mhurhangee/patent-ind-claim-en huggingface dataset:
A microfluidic device having a cavity defining a microfluidic volume, comprising: a plurality of meshes provided in the cavity , each mesh having a plurality of apertures and an outer surface ; said plurality of meshes being arranged in a layered configuration with the apertures of adjacent layers offset with respect to one another to define a plurality of circuitous pathways therethrough, wherein the apertures in each mesh are arranged in a grid, whereby the grid of one mesh is rotated with respect to the grid of an adjacent mesh; the outer surface of each mesh having a functionalising material applied thereto; wherein each mesh is formed of nickel. a plurality of meshes provided in the cavity , each mesh having a plurality of apertures and an outer surface ; said plurality of meshes being arranged in a layered configuration with the apertures of adjacent layers offset with respect to one another to define a plurality of circuitous pathways therethrough, wherein the apertures in each mesh are arranged in a grid, whereby the grid of one mesh is rotated with respect to the grid of an adjacent mesh; the outer surface of each mesh having a functionalising material applied thereto; wherein each mesh is formed of nickel.
A method for diagnosing tuberculosis disease (TB), the method comprising the step of testing a urine sample from a subject for the presence of SAA1 (Serum amyloid A1) and either of RETN (Resistin) or RBP4 (Retinol binding protein).
An air duct for a ventilation seat, comprising: an upper surface provided with a plurality of air outlets ; and a lower surface provided with an air inlet, and configured such that corners thereof are attached to corners of the upper surface to form an air passage, wherein the air duct comprises a spacer provided on at least one of the lower surface and the upper surface to extend toward the other surface; and a clamping portion provided on the upper surface which is coupled by clamping to clamping means provided on the lower surface .
Thermo-fusible conjugated fibers comprising a first component containing a polyester-based resin and a second component containing a polyolefin-based resin, wherein a melting point of the second component is 10°C or more lower than a melting point of the first component, the thermo-fusible conjugated fibers, characterized in that a work load at break obtained by dividing an area surrounded by a stress-strain curve and a horizontal axis by fineness [dtex] when the horizontal axis represents strain [cm] and a vertical axis represents stress [cN] and a tensile test is performed at a gauge length of 10 mm and a tensile speed of 20 mm/min is 1.9 cN·cm/dtex or more; a ratio of strength at break to elongation at break (strength at break [cN/dtex] / elongation at break [%]) obtained by a tensile test performed at a gauge length of 10 mm and a tensile speed of 20 mm/min is 0.005 to 0.040; a ratio of hot-temperature stretch ratio to low-temperature stretch ratio is in the range of 0.3 to 3.0; and a stretching temperature in stretching at a high temperature is in the range of 100 to 125°C and a stretching temperature in stretching at a low temperature is in the range of 60 to 90°C, wherein the workload at break, the strength at break, and the elongation at break are measured as defined in the description. the thermo-fusible conjugated fibers, characterized in that a work load at break obtained by dividing an area surrounded by a stress-strain curve and a horizontal axis by fineness [dtex] when the horizontal axis represents strain [cm] and a vertical axis represents stress [cN] and a tensile test is performed at a gauge length of 10 mm and a tensile speed of 20 mm/min is 1.9 cN·cm/dtex or more; a ratio of strength at break to elongation at break (strength at break [cN/dtex] / elongation at break [%]) obtained by a tensile test performed at a gauge length of 10 mm and a tensile speed of 20 mm/min is 0.005 to 0.040; a ratio of hot-temperature stretch ratio to low-temperature stretch ratio is in the range of 0.3 to 3.0; and a stretching temperature in stretching at a high temperature is in the range of 100 to 125°C and a stretching temperature in stretching at a low temperature is in the range of 60 to 90°C, wherein the workload at break, the strength at break, and the elongation at break are measured as defined in the description.
