Abstract: A timeline generation and solving tool is provided to parameterize a project at an application lifecycle management (“ALM”) tool, and generate and solve a timeline of features according to the parameterized project. The Scrum master may re-parameterize the project, causing a new timeline to be generated, solved, and visualized. In this fashion, the Scrum master may rapidly prototype many project parameterizations, resulting in many possible timelines. Without the use of a timeline generation and solving tool which interfaces with an ALM tool, retrieves project features, and converts project features to a common format suitable for computations based on working speeds, a Scrum master would need to generate and check a timeline by hand, and work indirectly by manually copying data out of the ALM tool, leading to a slow and potentially error-prone project roadmapping process which does not permit rapid prototyping of possible timelines.

Abstract: Systems and methods for enabling auditing access to protected data stored at a data service using smart contracts on a blockchain are disclosed. According to certain aspects, a compliance management system may maintain and update a public blockchain with transaction indicative of non-compliance events associated with access to the protected data. Auditors or other third parties may access the public blockchain to audit the access to the protected data. Additionally, the compliance management system may implement a private blockchain to manage access restrictions to the protected data and process data requests for the protected data.

Abstract: Embodiments herein relate to an apparatus for use in a hybrid laser. The apparatus may include a silicon substrate and a waveguide to facilitate transmission of an optical signal in a first direction that is orthogonal to a surface of the silicon substrate. The apparatus may further include a metal shunt that is less than or equal to 10 micrometers from the waveguide in a second direction that is orthogonal to the surface of the silicon substrate and orthogonal to the first direction. Other embodiments may be described and/or claimed.

Abstract: The present invention presents a ring assembly 1 disposed radially outwardly of an array of circumferentially arranged blades 38 of a gas turbine engine rotor R. The ring assembly 1 includes ring segments 2 disposed circumferentially one adjacent to another and having a first circumferential end 2a and a second circumferential end 2b circumferentially spaced apart from each other. The first end 2a of a ring segment 2 and the second end 2b of an adjacent ring segment 2 of the plurality of ring segments 2 are arranged facing each other. An integrally formed projecting seal part 92 is formed at the first end 2a. An integrally formed receiving seal part 94 is formed at the second end 2b facing the first end 2a. The receiving seal part 94 receives the projecting seal part 92 to form a mating connection between the ring segment 2 and the adjacent ring segment 2. A gas turbine engine including the ring assembly 1 is also provided.

Abstract: A simulated payload apparatus (SPA) for testing in a flight motion system (FMS), which has a body for mounting in the FMS, and which simulates an actual payload during the FMS test. The SPA may include a plurality of adjustable weights that are mountable on and/or removable from the body to vary the mass and/or center of gravity of the SPA. The SPA may include an adjustable bracket for interfacing with a motion drive of the FMS, in which the bracket is positionable along the body to vary the moment of inertia of the SPA. The SPA may include an onboard electronic measurement device that is configured to measure a motion characteristic of the SPA and/or communicate information about the measured motion characteristic in real-time during the FMS test. The SPA may include a laser alignment for aligning the SPA relative to test equipment of the FMS.

Abstract: NEW MATERIAL: Recombinant plasmid pTPGIF2 having a size of 4,660 base pairs and a structure obtained by inserting a DNA having a size of 52 base pairs and containing a sequence coding somatostatin into a BamHI incision site of a plasmid vector pTP70-1 capable or fusing a heteropeptide to a carboxy-terminal of a dihydrofolic acid reductase gene of E. coli. USE: Producton of fused protein containing somatostatin. PREPARATION: A somatostatin gene is integrated into a plasmid vector pTP70-1. pTPGIF2 is kept in stable state when introduced into E. coli. C600 strain. The E. coli. C600 train containing pTPGIF2 is deposited in Fermentation Research institute as FERM BP-1577.

Abstract: The present technique presents a turbomachine component having an airfoil e.g. a vane of a gas turbine. The airfoil wall defines an internal space which includes a first and a second cooling channels having a first and a second impingement inserts, that define a first main and a first peripheral flow channels in the first cooling channel and a second main and a second peripheral flow channels in the second cooling channel, respectively. Impingement jets ejected from the main flow channels via impingement holes of the corresponding impingement inserts are received in the corresponding peripheral flow channels. A channel connecting conduit conducts a flow of the cooling air from the first cooling channel to the second cooling channel. The channel connecting conduit includes an inlet connected to an outlet of the first cooling channel, and an outlet connected to an inlet of the second cooling channel.

Abstract: A photonic integrated circuit including having a semiconductor substrate having integrated a semiconductor light source, the semiconductor light source comprising: an optically active section comprising a gain section and configured to support a first number of wavelengths, an optically passive section comprising a passive waveguide optically coupled to the optically active section and a passive section mirror optically coupled to the passive waveguide, wherein the optically passive section is configured to support a second number of wavelengths that is lower than the first number; and the optically passive section further comprising a signal shifting structure configured to shift a signal of the light supported by the passive waveguide.

Abstract: The present disclosure provides for unique onion plants with QTLs conferring Fusarium basal rot and pink root resistance and lacking the complementary pinks trait and their progeny. Such plants may comprise an introgressed QTL associated with multiple disease resistance coupled with a desirable bulb color. In certain aspects, compositions, including distinct polymorphic molecular markers, and methods for producing, breeding, identifying, selecting, and the like of plants or germplasm with disease resistance and/or desirable bulb color are provided.

