mhurhangee/ep-ind-claims huggingface dataset:
A base station adapted to perform Enhanced Interference Mitigation & Traffic Adaptation, eIMTA, the base station comprising one or more processors configured to: select a radio network temporary identifier, RNTI, used for eIMTA; select a periodicity for monitoring a physical downlink control channel, PDCCH, with the RNTI used for eIMTA; select a set of subframes to monitor the PDCCH with the RNTI used for eIMTA within the periodicity; encode for transmission to a user equipment, UE, the RNTI used for eIMTA, the set of subframes to monitor the PDCCH with the RNTI used for eIMTA; transmit a configuration comprising the RNTI and the set of subframes to the UE; and transmit a reconfiguration signal to the UE according to the periodicity, wherein the reconfiguration signal includes an indicator index. select a radio network temporary identifier, RNTI, used for eIMTA; select a periodicity for monitoring a physical downlink control channel, PDCCH, with the RNTI used for eIMTA; select a set of subframes to monitor the PDCCH with the RNTI used for eIMTA within the periodicity; encode for transmission to a user equipment, UE, the RNTI used for eIMTA, the set of subframes to monitor the PDCCH with the RNTI used for eIMTA; transmit a configuration comprising the RNTI and the set of subframes to the UE; and transmit a reconfiguration signal to the UE according to the periodicity, wherein the reconfiguration signal includes an indicator index.
A floating coil configuration (24, 26) for a compressor of a closed cycle cryogenic cooler, the coil configuration comprising: a. a coil having a positive end and a negative end; and b. first and second springs (30, 32) concentrically located within the coil, each spring (30, 32) having a first end and a second end; characterized in that the positive end of the coil is coupled to the first end of the second spring and the negative end of the coil is coupled to the second end of the first spring and the second end of the first spring is electrically coupled to the first end of the second spring such that the first and second springs (30, 32) define an electrical path across the coil. a. a coil having a positive end and a negative end; and b. first and second springs (30, 32) concentrically located within the coil, each spring (30, 32) having a first end and a second end;
Method of manufacturing a final assembly comprising at least one layer made up of N'>1 helically wound metal filamentary elements, the method comprising: - a step of supplying a transitory assembly comprising at least one layer made up of M'>1 metal filamentary elements helically wound around a transitory core, - a step of separating the transitory assembly into at least: - a first split assembly comprising at least one layer made up of M1'≥1 helically wound metal filamentary element(s), the M1' metal filamentary element(s) originating from the layer made up of M'>1 metal filamentary elements of the transitory assembly, - a second split assembly comprising at least one layer made up of M2'>1 helically wound metal filamentary elements, the M2' metal filamentary elements originating from the layer made up of M'>1 metal filamentary elements of the transitory assembly, - the transitory core or one or more ensembles comprising the transitory core, characterized in that the method comprises a step of reassembling at least the first split assembly with the second split assembly to form the layer made up of N' helically wound metal filamentary elements and wherein M'>2. - a step of supplying a transitory assembly comprising at least one layer made up of M'>1 metal filamentary elements helically wound around a transitory core, - a step of separating the transitory assembly into at least: - a first split assembly comprising at least one layer made up of M1'≥1 helically wound metal filamentary element(s), the M1' metal filamentary element(s) originating from the layer made up of M'>1 metal filamentary elements of the transitory assembly, - a second split assembly comprising at least one layer made up of M2'>1 helically wound metal filamentary elements, the M2' metal filamentary elements originating from the layer made up of M'>1 metal filamentary elements of the transitory assembly, - the transitory core or one or more ensembles comprising the transitory core, - a first split assembly comprising at least one layer made up of M1'≥1 helically wound metal filamentary element(s), the M1' metal filamentary element(s) originating from the layer made up of M'>1 metal filamentary elements of the transitory assembly, - a second split assembly comprising at least one layer made up of M2'>1 helically wound metal filamentary elements, the M2' metal filamentary elements originating from the layer made up of M'>1 metal filamentary elements of the transitory assembly, - the transitory core or one or more ensembles comprising the transitory core,
