mhurhangee/ep-ind-claims huggingface dataset:
A method of wireless communication by a transmitting wireless device, the method comprising: mapping a plurality of codeblocks, CBs, for a multi-slot transport block, TB, to a plurality of codeblock groups, CBGs, the multi-slot TB spanning a number of slots determined to accommodate a radio link control, RLC, service data unit, SDU, without segmentation by a RLC layer of the transmitting wireless device; mapping a plurality of sets of one or more CBGs of the plurality of CBGs to a plurality of slots of the multi-slot TB, each set of CBGs being mapped to a respective slot of the plurality of slots such that all the CBs in each respective CBG are mapped to the respective slot and such that all the CBs in each respective CBG are entirely contained within the respective slot; and transmitting, to a receiving wireless device, the multi-slot TB including the plurality of CBs over the plurality of slots, each set of CBGs corresponding to a respective TB segment of a plurality of TB segments of the multi-slot TB. mapping a plurality of codeblocks, CBs, for a multi-slot transport block, TB, to a plurality of codeblock groups, CBGs, the multi-slot TB spanning a number of slots determined to accommodate a radio link control, RLC, service data unit, SDU, without segmentation by a RLC layer of the transmitting wireless device; mapping a plurality of sets of one or more CBGs of the plurality of CBGs to a plurality of slots of the multi-slot TB, each set of CBGs being mapped to a respective slot of the plurality of slots such that all the CBs in each respective CBG are mapped to the respective slot and such that all the CBs in each respective CBG are entirely contained within the respective slot; and transmitting, to a receiving wireless device, the multi-slot TB including the plurality of CBs over the plurality of slots, each set of CBGs corresponding to a respective TB segment of a plurality of TB segments of the multi-slot TB.
A rotary pump, including a magnetic rotor arranged in a pump housing and having a magnetic rotor plane, which rotor is operatively connected to a drive for conveying a fluid, wherein an inlet opening is provided at the pump housing for the inlet of the fluid into the pump housing and a radial outlet passage is provided for conveying the fluid out of the pump housing and wherein the drive is a bearingless motor having a stator configured as a bearing stator and drive stator and having a magnetic stator plane, which stator bears a drive coil and a bearing coil lying in the stator plane and/or a drive bearing coil, wherein the rotor is magnetically contactlessly journalled within the stator and an axial height of the rotor is smaller than or equal to half a diameter of the rotor so that the rotor is passively magnetically stabilized by reluctance forces with respect to the magnetic stator plane both against an axial displacement and against a tiling from an equilibrium position, characterized in that the outlet passage is radially outwardly conducted away from the pump housing in the region of the stator such that a center axis of the radial outlet passage coincides with the magnetic rotor plane or with the magnetic stator plane.
A blow molding mold adapted to be mounted to a blow molding device and having a cavity surface on an inner side thereof, wherein a preform having a bottomed tubular shape is fittable in the blow molding mold, and the blow molding device has a pressurized liquid supply function of supplying a pressurized liquid through a blow nozzle connected to a mouth tubular portion of the preform to stretch the preform toward the cavity surface to thereby mold a container and also has a head space defining function of defining head space (Hs) in the container by drawing back a part of the liquid filled into the container through the blow nozzle or by withdrawing a stretching rod, which is used to stretch the preform in a longitudinal direction, from the container filled with the liquid, and wherein the cavity surface includes a bottom forming surface, a trunk forming surface, a shoulder forming surface, and a mouth forming surface that correspond to external shapes of a bottom, a trunk, a shoulder, and a mouth of the container, respectively, and the trunk forming surface includes a flattened portion that, in a transverse section thereof, has a flattened shape.
Test system with a manipulation device, a testing unit and a housed integrated circuit, wherein the manipulation device comprises a receiving unit with a mount and the mount receives the housed integrated circuit and the housing integrated circuit has an upper side and a lower side, and a plurality of electrical connecting contacts is formed at the lower side, and an electrical connection is present between the mount and the connecting contacts and the manipulation device by means of the receiving unit in a first state provides the integrated circuit for the testing unit, and wherein in the first state the testing unit is arranged above the upper side of the integrated circuit and forms a connection with the manipulation device and the testing unit executes a functional test at the integrated circuit, characterised in that the integrated circuit has at the upper side in the housing an opening with a sensor device formed in the opening and the upper side of the integrated circuit is oriented in the direction of the testing unit and the electrical connecting contacts are electrically connected with the receiving unit of the manipulation device in order to check the function of the integrated sensor device.
