mhurhangee/ep-ind-claims huggingface dataset:
A method of receiving channel status information, CSI, in a radio communication system, by an Node B, comprising: determining whether carrier aggregation, CA, with a primary cell supporting the TDD mode and a secondary cell supporting the FDD mode is configured with respect to a user equipment, UE; selecting (1202; 1402) a second CSI transmission period for periodic CSI reporting of the secondary cell from a first set of CSI transmission periods, in response to determination that CA with the primary cell supporting the TDD mode and the secondary cell supporting the FDD mode is configured with respect to the UE, wherein the first set of CSI transmission periods comprises {1, 5, 10, 20, 40, 80, 160} being associated with a time duplex division, TDD, mode and a second set of CSI transmission periods comprises {2, 5, 10, 20, 40, 80, 160, 32, 64, 128} being associated with a frequency duplex division, FDD, mode; receiving (1206; 1406), from the UE, a periodic CSI report of the secondary cell in an uplink subframe of the primary cell determined according to the second CSI transmission period on a physical uplink shared channel, PUSCH, of the primary cell, in case that the UE has a PUSCH transmission for the primary cell in the uplink subframe being determined according to the second CSI transmission period; and receiving (1206; 1408), from the UE, the periodic CSI report of the secondary cell on a physical uplink control channel, PUCCH, in the uplink subframe of the primary cell, in case that the UE does not have a PUSCH transmission in the uplink subframe of the primary cell. determining whether carrier aggregation, CA, with a primary cell supporting the TDD mode and a secondary cell supporting the FDD mode is configured with respect to a user equipment, UE; selecting (1202; 1402) a second CSI transmission period for periodic CSI reporting of the secondary cell from a first set of CSI transmission periods, in response to determination that CA with the primary cell supporting the TDD mode and the secondary cell supporting the FDD mode is configured with respect to the UE, wherein the first set of CSI transmission periods comprises {1, 5, 10, 20, 40, 80, 160} being associated with a time duplex division, TDD, mode and a second set of CSI transmission periods comprises {2, 5, 10, 20, 40, 80, 160, 32, 64, 128} being associated with a frequency duplex division, FDD, mode; receiving (1206; 1406), from the UE, a periodic CSI report of the secondary cell in an uplink subframe of the primary cell determined according to the second CSI transmission period on a physical uplink shared channel, PUSCH, of the primary cell, in case that the UE has a PUSCH transmission for the primary cell in the uplink subframe being determined according to the second CSI transmission period; and receiving (1206; 1408), from the UE, the periodic CSI report of the secondary cell on a physical uplink control channel, PUCCH, in the uplink subframe of the primary cell, in case that the UE does not have a PUSCH transmission in the uplink subframe of the primary cell.
A supporting method for supporting a reinforcement structure (1, 2) in the production of precast concrete parts, wherein - in a first method step data of a reinforcement structure (1, 2) designed for the precast concrete part to be produced are provided, - in a second method step positions (33, 34) for supporting the reinforcement structure (1, 2) are calculated in a program-controlled electronic computing system in dependence on the provided data of the reinforcement structure (1, 2), and - in a third method step spacers are placed at the calculated positions (33, 34) for supporting the reinforcement structure (1, 2), characterised by the step that: - in a fourth method step a reinforcement structure (1, 2) produced in accordance with the data is placed on the spacers. - in a first method step data of a reinforcement structure (1, 2) designed for the precast concrete part to be produced are provided, - in a second method step positions (33, 34) for supporting the reinforcement structure (1, 2) are calculated in a program-controlled electronic computing system in dependence on the provided data of the reinforcement structure (1, 2), and - in a third method step spacers are placed at the calculated positions (33, 34) for supporting the reinforcement structure (1, 2), characterised by the step that: - in a fourth method step a reinforcement structure (1, 2) produced in accordance with the data is placed on the spacers.
A carrier (105, 205) for holding a plurality of containers (CA1, CA2, CA3, CA4, CB1, CB2, CB3, CB4), the carrier (105, 205) comprising: a plurality of panels including at least one central panel, at least one attachment panel foldably connected to the at least one central panel and configured to receive a portion of one or more containers of the plurality of containers (CA1, CA2, CA3, CA4, CB1, CB2, CB3, CB4), at least one side panel foldably connected to the at least one attachment panel, and at least one top panel foldably connected to the at least one side panel, the at least one central panel includes a plurality of openings and is for being positioned between and attached to adjacent containers of the plurality of containers (CA1, CA2, CA3, CA4, CB1, CB2, CB3, CB4), the at least one top panel has an outer free edge (157a, 157b, 257a, 257b) arranged to expose a portion of the at least one attachment panel. a plurality of panels including at least one central panel, at least one attachment panel foldably connected to the at least one central panel and configured to receive a portion of one or more containers of the plurality of containers (CA1, CA2, CA3, CA4, CB1, CB2, CB3, CB4), at least one side panel foldably connected to the at least one attachment panel, and at least one top panel foldably connected to the at least one side panel, the at least one central panel includes a plurality of openings and is for being positioned between and attached to adjacent containers of the plurality of containers (CA1, CA2, CA3, CA4, CB1, CB2, CB3, CB4), the at least one top panel has an outer free edge (157a, 157b, 257a, 257b) arranged to expose a portion of the at least one attachment panel.
