mhurhangee/ep-ind-claims huggingface dataset:
A method implemented by a system comprising a terminal and a base station, said method comprising: establishing (201, 301), by the terminal, a connection with the base station; during the step of establishing the connection with the base station, sending, by the terminal to the base station, terminal capability information which includes at least one field representing a terminal capability, wherein the terminal capability includes a latency capability and a data throughput capability; determining, by the base station, the terminal capability based on the terminal capability information; determining, by the base station, whether the terminal capability is within a capability interval, wherein the determining comprises determining whether the latency capability is within the capability interval; connecting, by the base station, the terminal to a mobile data network in accordance with the terminal capability information, wherein the connecting is performed if the base station determines that the terminal capability is within the capability interval, wherein endpoints of the capability interval are respectively a minimum latency capability and a maximum latency capability of the terminal supported by the mobile data network; determining, by the base station, a type of a service to be performed by the terminal based on the terminal capability information, and allocating, by the base station, network resources to the terminal in accordance with the type of the service; and processing, by the terminal, a service based on the network resources allocated by the base station. establishing (201, 301), by the terminal, a connection with the base station; during the step of establishing the connection with the base station, sending, by the terminal to the base station, terminal capability information which includes at least one field representing a terminal capability, wherein the terminal capability includes a latency capability and a data throughput capability; determining, by the base station, the terminal capability based on the terminal capability information; determining, by the base station, whether the terminal capability is within a capability interval, wherein the determining comprises determining whether the latency capability is within the capability interval; connecting, by the base station, the terminal to a mobile data network in accordance with the terminal capability information, wherein the connecting is performed if the base station determines that the terminal capability is within the capability interval, wherein endpoints of the capability interval are respectively a minimum latency capability and a maximum latency capability of the terminal supported by the mobile data network; determining, by the base station, a type of a service to be performed by the terminal based on the terminal capability information, and allocating, by the base station, network resources to the terminal in accordance with the type of the service; and processing, by the terminal, a service based on the network resources allocated by the base station.
A method for manufacturing a solar cell, comprising: forming a tunneling layer on a silicon substrate; forming a semiconductor layer on the tunneling layer, wherein the forming of the semiconductor layer includes depositing a semiconductor material, wherein the deposition temperature of the semiconductor layer is in a range from about 500°C to about 700°C and the deposition pressure is in a range from about 0.01 Torr to about 0.5 Torr; and forming an electrode (42, 44) connected to the semiconductor layer, wherein the forming of the tunneling layer and the forming of the semiconductor layer are performed by an in-situ process continuously performed in the same apparatus, wherein a pressure of the forming of the semiconductor layer is smaller than a pressure of the forming of the tunneling layer, characterised in that the forming the tunneling layer is performed at the temperature in a range from about 600°C to about 800°C and at the pressure in a range from about 0.01 Torr to about 2 Torr; wherein a difference between the temperature of the forming of the tunneling layer and the temperature of the forming of the semiconductor layer is 200°C or less. forming a tunneling layer on a silicon substrate; forming a semiconductor layer on the tunneling layer, wherein the forming of the semiconductor layer includes depositing a semiconductor material, wherein the deposition temperature of the semiconductor layer is in a range from about 500°C to about 700°C and the deposition pressure is in a range from about 0.01 Torr to about 0.5 Torr; and forming an electrode (42, 44) connected to the semiconductor layer, wherein the forming of the tunneling layer and the forming of the semiconductor layer are performed by an in-situ process continuously performed in the same apparatus, wherein a pressure of the forming of the semiconductor layer is smaller than a pressure of the forming of the tunneling layer,
A vaccine composition comprising (i) a yeast cell wall particle; (ii) a silicate bonded to a β-glucan, and (iii) an immunogenic, exogenous biological material loaded within the yeast cell wall particle, wherein the biological material comprises tumor lysate, a protein or a fragment thereof, nucleic acid, carbohydrate, or a combination thereof, and wherein the yeast cell wall particle is modified by capping with the silicate, wherein the term "capping" means that a polymeric structure covers or coats the yeast cell wall particle, and wherein the silicate is selected from the group consisting of tetraethylorthosilicate, tetramethylorthosilicate, tetrapropylorthosilicate, and tetrabutylorthosilicate.