A sports device comprising an abutment formed as a rod having a rigid support at its first end and a second end, which second end is formed as a free end and to which second end a person performing a movement can be connected at a body part via a rope by exerting a force on the second end, characterised in that a subregion of the rod has a rod cross-section, which rod cross-section has an element having an element height increasing from the central point of the rod cross-section towards a peripheral zone.
A method in a mobile communications device, comprising: detecting user activity with respect to a digital camera of the mobile communications device; and in response to detected user activity, and prior to receiving user input for triggering the capture of an image using the digital camera, initiating the acquisition of a position fix for the mobile communications device; wherein the mobile communications device is a PDA Pocket PC, a tablet equipped with GPS, a GPS-enabled camera-phone or a smart phone; and wherein initiating the acquisition of a position fix comprises obtaining assistance data for a satellite-based navigation-signal broadcast system. detecting user activity with respect to a digital camera of the mobile communications device; and in response to detected user activity, and prior to receiving user input for triggering the capture of an image using the digital camera, initiating the acquisition of a position fix for the mobile communications device; wherein the mobile communications device is a PDA Pocket PC, a tablet equipped with GPS, a GPS-enabled camera-phone or a smart phone; and wherein initiating the acquisition of a position fix comprises obtaining assistance data for a satellite-based navigation-signal broadcast system.
A heat sink assembly including: a heat sink having a base and fins extending from the base; and a spring clip disposed on the heat sink between the fins, the spring clip including: a first tab that forms a first angle with respect to the base of the heat sink; a second tab that forms a second angle with respect to the base of the heat sink; and a serpentine portion, interposed between the first tab and the second tab, and extending in a plane that is parallel to an upper surface of the base of the heat sink, wherein the spring clip is resilient such that the first and second tabs can be compressed toward the base of the heat sink without any permanent deformation of the spring clip. a heat sink having a base and fins extending from the base; and a spring clip disposed on the heat sink between the fins, the spring clip including: a first tab that forms a first angle with respect to the base of the heat sink; a second tab that forms a second angle with respect to the base of the heat sink; and a serpentine portion, interposed between the first tab and the second tab, and extending in a plane that is parallel to an upper surface of the base of the heat sink, wherein the spring clip is resilient such that the first and second tabs can be compressed toward the base of the heat sink without any permanent deformation of the spring clip.
A spermatic bio-stabiliser polypeptide FB-sp, CHARACTERIZED in that it has the amino acid sequence according to SEQ ID NO: 1 (using 1 letter nomenclature): RPGLPVFSPL.
A gate valve comprising: a valve body capable of closing a flow passage by being inserted between a pair of fluid pipes; a valve cage configured to be disposed between the pair of fluid pipes and accommodating the valve body; and a sealing band configured to cover between the pair of fluid pipes and the valve cage under a sealed state; the valve cage including a pair of protruding tubular portions protruding from a body of the valve cage in a pipe axis direction of the fluid pipes; and the sealing band including a pair of main body portions and a connecting portion connecting the pair of main body portions and formed unitarily therewith, the sealing band being constituted of a plurality of split members (Ba) split in a circumferential direction of the fluid pipes, the pair of main body portions being configured to cover the respective fluid pipes and the protruding tubular portions under a sealed state, the connecting portion being opposed to a lateral face of the valve cage body extending along the pipe axis direction. a valve body capable of closing a flow passage by being inserted between a pair of fluid pipes; a valve cage configured to be disposed between the pair of fluid pipes and accommodating the valve body; and a sealing band configured to cover between the pair of fluid pipes and the valve cage under a sealed state; the valve cage including a pair of protruding tubular portions protruding from a body of the valve cage in a pipe axis direction of the fluid pipes; and the sealing band including a pair of main body portions and a connecting portion connecting the pair of main body portions and formed unitarily therewith, the sealing band being constituted of a plurality of split members (Ba) split in a circumferential direction of the fluid pipes, the pair of main body portions being configured to cover the respective fluid pipes and the protruding tubular portions under a sealed state, the connecting portion being opposed to a lateral face of the valve cage body extending along the pipe axis direction.
A composition comprising at least one biological control agent selected from the group consisting of Bacillus subtilis AQ713 (NRRL Accession No. B-21661) and Bacillus subtilis AQ30002 (NRRL Accession No. B-50421) and at least one fungicide which is fluopicolide in a synergistically effective amount, wherein the weight ratio between said biological control agent and said fungicide is in the range of 1:0.005 to 1:0.5.