A propeller fan , comprising: a shaft portion disposed on a rotation axis (R) of the propeller fan ; and a blade disposed on an outer peripheral side of the shaft portion , and including a leading edge and a trailing edge , wherein the blade includes a negative pressure surface in which a plurality of recesses are formed, and the plurality of recesses include a first recess and a second recess disposed more on the trailing edge side than the first recess in a circumferential direction about the rotation axis (R) as a center, wherein the first recess has a depth larger than a depth of the second recess , and wherein each of the plurality of recesses has, in a cross section taken in the circumferential direction, a first opening end on the leading edge side and a second opening end on the trailing edge side, and characterized in that the first opening end has a radius of curvature (R1) smaller than a radius of curvature (R2) of the second opening end , and in each of the plurality of recesses , a depth on the leading edge side is larger than a depth on the trailing edge side. a shaft portion disposed on a rotation axis (R) of the propeller fan ; and a blade disposed on an outer peripheral side of the shaft portion , and including a leading edge and a trailing edge , wherein the blade includes a negative pressure surface in which a plurality of recesses are formed, and the plurality of recesses include a first recess and a second recess disposed more on the trailing edge side than the first recess in a circumferential direction about the rotation axis (R) as a center, wherein the first recess has a depth larger than a depth of the second recess , and wherein each of the plurality of recesses has, in a cross section taken in the circumferential direction, a first opening end on the leading edge side and a second opening end on the trailing edge side, and characterized in that the first opening end has a radius of curvature (R1) smaller than a radius of curvature (R2) of the second opening end , and in each of the plurality of recesses , a depth on the leading edge side is larger than a depth on the trailing edge side.
A method comprising: receiving , by a Mobility Management Entity, MME , of a carrier network, a request associated with a user equipment, UE , for a Non-IP Data Delivery, NIDD, connection via a service capability exposure function, SCEF ; transmitting , by the MME and to the SCEF , a connection management request to establish a session, the connection management request using a first SCEF identifier, ID, provisioned for NIDD via the SCEF ; receiving , by the MME and from a particular SCEF instance of the SCEF , a connection management answer for the session, the connection management answer including an identifier that is different from the first SCEF-ID, the identifier associated with the particular SCEF instance; and transmitting, by the MME and to the particular SCEF instance, a subsequent message for the session, wherein a second SCEF-ID of the subsequent message is associated with the identifier and is different from the first SCEF-ID. receiving , by a Mobility Management Entity, MME , of a carrier network, a request associated with a user equipment, UE , for a Non-IP Data Delivery, NIDD, connection via a service capability exposure function, SCEF ; transmitting , by the MME and to the SCEF , a connection management request to establish a session, the connection management request using a first SCEF identifier, ID, provisioned for NIDD via the SCEF ; receiving , by the MME and from a particular SCEF instance of the SCEF , a connection management answer for the session, the connection management answer including an identifier that is different from the first SCEF-ID, the identifier associated with the particular SCEF instance; and transmitting, by the MME and to the particular SCEF instance, a subsequent message for the session, wherein a second SCEF-ID of the subsequent message is associated with the identifier and is different from the first SCEF-ID.
An aircraft hand controller, comprising: a single hand grip structure having two opposite ends, wherein the single hand grip structure is configured to be rigidly mounted to an aircraft; a set of finger controls on the single hand grip structure, the set of finger controls including: a first finger control (204; 234) configured to control throttle of the aircraft, wherein the first finger control is mounted at one end of the hand grip structure and an opposite end of the hand grip structure is configured to be attached to the aircraft; and a second finger control , separate from the first, configured to control rotation about a first rotational axis of the aircraft, wherein the second finger control is mounted on the hand grip structure so as to be facing away from a pilot. a single hand grip structure having two opposite ends, wherein the single hand grip structure is configured to be rigidly mounted to an aircraft; a set of finger controls on the single hand grip structure, the set of finger controls including: a first finger control (204; 234) configured to control throttle of the aircraft, wherein the first finger control is mounted at one end of the hand grip structure and an opposite end of the hand grip structure is configured to be attached to the aircraft; and a second finger control , separate from the first, configured to control rotation about a first rotational axis of the aircraft, wherein the second finger control is mounted on the hand grip structure so as to be facing away from a pilot. a first finger control (204; 234) configured to control throttle of the aircraft, wherein the first finger control is mounted at one end of the hand grip structure and an opposite end of the hand grip structure is configured to be attached to the aircraft; and a second finger control , separate from the first, configured to control rotation about a first rotational axis of the aircraft, wherein the second finger control is mounted on the hand grip structure so as to be facing away from a pilot.