Abstract: A connector assembly includes a first and a second releasable and mateable connector. Each connector includes a front assembly composed of a manifold and a plurality of optical stems. Each manifold includes a plurality of inserts and a plurality of spherical seal assemblies. Each seal assembly is composed of a spherical ball, a ball dowel pin, and a ball actuator pin having a cam. Each spherical ball is configured to rotate about an axis defined by the two pins when the actuator pin cam traverses a groove fabricated in one of a plurality of guide rails disposed in the first connector. When the plurality of seal assemblies are in an open configuration, the optical stems of the first connector may slide through the inserts of the first connector, through the seals, and mate with the optical stems of the second connector within the inserts of the second connector.

Abstract: A marquee banner assembly includes one or more lightweight molding(s) that may be bowed under tension, at least one or more channels configured for the insertion of a flexible sign, and attachment brackets attachable to a substrate which may any vertical surface. The attachment brackets are angled to provide a curvature to the molding when the molding is attached to the brackets. The assembly may employ natural light alone, or any combination of natural light, artificial light.

Abstract: A ring segment and a turbomachine including the ring segment are provided. The ring segment installed on an inner circumferential surface of a casing and disposed to face an end of a blade existing inside the casing, the ring segment includes a segment body disposed inside the casing in a radial direction of the casing and having a channel through which cooling air flows, and a pair of segment protrusions protruding outward from the segment body, coupled to the inner circumferential surface of the casing, and spaced apart from each other along a flow direction of fluid flowing through the casing to form an RS cavity through which cooling air flows, wherein the segment body includes a cavity for supplying cooling air introduced from the RS cavity to the channel.

Abstract: An electrolyzer cell, electrolyzer setup, and related methods are provided for converting gaseous carbon dioxide to gas-phase products at elevated pressures with high conversion rates via electrolysis performed by the electrolyzer cell (100?). The electrolyzer cell (100?) is a multi-stack CO2 electrolyzer cell having individual stacks (40) that each include bipolar plate assemblies that have unique gas and fluid flow architecture formed therein.

Abstract: A process or may reduce start latency of serverless microservices. The processor may detect an incoming request or event to an application in a serverless microservice environment. The incoming request or event may initiate a chain of invocations of one or more microservices of the application. The processor may select an amount of selected microservices from the one or more microservices of the application. The amount of selected microservices may perform a task of the incoming request or event. The task may apply one or more predefined application-specific rules to one or more elements of the incoming request or event to determine the amount of selected microservices. The processor may trigger scaling up activation of the one or more microservices of the application. The processor may invoke the one or more microservices of the application to match the amount of selected microservices.

Abstract: Impingement insert for an airfoil of a blade/vane of a gas turbine is provided. The impingement insert includes a triple-walled section having a central wall, an outer and an inner peripheral walls, that define—a central channel at an inner surface of the central wall, an inner channel between the central wall and the inner peripheral wall, a middle channel between the inner peripheral wall and the outer peripheral wall, and an outer channel at an outer surface of the outer peripheral wall. Impingement cooling holes are provided in the outer peripheral wall that use the cooling air of the middle channel to eject impingement jets into the outer channel.

Abstract: The present invention presents a ring assembly 1 disposed radially outwardly of an array of circumferentially arranged blades 38 of a gas turbine engine rotor R. The ring assembly 1 includes ring segments 2 disposed circumferentially one adjacent to another and having a first circumferential end 2a and a second circumferential end 2b circumferentially spaced apart from each other. The first end 2a of a ring segment 2 and the second end 2b of an adjacent ring segment 2 of the plurality of ring segments 2 are arranged facing each other. An integrally formed projecting seal part 92 is formed at the first end 2a. An integrally formed receiving seal part 94 is formed at the second end 2b facing the first end 2a. The receiving seal part 94 receives the projecting seal part 92 to form a mating connection between the ring segment 2 and the adjacent ring segment 2. A gas turbine engine including the ring assembly 1 is also provided.

Abstract: There is provided a client device arranged to receive a live adaptive bitrate stream, the client device further arranged to: request a manifest file; and request a manifest update hint. The client device further arranged to receive a manifest update hint, the manifest update hint including an indication of when the manifest will be updated; and request an updated manifest file at a time indicated by the manifest update hint.

Abstract: A simulated payload apparatus (SPA) for testing in a flight motion system (FMS), which has a body for mounting in the FMS, and which simulates an actual payload during the FMS test. The SPA may include a plurality of adjustable weights that are mountable on and/or removable from the body to vary the mass and/or center of gravity of the SPA. The SPA may include an adjustable bracket for interfacing with a motion drive of the FMS, in which the bracket is positionable along the body to vary the moment of inertia of the SPA. The SPA may include an onboard electronic measurement device that is configured to measure a motion characteristic of the SPA and/or communicate information about the measured motion characteristic in real-time during the FMS test. The SPA may include a laser alignment for aligning the SPA relative to test equipment of the FMS.

Abstract: A turbine vane is provided.

Abstract: Geographical mapping and linking of security and risk indicator data. Cross-references are created between location indicators and geo-spatial areas based on a statistical algorithm, in accordance with geo-spatial data. The cross-references are stored in a first data table. A credit risk indicator (CRI) is generated for each geo-spatial area based on other data, forming CRI data that is stored in second data table. A security associated with one of the location indicators is identified among security data. A first link is created between the security and a geo-spatial area based on the cross-references in the first data table. Based on the first link, a second link is created between an indicator among the CRI data in the second data table and the security. The second link is used to form instrument-level data for the security that includes the indicator. The instrument-level data is stored in a third data table.