mhurhangee/ep-ind-claims huggingface dataset:
A master aircraft, comprising: a virtual reality flight emulator, comprising: a pilot control interface; wherein the flight emulator is configured to control with the pilot control interface a virtual or remote slave aircraft connected through a network to the flight emulator when a user of the flight emulator virtually teleports through the network into the virtual or remote slave aircraft characterised by the flight emulator comprising a plurality of galvanic vestibular stimulation devices worn by the user; and wherein the GVS devices are configured to minimize for the user the perception of the motion of, orientation of, or forces acting on the master aircraft while simulating the motion of, orientation of, or forces acting on the virtual or remote slave aircraft when the user is virtually teleported into the virtual or remote slave aircraft. a virtual reality flight emulator, comprising: a pilot control interface; wherein the flight emulator is configured to control with the pilot control interface a virtual or remote slave aircraft connected through a network to the flight emulator when a user of the flight emulator virtually teleports through the network into the virtual or remote slave aircraft characterised by the flight emulator comprising a plurality of galvanic vestibular stimulation devices worn by the user; and wherein the GVS devices are configured to minimize for the user the perception of the motion of, orientation of, or forces acting on the master aircraft while simulating the motion of, orientation of, or forces acting on the virtual or remote slave aircraft when the user is virtually teleported into the virtual or remote slave aircraft. a pilot control interface; wherein the flight emulator is configured to control with the pilot control interface a virtual or remote slave aircraft connected through a network to the flight emulator when a user of the flight emulator virtually teleports through the network into the virtual or remote slave aircraft characterised by the flight emulator comprising a plurality of galvanic vestibular stimulation devices worn by the user; and wherein the GVS devices are configured to minimize for the user the perception of the motion of, orientation of, or forces acting on the master aircraft while simulating the motion of, orientation of, or forces acting on the virtual or remote slave aircraft when the user is virtually teleported into the virtual or remote slave aircraft.
A method, comprising: selecting, by a second network element of a base station, a baseband processing combination, BPC, for a user equipment, when in a process of the user equipment accessing the second network element; and sending, by the second network element to a first network element of the base station, the BPC selected for the user equipment, wherein the second network element is connected to the first network element. selecting, by a second network element of a base station, a baseband processing combination, BPC, for a user equipment, when in a process of the user equipment accessing the second network element; and sending, by the second network element to a first network element of the base station, the BPC selected for the user equipment, wherein the second network element is connected to the first network element.
An inertial sensing system, comprising: a first multi-axis atomic inertial sensor (102, 230); a second multi-axis atomic inertial sensor (104, 232); an optical multiplexer (114, 210) optically coupled to the first and second multi-axis atomic inertial sensors, the optical multiplexer configured to sequentially direct light along different axes of the first and second multi-axis atomic inertial sensors, so that simultaneous measurements are obtained along corresponding axes of the first and second multi-axis atomic inertial sensors; and a plurality of micro-electrical-mechanical systems (MEMS) inertial sensors (106, 108) in operative communication with the first and second multi-axis atomic inertial sensors; wherein output signals from the first and second multi-axis atomic inertial sensors aid in correcting errors produced by the MEMS inertial sensors by sequentially updating output signals from the MEMS inertial sensors. a first multi-axis atomic inertial sensor (102, 230); a second multi-axis atomic inertial sensor (104, 232); an optical multiplexer (114, 210) optically coupled to the first and second multi-axis atomic inertial sensors, the optical multiplexer configured to sequentially direct light along different axes of the first and second multi-axis atomic inertial sensors, so that simultaneous measurements are obtained along corresponding axes of the first and second multi-axis atomic inertial sensors; and a plurality of micro-electrical-mechanical systems (MEMS) inertial sensors (106, 108) in operative communication with the first and second multi-axis atomic inertial sensors; wherein output signals from the first and second multi-axis atomic inertial sensors aid in correcting errors produced by the MEMS inertial sensors by sequentially updating output signals from the MEMS inertial sensors.
