mhurhangee/ep-ind-claims huggingface dataset:
A side airbag, comprising: a first panel having a first left face and a first right face, the first panel being folded along a fold line such that the first left face overlaps the first right face to form a first chamber therebetween; a second panel having a second left face and a second right face, the second panel being folded such that the second left face overlaps the second right face to form a second chamber therebetween; wherein the first panel has a hole that allows flow of gas from the first chamber to the second chamber, wherein the second left face has a second left edge part joined to the first left face along a line from a first upper edge part of the first left face to a first lower edge part of the first left face at a position closer to the fold line of the first panel than to a first left edge part of the first left face, wherein the second right face has a second right edge part joined to the first right face along a line from a second upper edge part of the first right face to a second lower edge part of the first right face at a position closer to the fold line of the first panel than to a first right edge part of the first right face, characterized in that the second left face has an upper left edge part joined to a rightmost upper edge part of the first left face, and has a lower left edge part joined to a rightmost lower edge part of the first left face at a position farther away from the first left edge part than the upper left edge part, and the second right face has an upper right edge part joined to a leftmost upper edge part of the first right face, and has a lower right edge part joined to a leftmost lower edge part of the first right face at a position farther away from the first right edge part than the upper right edge part. a first panel having a first left face and a first right face, the first panel being folded along a fold line such that the first left face overlaps the first right face to form a first chamber therebetween; a second panel having a second left face and a second right face, the second panel being folded such that the second left face overlaps the second right face to form a second chamber therebetween;
An apparatus comprising: a fixed compression plate and a movable compression plate configured to hold an inspection region of a subject, the movable compression plate being movable relative to the fixed compression plate in a direction in which the inspection region is compressed and released while a compression surface of the movable compression plate is maintained parallel to the fixed compression plate; a mechanism (18,18a,19,19a,23,23a,24,24a) configured to move the movable compression plate; an illumination optical system configured to irradiate the inspection region held by the fixed compression plate and the movable compression plate with a pulsed laser beam; and a detector configured to receive an acoustic wave that is generated as the result of the irradiation with the pulsed laser beam wherein the mechanism configured to move the movable compression plate includes a pair of linear guides (18,19,23,24) configured to guide both end portions of the movable compression plate in a moving direction, characterized in that drive mechanisms (18a,19a,23a,24a) are respectively provided along the linear guides and configured to drive the movable compression plate at the both end portions. a fixed compression plate and a movable compression plate configured to hold an inspection region of a subject, the movable compression plate being movable relative to the fixed compression plate in a direction in which the inspection region is compressed and released while a compression surface of the movable compression plate is maintained parallel to the fixed compression plate; a mechanism (18,18a,19,19a,23,23a,24,24a) configured to move the movable compression plate; an illumination optical system configured to irradiate the inspection region held by the fixed compression plate and the movable compression plate with a pulsed laser beam; and a detector configured to receive an acoustic wave that is generated as the result of the irradiation with the pulsed laser beam wherein the mechanism configured to move the movable compression plate includes a pair of linear guides (18,19,23,24) configured to guide both end portions of the movable compression plate in a moving direction, characterized in that drive mechanisms (18a,19a,23a,24a) are respectively provided along the linear guides and configured to drive the movable compression plate at the both end portions.
Powder distribution device for distributing pulverulent media, comprising a housing with a longitudinal axis, an inlet for inflow of air laden with powder and at least two outlets (4, 5, 6) for outflow of the air laden with powder, wherein the inlet is arranged at a first position of the longitudinal axis of the housing, wherein the outlets (4, 5, 6) are arranged at a second position of the longitudinal axis of the housing, wherein the second position differs from the first position, wherein a flow path for the air laden with powder is formed in the interior of the housing, wherein the area of the flow path in a section perpendicular to the longitudinal axis of the housing reduces at least section-wise in progression from the first position to the second position, wherein the inlet has a tubular section with an inlet axis or is formed as such, wherein the inlet axis lies in a plane perpendicular to the longitudinal axis of the housing, wherein the inlet axis and the longitudinal axis have a spacing (a) from one another, wherein the inlet axis in a section perpendicular to the longitudinal axis is tangential to the annularly formed flow path and wherein the outlets (4, 5, 6) have a tubular section with an outlet axis or are formed as such, wherein the outlet axis lies in a plane perpendicular to the longitudinal axis of the housing, wherein the outlet axis and the longitudinal axis have a spacing (b) from one another, wherein the outlet axis in a section perpendicular to the longitudinal axis is tangential to the annularly formed flow path, characterised in that a wall element forming an inner boundary of the flow path is arranged in the interior of the housing, wherein the wall element has a conical outer surface. wherein the area of the flow path in a section perpendicular to the longitudinal axis of the housing reduces at least section-wise in progression from the first position to the second position, wherein the inlet has a tubular section with an inlet axis or is formed as such, wherein the inlet axis lies in a plane perpendicular to the longitudinal axis of the housing, wherein the inlet axis and the longitudinal axis have a spacing (a) from one another, wherein the inlet axis in a section perpendicular to the longitudinal axis is tangential to the annularly formed flow path and wherein the outlets (4, 5, 6) have a tubular section with an outlet axis or are formed as such, wherein the outlet axis lies in a plane perpendicular to the longitudinal axis of the housing, wherein the outlet axis and the longitudinal axis have a spacing (b) from one another, wherein the outlet axis in a section perpendicular to the longitudinal axis is tangential to the annularly formed flow path, characterised in that a wall element forming an inner boundary of the flow path is arranged in the interior of the housing, wherein the wall element has a conical outer surface.
