mhurhangee/ep-ind-claims huggingface dataset:
A rotorcraft, comprising: a body; a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source; a hub coupled to the drive shaft; a rotor blade coupled to the hub; a swashplate positioned about the drive shaft; and a pitch link (118, 830a-830d) coupled between the swashplate and the hub corresponding to the rotor blade, the pitch link comprising: a housing comprising a first chamber and a second chamber, wherein a first housing opening allows a first fluid to flow into the first chamber and a second housing opening allows a second fluid to flow into the second chamber; and a piston assembly at least partially disposed within the housing and comprising a piston head and a piston rod coupled to the piston head, the piston head separating the first chamber from the second chamber, wherein the pitch link (118, 830a-830d) is coupled between the swashplate and the hub such that movement of the piston rod changes a distance between the swashplate and the hub; characterized in that the rotorcraft further comprises at least one fluid pump operable to provide the first fluid to the first chamber and the second fluid to the second chamber. a body; a power train coupled to the body and comprising a power source and a drive shaft coupled to the power source; a hub coupled to the drive shaft; a rotor blade coupled to the hub; a swashplate positioned about the drive shaft; and a pitch link (118, 830a-830d) coupled between the swashplate and the hub corresponding to the rotor blade, the pitch link comprising: a housing comprising a first chamber and a second chamber, wherein a first housing opening allows a first fluid to flow into the first chamber and a second housing opening allows a second fluid to flow into the second chamber; and a piston assembly at least partially disposed within the housing and comprising a piston head and a piston rod coupled to the piston head, the piston head separating the first chamber from the second chamber, wherein the pitch link (118, 830a-830d) is coupled between the swashplate and the hub such that movement of the piston rod changes a distance between the swashplate and the hub; characterized in that the rotorcraft further comprises at least one fluid pump operable to provide the first fluid to the first chamber and the second fluid to the second chamber. a housing comprising a first chamber and a second chamber, wherein a first housing opening allows a first fluid to flow into the first chamber and a second housing opening allows a second fluid to flow into the second chamber; and a piston assembly at least partially disposed within the housing and comprising a piston head and a piston rod coupled to the piston head, the piston head separating the first chamber from the second chamber, at least one fluid pump operable to provide the first fluid to the first chamber and the second fluid to the second chamber.
Thick-matter pump comprising two conveying cylinders (10, 11), two conveying pistons (12, 13) and a hydro drive with a hydro pump for the propulsion of the conveying pistons (12, 13), two drive cylinders (23, 24) and two drive pistons (25, 26), wherein the conveying pistons (12, 13) are guided into the respectively assigned conveying cylinder (10, 11) and are provided to be moved from a first dead point into a second dead point within a conveyor cycle, as well as comprising an configuration unit and a controller and/or regulating unit, which are provided to change at least one feed speed and /or one feed pressure of at least one conveying piston (12, 13) during the conveying cycle, wherein the controller and/or regulating unit is provided to divide the conveying cycle into at least two different sub-sections, for which the feed speed and/or the feed pressure can be individually configured, wherein the thick-matter pump comprises a control unit for entering at least one parameter for at least one sub-section, on which the feed speed and/or the feed pressure in the at least one sub-section at least depends, and a connecting piece hydraulically connects the drive cylinders (23, 24) to one another, characterized in that the connecting piece comprises a plurality of valve recesses, wherein the valve recesses are preferably provided for receiving built-in valves or of gate valve shafts. wherein the controller and/or regulating unit is provided to divide the conveying cycle into at least two different sub-sections, for which the feed speed and/or the feed pressure can be individually configured, wherein the thick-matter pump comprises a control unit for entering at least one parameter for at least one sub-section, on which the feed speed and/or the feed pressure in the at least one sub-section at least depends, and a connecting piece hydraulically connects the drive cylinders (23, 24) to one another, characterized in that the connecting piece comprises a plurality of valve recesses, wherein the valve recesses are preferably provided for receiving built-in valves or of gate valve shafts.
A multi-mode fuze system for use in a warhead for combating a target, said multi-mode fuze system comprise at least one target sensor electrically connected to a signal processing block and an I/O-block, where said I/O-block is possible to set by the operator of the warhead, where said target sensor is adapted to generate an electrical output in response to the rate of deceleration of the warhead and where said multi-mode fuze system is adapted to discriminate the hardness of the target based upon the electrical output of said target sensor and to select the mode of operation depending upon the said target discrimination, characterized in that the multi-mode fuze system is adapted to discriminate at least one type of target depending upon said target sensor's electrical output and that the multi-mode fuze system selects one of at least three modes of operation of the warhead, and wherein all electrical energy needed for operating the multi-mode fuze system is provided by said at least one target sensor.
