mhurhangee/ep-ind-claims huggingface dataset:
Method for providing information and a transmitted file for determining an originating station of the file transmitted in a peer network, wherein the peer network comprises source stations (QS1, QS2, QS3) and a destination station, having the following steps: - providing a file in each case having watermarks (W1, W2, W3) unique to the respective source station (QS1, QS2, QS3), wherein - the watermarks (W1, W2, W3) are provided with a plurality of sub-watermarks, - at least two versions of the files are provided, and - the watermarks of the versions are different; - transmitting parts of the files uniquely provided with watermarks for the respective station from the source stations (QS1, QS2, QS3) to the destination station; - assembling the transmitted parts of the files into the transmitted file; - creating the information by storing the sub-watermarks of the parts of the files transmitted in each case, wherein the destination station for a transmission of the transmitted file can be determined as the originating station on the basis of the information. - providing a file in each case having watermarks (W1, W2, W3) unique to the respective source station (QS1, QS2, QS3), wherein - the watermarks (W1, W2, W3) are provided with a plurality of sub-watermarks, - at least two versions of the files are provided, and - the watermarks of the versions are different; - transmitting parts of the files uniquely provided with watermarks for the respective station from the source stations (QS1, QS2, QS3) to the destination station; - assembling the transmitted parts of the files into the transmitted file; - creating the information by storing the sub-watermarks of the parts of the files transmitted in each case, wherein the destination station for a transmission of the transmitted file can be determined as the originating station on the basis of the information. - the watermarks (W1, W2, W3) are provided with a plurality of sub-watermarks, - at least two versions of the files are provided, and - the watermarks of the versions are different; - transmitting parts of the files uniquely provided with watermarks for the respective station from the source stations (QS1, QS2, QS3) to the destination station; - assembling the transmitted parts of the files into the transmitted file; - creating the information by storing the sub-watermarks of the parts of the files transmitted in each case, wherein the destination station for a transmission of the transmitted file can be determined as the originating station on the basis of the information.
An orthopedic distraction device comprising: an upper paddle for engaging a first bone of a joint; a lower paddle for engaging a second bone of the joint; and a displacement mechanism operable to displace the upper paddle relative to the lower paddle; and a controller operatively in communication with the displacement mechanism,; characterised in that the controller is configured to cause the displacement mechanism to apply varying displacement forces to displace the upper paddle from the lower paddle based on a joint angle of the first and second bones of the joint. an upper paddle for engaging a first bone of a joint; a lower paddle for engaging a second bone of the joint; and a displacement mechanism operable to displace the upper paddle relative to the lower paddle; and a controller operatively in communication with the displacement mechanism,; characterised in that the controller is configured to cause the displacement mechanism to apply varying displacement forces to displace the upper paddle from the lower paddle based on a joint angle of the first and second bones of the joint.
A method for processing a surface of an embossing tool, having the steps: - applying a first mask to the surface by means of a digital printing technique, - chemically processing the surface provided with the mask to achieve a surface structure, - applying a second, precisely fitting mask to the chemically processed surface by means of a digital printing technique, - chemically processing the surface provided with the second mask, - polishing the chemically processed surface, - activating the polished surface, - cleaning the activated surface, - chrome-plating the cleaned surface, - applying a third, precisely fitting mask to the chrome-plated surface, - metal-coating or mechanically or chemically post-treating the chrome-plated surface provided with the mask, wherein the last two steps are repeated at least once for partial regions to achieve different degrees of gloss on the structured surface. - applying a first mask to the surface by means of a digital printing technique, - chemically processing the surface provided with the mask to achieve a surface structure, - applying a second, precisely fitting mask to the chemically processed surface by means of a digital printing technique, - chemically processing the surface provided with the second mask, - polishing the chemically processed surface, - activating the polished surface, - cleaning the activated surface, - chrome-plating the cleaned surface, - applying a third, precisely fitting mask to the chrome-plated surface, - metal-coating or mechanically or chemically post-treating the chrome-plated surface provided with the mask,
A device for disinfecting an interior space comprising • a cart, which is configured to travel along a path through the interior space, and • a germicidal light source, characterized by • a drone, which has at least one electric drive for generating lift, wherein • the germicidal light source is fastened to the drone and • the drone is connected to the cart via an electrical line for supplying energy to the germicidal light source and the electric drive. • a cart, which is configured to travel along a path through the interior space, and • a germicidal light source, characterized by • a drone, which has at least one electric drive for generating lift, wherein • the germicidal light source is fastened to the drone and • the drone is connected to the cart via an electrical line for supplying energy to the germicidal light source and the electric drive.
