Abstract: A wheat variety designated 6PTWP59B, the plants and seeds of wheat variety 6PTWP59B, methods for producing a wheat plant produced by crossing the variety 6PTWP59B with another wheat plant, and hybrid wheat seeds and plants produced by crossing the variety 6PTWP59B with another wheat line or plant, and the creation of variants by backcrossing, mutagenesis or transformation of variety 6PTWP59B are disclosed. Methods for producing other wheat varieties or breeding lines derived from wheat variety 6PTWP59B and to wheat varieties or breeding lines produced by those methods are also provided.

Abstract: A wheat variety designated 6PDHJ97B, the plants and seeds of wheat variety 6PDHJ97B, methods for producing a wheat plant produced by crossing the variety 6PDHJ97B with another wheat plant, and hybrid wheat seeds and plants produced by crossing the variety 6PDHJ97B with another wheat line or plant, and the creation of variants by backcrossing, mutagenesis or transformation of variety 6PDHJ97B are disclosed. Methods for producing other wheat varieties or breeding lines derived from wheat variety 6PDHJ97B and to wheat varieties or breeding lines produced by those methods are also provided.

Abstract: A wheat variety designated 6PHLQ96B, the plants and seeds of wheat variety 6PHLQ96B, methods for producing a wheat plant produced by crossing the variety 6PHLQ96B with another wheat plant, and hybrid wheat seeds and plants produced by crossing the variety 6PHLQ96B with another wheat line or plant, and the creation of variants by backcrossing, mutagenesis or transformation of variety 6PHLQ96B are disclosed. Methods for producing other wheat varieties or breeding lines derived from wheat variety 6PHLQ96B and to wheat varieties or breeding lines produced by those methods are also provided.

Abstract: Disclosed herein are methods, devices, and systems for providing timing and bandwidth management of ultra-wideband, wireless data channels (including radio frequency and wireless optical data channels). According to one embodiment, a hub apparatus is disclosed for providing out-of-band bandwidth management for a free-space-optical (FSO) data channel associated with a first device. The hub apparatus includes a processor, a memory coupled with the processor, an FSO transmitter coupled with the processor, and an FSO receiver coupled with the processor. The FSO transmitter may be configured to transmit a control signal comprising timing information and bandwidth management information.

Abstract: A device for emergency disconnection of a high voltage electrical connection between a power source and a high voltage component of an electric aircraft in response to a crash. The device includes a controller, where the controller is configured to receive a sensor datum from a sensor of device, to determine a crash element between and initiate a disconnection protocol as a function of the crash element.

Abstract: The disclosure provides a battery management system and related method. A battery management system for an electric aircraft includes a control circuit communicatively connected to a plurality of sensors configured to detect a plurality of measurement data related to a battery pack. The control circuit is configured to: identify a state transition criterion as a function of an operating condition of the battery pack; and transition from a first state and a second state as a function of the state transition criterion.

Abstract: A gas turbine engine is provided. The gas turbine engine includes: a turbomachine having a compressor section, a combustion section, and a turbine section arranged in serial flow order, the compressor section having a high pressure compressor defining a high pressure compressor exit area (AHPCExit) in square inches; wherein the gas turbine engine defines a redline exhaust gas temperature (EGT) in degrees Celsius, a total sea level static thrust output (FnTotal) in pounds, and a corrected specific thrust, wherein the corrected specific thrust is greater than or equal to 42 and less than or equal to 90, the corrected specific determined as follows: FnTotal×EGT/(AHPCExit2×1000).

Abstract: A heat exchanger positioned within an annular duct of a gas turbine engine is provided. The heat exchanger extends substantially continuously along the circumferential direction and defining a heat exchanger height equal to at least 10% of a duct height. An effective transmission loss (ETL) for the heat exchanger positioned within the annular duct is between 5 decibels and 1 decibels for an operating condition of the gas turbine engine. The heat exchanger includes a heat transfer section defining an acoustic length (Li), and wherein an Operational Acoustic Reduction Ratio (OARR) is greater than or equal to 0.75 to achieve the ETL at the operating condition.

Abstract: A wheat variety designated 6PWEF05B, the plants and seeds of wheat variety 6PWEF05B, methods for producing a wheat plant produced by crossing the variety 6PWEF05B with another wheat plant, and hybrid wheat seeds and plants produced by crossing the variety 6PWEF05B with another wheat line or plant, and the creation of variants by backcrossing, mutagenesis or transformation of variety 6PWEF05B are disclosed. Methods for producing other wheat varieties or breeding lines derived from wheat variety 6PWEF05B and to wheat varieties or breeding lines produced by those methods are also provided.