A device for drying a floor layer of a floor structure, the device comprising: a hollow cylinder which can be inserted into an opening in the floor structure, wherein the hollow cylinder comprising an upper end, which, when the hollow cylinder is inserted in the opening, protrudes from the opening, and a lower end which can be placed in the opening on a floor layer of the floor structure, a conical member for sealing the opening between the floor structure and the hollow cylinder, characterized in that the conical member is slidably arranged on an outer cylinder surface of the hollow cylinder between the upper end and the lower end of the hollow cylinder. a hollow cylinder which can be inserted into an opening in the floor structure, wherein the hollow cylinder comprising an upper end, which, when the hollow cylinder is inserted in the opening, protrudes from the opening, and a lower end which can be placed in the opening on a floor layer of the floor structure, a conical member for sealing the opening between the floor structure and the hollow cylinder, characterized in that the conical member is slidably arranged on an outer cylinder surface of the hollow cylinder between the upper end and the lower end of the hollow cylinder.
A computer-implemented method comprising: processing a plurality of GNSS measurements to determine an auxiliary navigation solution for a vehicle by calculating a single difference by calculating the differences between a GNSS measurement provided by a first measurement source and GNSS measurements provided by other measurement sources; performing innovation sequence monitoring on the auxiliary navigation solution by applying innovation sequence monitoring to the single difference to identify a set of measurements in the plurality of measurements that are faulty or erroneous; and performing a solution separation method comprising: processing the set of measurements to determine a full navigation solution; processing subsets of the set of measurements to determine a set of navigation sub-solutions, wherein any measurements identified as faulty or erroneous are excluded from the calculations of the navigation sub-solutions; using the full solution and the sub-solutions to determine the integrity of the full solution. processing a plurality of GNSS measurements to determine an auxiliary navigation solution for a vehicle by calculating a single difference by calculating the differences between a GNSS measurement provided by a first measurement source and GNSS measurements provided by other measurement sources; performing innovation sequence monitoring on the auxiliary navigation solution by applying innovation sequence monitoring to the single difference to identify a set of measurements in the plurality of measurements that are faulty or erroneous; and performing a solution separation method comprising: processing the set of measurements to determine a full navigation solution; processing subsets of the set of measurements to determine a set of navigation sub-solutions, wherein any measurements identified as faulty or erroneous are excluded from the calculations of the navigation sub-solutions; using the full solution and the sub-solutions to determine the integrity of the full solution. processing the set of measurements to determine a full navigation solution; processing subsets of the set of measurements to determine a set of navigation sub-solutions, wherein any measurements identified as faulty or erroneous are excluded from the calculations of the navigation sub-solutions; using the full solution and the sub-solutions to determine the integrity of the full solution.
A battery module, comprising: - a housing defined by one or more walls, wherein a wall of the housing comprises an opening configured to create a passageway between an interior of the housing and an exterior of the housing; and - a connector barrel disposed within the opening, wherein the connector barrel is a hollow conduit comprising a first open end opposite a second open end, and wherein the connector barrel is configured to receive a low voltage signal connector through the first open end and a vehicle control module connector through the second open end, and wherein an external surface of the connector barrel comprises a pair of protrusions configured to enable intimate contact between the wall of the housing and the connector barrel. - a housing defined by one or more walls, wherein a wall of the housing comprises an opening configured to create a passageway between an interior of the housing and an exterior of the housing; and - a connector barrel disposed within the opening, wherein the connector barrel is a hollow conduit comprising a first open end opposite a second open end, and wherein the connector barrel is configured to receive a low voltage signal connector through the first open end and a vehicle control module connector through the second open end, and wherein an external surface of the connector barrel comprises a pair of protrusions configured to enable intimate contact between the wall of the housing and the connector barrel.