An aircraft capable of vertical take-off and landing, comprising: a fuselage; at least one processor carried by the fuselage; a first pair of aerodynamic, lift-generating wings (102, 102A) extending from the fuselage; a plurality of vectoring rotors (110, 110A) rotatably carried by the fuselage so as to be rotatable between a substantially vertical configuration relative to the fuselage and a substantially horizontal configuration relative to the fuselage and configured to be controlled by the at least one processor; wherein the vectoring rotors (110, 110A) are unsupported by the first pair of wings (102, 102A); wherein each of the vectoring rotors (110, 110A) is controllable independently of each other to provide lateral and yaw stability during low speed maneuvering; wherein transition from vertical flight to horizontal flight is enhanced by using sequential vectoring thrust wherein forward ones of the vectoring rotors (110, 110A) vector at a different speed and angle than rearward ones of the vectoring rotors (110, 110A); whereby one of the forward ones of the vectoring rotors (110, 110A) and the rearward ones of the vectoring rotors (110, 110A) provide more horizontal thrust than the other of the forward ones of the vectoring rotors (110, 110A) and the rearward ones of the vectoring rotors (110, 110A) until the aircraft reaches a speed above a stall speed of the first pair of wings (102, 102A). a fuselage; at least one processor carried by the fuselage; a first pair of aerodynamic, lift-generating wings (102, 102A) extending from the fuselage; a plurality of vectoring rotors (110, 110A) rotatably carried by the fuselage so as to be rotatable between a substantially vertical configuration relative to the fuselage and a substantially horizontal configuration relative to the fuselage and configured to be controlled by the at least one processor; wherein the vectoring rotors (110, 110A) are unsupported by the first pair of wings (102, 102A); wherein each of the vectoring rotors (110, 110A) is controllable independently of each other to provide lateral and yaw stability during low speed maneuvering; wherein transition from vertical flight to horizontal flight is enhanced by using sequential vectoring thrust wherein forward ones of the vectoring rotors (110, 110A) vector at a different speed and angle than rearward ones of the vectoring rotors (110, 110A); whereby one of the forward ones of the vectoring rotors (110, 110A) and the rearward ones of the vectoring rotors (110, 110A) provide more horizontal thrust than the other of the forward ones of the vectoring rotors (110, 110A) and the rearward ones of the vectoring rotors (110, 110A) until the aircraft reaches a speed above a stall speed of the first pair of wings (102, 102A).
Spinning position of an air spinning machine for producing a yarn from a fibre assembly consisting of fibres, - wherein the spinning position comprises a vortex chamber with an inlet opening for the fibre assembly being fed in a transporting direction into the vortex chamber during operation of the air spinning machine and further comprises a yarn forming element extending at least partially into the vortex chamber, - wherein the spinning position comprises air nozzles directing into the vortex chamber and ending in the vortex chamber in the area of a wall surrounding the vortex chamber, by means of which nozzles air can be introduced into the vortex chamber in a preset rotating direction, to give the fibre assembly a rotation in the said direction in the area of an inlet opening of the yarn forming element, - wherein the yarn forming element comprises a draw-off channel, through which the yarn can be drawn off out of the vortex chamber, - wherein a guiding device is arranged in the area of the inlet opening of the vortex chamber for guiding the fibre assembly, and - wherein the guiding device comprises at least two guiding sections spaced of each other, the distance between them decreasing at least in parts in the said transporting direction, characterized in that the guiding device further comprises at least one central guiding element, that in a sectional view perpendicular to the longitudinal axis of the draw-off channel extends at least partially between the guiding sections and effects a deflection of the fibres of the fibre assembly perpendicularly to the longitudinal axis of the draw-off channel. - wherein the spinning position comprises a vortex chamber with an inlet opening for the fibre assembly being fed in a transporting direction into the vortex chamber during operation of the air spinning machine and further comprises a yarn forming element extending at least partially into the vortex chamber, - wherein the spinning position comprises air nozzles directing into the vortex chamber and ending in the vortex chamber in the area of a wall surrounding the vortex chamber, by means of which nozzles air can be introduced into the vortex chamber in a preset rotating direction, to give the fibre assembly a rotation in the said direction in the area of an inlet opening of the yarn forming element, - wherein the yarn forming element comprises a draw-off channel, through which the yarn can be drawn off out of the vortex chamber, - wherein a guiding device is arranged in the area of the inlet opening of the vortex chamber for guiding the fibre assembly, and - wherein the guiding device comprises at least two guiding sections spaced of each other, the distance between them decreasing at least in parts in the said transporting direction,
