mhurhangee/ep-ind-claims huggingface dataset:
A respiratory mask assembly comprising: a mask frame and a cushion module, the mask frame comprising a breathing gas inlet configured to receive a supply of breathable gas and to deliver the breathable gas to the cushion module, and a cushion connector, the cushion module being configured to form a seal with a user's face; and the cushion module comprising a mask shell housing, the mask shell housing comprising a bias vent in communication with the cushion module, and configured to allow air to be exhausted from the cushion module through the bias vent; the mask frame being connected to the cushion module via the cushion connector, the cushion connector comprising a gas flow duct extending from the mask frame into the cushion module and arranged to deliver breathable gas to the cushion module from the breathing gas inlet; wherein the mask assembly further comprises: a diffuser comprising a diffuser frame, and diffuser material held by the diffuser frame and configured to extend over the bias vent, the diffuser material providing a tortuous air path from the bias vent through the diffuser; the diffuser frame comprising a mounting portion being configured to be mounted on the cushion connector, wherein the diffuser is removably mounted on the cushion module, and wherein the diffuser is sandwiched between the mask frame and the cushion module. a mask frame and a cushion module, the mask frame comprising a breathing gas inlet configured to receive a supply of breathable gas and to deliver the breathable gas to the cushion module, and a cushion connector, the cushion module being configured to form a seal with a user's face; and the cushion module comprising a mask shell housing, the mask shell housing comprising a bias vent in communication with the cushion module, and configured to allow air to be exhausted from the cushion module through the bias vent; the mask frame being connected to the cushion module via the cushion connector, the cushion connector comprising a gas flow duct extending from the mask frame into the cushion module and arranged to deliver breathable gas to the cushion module from the breathing gas inlet; wherein the mask assembly further comprises: a diffuser comprising a diffuser frame, and diffuser material held by the diffuser frame and configured to extend over the bias vent, the diffuser material providing a tortuous air path from the bias vent through the diffuser; the diffuser frame comprising a mounting portion being configured to be mounted on the cushion connector, wherein the diffuser is removably mounted on the cushion module, and wherein the diffuser is sandwiched between the mask frame and the cushion module.
A computer-implemented method comprising: displaying, by a processor, a graph of a set of interdependent files of an integrated development environment, IDE, project on a computer display, the graph depicting, for each file of the set of interdependent files, a starting point, and ending point, and one or more intermediate checkpoints; wherein the starting point, the ending point, and the one or more intermediate checkpoints each represent a time point; wherein each time point is associated with a state of file contents for said each file; wherein said each file has contents in a current state at a first time point; receiving, by a processor, input that indicates a particular time point that is earlier than the first time point; and re-creating, by a processor, an environment comprising file contents of the set of interdependent files; wherein the file contents in the environment has an historical state associated with the particular time point. displaying, by a processor, a graph of a set of interdependent files of an integrated development environment, IDE, project on a computer display, the graph depicting, for each file of the set of interdependent files, a starting point, and ending point, and one or more intermediate checkpoints; wherein the starting point, the ending point, and the one or more intermediate checkpoints each represent a time point; wherein each time point is associated with a state of file contents for said each file; wherein said each file has contents in a current state at a first time point; receiving, by a processor, input that indicates a particular time point that is earlier than the first time point; and re-creating, by a processor, an environment comprising file contents of the set of interdependent files; wherein the file contents in the environment has an historical state associated with the particular time point.
Curable composition, comprising a vinylester polymerisable compound, jointly with a sulphonated polyaromatic thermoplastic polymer and an N -vinyl lactam, characterised in that it further comprises: - a first non-vinylester polymerisable compound which comprises at least one isocyanurate group bearing a at least two (meth)acrylate groups; and - a second non-vinylester polymerisable compound which comprises at least one carbopolycyclic or heteropolycyclic group bearing at least two (meth)acrylate groups. - a first non-vinylester polymerisable compound which comprises at least one isocyanurate group bearing a at least two (meth)acrylate groups; and - a second non-vinylester polymerisable compound which comprises at least one carbopolycyclic or heteropolycyclic group bearing at least two (meth)acrylate groups.