A method for making a semi-conducting structure for a solar cell with N-doped regions having profiles and/or different dopant concentrations, comprising the following steps of: - implanting a doping species, in particular phosphorous, in a surface zone of a semiconductor substrate, - performing a localised recrystallization thermal annealing at a temperature preferably lower than 700°C, the localised recrystallization thermal annealing being carried out using a laser by exposing one or more first regions of the surface zone whereas portions (11b, 11c) of the surface zone are not exposed to the laser, and then - keeping the substrate for a predetermined waiting time greater than 1h preferably greater than 5h and advantageously greater than or equal to 24h, and then, - performing an annealing of activating the dopants of the first regions (13a, 13b, 13c) and said portions by thermally treating all of the first regions and said portions (11b, 11c). - implanting a doping species, in particular phosphorous, in a surface zone of a semiconductor substrate, - performing a localised recrystallization thermal annealing at a temperature preferably lower than 700°C, the localised recrystallization thermal annealing being carried out using a laser by exposing one or more first regions of the surface zone whereas portions (11b, 11c) of the surface zone are not exposed to the laser, and then - keeping the substrate for a predetermined waiting time greater than 1h preferably greater than 5h and advantageously greater than or equal to 24h, and then, - performing an annealing of activating the dopants of the first regions (13a, 13b, 13c) and said portions by thermally treating all of the first regions and said portions (11b, 11c).
Wound rotor, notably a wound rotor for an electric machine, the wound rotor comprising a shaft with main axis, the shaft comprising a slipring, the wound rotor comprising a winding wire and n wound poles (1, 2, 3,..., n-2, n-1, n) ordered in ascending numerical order obtained by rotation about the main axis, notably n wound poles (1, 2, 3,..., n-2, n-1, n) distributed radially about the main axis, characterized in that the n poles are wound with the wire in series turn by turn according to their ascending numerical order, although the last pole (n) is not the last to be wound.
A phosphor surface treatment method comprising the step of treating the surface of a red phosphor with a treating solution containing a surface treating agent, wherein said red phosphor is a Mn-activated complex fluoride having the formula: A 2 MF 6:Mn wherein M is one or more tetravalent elements selected from the group consisting of Si, Ti, Zr, Hf, Ge, and Sn, and A is one or more alkali metals selected from the group consisting of Li, Na, K, Rb, and Cs, and contains at least Na and/or K, and said surface treating agent is selected from: an organic amine having the formula: NR 1 R 2 R 3 wherein at least one of R 1, R 2 and R 3 is a substituted or unsubstituted monovalent hydrocarbon group, and the remainder is hydrogen, a quaternary ammonium salt having the formula: R 4 R 5 R 6 R 7 N + X - wherein R 4, R 5, R 6 and R 7 each are a substituted or unsubstituted monovalent hydrocarbon group, and X is a halogen atom, an alkyl betaine or a fluorochemical surfactant, having the formula: R 8 R 9 R 10 N + CH 2 COO - wherein R 8, R 9 and R 10 each are a substituted or unsubstituted monovalent hydrocarbon group, an alkoxysilane having the formula: R 11 Si(OR 12)(OR 13)(OR 14) wherein R 11 is a substituted or unsubstituted monovalent hydrocarbon group or alkoxy group, R 12, R 13 and R 14 each are a substituted or unsubstituted monovalent hydrocarbon group, and a fluorinated polymer. an organic amine having the formula: NR 1 R 2 R 3 wherein at least one of R 1, R 2 and R 3 is a substituted or unsubstituted monovalent hydrocarbon group, and the remainder is hydrogen, a quaternary ammonium salt having the formula: R 4 R 5 R 6 R 7 N + X - wherein R 4, R 5, R 6 and R 7 each are a substituted or unsubstituted monovalent hydrocarbon group, and X is a halogen atom, an alkyl betaine or a fluorochemical surfactant, having the formula: R 8 R 9 R 10 N + CH 2 COO - wherein R 8, R 9 and R 10 each are a substituted or unsubstituted monovalent hydrocarbon group, an alkoxysilane having the formula: R 11 Si(OR 12)(OR 13)(OR 14) wherein R 11 is a substituted or unsubstituted monovalent hydrocarbon group or alkoxy group, R 12, R 13 and R 14 each are a substituted or unsubstituted monovalent hydrocarbon group, and a fluorinated polymer.