A partition configured to be positioned within an aircraft, the partition comprising: a first divider assembly that includes a first wall portion having a first jamb member secured to an inboard surface thereof and a first door hingedly connected to the first jamb member, wherein the first jamb member includes a first LED light strip lighting that illuminates the first door, wherein the first jamb member includes a vertically extending channel running therethrough, wherein the first LED light strip is disposed in the channel and positioned to direct light toward an outboard surface of the first door, wherein the first LED light strip is positioned adjacent a first lens, and wherein the first door is movable between a stowed position and a deployed position, and a second divider assembly that includes a second wall portion having a second jamb member secured to an inboard surface thereof and a second door hingedly connected to the second jamb member, wherein the second jamb member includes a second LED light strip lighting that illuminates the second door, wherein the second jamb member includes a vertically extending channel running therethrough, and wherein the second LED light strip is disposed in the channel and positioned to direct light toward an outboard surface of the second door, wherein the second LED light strip is positioned adjacent a second lens, wherein the second door is movable between a stowed position and a deployed position, and wherein the second door is spaced apart from the first door. a first divider assembly that includes a first wall portion having a first jamb member secured to an inboard surface thereof and a first door hingedly connected to the first jamb member, wherein the first jamb member includes a first LED light strip lighting that illuminates the first door, wherein the first jamb member includes a vertically extending channel running therethrough, wherein the first LED light strip is disposed in the channel and positioned to direct light toward an outboard surface of the first door, wherein the first LED light strip is positioned adjacent a first lens, and wherein the first door is movable between a stowed position and a deployed position, and a second divider assembly that includes a second wall portion having a second jamb member secured to an inboard surface thereof and a second door hingedly connected to the second jamb member, wherein the second jamb member includes a second LED light strip lighting that illuminates the second door, wherein the second jamb member includes a vertically extending channel running therethrough, and wherein the second LED light strip is disposed in the channel and positioned to direct light toward an outboard surface of the second door, wherein the second LED light strip is positioned adjacent a second lens, wherein the second door is movable between a stowed position and a deployed position, and wherein the second door is spaced apart from the first door.
A method for evaluating annulus-tubing communication points in a production well, the production well having one or more strings of casing extending below a surface, and a string of production tubing within the strings of casing thereby forming an annulus, and the method comprising: placing up to 1,000 cc's of each of one or more tracer materials into a portable, hand-held vessel; causing the one or more tracer materials to be injected from the vessel into the annulus of the well under pressure as part of a lift gas, wherein each of the one or more tracer materials defines a material that is not native to the production fluids; further injecting the lift gas in order to cause the one or more tracer materials to contact the annulus-tubing communication points residing along the production tubing, and to enter the production tubing; producing formation fluids along with lift gas and the one or more tracer materials to the surface; detecting the one or more tracer materials at the surface by using a fluid analyzer, wherein the fluid analyzer is capable of detecting the one or more tracer materials at concentrations of less than 1,000 ppm; and measuring a concentration of each of the one or more tracer materials in the produced fluids as a function of time. placing up to 1,000 cc's of each of one or more tracer materials into a portable, hand-held vessel; causing the one or more tracer materials to be injected from the vessel into the annulus of the well under pressure as part of a lift gas, wherein each of the one or more tracer materials defines a material that is not native to the production fluids; further injecting the lift gas in order to cause the one or more tracer materials to contact the annulus-tubing communication points residing along the production tubing, and to enter the production tubing; producing formation fluids along with lift gas and the one or more tracer materials to the surface; detecting the one or more tracer materials at the surface by using a fluid analyzer, wherein the fluid analyzer is capable of detecting the one or more tracer materials at concentrations of less than 1,000 ppm; and measuring a concentration of each of the one or more tracer materials in the produced fluids as a function of time.