A radiography system comprising: a mammography apparatus that includes a radiation source, a radiation detector, a visible light source that emits visible light and a limitation unit that limits an irradiation region of the visible light, and a compression member adapted to compress a breast disposed between the radiation source and the radiation detector, wherein the mammography apparatus is adapted to capture a radiographic image of the breast in a compressed state using the radiation detector; a control device including an acquisition unit adapted to acquire region information indicating a region of an object of interest in the breast on the basis of said radiographic image captured by the mammography apparatus, characterized in that the control device further includes a display control unit that performs control for the visible light source and for the limitation unit to limit an irradiation region of the visible light such that the irradiation region is matched with the region of the object of interest on the basis of a position of the visible light source and an irradiation angle of the visible light, to display the region of the object of interest on the compression member, so as to be recognizable on the basis of the region information, wherein the mammography apparatus is adapted to continuously compress the breast from the capture of the radiographic image until the region of interest is displayed. a mammography apparatus that includes a radiation source, a radiation detector, a visible light source that emits visible light and a limitation unit that limits an irradiation region of the visible light, and a compression member adapted to compress a breast disposed between the radiation source and the radiation detector, wherein the mammography apparatus is adapted to capture a radiographic image of the breast in a compressed state using the radiation detector; a control device including an acquisition unit adapted to acquire region information indicating a region of an object of interest in the breast on the basis of said radiographic image captured by the mammography apparatus, characterized in that the control device further includes a display control unit that performs control for the visible light source and for the limitation unit to limit an irradiation region of the visible light such that the irradiation region is matched with the region of the object of interest on the basis of a position of the visible light source and an irradiation angle of the visible light, to display the region of the object of interest on the compression member, so as to be recognizable on the basis of the region information, wherein the mammography apparatus is adapted to continuously compress the breast from the capture of the radiographic image until the region of interest is displayed.
Self-collapsible container made of PET, adapted to be filled with a liquid and to be used in an upside-down position with a potable liquid dispenser, the container having a capacity of at least 5 liters, defining a longitudinal axis and comprising: a) a neck with an opening for pouring the liquid, b) a shoulder, c) a bottom, d) a central body, between said shoulder and said bottom, wherein the central body is provided with a plurality of adjacent ribs substantially parallel to a plane perpendicular to said longitudinal axis, each of said ribs having - a first flank proximal to the neck, with a first straight portion, - a second flank distal to the neck, with a second straight portion, - a crest between the first and second flank with a first rounded portion, - a concave root portion joining two adjacent ribs, wherein the first straight portion of a rib and the second straight portion of the adjacent rib facing the first straight portion form a first angle comprised between 70o and 90o; whereby during use, as the liquid flows out of the container, said container gradually collapses axially reducing its volume with respect to its original shape, the collapsing occurring as result of the force generated by atmospheric pressure due to the difference between external and internal pressure, characterized in that the concave root portion has a first radius of curvature comprised between 0,2 and 1 mm; a maximum dimension, measured along a line perpendicularly crossing the longitudinal axis, between the crest and the concave root portion, is comprised between 5 mm and 8 mm; the second straight portion is shorter than the first straight portion; and wherein a line perpendicular to the longitudinal axis and passing through the concave root portion divides the first angle into a second angle defined by the second straight portion and the line, and a third angle defined by the first straight portion and said line, the second angle being smaller than the third angle. a) a neck with an opening for pouring the liquid, b) a shoulder, c) a bottom, d) a central body, between said shoulder and said bottom, - a first flank proximal to the neck, with a first straight portion, - a second flank distal to the neck, with a second straight portion, - a crest between the first and second flank with a first rounded portion, - a concave root portion joining two adjacent ribs, wherein
A frame assembly for a patient interface, comprising: an upper headgear connector structured to connect to upper straps of headgear, the upper headgear connector including: a pair of upper headgear connector arms, each of the upper headgear connector arms extending and curving in an upward direction between a patient's eyes and ears in use and including one or more flexible portions structured and arranged to conform to varying facial profiles, wherein each of the flexible portions includes one or more hinges; and a lower headgear connector structured to connect to lower straps of headgear, the lower headgear connector including a pair of lower headgear connector arms. an upper headgear connector structured to connect to upper straps of headgear, the upper headgear connector including: a pair of upper headgear connector arms, each of the upper headgear connector arms extending and curving in an upward direction between a patient's eyes and ears in use and including one or more flexible portions structured and arranged to conform to varying facial profiles, wherein each of the flexible portions includes one or more hinges; and a lower headgear connector structured to connect to lower straps of headgear, the lower headgear connector including a pair of lower headgear connector arms.
