mhurhangee/patent-ind-claim-en huggingface dataset:
A data center system , comprising at least the following components: a data center , a power source module , and an energy conversion module , wherein - the data center is connected to at least two prime-rated electricity sources configured to provide electricity to the data center , wherein a first electricity source is an electricity grid and wherein a second electricity source is the power source module , wherein - the power source module comprises a gas-powered electricity generator (12, 12-1, 12-2) to generate electricity from gas, wherein the power source module is connected to a gas network , wherein the power source module is further connected to the data center , wherein - the energy conversion module is connected to a regenerative energy source configured to produce electricity, as well as to the gas network , wherein the energy conversion module is configured to generate gas, comprising or consisting of hydrogen and/or methane using electricity from the regenerative energy source , wherein the energy conversion module is configured to feed the generated gas into the gas network , wherein the system is configured to provide electricity from the power source module to the data center , such as to reduce a load on the electricity grid and such that the data center is supplied by the at least two prime-rated electricity sources simultaneously, wherein the system is configured to provide electricity from the power source module via the data center synchronously to the electricity provided by the electricity grid , wherein the electricity grid is connected to a common conducting element that is further connected to a bi-directional converter or a rectifier of the data center , characterized in that the power source module comprises a reciprocating gas engine (12-1) configured to burn gas provided to the power source module to generate AC-electricity, wherein the power source module is connected to the common conducting element enabling grid stabilization with the synchronized electricity sources at the data center . - the data center is connected to at least two prime-rated electricity sources configured to provide electricity to the data center , wherein a first electricity source is an electricity grid and wherein a second electricity source is the power source module , wherein - the power source module comprises a gas-powered electricity generator (12, 12-1, 12-2) to generate electricity from gas, wherein the power source module is connected to a gas network , wherein the power source module is further connected to the data center , wherein - the energy conversion module is connected to a regenerative energy source configured to produce electricity, as well as to the gas network , wherein the energy conversion module is configured to generate gas, comprising or consisting of hydrogen and/or methane using electricity from the regenerative energy source , wherein the energy conversion module is configured to feed the generated gas into the gas network , wherein
A method for discriminating a microorganism, the method comprising: a) a step of subjecting a sample containing a microorganism to mass spectrometry to obtain a mass spectrum; b) a reading step of reading a mass-to-charge ratio m/z of a peak derived from a marker protein from the mass spectrum; and c) a discrimination step of discriminating which bacterial species of Escherichia coli, Shigella bacteria, and Escherichia albertii the microorganism contained in the sample contains based on the mass-to-charge ratio m/z, wherein at least one of three ribosomal proteins S5, L31, and L13, is used as the marker protein. a) a step of subjecting a sample containing a microorganism to mass spectrometry to obtain a mass spectrum; b) a reading step of reading a mass-to-charge ratio m/z of a peak derived from a marker protein from the mass spectrum; and c) a discrimination step of discriminating which bacterial species of Escherichia coli, Shigella bacteria, and Escherichia albertii the microorganism contained in the sample contains based on the mass-to-charge ratio m/z,
A control information configuration method, performed by a first serving cell, wherein the first serving cell is scheduled by a second serving cell, and characterized in that the method comprises: sending first control information to a terminal, wherein the first control information is determined according to at least one of following: second control information sent by the second serving cell to the terminal; a configuration from a base station to the terminal; a characteristic of the terminal; and a capability supported by the terminal, wherein the first control information is used to schedule, on the first serving cell, transmission or resources of the first serving cell, and the second control information is used to schedule, on the second serving cell, transmission or resources of the first serving cell; wherein the first control information comprises first downlink control information, DCI, the second control information comprises second DCI; the first DCI comprises a carrier indicator field, CIF, and the second DCI comprises a CIF, wherein a number of bits of the CIF comprised in the first DCI is the same as a number of bits of the CIF comprised in the second DCI. second control information sent by the second serving cell to the terminal; a configuration from a base station to the terminal; a characteristic of the terminal; and a capability supported by the terminal, wherein the first control information is used to schedule, on the first serving cell, transmission or resources of the first serving cell, and the second control information is used to schedule, on the second serving cell, transmission or resources of the first serving cell; wherein the first control information comprises first downlink control information, DCI, the second control information comprises second DCI; the first DCI comprises a carrier indicator field, CIF, and the second DCI comprises a CIF, wherein a number of bits of the CIF comprised in the first DCI is the same as a number of bits of the CIF comprised in the second DCI.
