mhurhangee/ep-ind-claims huggingface dataset:
A terminal apparatus capable of short processing time, the terminal apparatus comprising: a reception unit configured to receive a first physical downlink control channel, PDCCH, with cyclic redundancy check scrambled by cell-radio network identifier, C-RNTI, including an uplink grant in a time division duplex TDD, serving cell configured with a TDD UL/DL configuration; and a transmission unit configured to perform uplink transmission in physical uplink shared channel, PUSCH, in a subframe n in the TDD serving cell upon a detection of the first PDCCH, wherein in a case that a first radio resource control, RRC, parameter associated with short processing time is received for the TDD serving cell, and the first PDCCH is decoded in a user equipment, UE, specific search space, a hybrid auto repeat request, HARQ, process corresponding to the uplink grant is determined as an asynchronous HARQ process, and value of UL HARQ round trip time, RTT, timer for the HARQ process is given according to a first table, in the case that the first RRC parameter is received for the TDD serving cell, and the first PDCCH is decoded in common search space, the HARQ process corresponding to the uplink grant is determined as a synchronous HARQ process, and value of UL HARQ RTT timer for the HARQ process is given according to a second table, the first table is TDD UL/DL Configuration Subframe index n 0 1 2 3 4 5 6 7 8 9 0 3 3 6 3 3 6 1 3 3 3 3 2 3 3 3 3 3 3 4 3 3 5 3 6 3 3 5 3 3 and the second table is TDD UL/DL Configuration Subframe index n 0 1 2 3 4 5 6 7 8 9 0 4 7 6 4 7 6 1 4 6 4 6 2 6 6 3 6 6 6 4 6 6 5 6 6 4 6 6 4 7 a reception unit configured to receive a first physical downlink control channel, PDCCH, with cyclic redundancy check scrambled by cell-radio network identifier, C-RNTI, including an uplink grant in a time division duplex TDD, serving cell configured with a TDD UL/DL configuration; and a transmission unit configured to perform uplink transmission in physical uplink shared channel, PUSCH, in a subframe n in the TDD serving cell upon a detection of the first PDCCH, wherein in a case that a first radio resource control, RRC, parameter associated with short processing time is received for the TDD serving cell, and the first PDCCH is decoded in a user equipment, UE, specific search space, a hybrid auto repeat request, HARQ, process corresponding to the uplink grant is determined as an asynchronous HARQ process, and value of UL HARQ round trip time, RTT, timer for the HARQ process is given according to a first table, in the case that the first RRC parameter is received for the TDD serving cell, and the first PDCCH is decoded in common search space, the HARQ process corresponding to the uplink grant is determined as a synchronous HARQ process, and value of UL HARQ RTT timer for the HARQ process is given according to a second table, the first table is TDD UL/DL Configuration Subframe index n 0 1 2 3 4 5 6 7 8 9 0 3 3 6 3 3 6 1 3 3 3 3 2 3 3 3 3 3 3 4 3 3 5 3 6 3 3 5 3 3 and the second table is TDD UL/DL Configuration Subframe index n 0 1 2 3 4 5 6 7 8 9 0 4 7 6 4 7 6 1 4 6 4 6 2 6 6 3 6 6 6 4 6 6 5 6 6 4 6 6 4 7
A needle-free injection device having a syringe end, the needle-free injection device comprising: an injector tube; a compressible main spring which can be selectively compressed to place the needle-free injection device in an armed configuration, the main spring being positioned within the injector tube; a hammer, the hammer being positioned within the injector tube; an upper handle pivotally attached to the needle-free injection device such that the upper handle pivots between an open and a closed position; a return sleeve engaged with the main spring; and an upper linkage engaged with the upper handle and the return sleeve, wherein the upper linkage causes the return sleeve to move away from the syringe end, causing the main spring to be compressed into the armed configuration, when the upper handle is moved from the open to the closed position, characterized in that the return sleeve is positioned outside of the injector tube, and the needle-free injection device further comprises a return spring biasing the return sleeve toward the syringe end of the needle-free injection device. an injector tube; a compressible main spring which can be selectively compressed to place the needle-free injection device in an armed configuration, the main spring being positioned within the injector tube; a hammer, the hammer being positioned within the injector tube; an upper handle pivotally attached to the needle-free injection device such that the upper handle pivots between an open and a closed position; a return sleeve engaged with the main spring; and an upper linkage engaged with the upper handle and the return sleeve, wherein the upper linkage causes the return sleeve to move away from the syringe end, causing the main spring to be compressed into the armed configuration, when the upper handle is moved from the open to the closed position, characterized in that the return sleeve is positioned outside of the injector tube, and the needle-free injection device further comprises a return spring biasing the return sleeve toward the syringe end of the needle-free injection device.