A friction damper for dampening out vibrations generated by a drum of a laundry treating machine, comprising: - a hollow piston body; - a piston rod adapted to move telescopically along a central longitudinal axis of said piston body; - a friction element made of a resilient material interposed in between the piston body and the piston rod such that friction occurs when said piston rod moves relative to said piston body; - fixation portions provided at free ends of the piston rod and the piston body to connect the friction damper to the laundry treating machine; - at least one stopper portion (74, 94) interposed in between the piston body and the piston rod for limitation of the motion of the friction element in the direction of the central longitudinal axis wherein the friction damper comprises two separate stopper portions (74, 94) with a first inclined surface and a second inclined surface facing, respectively, the opposite flat impact surfaces (43, 45) of the friction element, wherein said inclined surfaces (72, 92) are inclined with respect to the central longitudinal axis of said piston body, and are arranged to be stroked by said flat impact surface (43, 45) of the friction element, characterised in that the each inclined surface (72, 92) is arranged to form an annular cavity between the stopper portion (74, 94) and the piston rod such that when the friction element hits the stopper portion (74, 94), one of the free ends of the friction element smashes and enters partially into said annular cavity. - a hollow piston body; - a piston rod adapted to move telescopically along a central longitudinal axis of said piston body; - a friction element made of a resilient material interposed in between the piston body and the piston rod such that friction occurs when said piston rod moves relative to said piston body; - fixation portions provided at free ends of the piston rod and the piston body to connect the friction damper to the laundry treating machine; - at least one stopper portion (74, 94) interposed in between the piston body and the piston rod for limitation of the motion of the friction element in the direction of the central longitudinal axis wherein the friction damper comprises two separate stopper portions (74, 94) with a first inclined surface and a second inclined surface facing, respectively, the opposite flat impact surfaces (43, 45) of the friction element, wherein said inclined surfaces (72, 92) are inclined with respect to the central longitudinal axis of said piston body, and are arranged to be stroked by said flat impact surface (43, 45) of the friction element, characterised in that the each inclined surface (72, 92) is arranged to form an annular cavity between the stopper portion (74, 94) and the piston rod such that when the friction element hits the stopper portion (74, 94), one of the free ends of the friction element smashes and enters partially into said annular cavity.
Foundation system for the foundation of an offshore construction, comprising: - a monopile having an anchoring portion which can be anchored in the seabed and comprising a connecting portion arranged at the opposite end; - a platform structure which can be connected to the connecting portion of the monopile directly or indirectly via a transition piece and can be arranged above the water surface; and - at least two stabilization devices (20, 21, 22), characterized in that the stabilization devices can each be connected directly to the platform structure or indirectly to the platform structure via the transition piece and can be brought into contact with the seabed, so that tensile and/or compressive forces can be transmitted between the seabed and the platform structure; wherein, in the installed state of the foundation system, fastening points of the stabilization devices (20, 21, 22) on the platform structure or on the transition piece, together with the connecting portion of the monopile, span a plane having a horizontal extension component; and the stabilization devices (20, 21, 22) extend perpendicularly from the platform structure and/or from the transition piece in the direction of the seabed and are in contact with the seabed. - a monopile having an anchoring portion which can be anchored in the seabed and comprising a connecting portion arranged at the opposite end; - a platform structure which can be connected to the connecting portion of the monopile directly or indirectly via a transition piece and can be arranged above the water surface; and - at least two stabilization devices (20, 21, 22), characterized in that the stabilization devices can each be connected directly to the platform structure or indirectly to the platform structure via the transition piece and can be brought into contact with the seabed, so that tensile and/or compressive forces can be transmitted between the seabed and the platform structure; wherein, in the installed state of the foundation system, fastening points of the stabilization devices (20, 21, 22) on the platform structure or on the transition piece, together with the connecting portion of the monopile, span a plane having a horizontal extension component; and the stabilization devices (20, 21, 22) extend perpendicularly from the platform structure and/or from the transition piece in the direction of the seabed and are in contact with the seabed.