A fuel tube for a gasoline engine, the fuel tube comprising: an outer polymer layer constructed of a polyamide selected from a group consisting of polyamide 12, polyamide 11, polyamide 10-10, polyamide 6-10, polyamide 6-12, polyamide 12-12 and combinations thereof; an inner polymer layer constructed of a low oligomer polyamide selected from a group consisting of polyamide 6-10, polyamide 6-12, polyamide 10-10 and combinations thereof; and an intermediate layer of ethylene vinyl alcohol copolymer (EVOH), wherein the intermediate layer is a permeation barrier layer having an ethylene content of 24 to 29 mol percent and a thickness between 0.02 mm and 0.07 mm. an outer polymer layer constructed of a polyamide selected from a group consisting of polyamide 12, polyamide 11, polyamide 10-10, polyamide 6-10, polyamide 6-12, polyamide 12-12 and combinations thereof; an inner polymer layer constructed of a low oligomer polyamide selected from a group consisting of polyamide 6-10, polyamide 6-12, polyamide 10-10 and combinations thereof; and an intermediate layer of ethylene vinyl alcohol copolymer (EVOH), wherein the intermediate layer is a permeation barrier layer having an ethylene content of 24 to 29 mol percent and a thickness between 0.02 mm and 0.07 mm.
A cold room vent comprising: a mount mountable to a cold room structure; a valve housing coupled to said mount, said valve housing defining a heat chamber having an air passage entrance opening; at least one valve coupled to said valve housing; a thermally conductive heat sink plate mounted closely adjacent said valve housing air passage entrance opening, said heat sink plate having a front surface and a rear surface facing said valve housing, said heat sink plate having a plurality of vent openings therethrough, said heat sink plate also having a projection extending from said rear surface between two said vent openings of said plurality of vent openings and into said heat chamber, and a heat source coupled to and in thermal communication with said heat sink plate, whereby heat generated by the heat source is thermally conducted to the thermally conductive heat sink plate wherein the projection transfers heat to the heat chamber to warm the at least one valve characterized in that said at least one valve includes a gravity biased first pressure intake valve having a first weight which allows the opening of said gravity biased first pressure intake valve at a first air pressure level, and a gravity biased second pressure intake valve having a second weight which allows the opening of said gravity biased second pressure intake valve at a second air pressure level greater than said first air pressure level. a mount mountable to a cold room structure; a valve housing coupled to said mount, said valve housing defining a heat chamber having an air passage entrance opening; at least one valve coupled to said valve housing; a thermally conductive heat sink plate mounted closely adjacent said valve housing air passage entrance opening, said heat sink plate having a front surface and a rear surface facing said valve housing, said heat sink plate having a plurality of vent openings therethrough, said heat sink plate also having a projection extending from said rear surface between two said vent openings of said plurality of vent openings and into said heat chamber, and a heat source coupled to and in thermal communication with said heat sink plate, whereby heat generated by the heat source is thermally conducted to the thermally conductive heat sink plate wherein the projection transfers heat to the heat chamber to warm the at least one valve characterized in that said at least one valve includes a gravity biased first pressure intake valve having a first weight which allows the opening of said gravity biased first pressure intake valve at a first air pressure level, and a gravity biased second pressure intake valve having a second weight which allows the opening of said gravity biased second pressure intake valve at a second air pressure level greater than said first air pressure level.