An agent delivery device, comprising: two or more agent containers at a proximal end of the agent delivery device, wherein the two or more agent containers are configured to contain two or more fluids; an insertion section connected to the proximal end of the one or more agent containers, the insertion section comprising a tube defining two or more lumens , and the insertion section being coupled to the agent containers such that the two or more fluids may flow from the agent containers to the two or more lumens and out of two or more outlets of the two or more lumens; and a distal impingement structure at the distal end of the insertion section, the distal impingement structure comprising an impingement surface arranged relative to two or more outlets to impinge the two or more fluids dispensed from the two or more outlets to cause mixing of the two or more fluids for application of the fluids at a treatment site . two or more agent containers at a proximal end of the agent delivery device, wherein the two or more agent containers are configured to contain two or more fluids; an insertion section connected to the proximal end of the one or more agent containers, the insertion section comprising a tube defining two or more lumens , and the insertion section being coupled to the agent containers such that the two or more fluids may flow from the agent containers to the two or more lumens and out of two or more outlets of the two or more lumens; and a distal impingement structure at the distal end of the insertion section, the distal impingement structure comprising an impingement surface arranged relative to two or more outlets to impinge the two or more fluids dispensed from the two or more outlets to cause mixing of the two or more fluids for application of the fluids at a treatment site .
A method for multi-spindled production of linearly and/or circularly arranged machining patterns with a CNC machine tool, the CNC machine tool comprising a machining head which is connected to a Z-axis such that it is manually and/or automatically changeable and includes at least two tool spindles (3a-3d) for receiving tools (4a-4d), wherein said Z-axis is displaceable at least along two linear axial directions, and said Z-axis and/or the machining head have at least one rotational axis, and wherein the CNC machine tool is configured such that machining patterns are processable in that the machining head is movable to a position of the machining pattern by linearly displacing said Z axis along at least one of the linear axial directions, and the tools (4a-4d) of the machining head can be aligned with a contour of the machining pattern by rotating the machining head and/or the Z axis ; said method being characterized by the steps of: - moving to a position on the machining pattern with the machining head by linearly displacing said Z axis along one or more linear axial directions, - arranging the tools (4a-4d) of the machining head along a contour line of the machining pattern by rotating the machining head and/or the Z axis , - adjusting the distance between the tool spindles (3a-3d) prior to processing the machining pattern and/or prior to each drilling operation. - moving to a position on the machining pattern with the machining head by linearly displacing said Z axis along one or more linear axial directions, - arranging the tools (4a-4d) of the machining head along a contour line of the machining pattern by rotating the machining head and/or the Z axis , - adjusting the distance between the tool spindles (3a-3d) prior to processing the machining pattern and/or prior to each drilling operation.
Tandem effector with a precursor charge and with a main effector , - wherein the precursor charge extends along a longitudinal axis and is fitted as intended in front of the main effector of the tandem effector in a flight direction thereof that is coincident with the longitudinal axis , wherein the precursor charge has: - a casing , - an explosive arranged in the casing , characterized in that the precursor charge has: - a projectile means which is fitted on the casing and is configured to respond to the explosive being set off by sending out an armour-piercing projectile which precedes the main effector in the flight direction , - a fragmenting means which is fitted on the casing and is configured to respond to the explosive being set off by sending out a focussed burst of fire which precedes the main effector in the flight direction and is composed of a multiplicity of fragments , wherein the burst of fire is focussed by a radial velocity (VR) of the fragments being at most a fifth of the axial velocity (VA) thereof. - wherein the precursor charge extends along a longitudinal axis and is fitted as intended in front of the main effector of the tandem effector in a flight direction thereof that is coincident with the longitudinal axis , - a casing , - an explosive arranged in the casing , - a projectile means which is fitted on the casing and is configured to respond to the explosive being set off by sending out an armour-piercing projectile which precedes the main effector in the flight direction , - a fragmenting means which is fitted on the casing and is configured to respond to the explosive being set off by sending out a focussed burst of fire which precedes the main effector in the flight direction and is composed of a multiplicity of fragments , wherein the burst of fire is focussed by a radial velocity (VR) of the fragments being at most a fifth of the axial velocity (VA) thereof.