A gas treating apparatus comprising: a reaction chamber configured to process by a plasma a gas supplied from an outside, the processed gas containing a nitrogen oxide; and a nitrogen oxide reduction apparatus connected to the reaction chamber, wherein the nitrogen oxide reduction apparatus includes a cooling unit; characterised in that said cooling unit is configured to cool the processed gas to a temperature lower than a nitrogen oxide generation temperature by use of a low temperature inert gas, wherein the cooling unit includes a plurality of gas injection nozzles configured to inject said low-temperature inert gas, and wherein the gas injection nozzles are provided at multiple levels with different heights of the nitrogen oxide reduction apparatus. a reaction chamber configured to process by a plasma a gas supplied from an outside, the processed gas containing a nitrogen oxide; and a nitrogen oxide reduction apparatus connected to the reaction chamber, wherein the nitrogen oxide reduction apparatus includes a cooling unit; characterised in that said cooling unit is configured to cool the processed gas to a temperature lower than a nitrogen oxide generation temperature by use of a low temperature inert gas, wherein the cooling unit includes a plurality of gas injection nozzles configured to inject said low-temperature inert gas, and wherein the gas injection nozzles are provided at multiple levels with different heights of the nitrogen oxide reduction apparatus.
A semiconductor wafer mass metrology method comprising: controlling the temperature of a semiconductor wafer by: detecting information relating to an incoming temperature of the semiconductor wafer, wherein the information relating to the incoming temperature of the semiconductor wafer is detected before cooling or heating of the semiconductor wafer will be started if cooling or heating of the semiconductor wafer is performed; and controlling cooling or heating of the semiconductor wafer based on the detected information relating to the incoming temperature of the semiconductor wafer; wherein controlling the cooling or heating of the semiconductor wafer based on the detected information relating to the incoming temperature of the semiconductor wafer comprises setting a duration of the cooling or heating of the semiconductor wafer, or deciding not to perform the cooling or heating of the semiconductor wafer; and subsequently loading the semiconductor wafer onto a measurement area of a semiconductor wafer mass metrology apparatus. controlling the temperature of a semiconductor wafer by: detecting information relating to an incoming temperature of the semiconductor wafer, wherein the information relating to the incoming temperature of the semiconductor wafer is detected before cooling or heating of the semiconductor wafer will be started if cooling or heating of the semiconductor wafer is performed; and controlling cooling or heating of the semiconductor wafer based on the detected information relating to the incoming temperature of the semiconductor wafer; wherein controlling the cooling or heating of the semiconductor wafer based on the detected information relating to the incoming temperature of the semiconductor wafer comprises setting a duration of the cooling or heating of the semiconductor wafer, or deciding not to perform the cooling or heating of the semiconductor wafer; and detecting information relating to an incoming temperature of the semiconductor wafer, wherein the information relating to the incoming temperature of the semiconductor wafer is detected before cooling or heating of the semiconductor wafer will be started if cooling or heating of the semiconductor wafer is performed; and controlling cooling or heating of the semiconductor wafer based on the detected information relating to the incoming temperature of the semiconductor wafer; wherein controlling the cooling or heating of the semiconductor wafer based on the detected information relating to the incoming temperature of the semiconductor wafer comprises setting a duration of the cooling or heating of the semiconductor wafer, or deciding not to perform the cooling or heating of the semiconductor wafer; and subsequently loading the semiconductor wafer onto a measurement area of a semiconductor wafer mass metrology apparatus.