A method for transmitting a pilot signal, the method comprising: determining, by a network side device, at least one Channel State Information, CSI, feedback configuration to be transmitted to a user equipment, wherein one CSI feedback configuration corresponds to one Channel State Information-Reference Signal, CSI-RS, resource, and for each port of one CSI-RS resource, a pilot signal corresponding to the port is transmitted over one group of antenna elements corresponding to the port; and transmitting, by the network side device, the determined CSI feedback configuration to the user equipment to instruct the user equipment to receive a pilot signal over the CSI-RS resource corresponding to the CSI feedback configuration and to make signal measurement according to the received pilot signal; wherein after transmitting, by the network side device, the determined CSI feedback configuration to the user equipment, the method further comprises: selecting, by the network side device, at least one of the at least one CSI feedback configuration transmitted to the user equipment according to a measurement parameter fed back by the user equipment; and determining, by the network side device, a parameter of data transmission for the user equipment according to CSI reported by the user equipment for the selected CSI feedback configuration. determining, by a network side device, at least one Channel State Information, CSI, feedback configuration to be transmitted to a user equipment, wherein one CSI feedback configuration corresponds to one Channel State Information-Reference Signal, CSI-RS, resource, and for each port of one CSI-RS resource, a pilot signal corresponding to the port is transmitted over one group of antenna elements corresponding to the port; and transmitting, by the network side device, the determined CSI feedback configuration to the user equipment to instruct the user equipment to receive a pilot signal over the CSI-RS resource corresponding to the CSI feedback configuration and to make signal measurement according to the received pilot signal; wherein after transmitting, by the network side device, the determined CSI feedback configuration to the user equipment, the method further comprises: selecting, by the network side device, at least one of the at least one CSI feedback configuration transmitted to the user equipment according to a measurement parameter fed back by the user equipment; and determining, by the network side device, a parameter of data transmission for the user equipment according to CSI reported by the user equipment for the selected CSI feedback configuration. selecting, by the network side device, at least one of the at least one CSI feedback configuration transmitted to the user equipment according to a measurement parameter fed back by the user equipment; and determining, by the network side device, a parameter of data transmission for the user equipment according to CSI reported by the user equipment for the selected CSI feedback configuration.
A reverse power supply unit (20, 210) for supplying electrical power from a customer premises device (20,40) to an access node via a twisted copper pair, the reverse power supply unit including a rate of increase of current detector operable to detect if the current drawn from the reverse power supply unit over the twisted copper pair increases at a rate which exceeds a predetermined threshold which corresponds to a signature power consumption pattern indicative of a telephony device being in or transitioning into an off-hook state when connected directly to the reverse power supply unit and not being connected via a current limiting interface, and a current limiter for limiting the amount of current supplied by the reverse current supply unit in the event that the rate of change of current detector detects an increase in current at a rate which exceeds the predetermined threshold amount.
Wiring harness for a motor vehicle, - having at least one cable bundle comprising at least two cables, and a sheath, - wherein at least some section or some sections of the cable bundle is/are embedded in the sheath, - wherein the sheath has an indicating element on the outside, - wherein the indicating element is routed parallel to the cable bundle in order to indicate a position of the cable bundle, - wherein the indicating element extends substantially over the entire longitudinal extent of the sheath, characterized - in that the indicating element has a first protuberance, wherein the first protuberance is of bead-type configuration, - or - in that the indicating element has a depression on the outside of the sheath. - having at least one cable bundle comprising at least two cables, and a sheath, - wherein at least some section or some sections of the cable bundle is/are embedded in the sheath, - wherein the sheath has an indicating element on the outside, - wherein the indicating element is routed parallel to the cable bundle in order to indicate a position of the cable bundle, - wherein the indicating element extends substantially over the entire longitudinal extent of the sheath, characterized - in that the indicating element has a first protuberance, wherein the first protuberance is of bead-type configuration, - or - in that the indicating element has a depression on the outside of the sheath.