A rocket propulsion system, which comprises: - a combustion chamber, - a hydrogen-oxygen supply system connected to the combustion chamber, which system is configured to conduct hydrogen and oxygen into the combustion chamber, - a coolant supply system connected to the combustion chamber, which system is configured to supply a combustible coolant to the combustion chamber, and - an ignition system, which is configured to initiate combustion of the hydrogen-oxygen-coolant mixture in the combustion chamber, characterized in that - the ignition system comprises a catalyst chamber arranged in the combustion chamber, a hydrogen supply duct and an oxygen supply duct, and - the catalyst chamber can be supplied with hydrogen and oxygen in a substoichiometric mixture ratio via the hydrogen supply duct and the oxygen supply duct, wherein an overall combustion section is provided in the combustion chamber downstream of an exit area of the catalyst chamber, to which section gases exiting the catalyst chamber, oxygen flowing through the oxygen supply duct and coolant supplied to the combustion chamber via the coolant supply system can be supplied. - a combustion chamber, - a hydrogen-oxygen supply system connected to the combustion chamber, which system is configured to conduct hydrogen and oxygen into the combustion chamber, - a coolant supply system connected to the combustion chamber, which system is configured to supply a combustible coolant to the combustion chamber, and - an ignition system, which is configured to initiate combustion of the hydrogen-oxygen-coolant mixture in the combustion chamber, characterized in that - the ignition system comprises a catalyst chamber arranged in the combustion chamber, a hydrogen supply duct and an oxygen supply duct, and - the catalyst chamber can be supplied with hydrogen and oxygen in a substoichiometric mixture ratio via the hydrogen supply duct and the oxygen supply duct,
A poppy plant of Papaver somniferum having a trait such that on harvesting of its poppy capsules said plant yields a poppy straw having thebaine and oripavine constituting 100% by weight of the alkaloid combination consisting of morphine, codeine, thebaine and oripavine, there being no morphine or codeine in the alkaloid combination, said plant being obtainable by a method comprising the steps of: a) growing P.somniferum plants from seed of ATCC 97652, b) reproducing said plants, thereby maintaining the trait. a) growing P.somniferum plants from seed of ATCC 97652, b) reproducing said plants, thereby maintaining the trait.
Method for multicast transmission between a server and at least one of a plurality of clients (6,8) using a unicast protocol, said method comprising: - regularly transmitting by the server information permitting communication with the server over a multicast path (14,16) in order to enable a joint operation of multicast and unicast paths between the server and the at least one of a plurality of clients in a multicast association, said information comprising an identifier of said multicast association and a number of outbound streams indicating how many streams are part of said multicast association; - receiving by said server an initialization chunk of a four ways handshake, said initialization chunk comprising said identifier of said multicast association. - regularly transmitting by the server information permitting communication with the server over a multicast path (14,16) in order to enable a joint operation of multicast and unicast paths between the server and the at least one of a plurality of clients in a multicast association, said information comprising an identifier of said multicast association and a number of outbound streams indicating how many streams are part of said multicast association; - receiving by said server an initialization chunk of a four ways handshake, said initialization chunk comprising said identifier of said multicast association.
Railcar adapter, for connecting a railcar body to a bearing, comprising an adapter body having two lateral channels (14a, 14b) each delimited by a pair of opposed lugs (14c, 14d) and a lateral surface (14e, 14f) perpendicular to said opposed lugs, each lateral channels (14a, 14b) being adapted to cooperate with the railcar body, an inner surface acting as a bearing seat for said bearing and an outer surface in radial contact with the railcar body, characterized in that the inner surface comprises at least one central groove located on a first axis of symmetry (A 1) of the railcar adapter emerging in each lateral channel (14a, 14b), and said inner surface is provided with a second central groove located on a second symmetry axis (A 2) of the railcar adapter, perpendicular to said first symmetry axis (A 1).
A disposable grill comprising a base tray at least including a bottom part, one or more sidewalls protruding upwards from said bottom part and a top opening, grate means adapted to cover at least a part of said top opening, wherein said bottom part and said one or more sidewalls are formed by a biodegradable material, wherein said disposable grill further comprises at least one fireproof thermal insulating insert arranged in said base tray, characterised in that, said at least one thermal insulating insert is adapted to fit one or more sidewalls inside said base tray.
Pneumatic vehicle tyre for passenger cars or light-duty trucks with a carcass of a radial type of construction, with a breaker belt arranged radially outside the carcass and having a belt width B, measured in the axial direction A of the tyre, comprising at least two belt plies (3, 4) which are arranged one above the other in the radial direction R and are in each case formed by steel cords (8, 9) embedded in rubber and parallel within the belt ply (3, 4), the steel cords of one belt ply being formed in a criss-crossing arrangement in relation to the steel cords of the other belt ply, and with a profiled tread, formed radially outside the breaker belt, wherein, in a radial position between the carcass and the radially inner belt ply of the breaker belt, there is arranged so as to extend over the circumference of the tyre a strip of the width c, measured in the axial direction A, where 15 mm ≤ c ≤ (0.5 B), comprising reinforcing elements of a textile type of construction embedded in rubber, which are aligned - in particular parallel to one another - with an angle of inclination α in relation to the circumferential direction U, wherein the strip is arranged in relation to both axial edges of the belt with at least an axial distance a min, where a min = (0.2 B), and intersects the equatorial plane Ä-Ä of the tyre, characterized in that the reinforcing elements are aligned with an angle of inclination α in relation to the circumferential direction U where α = 90°.
