a hub and being rotatable about the axial centerline. The engine also includes a turbomachine downstream of the fan section. The turbomachine includes a core cowl that defines an engine inlet and encloses turbomachinery. Further, the engine includes an airflow diverting assembly downstream of the fan section and upstream of the engine inlet. The airflow diverting assembly includes at least one fluid passageway formed into at least a portion of the hub for diverting at least a portion of a boundary layer on a surface of the hub away from the surface of the hub to reduce distortion caused by the boundary layer in the turbomachinery.

Abstract: An aerosol cosmetic composition is provided that includes an oil soluble gloss enhancing film forming component, a solvent, a colorant, a propellant, and useful for application to hair or skin. An aerosol dispensing system and a method of preparing an aerosol sprayable color composition are also provided.

Abstract: A gas turbine is provided, the gas turbine engine including a turbomachine having an inlet splitter defining in part an inlet to a working gas flowpath and a fan duct splitter defining in part an inlet to a fan duct flowpath. The gas turbine engine also includes a primary fan driven by the turbomachine defining a primary fan tip radius R1, a primary fan hub radius R2, and a primary fan specific thrust rating TP; and a secondary fan downstream of the primary fan and driven by the turbomachine, the secondary fan defining a secondary fan tip radius R3, a secondary fan hub radius R4, and a secondary fan specific thrust rating TS; wherein the gas turbine engine defines an Effective Bypass Area, and wherein a ratio of R1 to R3 equals R 1 R 3 = ( EFP ) ? ( 1 - RqR ( Sec . - Fan ) 2 ) ( 1 - RqR Prim . - Fan 2 ) ? ( T P T S ) ? ( EBA ) .