A method for securing a computer including a microcore, at least one virtualised operating system, a plurality of peripheral drivers and at least one access mediator filtering the information stream associated with each peripheral driver and exposing a virtual peripheral to said virtualised operating system, said microcore including a clock driver, a scheduler and an interprocess communication manager, at least one virtual machine, associated with each operating system, being formed by said core, resource managers, the peripheral drivers and the access mediators, characterised in that the method includes, at the access mediators, the steps of: - intercepting any communication between one of the peripheral drivers and said virtualised operating system, - checking that the intercepted communication is in accordance with preset access rules for said virtualised operating system; - transmitting the intercepted communication to the recipient if the intercepted communication is in accordance with the preset access rules, and in that each virtualised operating system is permitted, at start, to communicate only with the mediators which have this operating system as a client. - intercepting any communication between one of the peripheral drivers and said virtualised operating system, - checking that the intercepted communication is in accordance with preset access rules for said virtualised operating system; - transmitting the intercepted communication to the recipient if the intercepted communication is in accordance with the preset access rules,
Test arrangement for in-situ partial discharge measurements in distribution transformers, comprising at least • one test system having at least the following test components: • an AC voltage source for producing a variable test voltage, • a measuring apparatus for recording current pulses caused by partial discharge, • an evaluation apparatus for the recorded current pulses, • an earthed test container in which at least some of the test components (12, 14) are arranged, • and a distribution transformer connected to the AC voltage source as a test object, characterized in that provision is made of insulation means (38, 40, 64, 66) on which the test object is arranged in an electrically insulated and elevated manner, wherein the insulation means (38, 40, 64, 66) form a distance which ensures that the test object is electrically insulated with respect to its standing area, and in that the test object is at least predominantly connected to the potential of the earthed test container by those parts of the test object which need to be earthed during normal operation. • one test system having at least the following test components: • an AC voltage source for producing a variable test voltage, • a measuring apparatus for recording current pulses caused by partial discharge, • an evaluation apparatus for the recorded current pulses, • an AC voltage source for producing a variable test voltage, • a measuring apparatus for recording current pulses caused by partial discharge, • an evaluation apparatus for the recorded current pulses, • an earthed test container in which at least some of the test components (12, 14) are arranged, • and a distribution transformer connected to the AC voltage source as a test object,
A protective layer transfer sheet comprising a transfer layer provided on one surface of a substrate, wherein the transfer layer has a single-layer structure composed only of a protective layer or a layered structure in which a protective layer is located nearest to a side of the substrate, and the protective layer contains a styrene resin and a particulate organofluorine compound, wherein the particulate organofluorine compound has a particle size of 2 μm or more and 5 μm or less, and wherein a content of the particulate organofluorine compound is 2% by mass or more and 35% by mass or less based on a total mass of the protective layer. the transfer layer has a single-layer structure composed only of a protective layer or a layered structure in which a protective layer is located nearest to a side of the substrate, and the protective layer contains a styrene resin and a particulate organofluorine compound, wherein the particulate organofluorine compound has a particle size of 2 μm or more and 5 μm or less, and wherein a content of the particulate organofluorine compound is 2% by mass or more and 35% by mass or less based on a total mass of the protective layer.
Motor vehicle headlight comprising a light source, a control device and a liquid crystal matrix component which is arranged in the beam path of light emanating from the light source, a polarizing beam splitter being arranged between the light source and the liquid crystal matrix component such that the polarizing beam splitter splits the light incident from the light source into a matrix beam path and a base beam path, the matrix beam path leading from the beam splitter to the liquid crystal matrix component and consisting of light components which have a first polarization direction, and the base beam path consisting of light components which have a second polarization direction, and the base beam path, without touching the liquid crystal matrix component, leading to a first optical element which focuses the light incident in the base beam path, characterized in that the liquid crystal matrix component is divided into matrix elements, in that a degree of reflection of each matrix element can be adjusted individually by the control device, in that the beams of the matrix beam path are reflected on the liquid crystal matrix component according to the adjustment, and in that the liquid crystal matrix component is arranged relative to the polarizing beam splitter such that the matrix beam path passes through the same polarizing beam splitter again after a reflection on the liquid crystal matrix component.
