mhurhangee/ep-ind-claims huggingface dataset:
A gymnastic accessory for performing gymnastic exercises, the gymnastic accessory including at least a twisting ring, the twisting ring including a first ring, typically an external ring, and a second ring, typically an internal ring, wherein the two rings are concentrically connected and rotatable in relation to each other about a common axis; wherein the first ring further includes at least two connecting means, the connection means preferably arranged symmetrically at the outer periphery of the first ring and adapted for joining with an unyielding or elastic rope, the second ring also including connecting means at the interior of the second ring, wherein these connecting means are adapted for direct or indirect mounting of connecting elements to a twisting belt; the twisting ring further including a number of the connecting elements in the form of straps, preferably four or more straps, wherein one or more and preferably all the straps are arranged with joining means for joining with complementary joining means either on the strap itself, on the second ring or on a twisting belt; wherein the straps and/or the joining means further include adjusting means for adjusting the length of the straps and thereby the spacing between the twisting belt and the second ring in the twisting ring, characterised in that the second ring includes a cutout - a groove - along the interior of the second ring, the cutout including an opening adapted for receiving one or more connecting elements, wherein the opening has a dimension which is narrower than the cutout itself.
System for detecting a crossing, by a vehicle, of an effect line of a red light on a set of traffic lights, on a road comprising at least four lanes, the system comprising at least two pieces of equipment situated on either side of the road, - each piece of equipment processing, as a maximum, n lanes and comprising a pair of presence zones equipping each lane, for between one and n lanes of the road; an image sensor, of which a field of vision is capable of viewing at least the between one and n lanes of the road equipped with at least one pair of presence zones, and thus defining an extremal lane of vision on the road as being the lane farthest away from the sensor among the between one and n lanes of the road; and a processor connected to at least, on the one hand, each pair of presence zones and, on the other hand, the sensor, the processor being capable of detecting the presence of a vehicle passing into a presence zone, said system being characterised in that it comprises an additional presence zone which is: - on the one hand, connected to a first piece of equipment and - on the other hand, situated in the extremal lane of vision of the second piece of equipment, the additional presence zone being upstream of any other presence zone (21, 22) which is found: - on the one hand, connected to said first piece of equipment and - on the other hand, situated in the extremal lane of vision of the first piece of equipment, to neutralise detections of presence of vehicles passing into any one of said other presence zones (21, 22) when said vehicles pass into the additional presence zone before passing into said other presence zone. - each piece of equipment processing, as a maximum, n lanes and comprising - on the one hand, connected to a first piece of equipment and - on the other hand, situated in the extremal lane of vision of the second piece of equipment, - on the one hand, connected to said first piece of equipment and - on the other hand, situated in the extremal lane of vision of the first piece of equipment,
Rubber mixture for the sheathing of one or more reinforcement system(s), characterized in that it comprises at least the following constituents: - at least one diene rubber and - from 0.1 to 3 phr of at least one cobalt compound as a first adhesion promoter and - from 0.1 to 5 phr of at least one other adhesion promoter with the molecular formula M(C n H 2n-x O 2) y, where M is a monovalent sodium cation or divalent magnesium cation or trivalent iron cation and where x is an integer from 0 to 2 and where y is an integer from 1 to 3 and where n is an integer from 10 to 37. - at least one diene rubber and - from 0.1 to 3 phr of at least one cobalt compound as a first adhesion promoter and - from 0.1 to 5 phr of at least one other adhesion promoter with the molecular formula M(C n H 2n-x O 2) y, where M is a monovalent sodium cation or divalent magnesium cation or trivalent iron cation and where x is an integer from 0 to 2 and where y is an integer from 1 to 3 and where n is an integer from 10 to 37.
Unbalanced shaft for the compensation of inertia forces and/or moments of inertia of an internal combustion engine, with an unbalanced portion, the mass center of gravity of which runs eccentrically with respect to the axis of rotation of the unbalanced shaft for generating the shaft unbalance, with a bearing portion adjacent to the unbalanced portion and with a bearing ring which is attached to this and the outer surface area of which serves as a raceway for the rolling bodies of a rolling bearing rotationally supporting the unbalanced shaft and the inner surface area of which, in a bearing circumferential region running in the unbalanced direction, is set back radially with respect to the outer enveloping circle of the unbalanced portion, characterized in that, for the purpose of mounting the bearing ring onto the bearing portion, the following geometric relations are provided: d ⁢ 2 ≥ d ⁢ 1 e > 1⁄2 ⁢ d ⁢ 2 - d ⁢ 1 e < 1⁄2 ⁢ d ⁢ 2 + d ⁢ 1 with d1 = outer enveloping circle diameter of the unbalanced portion and of the bearing portion, d2 = inside diameter of the bearing ring, e = center offset between d2 and d1. d1 = outer enveloping circle diameter of the unbalanced portion and of the bearing portion, d2 = inside diameter of the bearing ring, e = center offset between d2 and d1.