A communications device for transmitting or receiving signals for communicating data under control of a wireless communications network, the communications device comprising circuitry configured to receive, from the infrastructure equipment, first slot configuration information (S111) indicating one or more of a plurality of symbols of a slot are to be used for transmitting signals from the communications device, and one or more of the plurality of symbols are to be used for receiving signals at the communications device, or one or more of the plurality of symbols are flexible symbols; and to receive second slot configuration information indicating a configuration of one or more of the plurality of symbols of the slot (S112); and in a case that the first slot configuration information indicates one or more of the plurality of symbols are flexible symbols and the second slot configuration information indicates that one or more of the plurality of symbols of the slot are configured differently from the first slot configuration information (S114), to determine to receive one or more of the plurality of symbols based on the second slot configuration information, wherein the second slot configuration information has a dynamic characteristic of a higher rate of change of the second slot configuration information than one of the first slot configuration information. circuitry configured to receive, from the infrastructure equipment, first slot configuration information (S111) indicating one or more of a plurality of symbols of a slot are to be used for transmitting signals from the communications device, and one or more of the plurality of symbols are to be used for receiving signals at the communications device, or one or more of the plurality of symbols are flexible symbols; and to receive second slot configuration information indicating a configuration of one or more of the plurality of symbols of the slot (S112); and in a case that the first slot configuration information indicates one or more of the plurality of symbols are flexible symbols and the second slot configuration information indicates that one or more of the plurality of symbols of the slot are configured differently from the first slot configuration information (S114), to determine to receive one or more of the plurality of symbols based on the second slot configuration information, wherein the second slot configuration information has a dynamic characteristic of a higher rate of change of the second slot configuration information than one of the first slot configuration information.
A method comprising: receiving, by a first wireless device from a base station, an indication for wireless device assisted resource selection being enabled or disabled; receiving, by the first wireless device from a second wireless device and based on the indication for the wireless device assisted resource selection being enabled, a configuration message indicating a subset from a plurality of subsets in a resource pool; based on a sensing operation, selecting, by the first wireless device, one or more transmission resources from the subset; and transmitting, by the first wireless device, one or more transport blocks via the one or more transmission resources. receiving, by a first wireless device from a base station, an indication for wireless device assisted resource selection being enabled or disabled; receiving, by the first wireless device from a second wireless device and based on the indication for the wireless device assisted resource selection being enabled, a configuration message indicating a subset from a plurality of subsets in a resource pool; based on a sensing operation, selecting, by the first wireless device, one or more transmission resources from the subset; and transmitting, by the first wireless device, one or more transport blocks via the one or more transmission resources.
Rotating electrical machine , notably for a motor vehicle, comprising: - a heat sink provided with at least one housing , - an electrical module positioned in the housing and comprising at least one connection terminal , - a connector comprising at least one track linked electrically to the connection terminal and a housing intended to receive a link means, notably a head of a screw , ensuring a mechanical and electrical link between the track of the connector and the heat sink , and - an airflow loopback prevention element interposed between a bearing of the rotating electrical machine and the connector , characterized in that the airflow loopback prevention element is disposed to avoid the recirculation of hot air and comprises at least one sealing plug of the housing of the link means. - a heat sink provided with at least one housing , - an electrical module positioned in the housing and comprising at least one connection terminal , - a connector comprising at least one track linked electrically to the connection terminal and a housing intended to receive a link means, notably a head of a screw , ensuring a mechanical and electrical link between the track of the connector and the heat sink , and - an airflow loopback prevention element interposed between a bearing of the rotating electrical machine and the connector ,
A latch system comprising: a paddle button assembly that includes a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly , wherein the first hook assembly includes a first hook and the first striker assembly includes a first striker , wherein the first hook assembly includes a first rotary member that includes the first hook , wherein the first rotary member is movable between a first position where the first hook is engaged with the first striker and a second position where the first hook is not engaged with the first striker , wherein the first rotary member is enclosed in a housing and includes a first closeout member , wherein the housing includes a striker opening defined in a top wall thereof, and wherein the first closeout member is generally aligned with the striker opening so to prevent objects from entering the striker opening when the first rotary member is in the second position, and a first cable that extends between the paddle button assembly and the first latch assembly , wherein movement of the button from the home position to the actuation position moves the first cable , thereby disengaging the first hook assembly and the first striker assembly . a paddle button assembly that includes a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly , wherein the first hook assembly includes a first hook and the first striker assembly includes a first striker , wherein the first hook assembly includes a first rotary member that includes the first hook , wherein the first rotary member is movable between a first position where the first hook is engaged with the first striker and a second position where the first hook is not engaged with the first striker , wherein the first rotary member is enclosed in a housing and includes a first closeout member , wherein the housing includes a striker opening defined in a top wall thereof, and wherein the first closeout member is generally aligned with the striker opening so to prevent objects from entering the striker opening when the first rotary member is in the second position, and a first cable that extends between the paddle button assembly and the first latch assembly , wherein movement of the button from the home position to the actuation position moves the first cable , thereby disengaging the first hook assembly and the first striker assembly .