An absolute position magnetic sensor for measuring the angular position, on a theta stroke, of a shaft passing through said sensor and which comprises at least two systems for detecting the position of said shaft, characterized in that: - at least a first detection system comprises a continuous motion-converting mechanical system, the input shaft of which is connected to said shaft, with said at least first detection system generating a signal according to a periodic function having a theta/n period giving the periodic angular position of said shaft; - at least a second detection system generates an absolute signal on a theta stroke of said shaft; - theta and n are related by the following equations:. theta/n=360. N>1 - a first diametral magnetization magnet is connected with a hollow screw having a large diameter mounted about the shaft, and belongs to the first system, said screw rotates a pinion which a second magnet belonging to the second detection system is connected with. - at least a first detection system comprises a continuous motion-converting mechanical system, the input shaft of which is connected to said shaft, with said at least first detection system generating a signal according to a periodic function having a theta/n period giving the periodic angular position of said shaft; - at least a second detection system generates an absolute signal on a theta stroke of said shaft; - theta and n are related by the following equations:. theta/n=360. N>1. theta/n=360. N>1 - a first diametral magnetization magnet is connected with a hollow screw having a large diameter mounted about the shaft, and belongs to the first system, said screw rotates a pinion which a second magnet belonging to the second detection system is connected with.
A swellable packer assembly for positioning in a wellbore, the swellable packer assembly comprising: a mandrel; a swellable sealing element (104, 124) disposed radially about the mandrel, the sealing element formed of a material responsive to exposure to a trigger fluid to radially expand from the mandrel; at least one retaining element fixedly coupled to the mandrel adjacent the sealing element such that the at least one retaining element limits longitudinal movement of the sealing element along the mandrel; and a shroud sealingly coupled to the at least one retaining element to fluidly isolate the sealing element from an exterior of the shroud and to define an annular cavity disposed radially between the sealing element and the shroud, the shroud selectively removable from the mandrel downhole, and configured to be dissolved with the trigger fluid at a predetermined downhole location, so as to expose the sealing element to the trigger fluid in the wellbore. a mandrel; a swellable sealing element (104, 124) disposed radially about the mandrel, the sealing element formed of a material responsive to exposure to a trigger fluid to radially expand from the mandrel; at least one retaining element fixedly coupled to the mandrel adjacent the sealing element such that the at least one retaining element limits longitudinal movement of the sealing element along the mandrel; and a shroud sealingly coupled to the at least one retaining element to fluidly isolate the sealing element from an exterior of the shroud and to define an annular cavity disposed radially between the sealing element and the shroud, the shroud selectively removable from the mandrel downhole, and configured to be dissolved with the trigger fluid at a predetermined downhole location, so as to expose the sealing element to the trigger fluid in the wellbore.
Electromechanical relay comprising: a contact assembly comprising at least one stationary contact and at least one movable contact, an electromagnetic actuator assembly for actuating the at least one movable contact, wherein the electromagnetic actuator assembly comprises a coil assembly (116, 120, 122) for generating a magnetic field and a movable actuator arm that engages with the movable contact for actuating the movable contact in response to said magnetic field, wherein said actuator arm is slidable in a direction across to a longitudinal axis of the movable contact, and a housing that encases the contact assembly and the electromagnetic actuator assembly, wherein the electromechanical relay further comprises a rotatable test button with operating means that can engage with the actuator arm for manually operating the at least one movable contact from outside the housing by rotating said test button, characterized in that the test button is rotatable around an axis that extends across to the actuator arm, wherein the test button comprises a cam protrusion that is operable to engage with guiding means formed at the actuator arm for translating the rotating movement of the test button into a linear movement of the actuator arm. a contact assembly comprising at least one stationary contact and at least one movable contact, an electromagnetic actuator assembly for actuating the at least one movable contact, wherein the electromagnetic actuator assembly comprises a coil assembly (116, 120, 122) for generating a magnetic field and a movable actuator arm that engages with the movable contact for actuating the movable contact in response to said magnetic field, wherein said actuator arm is slidable in a direction across to a longitudinal axis of the movable contact, and a housing that encases the contact assembly and the electromagnetic actuator assembly, wherein the electromechanical relay further comprises a rotatable test button with operating means that can engage with the actuator arm for manually operating the at least one movable contact from outside the housing by rotating said test button, characterized in that the test button is rotatable around an axis that extends across to the actuator arm, wherein the test button comprises a cam protrusion that is operable to engage with guiding means formed at the actuator arm for translating the rotating movement of the test button into a linear movement of the actuator arm.