A filter element assembly for filtering diesel fuel, comprising: a vessel defined by a peripheral wall having a cuboid configuration with a first face defining a first opening and an opposing second face defining a second opening, said first opening being sealed by an impermeable barrier and said second opening being covered by a permeable member, wherein said permeable member defines a water diffuser; filter media disposed inside said vessel defining an edge sealably affixed at said peripheral wall thereby bifurcating said vessel into an unfiltered chamber and a filtered chamber whereby fuel passes from said unfiltered chamber to said filtered chamber through said filter media; and a water separator disposed externally to said vessel for separating water from filtered diesel fuel received via said water diffuser, wherein said water separator includes a tubular frame and a water separator medium and an air modulator for modulating an amount of air passing through said water separator, wherein said air modulator comprises a vertical tube extending downwardly into the tubular frame, and said vertical tube defining upper air aperture and a lower air aperture spaced beneath said upper air aperture, wherein the water separator is configured to receive filtered diesel fuel from the vessel through the water separator medium and to guide the filtered diesel fuel to a lower end of the vertical tube of the air modulator, where the filtered diesel fuel flows from the lower end of the vertical tube to an upper end of the vertical tube and exits the filter assembly at the upper end of the vertical tube. a vessel defined by a peripheral wall having a cuboid configuration with a first face defining a first opening and an opposing second face defining a second opening, said first opening being sealed by an impermeable barrier and said second opening being covered by a permeable member, wherein said permeable member defines a water diffuser; filter media disposed inside said vessel defining an edge sealably affixed at said peripheral wall thereby bifurcating said vessel into an unfiltered chamber and a filtered chamber whereby fuel passes from said unfiltered chamber to said filtered chamber through said filter media; and a water separator disposed externally to said vessel for separating water from filtered diesel fuel received via said water diffuser, wherein said water separator includes a tubular frame and a water separator medium and an air modulator for modulating an amount of air passing through said water separator, wherein said air modulator comprises a vertical tube extending downwardly into the tubular frame, and said vertical tube defining upper air aperture and a lower air aperture spaced beneath said upper air aperture, wherein the water separator is configured to receive filtered diesel fuel from the vessel through the water separator medium and to guide the filtered diesel fuel to a lower end of the vertical tube of the air modulator, where the filtered diesel fuel flows from the lower end of the vertical tube to an upper end of the vertical tube and exits the filter assembly at the upper end of the vertical tube.
Coaxial ground heat exchanger having a central core tube and having an expandable cladding tube which delimits an annular gap extending outwards from the core tube, wherein the core tube and the annular gap are formed for a throughflow with a flowable heat carrier medium, characterized in that the cladding tube is formed by a hose-like cladding which is expandable by way of increased inner pressure, said cladding surrounding the core tube in a folded-together state and, following the introduction into the ground heat exchanger bore, being able to be brought into a stable final form by way of a flowable medium, fed with positive pressure, such that, in the installed state of the probe, it directly abuts a wall of a ground heat exchanger bore.
A method for removing space debris having a ballistic coefficient (β) of between 0.02 and 50 Newtons/metre 2, the method comprising hastening orbital decay of the debris by creating a transient gaseous cloud at an altitude of at least 100 km above Earth, the cloud having a density sufficient to slow the debris so the debris falls into Earth's atmosphere, wherein the cloud is created to have a shape of one of a sphere, hemisphere, sector of a sphere limiting to a conical shape and sphere with sector removed, wherein creating the cloud includes performing a Prandtl-Meyer expansion of gas by a nozzle.