A method of asynchronously controlling a winding machine, the method comprising: producing a system master count that varies from an initial count value to a final count value over a series of repeating system operational cycles; providing at least one sub-system master count, that begins when the system master count reaches a respective first lock-on count value; operating at least one machine component based on a component operating profile and the value of a sub-system master count; stopping at least one sub-system master count without stopping the system master count; and starting at least one previously-stopped sub-system master count at a second lock-on count value that is the same as or different from the respective first lock-on count value; wherein the rate of the system master count and at least one sub-system master count are not equal during at least part of an operational cycle; and further comprising receiving feedback during the operation of the at least one component; wherein based on the feedback, the rate of a sub-system master count is varied. producing a system master count that varies from an initial count value to a final count value over a series of repeating system operational cycles; providing at least one sub-system master count, that begins when the system master count reaches a respective first lock-on count value; operating at least one machine component based on a component operating profile and the value of a sub-system master count; stopping at least one sub-system master count without stopping the system master count; and starting at least one previously-stopped sub-system master count at a second lock-on count value that is the same as or different from the respective first lock-on count value; wherein the rate of the system master count and at least one sub-system master count are not equal during at least part of an operational cycle; and further comprising receiving feedback during the operation of the at least one component; wherein based on the feedback, the rate of a sub-system master count is varied.
A method for wireless communication in a system that supports a first transmission time interval, TTI, duration and a second TTI duration that is less than the first TTI duration, the method comprising: identifying , at a user equipment, UE , a first uplink control channel message scheduled for a first transmission time during a TTI having the first TTI duration; identifying , at the UE , a second uplink control channel message scheduled for a second transmission time during a TTI having the second TTI duration; determining , at the UE , that the first transmission time overlaps with the second transmission time; and transmitting , from the UE to a base station , the second uplink control channel message based at least in part on the determination that the first transmission time overlaps with the second transmission time, wherein the second uplink control channel message comprises a portion of a periodic channel state information, P-CSI, report associated with the first TTI duration and refraining from transmitting the first uplink control channel message based at least in part on the determination that the first transmission time overlaps with the second transmission time. identifying , at a user equipment, UE , a first uplink control channel message scheduled for a first transmission time during a TTI having the first TTI duration; identifying , at the UE , a second uplink control channel message scheduled for a second transmission time during a TTI having the second TTI duration; determining , at the UE , that the first transmission time overlaps with the second transmission time; and transmitting , from the UE to a base station , the second uplink control channel message based at least in part on the determination that the first transmission time overlaps with the second transmission time, wherein the second uplink control channel message comprises a portion of a periodic channel state information, P-CSI, report associated with the first TTI duration and refraining from transmitting the first uplink control channel message based at least in part on the determination that the first transmission time overlaps with the second transmission time.
Lubrication unit for a turbomachine , notably an aircraft turbojet engine, the lubrication unit comprising: - at least two pumps (30; 32), and - a body which exhibits a passage communicating with each of the pumps (30; 32), characterized in that the material of the body exhibits a stack of layers (40; 140) in a direction of stacking (44; 144), the pumps (30; 32) being housed in the said stack of layers (40; 140), and in that the passage exhibits an end (86; 186) in the direction of stacking (44; 144) of the layers (40; 140), and a profile (78; 178) with a first straight line (80; 180) and a second straight line (82; 182) which form the said end (86; 186) and which are inclined with respect to the layers (40; 140) of the stack. - at least two pumps (30; 32), and - a body which exhibits a passage communicating with each of the pumps (30; 32),