Abstract: Systems include a plurality of sensors coupled to a person support apparatus, at least one moisture sensor configured to sense a moisture level between the person and the support surface, and at least one computing device coupled to the plurality of sensors coupled to the person support apparatus and the at least one moisture sensor. The at least one computing device receives data from the plurality of sensors coupled to the person support apparatus and the at least one moisture sensor, obtains data from an electronic medical record associated with the person supported by the person support apparatus, calculates a pressure injury score indicative of a likelihood that the person will develop a pressure injury based on the data from the plurality of sensors, the at least one moisture sensor, and the electronic medical record, and alters a treatment plan for the person based on the calculated pressure injury score.

Abstract: An internal core profile for a turbine nozzle airfoil of a gas turbine is provided. The turbine nozzle may include an airfoil core having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil core profile sections at each Z distance, and the plurality of airfoil core profile sections, when joined together by smooth continuous arcs, define an airfoil core shape.

Abstract: An internal core profile for a turbine nozzle airfoil of a gas turbine is provided. The turbine nozzle may include an airfoil core having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil core profile sections at each Z distance, and the plurality of airfoil core profile sections, when joined together by smooth continuous arcs, define an airfoil core shape.

Abstract: An airfoil profile for a turbine blade of a gas turbine is provided. The turbine blade may include an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections at each Z distance, and the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.

Abstract: An internal core profile for a second stage turbine nozzle airfoil of a gas turbine is provided. The turbine nozzle may include an airfoil core having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil core profile sections at each Z distance, and the plurality of airfoil core profile sections, when joined together by smooth continuous arcs, define an airfoil core shape.

Abstract: An airfoil profile for a turbine blade of a gas turbine is provided. The turbine blade may include an airfoil portion having an uncoated nominal profile substantially in accordance with Cartesian coordinate values of X, Y, and Z set forth in Table 1, wherein the X, Y, and Z coordinates are distances in inches measured in a Cartesian coordinate system, the corresponding X and Y coordinates, when connected by a smooth continuous arc, define one of a plurality of airfoil profile sections at each Z distance, and the plurality of airfoil profile sections, when joined together by smooth continuous arcs, define an airfoil shape.

Abstract: The present disclosure provides methods, computer readable media, and a system comprising: a hierarchical data storage architecture comprising the following storage tiers: a first tier configured to store a data element associated with a first range of recall probability scores, and a second tier configured to store a data element associated with a second range of recall probability scores; a computing agent configured to perform the following: compute a recall probability score for the data element stored in the hierarchical data storage architecture, and affect a transfer of the data element between the first and second tier; and a graphical user interface (GUI) comprising at least one functional GUI element configured to: enable an end-user to input a desired balance between speed of data retrieval and cost of data storage, wherein the desired balance impacts the plurality of ranges of recall probability scores associated with the first and second tier.

Abstract: The present disclosure provides methods, computer readable media, and a system comprising: a hierarchical data storage architecture comprising the following storage tiers: a first tier configured to store a data element associated with a first range of recall probability scores, and a second tier configured to store a data element associated with a second range of recall probability scores; a computing agent configured to perform the following: compute a recall probability score for the data element stored in the hierarchical data storage architecture, and affect a transfer of the data element between the first and second tier; and a graphical user interface (GUI) comprising at least one functional GUI element configured to: enable an end-user to input a desired balance between speed of data retrieval and cost of data storage, wherein the desired balance impacts the plurality of ranges of recall probability scores associated with the first and second tier.

Abstract: The present disclosure provides methods, computer readable media, and a system (the “platform”) for recall probability-based data storage and retrieval. The platform may comprise a hierarchical data storage architecture having at least one of the following storage tiers: a first tier, and a second tier; at least one computing agent, wherein the at least one computing agent is configured to: compute a recall probability for a data element stored in the data storage, and effect a transfer of the data element based on, at least in part, the recall probability, wherein the transfer of the data element is between at least the following: the first tier, and the second tier; and a graphical user interface (GUI) comprising at least one functional GUI element configured to: enable an end-user to specific a desired balance between at least one of the following elements: speed of data retrieval, and cost of data storage.

Abstract: Systems include a plurality of sensors coupled to a person support apparatus, at least one moisture sensor configured to sense a moisture level between the person and the support surface, and at least one computing device coupled to the plurality of sensors coupled to the person support apparatus and the at least one moisture sensor. The at least one computing device receives data from the plurality of sensors coupled to the person support apparatus and the at least one moisture sensor, obtains data from an electronic medical record associated with the person supported by the person support apparatus, calculates a pressure injury score indicative of a likelihood that the person will develop a pressure injury based on the data from the plurality of sensors, the at least one moisture sensor, and the electronic medical record, and alters a treatment plan for the person based on the calculated pressure injury score.

Abstract: An integral unit that may serve as a backrest and a storage unit is provided.