A gas turbine comprising: a turbine disk rotatable about a rotational axis, when a turbine rotor blade for receiving combustion gas obtained by burning fuel is connected to a side periphery and energy of the combustion gas received by the turbine rotor blade is transmitted; the turbine disk being characterised by a radial passage that, in a cross-section at a virtual curved plane that is a curved plane about the rotational axis and in which distances from all points on the curved plane to the rotational axis are all equal, is a hole formed to include a portion having a shape in which a length in a circumferential direction of the turbine disk is longer than a length in a direction parallel to the rotational axis, and is formed in the turbine disk from a side of the rotational axis toward an outside of the turbine disk; wherein the radial passage includes a first open end opened to a space formed at an inner side of the side periphery of the turbine disk, and a second open end opened to the side periphery of the turbine disk, wherein the radial passage includes a portion other than that included in a virtual plane that includes the rotational axis, and wherein the radial passage is disposed such that, when the radial passage is seen in a projection view projected on a plane perpendicular to the rotational axis from a direction of the rotational axis, the radial passage is inclined at an angle equal to or more than 10 degrees and equal to or less than 45 degrees relative to a virtual reference plane including the first open end and the rotational axis. a turbine disk rotatable about a rotational axis, when a turbine rotor blade for receiving combustion gas obtained by burning fuel is connected to a side periphery and energy of the combustion gas received by the turbine rotor blade is transmitted; the turbine disk being characterised by a radial passage that, in a cross-section at a virtual curved plane that is a curved plane about the rotational axis and in which distances from all points on the curved plane to the rotational axis are all equal, is a hole formed to include a portion having a shape in which a length in a circumferential direction of the turbine disk is longer than a length in a direction parallel to the rotational axis, and is formed in the turbine disk from a side of the rotational axis toward an outside of the turbine disk; wherein the radial passage includes a first open end opened to a space formed at an inner side of the side periphery of the turbine disk, and a second open end opened to the side periphery of the turbine disk, wherein the radial passage includes a portion other than that included in a virtual plane that includes the rotational axis, and wherein the radial passage is disposed such that, when the radial passage is seen in a projection view projected on a plane perpendicular to the rotational axis from a direction of the rotational axis, the radial passage is inclined at an angle equal to or more than 10 degrees and equal to or less than 45 degrees relative to a virtual reference plane including the first open end and the rotational axis.
Gearbox arrangement of a rail vehicle, having at least one helically toothed spur gear pair comprising a driving pinion and a driven gear as meshing spur gears, which are mounted in a gearbox housing by way of cylindrical roller bearings (5, 5A), wherein, to at least one of the spur gears, there is fastened at least one thrust collar with an associated contact region (8, 8A) for absorbing axial forces, characterized in that each thrust collar is formed substantially as a thrust disk (7, 7A) with an associated contact region (8, 8A) on the circumferential region of the thrust disk (7, 7A), wherein at least the circumferential region of the thrust disk (7, 7A) is impinged on at least in sections with lubricant independently of the rotational movement.
A netting comprising an array of polymeric strands periodically joined together at bond regions throughout the array, the netting has first and second, generally opposed major surfaces, wherein the bond regions are generally perpendicular to the first and second major surfaces, wherein the array comprises a first plurality of strands having first and second, generally opposed major surfaces, wherein the array comprises a second plurality of strands having first and second, generally opposed major surfaces, wherein the first major surface of the netting comprises the first major surfaces of the first and second plurality of strands, wherein the second major surface of the netting comprises the second major surfaces of the first and second plurality of strands, wherein the first major surface of the first plurality of strands comprises a first material, wherein the second major surface of the first plurality of strands comprises a second material, wherein the first major surface of the second plurality of strands comprises a third material, wherein the second major surface of the second plurality of strands comprises a fourth material, wherein the first and second materials are different, and wherein the first material does not extend to the second major surface of the first plurality of strands.
A system for teleoperation of a machine having at least one actuated mechanism and a predetermined number of degrees of freedom, said system comprising: a control station remotely located from a location of said machine, said machine controlled from said control station to perform a predetermined function; a two way real-time communication link between said machine and said remotely located control station; and a controlling device associated with said machine at said machine location, said machine having predetermined safety limits which are stored in said controlling device and said stored safety limits are extracted (48; 602) and automatically mapped to said control station using said two way real-time communication link, characterised in that said safety limits include mechanical limits that limit a joint rotation range of said machine. a control station remotely located from a location of said machine, said machine controlled from said control station to perform a predetermined function; a two way real-time communication link between said machine and said remotely located control station; and a controlling device associated with said machine at said machine location, said machine having predetermined safety limits which are stored in said controlling device and said stored safety limits are extracted (48; 602) and automatically mapped to said control station using said two way real-time communication link, characterised in that said safety limits include mechanical limits that limit a joint rotation range of said machine.