A computer program comprising instructions which, when the program is executed by a computer of a dart game device including at least two cameras each positioned in predetermined different directions, cause the computer program to provide a dart pin hit location identification by carrying out the steps of: obtaining at least two dart target photographing images in response to a dart pin throw, wherein the dart target photographing image includes an image of a dart target and at least one dart pin hitting the dart target, and the at least two dart target photographing images are generated by the at least two cameras ; generating, by a dart pin location identification neural network model , hit location information of the at least one dart pin based on the at least two dart target photographing images, wherein said step of generating the hit location information of the at least one dart pin includes: generating input data that is a single image by performing a merging operation on the at least two dart target photographing images; and generating the hit location information of the at least one dart pin by processing the input data by the dart pin location identification neural network model . obtaining at least two dart target photographing images in response to a dart pin throw, wherein the dart target photographing image includes an image of a dart target and at least one dart pin hitting the dart target, and the at least two dart target photographing images are generated by the at least two cameras ; generating, by a dart pin location identification neural network model , hit location information of the at least one dart pin based on the at least two dart target photographing images, wherein said step of generating the hit location information of the at least one dart pin includes: generating input data that is a single image by performing a merging operation on the at least two dart target photographing images; and generating the hit location information of the at least one dart pin by processing the input data by the dart pin location identification neural network model . generating input data that is a single image by performing a merging operation on the at least two dart target photographing images; and generating the hit location information of the at least one dart pin by processing the input data by the dart pin location identification neural network model .
A harvester head for forestry applications comprising: at least one hydraulic actuator with a cylinder and a piston , the hydraulic actuator having at least a cylinder chamber and a piston rod chamber , both chambers being connected to a hydraulic circuit, an additional hydraulic connection being parallel to the hydraulic actuator and to both chambers wherein the piston is separating the cylinder chamber and the piston rod chamber , characterized in that the additional hydraulic connection having a cavity provided in the piston , hydraulically connecting the cylinder chamber with the piston rod chamber , and a check valve in connection with the cavity , allowing hydraulic medium flow in an opening direction of the check valve , so that hydraulic medium can flow through the cavity and the check valve . at least one hydraulic actuator with a cylinder and a piston , the hydraulic actuator having at least a cylinder chamber and a piston rod chamber , both chambers being connected to a hydraulic circuit, an additional hydraulic connection being parallel to the hydraulic actuator and to both chambers wherein the piston is separating the cylinder chamber and the piston rod chamber , characterized in that the additional hydraulic connection having a cavity provided in the piston , hydraulically connecting the cylinder chamber with the piston rod chamber , and a check valve in connection with the cavity , allowing hydraulic medium flow in an opening direction of the check valve , so that hydraulic medium can flow through the cavity and the check valve .
A pair of sliding components having annular sliding surfaces (S) that slide with respect to each other in which plural dimples are arranged on at least the sliding surface (S) on one side, one circumferential edge of the sliding surface (S) is a sealed fluid side, the other circumferential edge is a leakage side, the plural dimples are randomly arranged to form random dimple groups (11; 11-P, 11-L), and the dimples of a pumping random dimple group (11-P) are arranged in such a manner that a radial-direction coordinate average of centers of the dimples of the pumping random dimple group (11-P) is smaller than a sliding radius (Rm) of the sliding surface (S), the pumping random dimple group (11-P) is arranged on the sliding surface (S) on the leakage side, and a lubricating random dimple group (11-L) is arranged on the sliding surface (S) on the sealed fluid side, and a deep groove being isolated from the leakage side and communicating with the sealed fluid side is arranged on the sliding surface (S), and a circumferential deep groove of the deep groove is arranged between the pumping random dimple group (11-P) and the lubricating random dimple group (11-L), characterized in that the dimples of the lubricating random dimple group (11-L) are arranged in such a manner that the angular-direction standard deviation of the dimples of the random dimple group (11; 11-P, 11-L) is less than one. the pumping random dimple group (11-P) is arranged on the sliding surface (S) on the leakage side, and a lubricating random dimple group (11-L) is arranged on the sliding surface (S) on the sealed fluid side, and a deep groove being isolated from the leakage side and communicating with the sealed fluid side is arranged on the sliding surface (S), and a circumferential deep groove of the deep groove is arranged between the pumping random dimple group (11-P) and the lubricating random dimple group (11-L), characterized in that the dimples of the lubricating random dimple group (11-L) are arranged in such a manner that the angular-direction standard deviation of the dimples of the random dimple group (11; 11-P, 11-L) is less than one.