Method for the individualised and automated control of the means for closing off at least one window (1, 2) of a building, the said method consisting in: - determining coordinates of at least one dazzle cone (C1/1, C1/2, C2/1, C2/2) associated with a window and with a dazzle-sensitive zone situated inside the building, the said at least one dazzle cone being defined by, on the one hand, a vertex positioned at the sensitive zone and a directrix curve superimposed on the perimeter of the said at least one window (1, 2); - determining the orientation of the direct rays of sunlight, the orientation of the said rays being defined by a solar azimuth (As) and a solar elevation (Es); - periodically checking whether the orientation of the rays of sunlight falls within at least one predetermined dazzle cone (C1/1, C1/2, C2/1, C2/2); the direction of the rays of sunlight being parallel to one of the directions contained within the dazzle cone and passing through the vertex of the said cone; - acting on the closing-off means associated with the said at least one window (1, 2) for which the orientation of the rays of sunlight falls within at least one dazzle cone (C1/1, C1/2, C2/1, C2/2). - determining coordinates of at least one dazzle cone (C1/1, C1/2, C2/1, C2/2) associated with a window and with a dazzle-sensitive zone situated inside the building, the said at least one dazzle cone being defined by, on the one hand, a vertex positioned at the sensitive zone and a directrix curve superimposed on the perimeter of the said at least one window (1, 2); - determining the orientation of the direct rays of sunlight, the orientation of the said rays being defined by a solar azimuth (As) and a solar elevation (Es); - periodically checking whether the orientation of the rays of sunlight falls within at least one predetermined dazzle cone (C1/1, C1/2, C2/1, C2/2); the direction of the rays of sunlight being parallel to one of the directions contained within the dazzle cone and passing through the vertex of the said cone; - acting on the closing-off means associated with the said at least one window (1, 2) for which the orientation of the rays of sunlight falls within at least one dazzle cone (C1/1, C1/2, C2/1, C2/2).
A radiation detector comprising: a photoelectric conversion element array having a light receiving unit including a plurality of photoelectric conversion elements one-dimensionally or two-dimensionally arrayed, and a plurality of bonding pads electrically connected to the photoelectric conversion elements and arranged outside the light receiving unit; a scintillator layer stacked on the photoelectric conversion element array so as to cover the light receiving unit and configured to convert radiation into light; a resin frame formed on the photoelectric conversion element array, when viewed from a stacking direction of the scintillator layer, so as to pass between the scintillator layer and the bonding pads away from the scintillator layer and the bonding pads and so as to surround the scintillator layer; a protection film covering the scintillator layer and having an outer edge located on the resin frame; and a coating resin layer arranged along the resin frame so as to cover the outer edge of the protection film, characterized in that a first distance between an inner edge of the resin frame and an outer edge of the scintillator layer is shorter than a second distance between an outer edge of the resin frame and an outer edge of the photoelectric conversion element array, and the outer edge of the protection film and a groove of the resin frame corresponding to the outer edge of the protection film are in a processed state with a laser beam and are finely corrugated when viewed from the stacking direction. a photoelectric conversion element array having a light receiving unit including a plurality of photoelectric conversion elements one-dimensionally or two-dimensionally arrayed, and a plurality of bonding pads electrically connected to the photoelectric conversion elements and arranged outside the light receiving unit; a scintillator layer stacked on the photoelectric conversion element array so as to cover the light receiving unit and configured to convert radiation into light; a resin frame formed on the photoelectric conversion element array, when viewed from a stacking direction of the scintillator layer, so as to pass between the scintillator layer and the bonding pads away from the scintillator layer and the bonding pads and so as to surround the scintillator layer; a protection film covering the scintillator layer and having an outer edge located on the resin frame; and a coating resin layer arranged along the resin frame so as to cover the outer edge of the protection film, characterized in that a first distance between an inner edge of the resin frame and an outer edge of the scintillator layer is shorter than a second distance between an outer edge of the resin frame and an outer edge of the photoelectric conversion element array, and the outer edge of the protection film and a groove of the resin frame corresponding to the outer edge of the protection film are in a processed state with a laser beam and are finely corrugated when viewed from the stacking direction.