Electric motor with integrated control electronics, having an electric motor and an electronic circuit for supplying the electric motor, comprising a terminal box which comprises an upper part, that is to say a lid, which can be placed onto a lower part, wherein the upper part comprises a plug-in connector and the lower part comprises a mating plug-in connector corresponding to the plug-in connector, and thus a supply to the circuit in the upper part is formed by way of the plug-in connection, and the connection lines for the stator windings of the electric motor are guided by way of the plug-in connection from the electronic circuit arranged in the upper part, characterized in that an electronic circuit with converter functionality is encompassed in the upper part, wherein a selector switch configured as a DIP switch is provided on an inner side of the upper part, wherein in a first switch position the electronic motor is ready for operation and cannot be parameterized, for which purpose the converter motor comprises a non-volatile memory in which machine-related parameters and acceleration ramp parameters are stored at the time of manufacture, said parameters corresponding to the values of physical variables of the electric motor, wherein in a second switch position the converter motor is ready for operation and can be parameterized, wherein the selector switch is accessible once the upper part has been lifted away from the lower part, wherein, for the parameterization, a connection device is provided for a bus connection for connecting to further bus subscribers, wherein, for the parameterization, a bus connection is provided by modulating higher-frequency AC components onto the supply lines, wherein, during the parameterization, machine-related parameters and/or acceleration ramp parameters can be changed.
Method for calibrating a test chamber which encloses an inner volume, said test chamber being designed as a film chamber comprising at least one flexible wall portion (14, 16) and being connected in a gas-conducting manner to a pressure sensor, to a vacuum pump, and via a calibration valve to a calibration chamber enclosing a calibration volume, the method comprising the following steps: evacuating the film chamber; measuring the pressure characteristic over time inside of the film chamber after the evacuation has been completed; characterized by connecting the calibration volume in a gas-conducting manner to the inner volume of the film chamber while measuring the pressure characteristic, wherein the pressure is measured before the gas-conducting connection to the film chamber is made and during the gas-conducting connection to the film chamber, and wherein the pressure in the calibration chamber before connection to the film chamber is higher or lower than the pressure in the film chamber, and calculating the film chamber volume as V F = V V p v − p G p G − p F o r V F ≈ V V p V p G − p F where V F: film chamber volume, V V: calibration volume, P V: pressure in the calibration chamber before connection with the film chamber volume, P G: pressure in the test chamber after connection with the calibration volume, and P F: pressure in the film chamber before connection with the calibration volume. evacuating the film chamber; measuring the pressure characteristic over time inside of the film chamber after the evacuation has been completed; characterized by connecting the calibration volume in a gas-conducting manner to the inner volume of the film chamber while measuring the pressure characteristic, wherein the pressure is measured before the gas-conducting connection to the film chamber is made and during the gas-conducting connection to the film chamber, and wherein the pressure in the calibration chamber before connection to the film chamber is higher or lower than the pressure in the film chamber, and calculating the film chamber volume as V F = V V p v − p G p G − p F o r V F ≈ V V p V p G − p F where V F: film chamber volume, V V: calibration volume, P V: pressure in the calibration chamber before connection with the film chamber volume, P G: pressure in the test chamber after connection with the calibration volume, and P F: pressure in the film chamber before connection with the calibration volume. V F: film chamber volume, V V: calibration volume, P V: pressure in the calibration chamber before connection with the film chamber volume, P G: pressure in the test chamber after connection with the calibration volume, and P F: pressure in the film chamber before connection with the calibration volume.
A protective helmet, in particular a protective motorcycle helmet, comprising an outer shell for distributing impact forces, a battery socket, which is firmly connected to the outer shell, for detachably accommodating a battery, and a line assembly, which is electrically connected to the battery socket, for supplying electricity by means of the accommodated battery to an electric apparatus which is mechanically coupled to the outer shell, whereas the battery socket having a pole assembly for the electrical and detachable coupling of the accommodated battery, and the electrical device being a digital device for wireless communication, characterized in that in that the battery socket has a battery frame, arranged on the inside with respect to the outer shell, for receiving the battery in a form-fitting manner, with a battery frame opening for introducing the battery into the battery frame, in that the battery frame adjoins a lower edge of the outer shell, and in that the battery frame opening is arranged essentially at the lower edge of the outer shell.