A doped protective coating for extending a lifetime of an organic photoconductor, the coating including: an in-situ cross-linked polymer matrix and a substantially uniformly distributed dopant therein, the dopant comprising a charge transport molecular species; and, wherein the coating is formed from a matrix polymer species comprising a monomer, the dopant, an initiator, a cross-linker, and a solvent in which both the matrix polymer species and the dopant are soluble; and characterized in that the monomer is selected from the group consisting of multifunctional acrylates, styrene, divinyl benzene, iso-cyanates, and di-iso-cyanates and in that the dopant is selected from the group consisting of aryl hydrazones and their substituted analogs, and aminoaryl oxadiazoles and their substituted analogs. an in-situ cross-linked polymer matrix and a substantially uniformly distributed dopant therein, the dopant comprising a charge transport molecular species; and, wherein the coating is formed from a matrix polymer species comprising a monomer, the dopant, an initiator, a cross-linker, and a solvent in which both the matrix polymer species and the dopant are soluble; and characterized in that the monomer is selected from the group consisting of multifunctional acrylates, styrene, divinyl benzene, iso-cyanates, and di-iso-cyanates
A cooled isolation valve (10, 200), comprising: a valve body; a stationary element coupled to the valve body and stationary with respect to the valve body; a movable closure element being movable with respect to the stationary element between a closed position in which the movable closure element and the stationary element are brought together and an open position, one of the movable closure element and the stationary element comprising a sealing element, in the closed position of the movable closure element, the sealing element providing a seal between the movable closure element and the stationary element; and a fluid channel formed in contact with the movable closure element and movable with the movable closure element with respect to the stationary element, such that a fluid in the fluid channel effects heat transfer in the movable closure element; characterised in that the cooled isolation valve (10, 200) further comprises a temperature sensor measuring the temperature of the valve (10, 200) and a pilot valve that modulates the flow of the cooling fluid in order to regulate the temperature of the valve (10, 200) as measured by the temperature sensor and a sensor for detecting whether the movable closure element is in the open position or the closed position, wherein an actuator is configured to inhibit flow of the cooling fluid when the sensor detects that the movable closure element is in the closed position. a valve body; a stationary element coupled to the valve body and stationary with respect to the valve body; a movable closure element being movable with respect to the stationary element between a closed position in which the movable closure element and the stationary element are brought together and an open position, one of the movable closure element and the stationary element comprising a sealing element, in the closed position of the movable closure element, the sealing element providing a seal between the movable closure element and the stationary element; and a fluid channel formed in contact with the movable closure element and movable with the movable closure element with respect to the stationary element, such that a fluid in the fluid channel effects heat transfer in the movable closure element; characterised in that the cooled isolation valve (10, 200) further comprises a temperature sensor measuring the temperature of the valve (10, 200) and a pilot valve that modulates the flow of the cooling fluid in order to regulate the temperature of the valve (10, 200) as measured by the temperature sensor and a sensor for detecting whether the movable closure element is in the open position or the closed position, wherein an actuator is configured to inhibit flow of the cooling fluid when the sensor detects that the movable closure element is in the closed position.
A gas turbine engine compressor stage comprising: a rotor; compressor blades supported by the rotor, the blades include an inner flow path surface each supporting an airfoil that has a chord extending radially along a span to a tip, a shroud supported at the tip and providing an outer flow path surface, wherein the shroud provides a noncontiguous ring about the compressor stage; wherein the airfoils have an aspect ratio corresponding to the airfoil span to the airfoil chord, the shroud extends the full chord, wherein the aspect ratio is in a range of 1.6 to 2.8. a rotor; compressor blades supported by the rotor, the blades include an inner flow path surface each supporting an airfoil that has a chord extending radially along a span to a tip, a shroud supported at the tip and providing an outer flow path surface, wherein the shroud provides a noncontiguous ring about the compressor stage; wherein the airfoils have an aspect ratio corresponding to the airfoil span to the airfoil chord, the shroud extends the full chord, wherein the aspect ratio is in a range of 1.6 to 2.8.
