Abstract: Embodiments include in response to monitoring a processor during operation, detecting a first number of throttling amounts in the processor, determining that the first number of throttling amounts fulfills a first condition regarding a throttling amounts threshold, and modifying a voltage level of the processor by a first amount. Embodiments include in response to modifying the voltage level of the processor by the first amount, detecting a second number of throttling amounts in the processor, determining that the second number of throttling amounts fulfills a second condition regarding the throttling amounts threshold, and modifying the voltage level of the processor by a second amount.

Abstract: Deployment of arrangements of computing components coupled over a communication fabric are presented herein. In one example, a method includes detecting first computing components communicatively coupled to a first communication fabric having a first communication fabric type, and detecting second computing components communicatively coupled to a second communication fabric having a second communication fabric type. The method also includes receiving user commands to form compute units among a pool of computing components comprising the first computing components and the second computing components. Based at least on the user commands, the method includes forming the compute units for use by one or more users.

Abstract: Disaggregated computing architectures, platforms, and systems are provided herein. In one example, a method includes instructing a communication fabric to establish a first logical partition in the communication fabric that includes a first processing device and a memory device, and directing transfer of configuration data for storage by the memory device over the first logical partition. After transfer of the configuration data, the method includes instructing the communication fabric to remove the first logical partition in the communication fabric, where the configuration data remains stored by the memory device after removal of the first logical partition. The method also includes instructing the communication fabric to establish a second logical partition in the communication fabric that includes at least a second processing device and the memory device comprising the configuration data, where the second processing device is operated using the configuration data.

Abstract: Deployment of arrangements of computing components coupled over communication fabrics are presented herein. In one example, a method includes forming a compute unit to include at least a selected disaggregated computing component and at least a selected converged computing element. The selected disaggregated computing component is added to the compute unit from a pool of disaggregated computing components having a granularity comprising the disaggregated computing components arbitrarily and separately coupled to a communication fabric. The selected converged computing element is added to the compute unit from a pool of converged computing elements having a granularity comprising sets of computing components with fixed relationships to associated processors.

Abstract: An oral product includes a body that is wholly receivable in an oral cavity. The body includes a mouth-soluble polymer matrix, cellulosic fibers embedded in the mouth-soluble polymer matrix, and nicotine or a derivative thereof dispersed in the mouth-soluble polymer matrix. The oral product is adapted to release the nicotine or a derivative thereof from the body when the body is received within the oral cavity and exposed to saliva.

Abstract: Aspects of the present disclosure relate to methods, systems, and apparatus for wireless gravitational wave communication. In one or more embodiments, a method of wireless gravitational wave communication includes generating one or more gravitational wave signals at a first site. The generating of the one or more gravitational wave signals includes rotating and/or angularly accelerating one or more rotatable masses at a plurality of states. The method includes transmitting the one or more gravitational wave signals to a receiver in a wireless manner, and receiving the one or more gravitational wave signals at a second site using the receiver. The method includes determining (such as by decoding) information from the one or more gravitational wave signals.

Abstract: Aspects of the present disclosure relate to generation of a semi-coherent gravitational wave beam and related apparatus, systems, and methods, such as for at least gravitational wave communication. In one or more embodiments, a gravitational wave generator includes a generator frame, and a first rotatable mass mounted to the generator frame. The first rotatable mass is rotatable about a generator axis and rotatable relative to the generator frame to generate one or more gravitational waves. The gravitational wave generator includes one or more wave guide stages that include two or more guide assemblies. The two or more guide assemblies each include a guide frame, and a second rotatable mass mounted to the guide frame. The second rotatable mass is rotatable about a guide axis and rotatable relative to the guide frame to at least partially focus the one or more gravitational waves into one or more collimated beams.

Abstract: Aspects of the present disclosure relate to testing apparatus and methods for measuring forces between objects. The apparatus and methods are used to detect a change in the local gravitational constant resulting from non-Newtonian effects of General Relativity and/or a novel radial dilation influence. Detection is facilitated by measuring a force difference between a stationary state and a spinning state of attractive forces between objects. The apparatus and methods are used to detect a change in electromechanical influence of forces due to the Barnett affect and other anomalous electromagnetic force contributors. A testing apparatus includes a central target arrangement. The central target arrangement includes a pair of masses, and a target coupled to the pair of masses. The testing apparatus includes a detector configured to recognize the target, and a first rotatable mass. The first rotatable mass is supported independently of the target and the pair of target masses.

Abstract: Embodiments presented herein provide techniques for evaluating an asynchronous application using a test framework. The test framework may perform a load test of an asynchronous application or service composed from a collection of applications or services. To do so, the test framework may submit transactions to a distributed application at a specified transaction rate and monitor how the distributed application operates at that transaction rate. An aggregate load test component may evaluate the remaining work pending at work accumulation points of the distributed application to determine whether the distributed application can sustain the specified transaction rate. A transaction tracking component may initiate transactions to generate load at the specified transaction rate without blocking while the transactions are processed by the distributed application.