A first policy handler to manage a global policy in a distributed environment, the first policy handler comprising: a parser to identify a first sub-policy of the global policy that is capable of enforcement by the first policy handler; an attester to sign the first sub-policy; and a director to: determine whether to forward the global policy to a second policy handler based on a signature status of the global policy, and forward the global policy to the second policy handler when the signature status of the global policy is indicative of an unsigned second sub-policy. a parser to identify a first sub-policy of the global policy that is capable of enforcement by the first policy handler; an attester to sign the first sub-policy; and a director to: determine whether to forward the global policy to a second policy handler based on a signature status of the global policy, and forward the global policy to the second policy handler when the signature status of the global policy is indicative of an unsigned second sub-policy. determine whether to forward the global policy to a second policy handler based on a signature status of the global policy, and forward the global policy to the second policy handler when the signature status of the global policy is indicative of an unsigned second sub-policy.
A method of heating a surface while fabricating a 3-D object, the method being characterized in that it comprises: monitoring, by at least one sensor, the temperature of first and second locations on a surface, and outputting, by the at least one sensor, a first temperature feedback signal from the first location and a second temperature feedback signal from the second location; controlling the energy radiated by an energy source during a first stage of the fabrication process using the first temperature feedback signal from the first location on the surface, the first location having raw build material; to thereby control the first location to be at a first target temperature during the first stage; and controlling the energy radiated by the energy source during a second stage of the fabrication process using the second temperature feedback signal from the second location on the surface, the second location having build material with agent deposited thereon, to thereby control the second location to be at a second target temperature during the second stage. monitoring, by at least one sensor, the temperature of first and second locations on a surface, and outputting, by the at least one sensor, a first temperature feedback signal from the first location and a second temperature feedback signal from the second location; controlling the energy radiated by an energy source during a first stage of the fabrication process using the first temperature feedback signal from the first location on the surface, the first location having raw build material; to thereby control the first location to be at a first target temperature during the first stage; and controlling the energy radiated by the energy source during a second stage of the fabrication process using the second temperature feedback signal from the second location on the surface, the second location having build material with agent deposited thereon, to thereby control the second location to be at a second target temperature during the second stage.
Method for operating a blower lance arrangement (hot blast lance arrangement), in which a hot blast is blown onto the molten pool and/or the aggregate material in a converter, the hot blast lance being fed by a hot blast source via a hot blast line, the hot blast lance being connected releasably to the hot blast source in such a way that the connection can be automatically opened and closed again for each batch, that is to say between the batches, characterized in that the hot blast lance can be moved vertically and relative to the stationary hot blast line via a lance carriage, and the hot blast lance is connected to the hot blast line via the hot blast closure by way of automatic actuable bayonet closure means, and the bayonet closure is locked automatically by means of a plurality of hydraulic operating cylinder loads when the connecting bayonet end position is reached.
A composition comprising tapentadol or its pharmaceutically acceptable salt(s) and at least one nasal carrier, for use in the treatment of pain, wherein the composition is applied to the nasal mucosa.
A rough cast blading of a turbomachine blade produced according to the lost-wax casting technique, the blade including an airfoil having a leading edge and a trailing edge opposite each other and connected by a pressure sidewall and a suction sidewall extending between a blade root and a blade tip, characterized in that, in order to produce on said blade a thin trailing edge which is not deformed by a subsequent material removal operation, said rough cast blading of said blade includes on a suction sidewall and/or on a pressure sidewall of said blading intended to respectively form said suction sidewall and/or said pressure sidewall of the blade, a casting allowance extending from a trailing edge of said blading intended to form said trailing edge of the blade over a determined width in the direction of a leading edge of said blading intended to form said leading edge of the blade, except for a reserved area extending in width according to the chord length of said blade between said trailing edge of the blading and the casting allowance and over at least part of the height of the blading.
An apparatus, comprising: an actuator to move a stem of a valve, the actuator including a housing defining a bore and a piston disposed in the bore; a rod movably coupled to the housing to extend into the bore; wherein the piston is movable on one hand by a fluid to flow into the bore or on the other hand by the rod; characterized in that the apparatus further comprises a lock to hold the rod in a first position on the housing where the rod is to disable a supply of the fluid to the bore. an actuator to move a stem of a valve, the actuator including a housing defining a bore and a piston disposed in the bore; a rod movably coupled to the housing to extend into the bore; wherein the piston is movable on one hand by a fluid to flow into the bore or on the other hand by the rod; characterized in that the apparatus further comprises a lock to hold the rod in a first position on the housing where the rod is to disable a supply of the fluid to the bore.