An electronic device, comprising: a housing comprising a housing surface; and an antenna device configured to perform communication by receiving a magnetic field transmitted from a transmitter, wherein the antenna device comprises: an antenna coil arranged in a peripheral portion of the housing surface such that windings of the antenna coil are parallel to the housing surface, the antenna coil being configured to be inductively coupled to the transmitter; and a magnetic sheet configured to attract a magnetic field transmitted from the transmitter to the antenna coil, wherein a first region of the antenna coil is located closer to a central portion of the housing surface than a second region of the antenna coil; and the magnetic sheet is arranged between the first region of the antenna coil and the housing surface, but not between the second region of the antenna coil and the housing surface, or the second region of the antenna coil is arranged between the magnetic sheet and the housing surface, but the first region of the antenna coil is not arranged between the magnetic sheet and the housing surface. a housing comprising a housing surface; and an antenna device configured to perform communication by receiving a magnetic field transmitted from a transmitter, wherein the antenna device comprises: an antenna coil arranged in a peripheral portion of the housing surface such that windings of the antenna coil are parallel to the housing surface, the antenna coil being configured to be inductively coupled to the transmitter; and a magnetic sheet configured to attract a magnetic field transmitted from the transmitter to the antenna coil, wherein an antenna coil arranged in a peripheral portion of the housing surface such that windings of the antenna coil are parallel to the housing surface, the antenna coil being configured to be inductively coupled to the transmitter; and a magnetic sheet configured to attract a magnetic field transmitted from the transmitter to the antenna coil, wherein a first region of the antenna coil is located closer to a central portion of the housing surface than a second region of the antenna coil; and the magnetic sheet is arranged between the first region of the antenna coil and the housing surface, but not between the second region of the antenna coil and the housing surface, or the second region of the antenna coil is arranged between the magnetic sheet and the housing surface, but the first region of the antenna coil is not arranged between the magnetic sheet and the housing surface.
A method for cooling a turbine stage of a gas turbine engine comprising: removing gas from a compressor stage using a compressor bleed structure, the compressor stage having a flow path pressure greater than or equal to a minimum pressure threshold during at least one stage of operation, relative to fluid flow through the compressor during the at least one stage of operation; cooling said gas using a heat exchanger housed in an outer diameter structure of the gas turbine engine; providing at least a portion of said cooled gas to an active turbine stage cooling system of a turbine section from said heat exchanger, the turbine section including a high pressure turbine portion and a low pressure turbine portion, the active turbine stage cooling system cooling a second stage of the high pressure turbine portion relative to fluid flow through said high pressure turbine portion, wherein fluid exiting the heat exchanger does not exceed a maximum cooling temperature of the second stage of the turbine; and wherein fluid at said compressor stage has a fluid pressure in excess of the minimum pressure threshold, the minimum pressure threshold being a magnitude of pressure required to prevent backflow of a cooling fluid entering said active cooling system of said at least one turbine stage; and wherein the gas exiting said heat exchanger at said output is greater than or equal to the minimum threshold pressure during the at least one stage of operation and less than or equal to the maximum threshold temperature during the at least one stage of operation. removing gas from a compressor stage using a compressor bleed structure, the compressor stage having a flow path pressure greater than or equal to a minimum pressure threshold during at least one stage of operation, relative to fluid flow through the compressor during the at least one stage of operation; cooling said gas using a heat exchanger housed in an outer diameter structure of the gas turbine engine; providing at least a portion of said cooled gas to an active turbine stage cooling system of a turbine section from said heat exchanger, the turbine section including a high pressure turbine portion and a low pressure turbine portion, the active turbine stage cooling system cooling a second stage of the high pressure turbine portion relative to fluid flow through said high pressure turbine portion, wherein fluid exiting the heat exchanger does not exceed a maximum cooling temperature of the second stage of the turbine; and wherein fluid at said compressor stage has a fluid pressure in excess of the minimum pressure threshold, the minimum pressure threshold being a magnitude of pressure required to prevent backflow of a cooling fluid entering said active cooling system of said at least one turbine stage; and wherein the gas exiting said heat exchanger at said output is greater than or equal to the minimum threshold pressure during the at least one stage of operation and less than or equal to the maximum threshold temperature during the at least one stage of operation.