A nuclear reactor including a pressure vessel housing a core of fissile material and an upper core plate substantially covering the core, a control rod guide tube having an extended axial length, for guiding a control rod assembly comprising a plurality of individual control rods, into and out of the core, the control rod guide tube extending between the upper core plate and an upper support plate supported above the upper core plate, the control rod guide tube comprising: a lower guide tube section connected at a first end to the upper core plate and terminating at a second end at an intermediate coupling; an upper guide tube section connected at a first end portion to the upper support plate and terminating at a second end at the intermediate coupling; a plurality of control rod guide cards supported in spaced relationship to each other along the length of the lower guide tube section and the upper guide tube section, the plurality of control rod guide cards are configured to align the plurality of individual control rods; and an extended control rod guide assembly supported at the intermediate coupling and having a peripheral radially extending flange (96, 98) extending into a recess of the intermediate coupling, characterized in that the extended control rod guide assembly extends from the peripheral radially extending flange (96, 98) axially a finite distance into at least one of an interior of the lower guide tube section or the upper guide tube section, the extended control rod guide assembly being arranged for providing continuous support over the length of the extended control rod guide assembly for at least some of the plurality of the control rods. a lower guide tube section connected at a first end to the upper core plate and terminating at a second end at an intermediate coupling; an upper guide tube section connected at a first end portion to the upper support plate and terminating at a second end at the intermediate coupling; a plurality of control rod guide cards supported in spaced relationship to each other along the length of the lower guide tube section and the upper guide tube section, the plurality of control rod guide cards are configured to align the plurality of individual control rods; and an extended control rod guide assembly supported at the intermediate coupling and having a peripheral radially extending flange (96, 98) extending into a recess of the intermediate coupling, characterized in that the extended control rod guide assembly extends from the peripheral radially extending flange (96, 98) axially a finite distance into at least one of an interior of the lower guide tube section or the upper guide tube section, the extended control rod guide assembly being arranged for providing continuous support over the length of the extended control rod guide assembly for at least some of the plurality of the control rods.
A catheter anchoring device for securing a percutaneous medical catheter inserted at a skin puncture site to a skin of a body, the catheter anchoring device comprising: a catheter capture portion configured to engage with a portion of the catheter protruding from the skin when the catheter is subcutaneously placed in a body; and a skin attachment portion coupled to the catheter capture portion, the skin attachment portion configured to adhesively attach the anchoring device to the skin, wherein the skin attachment portion is primarily attached to the skin overlaying and lateral to the subcutaneously located catheter, wherein the skin attachment portion comprises an adhesive surface configured to adhesively attach the anchoring device to the skin, characterized in that more than 50% of the adhesive surface of the skin attachment portion is configured to be attached to the skin overlaying and lateral to the subcutaneous catheter from a vein puncture site to a portion of the vein adjacent to the tip of the subcutaneously located catheter. a catheter capture portion configured to engage with a portion of the catheter protruding from the skin when the catheter is subcutaneously placed in a body; and a skin attachment portion coupled to the catheter capture portion, the skin attachment portion configured to adhesively attach the anchoring device to the skin, wherein the skin attachment portion is primarily attached to the skin overlaying and lateral to the subcutaneously located catheter, wherein the skin attachment portion comprises an adhesive surface configured to adhesively attach the anchoring device to the skin, characterized in that more than 50% of the adhesive surface of the skin attachment portion is configured to be attached to the skin overlaying and lateral to the subcutaneous catheter from a vein puncture site to a portion of the vein adjacent to the tip of the subcutaneously located catheter.
A sintered alloy represented by a composition consisting of, in percentage by mass, Cr: 10.37 to 39.73, Ni: 5.10 to 24.89, Si: 0.14 to 2.52, Cu: 1.0 to 10.0, P: 0.1 to 1.5, C: 0.18 to 3.2, at least one element selected from the group consisting of Mo, V, W, Nb and Ti: 0 to 5, and the balance of Fe plus unavoidable impurities, the sintered alloy consisting of: a phase A including a Cr concentration of 25 to 45 mass%, a Si concentration of 1.0 to 3.0 mass%, and a precipitated metallic carbide having an average particle diameter DA of 10 to 50 μm; and a phase B including a Cr concentration of 12 to 25 mass%, a Si concentration of 1.0 mass% or less, and a precipitated metallic carbide having an average particle diameter DB of 10 μm or less, wherein the average particle diameter is obtained as mentioned in the description and refers to respective circular shaped particles, wherein the Cr concentration of the phase B is lower than that of the phase A, wherein the Si concentration of the phase B is lower than that of the phase A, wherein each of the phase A and the phase B has an austenitic structure, wherein a maximum dimension of the phase A is within a range of 100 μm or more and 500 μm or less, wherein the phase A occupies 20 to 80% of a total area of the phase A and the phase B, wherein the phase A is dispersed in the phase B and the average particle diameter DA is larger than the average particle diameter DB, and wherein a density ratio of the sintered alloy is 90% or more. a phase A including a Cr concentration of 25 to 45 mass%, a Si concentration of 1.0 to 3.0 mass%, and a precipitated metallic carbide having an average particle diameter DA of 10 to 50 μm; and a phase B including a Cr concentration of 12 to 25 mass%, a Si concentration of 1.0 mass% or less, and a precipitated metallic carbide having an average particle diameter DB of 10 μm or less, wherein the average particle diameter is obtained as mentioned in the description and refers to respective circular shaped particles, wherein the Cr concentration of the phase B is lower than that of the phase A, wherein the Si concentration of the phase B is lower than that of the phase A, wherein each of the phase A and the phase B has an austenitic structure, wherein a maximum dimension of the phase A is within a range of 100 μm or more and 500 μm or less, wherein the phase A occupies 20 to 80% of a total area of the phase A and the phase B, wherein the phase A is dispersed in the phase B and the average particle diameter DA is larger than the average particle diameter DB, and wherein a density ratio of the sintered alloy is 90% or more.