Abstract: An aircraft wing box is disclosed having a first cover, a second cover, a partition extending between the first and second cover and configured to provide a fuel tight boundary between the first and second covers, a first joint coupling the partition to the first cover, and a second joint coupling the partition to the second cover. The first joint is a slip joint configured to inhibit fuel leakage across the slip joint whilst permitting relative movement between the partition and the first cover.

Abstract: Embodiments of snout extension agricultural tools for combine heads are disclosed. Said tools assist in harvesting of crops in order to maximize yield of crops and downed crops.

Abstract: An aircraft wing box is disclosed having a fuel tank with a fuel-tight boundary, upper and lower covers, forward and aft spars, and a partition including an inboard portion, an outboard portion, and a third portion between the inboard and outboard portions. Each cover is attached to each spar, the inboard portion of the partition is joined to each cover and joined to one of the spars, the outboard portion of the partition is joined to each cover and joined to one of the spars, each cover is joined to the partition. The inboard part, outboard part and third part of the partition are integrally formed as a single-piece; and the single-piece provides part of the fuel-tight boundary of the fuel tank.

Abstract: A combine header having a snout extension with a flat bottom surface base component converging toward each other, a cover arching over the base component and conforming to and at least as wide as the snout. Connecting plates on opposite sides of the snout extension tool attaching the snout extension tool to the snout.

Abstract: Systems and methods for predicting multiple health care outcomes are provided. In one embodiment, a method includes receiving clinical data relating to a patient, calculating, with a multi-tasking deep neural network model, a plurality of health outcomes for the patient based on the received clinical data, and displaying one or more of the plurality of health outcomes. In this way, the richness of health care data may be leveraged to predict multiple health care outcomes with a single predictive model.

Abstract: An aircraft wing box is disclosed having a fuel tank with a fuel-tight boundary, upper and lower covers, forward and aft spars, and a partition including an inboard portion, an outboard portion, and a third portion between the inboard and outboard portions. Each cover is attached to each spar, the inboard portion of the partition is joined to each cover and joined to one of the spars, the outboard portion of the partition is joined to each cover and joined to one of the spars, each cover is joined to the partition. The inboard part, outboard part and third part of the partition are integrally formed as a single-piece; and the single-piece provides part of the fuel-tight boundary of the fuel tank.

Abstract: An aircraft wing box is disclosed having a first cover, a second cover, a partition extending between the first and second cover and configured to provide a fuel tight boundary between the first and second covers, a first joint coupling the partition to the first cover, and a second joint coupling the partition to the second cover. The first joint is a slip joint configured to inhibit fuel leakage across the slip joint whilst permitting relative movement between the partition and the first cover.

Abstract: A wearable connection and resistance training system having a waist strap, and left and right upper leg straps and an attachment point device which serves as a connection piece configured to be held underneath a user's torso and between the user's legs to provide rotational resistance to improve and strengthen rotational abilities of a user. An alignment attachment piece and foot straps can also be attached to provide downward force/tension.

Abstract: A management system for managing, streamlining and automating the process of obtaining contributions for philanthropic entities (e.g., charities and other non-profit organizations), wherein user friendly Internet based processes are provided to (potential and actual) contributors that substantially eases the burden on such contributors in, e.g., contributing to such entities via planned giving or estate planning. For each of the philanthropic entities, the management system automates and facilitates the marketing and estate planning aspects for obtaining contributions in a manner that is consistent with the avowed beliefs and/or values of the entity, and that provides potential and actual contributors with contacts to professionals that also share the beliefs and/or values of the entity.

Abstract: A sound suppressor with integrated ablative injection system for firearms or similar devices includes a hollow elongate body, having a projectile entry via a proximal threaded base cap featuring an opening into which the barrel is affixed, an interior space through which the projectile and propellant gasses pass and a distal threaded end cap opposite of the projectile entry featuring an opening through which the projectile and propellant gases exit. The elongate body contains within a blast chamber through which the projectile passes and into which propellant gas enters and expands. Subsequent to the blast chamber, the elongate body contains a plurality of individual serially placed baffles designed to slow and disrupt the flow of propellant gasses. The device features an injection port, affixed to which is a valve or fitting into which an ablative media is injected and through which said ablative media is introduced into the blast chamber.

Abstract: A system and method for determining near-wellbore fracture characteristics of an isolated portion of a hydraulically fractured well are provided. A valve located in a string extending to the isolated portion of the well is utilized to reduce the wellbore storage effects of fluid in the string on pressure measurements within the isolated zone of the wellbore.