An equalisation unit for use in a secondary part, which can be either engaged or disengaged by means of a clutch assembly with a clutch device, of an overall drive train of a motor vehicle, which in addition to the secondary part has a continuously driven primary part, the equalisation unit having an oil-delivering device, which delivers oil for oiling the clutch and bearing when the secondary part of the drive train is engaged and is deactivated and does not deliver oil for oiling the clutch and bearing when the secondary part of the drive train is decoupled from the primary part, the equalisation unit having an axial rolling bearing (13', 13"), characterised in that the equalisation unit is formed in such a manner that the axial rolling bearing (13', 13") still rotates but is not supplied with oil when the secondary part is decoupled and the oil-delivering device is deactivated, wherein the axial rolling bearing (13', 13") is formed as an axial rolling bearing with emergency lubrication and has a bearing ring that forms a bearing running face, on which an oil collection channel is provided on the radial outer side to ensure emergency lubrication.
Method for operating a communication system having multiple nodes that have access to a common channel of the communication system, wherein the method involves a transmission process for transmitting a message via the channel being monitored for bit errors, wherein the occurrence of a bit error results in a signalling message for signalling the bit error being transmitted via the channel, wherein a signalling rate (r) of the signalling messages is measured, characterized in that a bit error rate of the channel is ascertained on the basis of the signalling rate (r) and a channel occupancy (p) of the channel and a capacity (c) of the channel.
A process for preparing a substituted 3-((pyrrol-2-yl)methylene)-2-pyrrolone of formula or a salt thereof: comprising: a) reacting a compound of formula or a compound of formula: with a compound of formula: to obtain the substituted 3-((pyrrol-2-yl)methylene)-2-pyrrolone of formula, wherein R 1 and R 4 are optionally and independently H, C 1 -C 8 alkyl, silyl; R 2 and R 3 together form a substituted fused aromatic ring; R independently is C 1 -C 8 alkyl; R 5 is H or C 1 -C 8 alkyl; R 6, R 7, and R 8 independently are H, C 1 -C 8 alkyl, silyl, or COR" wherein R" is H, C 1 -C 8 alkyl, OH, SH, NH 2, O-C 1 -C 8 alkyl, NH-C 1 -C 12 alkyl, or N, N -di-C 1 -C 12 alkyl,; and R 9 and R 10 are independently selected from C 1 -C 12 alkyl or silyl; X is Cl, Br, or I. and b) optionally reacting the substituted 3-((pyrrol-2-yl)methylene)-2-pyrrolone of formula with a salt forming agent to obtain the salt thereof; wherein the reaction between the compound of formula and the compound of formula in the reacting step a) is conducted in the presence of a catalyst and in a solvent. a) reacting a compound of formula or a compound of formula: with a compound of formula: to obtain the substituted 3-((pyrrol-2-yl)methylene)-2-pyrrolone of formula, wherein R 1 and R 4 are optionally and independently H, C 1 -C 8 alkyl, silyl; R 2 and R 3 together form a substituted fused aromatic ring; R independently is C 1 -C 8 alkyl; R 5 is H or C 1 -C 8 alkyl; R 6, R 7, and R 8 independently are H, C 1 -C 8 alkyl, silyl, or COR" wherein R" is H, C 1 -C 8 alkyl, OH, SH, NH 2, O-C 1 -C 8 alkyl, NH-C 1 -C 12 alkyl, or N, N -di-C 1 -C 12 alkyl,; and R 9 and R 10 are independently selected from C 1 -C 12 alkyl or silyl; X is Cl, Br, or I. and b) optionally reacting the substituted 3-((pyrrol-2-yl)methylene)-2-pyrrolone of formula with a salt forming agent to obtain the salt thereof;