Structure and equipment system for installation in an aircraft, comprising: a plurality of vertical supports, a rail device, at least one connector, a plurality of guiding elements, a plurality of pivot joints, and a plurality of locking devices, wherein the rail device can be attached to a structure of the aircraft and is designed to guide the guiding elements along an axis of extension of the rail device and, in so doing, move them relative to the structure, wherein by means of the at least one connector, the vertical supports are arranged parallel to and at a distance from one another and are connected to form a grid arrangement, wherein the guiding elements are arranged on the grid arrangement, wherein the pivot joints are attached to upper ends of the vertical supports and are designed to pivot the vertical supports about the upper end thereof, wherein the locking devices each have a first locking element which is arranged at a lower end of a vertical support and can be locked in a second locking element which can be positioned on the structure, and wherein the grid arrangement can be inserted into the structure of the aircraft as far as an installation position by means of the guiding elements on the rail device with vertical supports pivoted upwards from the vertical, by pivoting down into a vertical orientation, the first locking elements can interlock with correspondingly arranged second locking elements so that a load-bearing support structure can be formed thereby. a plurality of vertical supports, a rail device, at least one connector, a plurality of guiding elements, a plurality of pivot joints, and a plurality of locking devices, wherein the rail device can be attached to a structure of the aircraft and is designed to guide the guiding elements along an axis of extension of the rail device and, in so doing, move them relative to the structure, wherein by means of the at least one connector, the vertical supports are arranged parallel to and at a distance from one another and are connected to form a grid arrangement, wherein the guiding elements are arranged on the grid arrangement, wherein the pivot joints are attached to upper ends of the vertical supports and are designed to pivot the vertical supports about the upper end thereof, wherein the locking devices each have a first locking element which is arranged at a lower end of a vertical support and can be locked in a second locking element which can be positioned on the structure, and wherein the grid arrangement can be inserted into the structure of the aircraft as far as an installation position by means of the guiding elements on the rail device with vertical supports pivoted upwards from the vertical, by pivoting down into a vertical orientation, the first locking elements can interlock with correspondingly arranged second locking elements so that a load-bearing support structure can be formed thereby.
A high-thermal-sensitivity ablation catheter tip comprising an electrically-conductive housing having a conductive shell with a domed distal end and a cylindrical body joined to a proximal end of the domed distal end, a plurality of thermal sensors in thermal communication with an inner surface of the cylindrical body of the conductive shell, the plurality of thermal sensors arranged in two circumferential rings within the cylindrical body of the conductive shell, wherein the first circumferential ring is longitudinally offset relative to the second circumferential ring, a flexible electronic circuit (290; 330; 340; 350) distributed around the inner surface of the cylindrical body of the conductive shell, the plurality of thermal sensors positioned on and coupled to the flexible electronic circuit (290; 330; 340; 350), and a wired or wireless communication pathway at least partially disposed on the flexible electronic circuit (290; 330; 340; 350) communicatively connected to the plurality of thermal sensors. an electrically-conductive housing having a conductive shell with a domed distal end and a cylindrical body joined to a proximal end of the domed distal end, a plurality of thermal sensors in thermal communication with an inner surface of the cylindrical body of the conductive shell, the plurality of thermal sensors arranged in two circumferential rings within the cylindrical body of the conductive shell, wherein the first circumferential ring is longitudinally offset relative to the second circumferential ring, a flexible electronic circuit (290; 330; 340; 350) distributed around the inner surface of the cylindrical body of the conductive shell, the plurality of thermal sensors positioned on and coupled to the flexible electronic circuit (290; 330; 340; 350), and a wired or wireless communication pathway at least partially disposed on the flexible electronic circuit (290; 330; 340; 350) communicatively connected to the plurality of thermal sensors.