A metallic and composite material joint comprising: a composite member comprising a cylinder having a flared end extending along a centerline axis , an outer surface of the flared end oriented at a first angle relative to the centerline axis; a metallic member perimetrically surrounding the outer surface of the flared end and having an inner surface oriented at a second angle relative to the centerline axis, wherein, before assembly, the inner surface of the metallic member and the outer surface of the composite member are separated by a first gap at a first location and are separated by a second gap at a second location , the first gap being greater than the second gap, the first location being axially spaced from the second location, and the first gap and the second gap being measured in a direction substantially orthogonal to the centerline axis. a composite member comprising a cylinder having a flared end extending along a centerline axis , an outer surface of the flared end oriented at a first angle relative to the centerline axis; a metallic member perimetrically surrounding the outer surface of the flared end and having an inner surface oriented at a second angle relative to the centerline axis, wherein, before assembly, the inner surface of the metallic member and the outer surface of the composite member are separated by a first gap at a first location and are separated by a second gap at a second location , the first gap being greater than the second gap, the first location being axially spaced from the second location, and the first gap and the second gap being measured in a direction substantially orthogonal to the centerline axis.
A display apparatus including a light-emitting device , the light-emitting device comprising a substrate on which a light source is provided, wherein the light source is configured to emit first-wavelength light other than white light, and the light source includes a light-emitting point (LP); a wavelength conversion sheet configured to perform wavelength conversion of the first-wavelength light into a second-wavelength light different from the first wavelength; and a reflective member comprising a resin, wherein the reflective member is placed on the substrate and includes an opening into which the light source is inserted, a sloped section having a first thickness (T1), and the first thickness (T1) is a dimension of the sloped section in a direction orthogonal to a sloped surface , a bottom surface section coupled to a bottom end of the sloped section , wherein the bottom surface section has a second thickness (T3), the first thickness (T1) is greater than the second thickness (T3), the light source has a first distance (L3) from the substrate to the light-emitting point (LP) of the light source, and the second thickness (T3) is smaller than the first distance (L3). a substrate on which a light source is provided, wherein the light source is configured to emit first-wavelength light other than white light, and the light source includes a light-emitting point (LP); the light source is configured to emit first-wavelength light other than white light, and the light source includes a light-emitting point (LP); a wavelength conversion sheet configured to perform wavelength conversion of the first-wavelength light into a second-wavelength light different from the first wavelength; and a reflective member comprising a resin, wherein the reflective member is placed on the substrate and includes an opening into which the light source is inserted, a sloped section having a first thickness (T1), and the first thickness (T1) is a dimension of the sloped section in a direction orthogonal to a sloped surface , a bottom surface section coupled to a bottom end of the sloped section , wherein the bottom surface section has a second thickness (T3), the first thickness (T1) is greater than the second thickness (T3), an opening into which the light source is inserted, a sloped section having a first thickness (T1), and the first thickness (T1) is a dimension of the sloped section in a direction orthogonal to a sloped surface , a bottom surface section coupled to a bottom end of the sloped section , wherein the bottom surface section has a second thickness (T3), the first thickness (T1) is greater than the second thickness (T3), the light source has a first distance (L3) from the substrate to the light-emitting point (LP) of the light source, and the second thickness (T3) is smaller than the first distance (L3).
A method for operating a gas engine with a lean gas, wherein the lean gas is mixed with an air inflow in at least one Venturi mixer so as to form a mixture, and wherein the mixture is fed to the gas engine as fuel, characterized in that the lean gas contains less than 20% by volume of methane and in that the mixture is preheated to a temperature (θ 1 ) between 120°C and 150°C before entering the gas engine .