A method carried out by a base station, comprising the steps of: (a) generating a code sequence containing system information of the base station; (b) generating a physical broadcast channel, PBCH, sequence by modulating the code sequence; (c) selecting a physical resource block, PRB, for a PBCH contained in the PBCH sequence; and (d) carrying out mapping between the PBCH and a resource element, RE, in the PRB thus selected, the PRB including a distributed PRB frequency division multiplexing format or a centralized PRB frequency division multiplexing format, wherein the step (c) includes a step of selecting the PRB with respect to the PBCH in accordance with an identifier of the base station and with an index of the PBCH contained in the PBCH sequence. (a) generating a code sequence containing system information of the base station; (b) generating a physical broadcast channel, PBCH, sequence by modulating the code sequence; (c) selecting a physical resource block, PRB, for a PBCH contained in the PBCH sequence; and (d) carrying out mapping between the PBCH and a resource element, RE, in the PRB thus selected,
A method comprising: installing, onto a first computing environment on a computing device, a device driver for a device available to the first computing environment; retrieving, from an external media device that does not include the device driver, data associated with a second computing environment and comprising a virtual machine image associated with the second computing environment; executing, by a virtual machine on the computing device, the second computing environment, based on the retrieved data; identifying, by a device discovery agent, a device available to the second computing environment; determining, by a device driver discovery agent, that the device driver installed in the first computing environment is associated with the device available to the second computing environment; receiving or retrieving, by the device driver discovery agent information required to install the device driver into the second computing environment; and importing, by a device driver installation agent in communication with the device driver discovery agent, using the information received or retrieved by the device driver discovery agent and without user input, the device driver into the second computing environment. installing, onto a first computing environment on a computing device, a device driver for a device available to the first computing environment; retrieving, from an external media device that does not include the device driver, data associated with a second computing environment and comprising a virtual machine image associated with the second computing environment; executing, by a virtual machine on the computing device, the second computing environment, based on the retrieved data; identifying, by a device discovery agent, a device available to the second computing environment; determining, by a device driver discovery agent, that the device driver installed in the first computing environment is associated with the device available to the second computing environment; receiving or retrieving, by the device driver discovery agent information required to install the device driver into the second computing environment; and importing, by a device driver installation agent in communication with the device driver discovery agent, using the information received or retrieved by the device driver discovery agent and without user input, the device driver into the second computing environment.
A method for controlling a spacecraft maneuver, the method comprising: using solar wing current feedback as the only closed-loop feedback sensor for attitude control; and controlling with a spin controller a spacecraft spin axis orientation and spin rate, wherein the spin controller commands the spacecraft spin axis orientation to align with an inertial fixed-direction and to rotate at a specified spin rate by using a momentum vector, and characterized in that wherein the spin controller commands the spacecraft to spin along any of three principle axes. using solar wing current feedback as the only closed-loop feedback sensor for attitude control; and controlling with a spin controller a spacecraft spin axis orientation and spin rate, wherein the spin controller commands the spacecraft spin axis orientation to align with an inertial fixed-direction and to rotate at a specified spin rate by using a momentum vector, and characterized in that wherein the spin controller commands the spacecraft to spin along any of three principle axes.