A system for monitoring a lubricant supplying at least one aircraft engine, comprising: a lubricant sensor, which measures a lubricant quantity value indicative of an amount of lubricant supplying the engine; a data acquisition unit, which reads the lubricant quantity value from the lubricant sensor at a fixed time interval; a message generation unit, characterized in that the message generation unit is arranged to generate a lubricant quantity monitoring message according to the lubricant quantity value read at the fixed time interval, wherein the lubricant quantity monitoring message comprises flight-phase lubricant quantity monitoring information for a specific flight phase of the engine and lubricant addition information comprising information of whether lubricant is added during a flight stop and quantity of lubricant addition, wherein the flight-phase lubricant quantity monitoring information is based on each said lubricant quantity value; and wherein the quantity of lubricant addition is determined according to lubricant quantity detected during the flight stop, wherein the lubricant quantity monitoring message further comprises lubricant consumption information, and the lubricant consumption information is calculated according to the flight-phase lubricant quantity monitoring information for a specific flight phase of the engine and/or the lubricant addition information, to evaluate a performance of the engine. a lubricant sensor, which measures a lubricant quantity value indicative of an amount of lubricant supplying the engine; a data acquisition unit, which reads the lubricant quantity value from the lubricant sensor at a fixed time interval; a message generation unit, characterized in that the message generation unit is arranged to generate a lubricant quantity monitoring message according to the lubricant quantity value read at the fixed time interval, wherein the lubricant quantity monitoring message comprises flight-phase lubricant quantity monitoring information for a specific flight phase of the engine and lubricant addition information comprising information of whether lubricant is added during a flight stop and quantity of lubricant addition, wherein the flight-phase lubricant quantity monitoring information is based on each said lubricant quantity value; and wherein the quantity of lubricant addition is determined according to lubricant quantity detected during the flight stop, wherein the lubricant quantity monitoring message further comprises lubricant consumption information, and the lubricant consumption information is calculated according to the flight-phase lubricant quantity monitoring information for a specific flight phase of the engine and/or the lubricant addition information, to evaluate a performance of the engine.
A device for administering a humidified aerosol to a patient interface, comprising: - at least one first tube for receiving and guiding a first gas flow comprising a humidified aerosol; - at least one second tube for receiving and guiding a second gas flow comprising humidified respiratory gases; - at least one third tube for receiving and guiding a liquid flow comprising a thermally balancing liquid; wherein the first tube, the second tube and the third tube are provided in a coaxial arrangement with respect to each other, wherein the third tube covers the first tube and the second tube; and - at least one mixing chamber for receiving and mixing the first gas flow and the second gas flow and obtaining enriched respiratory gases comprising the humidified aerosol, the mixing chamber having at least one outlet for administering the enriched respiratory gases comprising the humidified aerosol. - at least one first tube for receiving and guiding a first gas flow comprising a humidified aerosol; - at least one second tube for receiving and guiding a second gas flow comprising humidified respiratory gases; - at least one third tube for receiving and guiding a liquid flow comprising a thermally balancing liquid; wherein the first tube, the second tube and the third tube are provided in a coaxial arrangement with respect to each other, wherein the third tube covers the first tube and the second tube; and - at least one mixing chamber for receiving and mixing the first gas flow and the second gas flow and obtaining enriched respiratory gases comprising the humidified aerosol, the mixing chamber having at least one outlet for administering the enriched respiratory gases comprising the humidified aerosol.
A method for determining the optimum trim and draft for a vessel in ballast and laden conditions using the analysis of historic vessel data for the vessel being optimised, the method comprising the steps of: - collecting operational data from the vessel for one or more of its previous voyages, with the operational data comprising one or more operational parameters or data tags; - filtering out error and noise created by a chosen source of the operational data; - filtering out an effect of adverse weather, hull fouling and/or other conditions which have been found to decrease the accuracy of the process; - processing the operational data that has been filtered, by placing the filtered operational data into classes or bins of increasing size of speed, draft and trim to determine the average power for each historic speed, draft and trim condition; - producing a database of optimum draft and trim conditions based on the processed operational data, and providing the database to an operator, such as the Captain, or as an input to an automatic draft and trim optimisation system; - calculating a predicted fuel consumption for each speed, draft and trim condition based on the operational data, to estimate achievable fuel savings; and - comparing the predicted fuel consumption with an achieved fuel consumption for the vessel to determine savings achieved using information on a current fuel price. - collecting operational data from the vessel for one or more of its previous voyages, with the operational data comprising one or more operational parameters or data tags; - filtering out error and noise created by a chosen source of the operational data; - filtering out an effect of adverse weather, hull fouling and/or other conditions which have been found to decrease the accuracy of the process; - processing the operational data that has been filtered, by placing the filtered operational data into classes or bins of increasing size of speed, draft and trim to determine the average power for each historic speed, draft and trim condition; - producing a database of optimum draft and trim conditions based on the processed operational data, and providing the database to an operator, such as the Captain, or as an input to an automatic draft and trim optimisation system; - calculating a predicted fuel consumption for each speed, draft and trim condition based on the operational data, to estimate achievable fuel savings; and - comparing the predicted fuel consumption with an achieved fuel consumption for the vessel to determine savings achieved using information on a current fuel price.