A method for optimizing the mobility robustness of a mobile radio communication network with respect to moving user equipments being supposed to be handed over within the mobile radio communication network from a source cell to a target cell, the method comprising detecting, by a base station based on reporting information from the user equipments, handover problems which have been occurred within a predefined time interval, classifying, by the base station, the detected handover problems into a first category, into a second category and into a third category, determining, by the base station, at least one information being related to at least one of the detected handover problems, wherein the at least one information represents a refinement of at least one of the three categories or wherein the at least one information represents a further category, counting, by the base station, a first number of handover problems which have been classified into the first category, a second number of handover problems which have been classified into the second category and a third number of handover problems which have been classified into the third category, reporting, by the base station, a key performance indicator message (160a, 260) to a central unit of the mobile radio communication network, wherein the key performance indicator message (160a, 260) is indicative for the first number, the second number and the third number and for the determined at least one information, and adapting, by the central unit, based on the reported key performance indicator message (160a, 260), the value of at least one mobility related network configuration parameter of the mobile radio communication network such that the mobility robustness of the mobile radio communication network is optimized, wherein at least some of the handover problems occur with handovers which have been triggered by a two condition based measurement event, wherein a first result of a first individual measurement event is compared with a first threshold and a second result of a second individual measurement event is compared with a second threshold, and the at least one information being related to at least one of the detected handover problems is indicative for one of the two thresholds, which one has to be changed in order to at least reduce the respective handover problem.
A bending frame for extending travel of an actuator for a mechanically actuated proportional valve for fuel supply in an orbital propulsion system, - wherein the bending frame comprises a plurality of bendable longitudinal struts, which are arranged around a longitudinal axis on which the travel of the actuator runs; - wherein the longitudinal struts each extend in a direction of the longitudinal axis, and an application of force enacted by the actuator along the travel on the longitudinal struts causes their bending in a direction perpendicular to the longitudinal axis; - wherein respective cross struts extend out to the longitudinal axis from each of the longitudinal struts, wherein a first end of a respective cross strut is articulated to a respective longitudinal strut, and a second end of the respective cross strut opposite to the first end is provided in order to transmit force to the value in the direction of the longitudinal axis for the purpose of actuation thereof; - wherein the longitudinal struts and the cross struts interact with one another in such a way that the bending of the longitudinal struts causes the second ends of the cross struts to be displaced in the direction of the longitudinal axis, thereby extending the travel for mechanically actuating the valve; characterized in that the longitudinal struts each comprise two substruts (201, 202) which are articulated to one another at a connection point; and that the cross strut extending out from a respective longitudinal strut is articulated with its first end at the respective longitudinal strut to the position of the connection point. - wherein the bending frame comprises a plurality of bendable longitudinal struts, which are arranged around a longitudinal axis on which the travel of the actuator runs; - wherein the longitudinal struts each extend in a direction of the longitudinal axis, and an application of force enacted by the actuator along the travel on the longitudinal struts causes their bending in a direction perpendicular to the longitudinal axis; - wherein respective cross struts extend out to the longitudinal axis from each of the longitudinal struts, wherein a first end of a respective cross strut is articulated to a respective longitudinal strut, and a second end of the respective cross strut opposite to the first end is provided in order to transmit force to the value in the direction of the longitudinal axis for the purpose of actuation thereof; - wherein the longitudinal struts and the cross struts interact with one another in such a way that the bending of the longitudinal struts causes the second ends of the cross struts to be displaced in the direction of the longitudinal axis, thereby extending the travel for mechanically actuating the valve;
Method for cooling a strand portion of a metal strand in a cooling zone of a continuous casting machine by means of a cooling device, comprising in each case a number of switching valves and cooling nozzles, in which - for cooling, the strand portion is conveyed through the cooling zone and - the switching valves are activated by binary pulse width modulated control signals (38-46, 52), whereby coolant flows (q) through the cooling nozzles are alternately allowed to pass or interrupted, whereby, for cooling, a coolant is intermittently applied to the strand portion in the cooling zone, characterized in that - the binary pulse width modulated control signals (38-46, 52) are defined in such a way that at least one of the control signals (38-46, 52) has a phase shift (φ, φ 1, φ 2, Δφ) in relation to another of the control signals (38-46, 52). - for cooling, the strand portion is conveyed through the cooling zone and - the switching valves are activated by binary pulse width modulated control signals (38-46, 52), whereby coolant flows (q) through the cooling nozzles are alternately allowed to pass or interrupted, whereby, for cooling, a coolant is intermittently applied to the strand portion in the cooling zone, - the binary pulse width modulated control signals (38-46, 52) are defined in such a way that at least one of the control signals (38-46, 52) has a phase shift (φ, φ 1, φ 2, Δφ) in relation to another of the control signals (38-46, 52).