Abstract: The condition of the reinforcing (4) of steel conveyor belts (1) is sensed ultrasonically. Transmitters (T) and receivers (R) are located on the belt. The transmitters are energised for a first fraction of a time interval and the receivers are enabled for a second, and later, fraction of the time interval. The time delay between the first and second fractions is related to the anticipated propagation delay between the transmitters and receivers. In addition, a longitudinally extending rip in the belt can be detected by detecting the absence of, or a reduction in, a received signal at one receiver sent by a transversely located transmitter. A method of ultrasonically assessing the quality of a vulcanised splice (8) in such a belt (1) is also disclosed. A transducer (14) able to function as a transmitter or receiver is also disclosed together with a method of mounting it in contact with the underside of the belt.

Abstract: A telecommunication system includes telecommunication resources, points, and a connection manager. The connection manager is configured to establish connections between the telecommunications resources and the points in response to a request from an application. The connection manager uses routing tables to select the most efficient route from the available routes between a telecommunications resource and a point. The routing tables establish the connection by sending a request to allocate a telecommunications resource to a session manager.

Abstract: A system and method in accordance with the invention allow a user to select when messages relating to medication events are sent and to select the content parameters of those messages. In one aspect, a user selects certain event types, the occurrence of which will cause a message to be sent to the user. For example, the user may select a message type that pertains to the availability of a medication in an automated dispensing machine for that user's patient. In another aspect, the user may customize the contents of the message to include or exclude certain information. For example, the user may desire the message to indicate only the patient's name and not the patient's gender or age. In yet another aspect, the user may filter messages so that only certain messages are sent. For example, the user may select a filter that permits only messages pertaining to his or her patients to be sent.

Abstract: Methods of the invention include the application of fluorescent technology, total genome amplification, high throughput automated microsatellite fragment analysis, robotics, and novel computational methods. Computational methods include determining a microsatellite instability (MSI) phenotype (frequency and significance of MSI over multiple loci) using SP-PCR at higher than 0.5 genome equivalents (0.5 to 2 genome equivalents).

Abstract: The present invention relates to methods for robust controlled auto-ignition and spark ignited combustion controls in gasoline direct-injection engines, including transients, using either exhaust re-breathing or a combination of exhaust re-compression and re-breathing valve strategy. These methods are capable of enabling engine operation with either lean of stoichiometric or stoichiometric air/fuel ratio for oxides of nitrogen (NOx) control, with varying exhaust gas recirculation (EGR) rates and throttle valve positions for knock control, and with a combination of homogeneous charge compression ignition (HCCI) and spark ignition (SI) combustion modes to optimize fuel economy over a wide range of engine operating conditions.

Abstract: A method of monitoring the condition of magnetically permeable reinforcing cords (2) of a conveyor belt (1) is disclosed. The method comprises the steps of: (i) longitudinally magnetizing the cords (2) with a substantially constant unidirectional magnetic field, (ii) moving the conveyor belt (1) relative to a plurality of magnetic sensors (5) spaced apart and extending transversely relative to the belt (1), (iii) interrogating the sensors (5) at spaced apart intervals of time, (iv) using the sensors (5) to each detect the presence of a north polarity fringing magnetic field, a south polarity fringing magnetic field, or no fringing magnetic field, and (v) recording the output of each sensor (5).

Abstract: A method is provided for control of transition between combustion modes of a direct-injection engine operable in a homogeneous charge compression ignition (HCCI) mode at lower loads and a spark ignition flame propagation (SI) mode at higher loads. The engine includes a variable valve actuation system including two-step high and low lift valve actuation and separate cam phasing for both intake and exhaust valves. The method includes operating the engine at steady state, with fuel-air-exhaust gas mixtures at predetermined conditions, for each speed and load, and controlling the engine during mode changes between the HCCI mode and the SI mode by switching the exhaust and intake valves between low lift for HCCI operation and high lift for SI operation.

Abstract: A method is provided for control of a direct-injection engine operated with controlled auto-ignition (HCCI) during load transient operations between modes of lean combustion low load (HCCI/Lean) and stiochiometric combustion medium load (HCCI/Stoich.). The method includes 1) operating the engine at steady state, within a homogeneous charge compression-ignition (HCCI) load range, with fuel-air-exhaust gas mixtures at predetermined conditions, for each speed and load, and controlling the engine during changes of operating mode between one to another of the HCCI/Stoich. medium load mode and the HCCI/Lean lower load mode by synchronizing change rates of predetermined controlled inputs to the current engine fueling change rate.

Abstract: A direct injection controlled auto-ignition engine is operated at steady state, within a homogeneous charge compression-ignition (HCCI) load range and with fuel-air-diluent mixtures at predetermined conditions, for each speed and load, of engine control inputs, including at least injection timing (FI), spark timing (SI), throttle position, exhaust gas recirculation (EGR) valve setting and exhaust recompression obtained by negative valve overlap (NVO). During engine speed transients, the control inputs are synchronized to changes in the current engine speed, and also with any concurrent changes in the engine fueling rate. Inputs that are inactive during all or part of a speed change have a zero change rate while inactive. The method maintains robust auto-ignition combustion during speed transients with constant or variable fueling rates and with or without load changes.