An ophthalmic surgical laser system to correct low hyperopia and/or myopia, comprising: a laser delivery system for delivering a femtosecond laser beam into a cornea of an eye; an XY-scan device to deflect the laser beam laterally; a Z-scan device to modify a depth of a focus of the laser beam; and a controller configured to control the XY-scan device and the Z-scan device to form an incised lenticule in a corneal stroma with the laser beam; wherein the laser system is configured to determine: a top lenticular incision to correct hyperopia and/or myopia having a circumference; a bottom lenticular incision to correct hyperopia and/or myopia, symmetric to the top lenticular incision having a circumference; and a shape with no correction power to space the top lenticular incision and the bottom lenticular incisions and thereby increase the thickness of the incised lenticule; and wherein the controller is configured to control the XY-scan device and the Z-scan device to incise: the spaced top lenticular incision; the spaced bottom lenticular incision; and a transition ring incision intersecting both the top lenticular incision circumference and the bottom lenticular incision circumference. a laser delivery system for delivering a femtosecond laser beam into a cornea of an eye; an XY-scan device to deflect the laser beam laterally; a Z-scan device to modify a depth of a focus of the laser beam; and a controller configured to control the XY-scan device and the Z-scan device to form an incised lenticule in a corneal stroma with the laser beam; wherein the laser system is configured to determine: a top lenticular incision to correct hyperopia and/or myopia having a circumference; a bottom lenticular incision to correct hyperopia and/or myopia, symmetric to the top lenticular incision having a circumference; and a shape with no correction power to space the top lenticular incision and the bottom lenticular incisions and thereby increase the thickness of the incised lenticule; and a top lenticular incision to correct hyperopia and/or myopia having a circumference; a bottom lenticular incision to correct hyperopia and/or myopia, symmetric to the top lenticular incision having a circumference; and a shape with no correction power to space the top lenticular incision and the bottom lenticular incisions and thereby increase the thickness of the incised lenticule; and wherein the controller is configured to control the XY-scan device and the Z-scan device to incise: the spaced top lenticular incision; the spaced bottom lenticular incision; and a transition ring incision intersecting both the top lenticular incision circumference and the bottom lenticular incision circumference. the spaced top lenticular incision; the spaced bottom lenticular incision; and a transition ring incision intersecting both the top lenticular incision circumference and the bottom lenticular incision circumference.
An airframe component for an aircraft, the airframe component comprising: a skin defining an aerodynamic surface having a side edge; and a sound absorber comprising: a perforated panel disposed at or adjacent the side edge of the aerodynamic surface, the perforated panel having a front side exposed to an ambient environment outside of the airframe component and an opposite back side, the panel comprising perforations extending through a thickness of the panel for permitting passage of sound waves therethrough; and a boundary surface spaced apart from the perforated panel, the boundary surface and the back side of the perforated panel at least partially defining a cavity in the airframe component for attenuating some of the sound waves entering the cavity via the perforations in the perforated panel; wherein the perforated panel is a part of a closing rib of the airframe component, the closing rib supporting the skin; and/or wherein the boundary surface is a part of a rib of the airframe component, the rib supporting the skin. a skin defining an aerodynamic surface having a side edge; and a sound absorber comprising: a perforated panel disposed at or adjacent the side edge of the aerodynamic surface, the perforated panel having a front side exposed to an ambient environment outside of the airframe component and an opposite back side, the panel comprising perforations extending through a thickness of the panel for permitting passage of sound waves therethrough; and a boundary surface spaced apart from the perforated panel, the boundary surface and the back side of the perforated panel at least partially defining a cavity in the airframe component for attenuating some of the sound waves entering the cavity via the perforations in the perforated panel; wherein the perforated panel is a part of a closing rib of the airframe component, the closing rib supporting the skin; and/or wherein the boundary surface is a part of a rib of the airframe component, the rib supporting the skin. a perforated panel disposed at or adjacent the side edge of the aerodynamic surface, the perforated panel having a front side exposed to an ambient environment outside of the airframe component and an opposite back side, the panel comprising perforations extending through a thickness of the panel for permitting passage of sound waves therethrough; and a boundary surface spaced apart from the perforated panel, the boundary surface and the back side of the perforated panel at least partially defining a cavity in the airframe component for attenuating some of the sound waves entering the cavity via the perforations in the perforated panel; wherein the perforated panel is a part of a closing rib of the airframe component, the closing rib supporting the skin; and/or wherein the boundary surface is a part of a rib of the airframe component, the rib supporting the skin. wherein the perforated panel is a part of a closing rib of the airframe component, the closing rib supporting the skin; and/or wherein the boundary surface is a part of a rib of the airframe component, the rib supporting the skin.