An adjustable shoe which stands on a substrate, having - at least one shoe sole and - at least one shoe heel wherein the shoe sole is subdivided into at least two sole parts, specifically a toe part and a heel part, which when viewed in a longitudinal direction of the shoe sole are arranged at least indirectly after one another, wherein adjacent sole parts are each interconnected by means of at least one hinge mechanism, wherein the sole parts are twistable relative to each other by means of the hinge mechanism, wherein at least the heel part and at least one further sole part adjacent to the heel part can be interconnected in a torque-proof manner in at least one locking position in a vertical state of the shoe, wherein the shoe heel is movable relative to the shoe sole at least between an active position and a passive position, the shoe thus being adjustable at least between the vertical state thereof and the horizontal state thereof, wherein the shoe sole has a shoe heel compartment, within which the shoe heel can be stored when it is in its passive position, wherein, with the shoe heel in the active position, in which the shoe heel is arranged in a force transmitting manner at least on the heel part and is standing with a shoe heel surface on the substrate, a heel surface, which is arranged on a bottom of the heel part that faces the substrate, is spaced at a distance from the substrate, wherein the heel surface is in direct contact with the substrate in the passive position of the shoe heel. - at least one shoe sole and - at least one shoe heel
A single-wheeled vehicle, comprising a motor, pedals and a wheel, the motor comprising a motor housing and a spindle, wherein two ends of the spindle are fixedly connected to the pedals respectively, the wheel is spherical or elliptical and is of a hollow structure having two ends formed with openings, and the wheel is arranged on the motor housing in a sleeving manner, is fixedly connected to the motor housing, and comprises a sleeve made from an elastic material, characterized in that each said pedal comprises a conical shield plate, and ends, close to the wheel, of the shield plates have a diameter equal to that of the openings of the wheel.
A dental device for anchoring a dental appliance to a patient's mouth, wherein the dental device comprises: an anchor, having an insertion end and a distal end, said distal end having formed therein a first hollow; an abutment, having an insertion end and a distal end, said distal end having a substantially concave surface and having formed therein a second, threaded hollow; said insertion end of said abutment being connectable within said first hollow; a pivotable collar having a substantially hemispherical convex bottom and further having formed through it a third hollow extending from top to bottom; said bottom of said pivotable collar configured to pivotally rest against said concave surface of said abutment; an attachment screw, having an insertion end and a distal end; wherein said attachment screw is configured to extend partially through said collar so that said insertion end of said attachment screw is interconnected with said second threaded hollow, so as to secure said collar to said abutment, whereby the orientation of said pivotable collar is adjustable when said retention screw is not interconnected with said second threaded hollow and is not adjustable when said retention screw is interconnected with said second threaded hollow; characterized in that said first hollow is a threaded hollow. an anchor, having an insertion end and a distal end, said distal end having formed therein a first hollow; an abutment, having an insertion end and a distal end, said distal end having a substantially concave surface and having formed therein a second, threaded hollow; said insertion end of said abutment being connectable within said first hollow; a pivotable collar having a substantially hemispherical convex bottom and further having formed through it a third hollow extending from top to bottom; said bottom of said pivotable collar configured to pivotally rest against said concave surface of said abutment; an attachment screw, having an insertion end and a distal end; wherein said attachment screw is configured to extend partially through said collar so that said insertion end of said attachment screw is interconnected with said second threaded hollow, so as to secure said collar to said abutment, whereby the orientation of said pivotable collar is adjustable when said retention screw is not interconnected with said second threaded hollow and is not adjustable when said retention screw is interconnected with said second threaded hollow; characterized in that said first hollow is a threaded hollow.
Gas burner comprising • a cylindrical casing which is open from below for the flow of combustion air; • a combustion primary head with axial main performance fuel nozzles, which primary head is arranged in the axis of the cylindrical casing; • an income tube portion in front of the primary head divided into a plurality of tubes arranged in a circle, • a gas distributor, the income tube portion leading into the gas distributor, • a tube portion leading from the gas distributor to the primary head, • other fuel nozzles of the plurality of fuel tubes - arranged on the output of the casing, and - being orientated into a gas burner output • a swirler, the primary head being provided with the swirler; • radial stabilization nozzles around the circumference of the primary head provided in front of the swirler in the direction of the gas burner output; • a reduction piece - arranged on the tube portion leading from the gas distributor to the primary head, and - provided with a passing-through opening which is smaller than an opening in the tube portion; and • wherein the primary head is arranged on the reduction piece. • a cylindrical casing which is open from below for the flow of combustion air; • a combustion primary head with axial main performance fuel nozzles, which primary head is arranged in the axis of the cylindrical casing; • an income tube portion in front of the primary head divided into a plurality of tubes arranged in a circle, • a gas distributor, the income tube portion leading into the gas distributor, • a tube portion leading from the gas distributor to the primary head, • other fuel nozzles of the plurality of fuel tubes - arranged on the output of the casing, and - being orientated into a gas burner output - arranged on the output of the casing, and - being orientated into a gas burner output • a swirler, the primary head being provided with the swirler; • radial stabilization nozzles around the circumference of the primary head provided in front of the swirler in the direction of the gas burner output; • a reduction piece - arranged on the tube portion leading from the gas distributor to the primary head, and - provided with a passing-through opening which is smaller than an opening in the tube portion; and - arranged on the tube portion leading from the gas distributor to the primary head, and - provided with a passing-through opening which is smaller than an opening in the tube portion; and • wherein the primary head is arranged on the reduction piece.