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 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: Various implementations of a pipette tip system are disclosed having a number of innovative features. In one implementation, a pipette tip tray includes a support plate and one or more sleeves extending downward from the bottom of the support plate. The sleeves can be configured to increase the stability of pipette tips stored in the tray. In another implementation, a pipette tip rack includes a rack base having one or more support walls extending underneath a pipette tip tray having downward extending sleeves. The thickness of the sidewalls of the sleeves can be reduced in the area of the support walls so that the support walls can reach the bottom of the support plate. In another implementation, a pipette tip rack includes a cover having a cushioning layer on the bottom of the cover that contacts the top of the pipette tips and stabilizes them during handling and transport.

Abstract: A heat exchanger positioned within an annular duct of a gas turbine engine is provided. The heat exchanger extends substantially continuously along the circumferential direction and defining a heat exchanger height equal to at least 10% of a duct height. An effective transmission loss (ETL) for the heat exchanger positioned within the annular duct is between 5 decibels and 1 decibels for an operating condition of the gas turbine engine. The heat exchanger includes a heat transfer section defining an acoustic length (Li), and wherein an Operational Acoustic Reduction Ratio (OARR) is greater than or equal to 0.75 to achieve the ETL at the operating condition.

Abstract: A cell culture vessel has a wall and cell culture surface having a plurality of microcavities for culturing cells in three-dimensional conformation, referred to as “spheroids”. The inner surface of the wall and the cell culture surface define a cell culture chamber of the vessel. The wall is attached to the cell culture surface in a way that does not provide flat surfaces on or around the cell culture surface so that the vessel provides an environment suitable for the production of a homogeneous population of three-dimensional cell clusters, or spheroids.

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: The present disclosure provides a non-linear, heart rate adaptive, cardiac artifact filter designed to reduce cardiac artifacts in a patient's impedance respiration signal. The patient's impedance respiration signal may be acquired using electrocardiogram (“ECG”) sensors and may be impacted by the patient's cardiac activity. This impact occurs at a single dynamically changing frequency determined from heart rate measurement. The adaptive cardiac artifact filter can be used to filter unwanted cardiac artifacts from the impedance respiration signal to provide a more accurate representation of the patient's cardiac activity. A filtered impedance respiration signal can then be displayed or analyzed to further the monitoring and treatment of the patient. The heart rate adaptive, cardiac artifact filter may be implemented in a physiological monitoring device that may be, in turn, a part of a system.

Abstract: A consolidation terminal includes a body defining an interior, a stub cable port defined in the body, and a stub cable extending through the stub cable port, the stub cable including an optical fiber. The consolidation terminal further includes a splitter disposed in the interior, wherein the optical fiber is connected as an input to the splitter. The consolidation terminal includes a plurality of connector ports defined in the body, at least one single fiber connector disposed within at least one of the plurality of connector ports, the at least one single fiber connector connected to an output optical fiber from the splitter, and at least one multi-fiber connector disposed within at least one of the plurality of connector ports, the at least one multi-fiber connector connected to a plurality of output optical fibers from the splitter.

Abstract: Embodiments of negative pressure wound therapy apparatuses and methods for using such apparatuses are disclosed. In some embodiments, a negative pressure wound therapy apparatus includes a controller configured to determine a level of exudate in a canister (or a dressing) based at least in part on one or more characteristics of pressure signals generated by a negative pressure source and monitored by a pressure sensor. One such characteristic of the pressure signals can be amplitude, which may increase as a level of exudate in the canister (or dressing) increases. The canister (or dressing) can include a filter configured to become occluded in order to prevent overflow of the canister (or dressing). The controller can be additionally configured to detect and indicate a canister (or dressing) pre-full condition before the filter becomes occluded. More efficient and reliable operation of the negative pressure wound therapy apparatus can thereby be attained.

Abstract: An article is described herein that includes: a substrate having a glass, glass-ceramic or a ceramic composition and comprising a primary surface; and a protective film disposed on the primary surface. The protective film comprises a thickness of greater than 1.5 microns and a maximum hardness of greater than 15 GPa at a depth of 500 nanometers, as measured on the film disposed on the substrate. Further, the protective film comprises a metal oxynitride that is graded such that an oxygen concentration in the film varies by 1.3 or more atomic %. In addition, the substrate comprises an elastic modulus less than an elastic modulus of the film.

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.