Luminaire comprising a housing, a light exit opening defined by the housing, a cover of the light exit opening, as well as an arrangement for emitting light characterized in that the arrangement for emitting light comprises - an LED luminaire in an elongated arrangement, - a carrier element which carries the LED luminaire, and - a light-emitting element which may be connected to the carrier element, wherein the light-emitting element comprises a first region (41, 51, 61, 71) in which light passing through is widely scattered, and wherein the light-emitting element comprises a second region (40, 50, 60, 70) in which light passing through is significantly less scattered than in the first region (41, 51, 61, 71), wherein the cover is arranged downstream in the optical path of the light-emitting element, while the cover comprises a central region close to the light emitting element, and wherein the cover has a lateral portion farther away from the light emitting element, and wherein the cover has different light emission characteristics in the lateral region and in the central region. - an LED luminaire in an elongated arrangement, - a carrier element which carries the LED luminaire, and - a light-emitting element which may be connected to the carrier element,
A pharmaceutical dosage unit for sublingual, buccal, pulmonary or oral administration, said dosage unit having a weight of 20-500 mg and comprising 1-80 wt.% of a microgranulate that is distributed throughout a solid hydrophilic matrix; said microgranulate being characterised in that it: - has a volume weighted average diameter of 5-100 μm; - contains at least 0.01 wt.%, preferably at least 0.1 wt.% of one or more cannabinoids having a solubility in demineralised water of 37 °C (neutral pH) of less than 200 mg/l; - contains at least 10 wt.% of a sugar fatty acids ester emulsifier with an HLB of more than 7; and - is capable of forming a micro-emulsion upon contact with saliva or water wherein the cannabinoids and the sugar fatty acid ester emulsifier together represent at least 60 wt.% of the microgranulate. - has a volume weighted average diameter of 5-100 μm; - contains at least 0.01 wt.%, preferably at least 0.1 wt.% of one or more cannabinoids having a solubility in demineralised water of 37 °C (neutral pH) of less than 200 mg/l; - contains at least 10 wt.% of a sugar fatty acids ester emulsifier with an HLB of more than 7; and - is capable of forming a micro-emulsion upon contact with saliva or water
A cooling head with connecting lines (13,14) in a vacuum insulation for a cooling system for cooling objects to semi-cryogenic or cryogenic temperatures from 283K to 4K, in particular 190K to 4K, comprising insulating means for insulating the cooling head, wherein the insulating means of the cooling head are formed by a vacuum chamber in which the cooling head is arranged, and connecting lines (13,14) connected to the cooling head for supplying to, and returning from, the cooling head coolant cooled to semi-cryogenic or cryogenic temperatures, wherein insulating means for insulating the connecting lines (13,14) are provided, wherein the insulating means of the connecting lines (13,14) designed as flexible lines are formed by a vacuum insulation, wherein the vacuum chamber and the vacuum insulation of the connecting lines (13,14) are in direct communication with each other and can be connected to a shared vacuum source, and wherein the connecting lines (13,14) are led out of the vacuum insulation on their ends facing away from the cooling head and the vacuum chamber comprises a connection for connecting to the shared vacuum source, and wherein the vacuum insulation comprises an enveloping hose surrounding the connecting lines (13,14) while forming a substantially annular hollow space, said enveloping hose being designed as a flexible enveloping hose, and at least one spacer is provided in the hollow space between the connecting lines (13,14) and the enveloping hose.
A cooling member comprising: a fluid-tight sealed body that is formed by sheet members being joined to each other at at least one joint portion; a coolant that is enclosed in the sealed body; and a heat dissipation plate that is fluid-tightly joined to an inner surface of the sealed body at at least one portion where the sheet members are joined together and that has a heat absorption portion that is located inside the sealed body and a heat dissipation portion that is located outside the sealed body. a fluid-tight sealed body that is formed by sheet members being joined to each other at at least one joint portion; a coolant that is enclosed in the sealed body; and a heat dissipation plate that is fluid-tightly joined to an inner surface of the sealed body at at least one portion where the sheet members are joined together and that has a heat absorption portion that is located inside the sealed body and a heat dissipation portion that is located outside the sealed body.
A method for controlling the torque transfer on a power train for a vehicle in which a driving torque is generated by a prime mover and is conveyed downstream via an output shaft from the prime mover to a clutch device, then to an input shaft of a gearbox, to an output propeller shaft leading from the gearbox and, via a differential gear, to the driveshafts of the vehicle's wheels, characterised in that the method comprises: A) calculating a maximum torque T max which is the largest load tolerated by the power train downstream of the clutch device, B) determining a torque T t which is transferable by the clutch device and is less than or equal to T max, C) determining a clutch actuator signal appropriate to engaging the clutch device so that the maximum load upon the power train downstream of the clutch device, from the torque transmitted by the clutch device, will be T t, and D) using the clutch actuator signal determined to control the clutch actuator. A) calculating a maximum torque T max which is the largest load tolerated by the power train downstream of the clutch device, B) determining a torque T t which is transferable by the clutch device and is less than or equal to T max, C) determining a clutch actuator signal appropriate to engaging the clutch device so that the maximum load upon the power train downstream of the clutch device, from the torque transmitted by the clutch device, will be T t, and D) using the clutch actuator signal determined to control the clutch actuator.