A recombinant vesicular stomatitis virus vector encoding and expressing a membrane-anchored HIV Env immunogen and a natural VSV attachment protein having a truncated cytoplasmic tail, wherein the G gene is transferred to a position towards the 5'-terminus in the negative-sense RNA genome of the recombinant VSV vector, and the gene encoding the HIV Env immunogen is inserted into gene position 4 so that the genes in the VSV vector are arranged sequentially in the order 3'- - - -(HIV Env)- - -54', wherein the HIV Env immunogen is constructed to contain the VSV G transmembrane domain and a VSV G or cellular CD5 signal peptide, wherein the nucleotide sequence of the HIV Env immunogen has a codon bias consistent with the VSV genome and the VSV genome is stabilized with synonymous codons.
A computer system for anomaly detection using application telemetry, the computer system comprising: an electronic processor configured to receive telemetry data originating from a plurality of client applications, the telemetry data including data points representing errors associated with one or more operations of the plurality of client applications; the electronic processor is further configured to associate each data point with a branch of a plurality of branches included in a hierarchical map of data classes; for each of the plurality of branches included in the hierarchical map generate (506, 508) one or more metrics based on the number of data points associated with the branch; access a predictive scoring model to determine a prediction error associated with a branch of interest, wherein the prediction error is a difference between a predicted metric associated with the branch of interest and the generated one or more metrics for the branch of interest; and detect an anomaly when the prediction error is greater than a threshold; output an alert message associated with the anomaly; and a display device (139 to display the alert message. an electronic processor configured to receive telemetry data originating from a plurality of client applications, the telemetry data including data points representing errors associated with one or more operations of the plurality of client applications; the electronic processor is further configured to associate each data point with a branch of a plurality of branches included in a hierarchical map of data classes; for each of the plurality of branches included in the hierarchical map generate (506, 508) one or more metrics based on the number of data points associated with the branch; access a predictive scoring model to determine a prediction error associated with a branch of interest, wherein the prediction error is a difference between a predicted metric associated with the branch of interest and the generated one or more metrics for the branch of interest; and detect an anomaly when the prediction error is greater than a threshold; receive telemetry data originating from a plurality of client applications, the telemetry data including data points representing errors associated with one or more operations of the plurality of client applications; the electronic processor is further configured to associate each data point with a branch of a plurality of branches included in a hierarchical map of data classes; for each of the plurality of branches included in the hierarchical map generate (506, 508) one or more metrics based on the number of data points associated with the branch; access a predictive scoring model to determine a prediction error associated with a branch of interest, wherein the prediction error is a difference between a predicted metric associated with the branch of interest and the generated one or more metrics for the branch of interest; and detect an anomaly when the prediction error is greater than a threshold; output an alert message associated with the anomaly; and a display device (139 to display the alert message.
A method performed at a user equipment, UE, of linking carriers in a multi-carrier network, wherein the multi-carrier network includes a first downlink carrier, a second downlink carrier, and a third downlink carrier between a base station and the UE, comprising: receiving a Radio Resource Control, RRC, signaling; linking the first downlink carrier with the second downlink carrier using information in said RRC signaling, wherein said information includes the linking of the first downlink carrier with the second downlink carrier, and wherein said information indicates that the second downlink carrier can perform cross-carrier scheduling on the first downlink carrier; linking the first downlink carrier with the third downlink carrier using information in said RRC signaling, wherein said information includes the linking of the first downlink carrier with the third downlink carrier, and wherein said information indicates that the third downlink carrier can perform cross-carrier scheduling on the first downlink carrier; wherein the first downlink carrier may only be scheduled by one of the second or third downlink carrier at a time; and determining, when the second and third downlink carrier is active, whether the second downlink carrier or the third downlink carrier is used to perform cross-carrier scheduling on the first downlink carrier based on a predefined rule. receiving a Radio Resource Control, RRC, signaling; linking the first downlink carrier with the second downlink carrier using information in said RRC signaling, wherein said information includes the linking of the first downlink carrier with the second downlink carrier, and wherein said information indicates that the second downlink carrier can perform cross-carrier scheduling on the first downlink carrier; linking the first downlink carrier with the third downlink carrier using information in said RRC signaling, wherein said information includes the linking of the first downlink carrier with the third downlink carrier, and wherein said information indicates that the third downlink carrier can perform cross-carrier scheduling on the first downlink carrier; wherein the first downlink carrier may only be scheduled by one of the second or third downlink carrier at a time; and determining, when the second and third downlink carrier is active, whether the second downlink carrier or the third downlink carrier is used to perform cross-carrier scheduling on the first downlink carrier based on a predefined rule.