A wireless base station that is adapted to transmit MBMS data to mobile stations in the cell of said wireless base station and that comprises: a storage unit that is adapted to store a flag that indicates whether or not its own wireless base station is a master base station; a determination unit that, when its own wireless base station is a master base station, is adapted to determine a wireless parameter set that is set in channels used for transmission of MBMS data; a notification unit that, when its own wireless base station is a master base station, is adapted to report the wireless parameter set that was determined in said determination unit to other wireless base stations; an acquisition unit that, when its own wireless base station is not a master base station, is adapted to acquire a wireless parameter set that was reported from a master base station; and a setting unit that, when its own wireless base station is a master base station, is adapted to set the wireless parameter set that was determined in said determination unit in said channels, and when its own wireless base station is not a master base station, to set the wireless parameter set that was acquired in said acquisition unit in said channels. a storage unit that is adapted to store a flag that indicates whether or not its own wireless base station is a master base station; a determination unit that, when its own wireless base station is a master base station, is adapted to determine a wireless parameter set that is set in channels used for transmission of MBMS data; a notification unit that, when its own wireless base station is a master base station, is adapted to report the wireless parameter set that was determined in said determination unit to other wireless base stations; an acquisition unit that, when its own wireless base station is not a master base station, is adapted to acquire a wireless parameter set that was reported from a master base station; and a setting unit that, when its own wireless base station is a master base station, is adapted to set the wireless parameter set that was determined in said determination unit in said channels, and when its own wireless base station is not a master base station, to set the wireless parameter set that was acquired in said acquisition unit in said channels.
A gas turbine engine, comprising: a case extending circumferentially around a central axis of the gas turbine engine; a boss (40, 140) protruding from the case away from the central axis, the boss (40, 140) defining an internal passage (42c, 142c); a tubular member received within the internal passage (42c, 142c) of the boss (40, 140) and secured to the boss (40, 140), characterised in that: the tubular member defines a conduit for feeding lubricant to a bearing via a tube; and the gas turbine engine further comprises: an annular gap extending all around the tubular member and located between the tubular member and the boss (40, 140); and a fitting hydraulically connecting a fluid source to the tubular member, the fitting having a portion received within the tubular member and encircled by both of the annular gap and the tubular member, the fitting sealingly engaged to the tubular member. a case extending circumferentially around a central axis of the gas turbine engine; a boss (40, 140) protruding from the case away from the central axis, the boss (40, 140) defining an internal passage (42c, 142c); a tubular member received within the internal passage (42c, 142c) of the boss (40, 140) and secured to the boss (40, 140), characterised in that: the tubular member defines a conduit for feeding lubricant to a bearing via a tube; and the gas turbine engine further comprises: an annular gap extending all around the tubular member and located between the tubular member and the boss (40, 140); and a fitting hydraulically connecting a fluid source to the tubular member, the fitting having a portion received within the tubular member and encircled by both of the annular gap and the tubular member, the fitting sealingly engaged to the tubular member. the tubular member defines a conduit for feeding lubricant to a bearing via a tube; and the gas turbine engine further comprises: an annular gap extending all around the tubular member and located between the tubular member and the boss (40, 140); and a fitting hydraulically connecting a fluid source to the tubular member, the fitting having a portion received within the tubular member and encircled by both of the annular gap and the tubular member, the fitting sealingly engaged to the tubular member. an annular gap extending all around the tubular member and located between the tubular member and the boss (40, 140); and a fitting hydraulically connecting a fluid source to the tubular member, the fitting having a portion received within the tubular member and encircled by both of the annular gap and the tubular member, the fitting sealingly engaged to the tubular member.
A terminal comprising: a receiving unit adapted to receive, from a base station apparatus, one or more synchronization signal blocks associated with one or more beams transmitted from the base station apparatus, the one or more synchronization signal blocks including information on initial access; a control unit adapted to select a synchronization signal block used for determining a resource for transmitting a preamble from the one or more synchronization blocks, based on at least one of received power and received quality of the one or more synchronization signal blocks; and a transmitting unit adapted to transmit the preamble to the base station apparatus using the resource, characterized in that if information included in the selected synchronization signal block indicates that a cell, on which the synchronization signal block is received, is restricted, the control unit is adapted to exclude the synchronization signal block from candidates of the synchronization signal block used for the initial access. a receiving unit adapted to receive, from a base station apparatus, one or more synchronization signal blocks associated with one or more beams transmitted from the base station apparatus, the one or more synchronization signal blocks including information on initial access; a control unit adapted to select a synchronization signal block used for determining a resource for transmitting a preamble from the one or more synchronization blocks, based on at least one of received power and received quality of the one or more synchronization signal blocks; and a transmitting unit adapted to transmit the preamble to the base station apparatus using the resource, characterized in that if information included in the selected synchronization signal block indicates that a cell, on which the synchronization signal block is received, is restricted, the control unit is adapted to exclude the synchronization signal block from candidates of the synchronization signal block used for the initial access.
Armoured vehicle having an A pillar and a front windscreen, in particular made of an armour material, which is surrounded at least partially by a windscreen frame supported against a front surface of the A pillar, characterized in that at least one armour element (5, 7) is fastened to the windscreen frame on the side and/or on the front of the vehicle.