A controlled environment virtual reality system, the system comprising: a profile subsystem that stores an inmate profile of the inmate; a communication subsystem configured to: transmit, via a network, authentication information to a monitoring system; and receive, via the network, an approval message from the monitoring system based on the authentication information; and a virtual reality subsystem having one or more processors and/or circuits configured to: retrieve the inmate profile associated with the inmate from the profile subsystem, wherein the inmate profile includes content preferences; initiate, based on the approval message, a virtual reality session involving a first communication device used by the inmate of the controlled environment; and personalize the virtual reality session based on the content preferences and based on a global preference of an administrator of the controlled environment virtual reality system. a profile subsystem that stores an inmate profile of the inmate; a communication subsystem configured to: transmit, via a network, authentication information to a monitoring system; and receive, via the network, an approval message from the monitoring system based on the authentication information; and a virtual reality subsystem having one or more processors and/or circuits configured to: retrieve the inmate profile associated with the inmate from the profile subsystem, wherein the inmate profile includes content preferences; initiate, based on the approval message, a virtual reality session involving a first communication device used by the inmate of the controlled environment; and personalize the virtual reality session based on the content preferences and based on a global preference of an administrator of the controlled environment virtual reality system. transmit, via a network, authentication information to a monitoring system; and receive, via the network, an approval message from the monitoring system based on the authentication information; and a virtual reality subsystem having one or more processors and/or circuits configured to: retrieve the inmate profile associated with the inmate from the profile subsystem, wherein the inmate profile includes content preferences; initiate, based on the approval message, a virtual reality session involving a first communication device used by the inmate of the controlled environment; and personalize the virtual reality session based on the content preferences and based on a global preference of an administrator of the controlled environment virtual reality system. retrieve the inmate profile associated with the inmate from the profile subsystem, wherein the inmate profile includes content preferences; initiate, based on the approval message, a virtual reality session involving a first communication device used by the inmate of the controlled environment; and personalize the virtual reality session based on the content preferences and based on a global preference of an administrator of the controlled environment virtual reality system.
An assembly comprising: a turbine housing that comprises a bore, a wastegate seat and two wastegate passages (1623-1, 1623-2) that extend to the wastegate seat; a rotatable wastegate shaft configured for receipt by the bore; a wastegate arm extending from the wastegate shaft; and a wastegate plug extending from the wastegate arm; characterized in that the wastegate plug comprises a toroidal portion (1010, 1020, 1030, 1040) with a profile defined in part by a portion of a torus, for contacting the wastegate seat in a closed state, and defined in part by two plug portions (1357, 1359), for defining clearances with respect to the wastegate seat in an open state and wherein in the closed state each of the two plug portions of the wastegate plug extends into a respective one of the wastegate passages. a turbine housing that comprises a bore, a wastegate seat and two wastegate passages (1623-1, 1623-2) that extend to the wastegate seat; a rotatable wastegate shaft configured for receipt by the bore; a wastegate arm extending from the wastegate shaft; and a wastegate plug extending from the wastegate arm; characterized in that the wastegate plug comprises a toroidal portion (1010, 1020, 1030, 1040) with a profile defined in part by a portion of a torus, for contacting the wastegate seat in a closed state, and defined in part by two plug portions (1357, 1359), for defining clearances with respect to the wastegate seat in an open state and wherein in the closed state each of the two plug portions of the wastegate plug extends into a respective one of the wastegate passages.
A method at a computing device for identification of secure binary images, the method comprising: dissecting a binary image into routines and functions; disassembling byte code for the dissected routines and functions; retrieving local parameters, wherein the local parameters are routine and function parameters; counting a number of conditional routines that are configured to operate on each of the local parameters; and creating a confidence score for each dissected routine and function, the confidence score being based on the number of conditional routines. dissecting a binary image into routines and functions; disassembling byte code for the dissected routines and functions; retrieving local parameters, wherein the local parameters are routine and function parameters; counting a number of conditional routines that are configured to operate on each of the local parameters; and creating a confidence score for each dissected routine and function, the confidence score being based on the number of conditional routines.