A heat exchanger, in particular an evaporator, having a plurality of refrigerant-carrying pipes which are arranged one next to the other and which end in at least one collecting vessel, and having at least one cold accumulator, consisting of a plurality of cold accumulator elements, in which a cold accumulating medium is provided, wherein the heat exchanger has two first and second regions (1' and 1") which are arranged parallel to one another, and the cold accumulator is arranged in the second region (1"), wherein the refrigerant-carrying pipes (6, 7) of the first and second regions (1', 1") are arranged in line with one another and have a corresponding width (b1, b2, b3), and the first and second region (1' and 1") have common, continuous corrugated fins, characterised in that at least one refrigerant-carrying pipe is arranged in at least one cold accumulator element.
A baler comprising: a pick-up assembly (15, 16, 17) configured to pick up crop material; a compression assembly positioned downstream of the pick-up assembly (15, 16, 17) for receiving the crop material from the pick-up assembly (15, 16, 17), the compression assembly comprising at least one pair of opposing compression rollers (100a, 100b) configured to generate a pressure on the crop material when passing therethrough, the at least one pair of opposing compression rollers (100a, 100b) define an adjustable gap therebetween, such that the crop material is pre-compressed when passing therethrough; and a bale chamber positioned downstream of the compression assembly for forming a bale, characterized in that the baler further comprising at least one hydraulic cylinder to link together the at least one pair of opposing compression rollers (100a, 100b) of the compression assembly. a pick-up assembly (15, 16, 17) configured to pick up crop material; a compression assembly positioned downstream of the pick-up assembly (15, 16, 17) for receiving the crop material from the pick-up assembly (15, 16, 17), the compression assembly comprising at least one pair of opposing compression rollers (100a, 100b) configured to generate a pressure on the crop material when passing therethrough, the at least one pair of opposing compression rollers (100a, 100b) define an adjustable gap therebetween, such that the crop material is pre-compressed when passing therethrough; and a bale chamber positioned downstream of the compression assembly for forming a bale, characterized in that the baler further comprising at least one hydraulic cylinder to link together the at least one pair of opposing compression rollers (100a, 100b) of the compression assembly.
A high speed data contact set comprising: an insert shroud and a termination subassembly, the insert shroud comprising: a hollow body having a top, a bottom, a front, a rear, and first side and a second side; said termination subassembly being located inside the hollow body of the insert shroud; a plurality of protective arms (120a, 120b, 120c, 120d) extending from the front of said hollow body for protecting contact beams (242, 242a, 244, 244a, 246, 246a, 248, 248a) of said termination subassembly inserted into said insert shroud, each said protective arm (120a, 120b, 120c, 120d) having beveled edges at its distal end and an angled shoulder spaced from said distal end of said protective arm (120a, 120b, 120c, 120d), said beveled edges providing a first stage of contact pre-alignment during engagement and said shoulder providing a second stage of contact pre-alignment during engagement; a plurality of raised bosses on said top of said hollow body, as well as corresponding hollows in the bottom of said hollow body; a latch on each of said first and second sides of said hollow body, and wherein the termination subassembly comprises a plurality of pairs of contact beams, the contact beams in each pair being of the same orientation and the pairs of contact beams having alternating orientations, and wherein the protective arms (120a, 120b, 120c, 120d) each cover one side of a pair of contact beams so that, viewed from the top and from the bottom, the pairs of contact beams are exposed and covered alternatively. a hollow body having a top, a bottom, a front, a rear, and first side and a second side; said termination subassembly being located inside the hollow body of the insert shroud; a plurality of protective arms (120a, 120b, 120c, 120d) extending from the front of said hollow body for protecting contact beams (242, 242a, 244, 244a, 246, 246a, 248, 248a) of said termination subassembly inserted into said insert shroud, each said protective arm (120a, 120b, 120c, 120d) having beveled edges at its distal end and an angled shoulder spaced from said distal end of said protective arm (120a, 120b, 120c, 120d), said beveled edges providing a first stage of contact pre-alignment during engagement and said shoulder providing a second stage of contact pre-alignment during engagement; a plurality of raised bosses on said top of said hollow body, as well as corresponding hollows in the bottom of said hollow body; a latch on each of said first and second sides of said hollow body, and wherein the termination subassembly comprises a plurality of pairs of contact beams, the contact beams in each pair being of the same orientation and the pairs of contact beams having alternating orientations, and wherein the protective arms (120a, 120b, 120c, 120d) each cover one side of a pair of contact beams so that, viewed from the top and from the bottom, the pairs of contact beams are exposed and covered alternatively.
A computer-implemented method for locating code image regions in an initial image of a code-bearing object, wherein first candidates for code image regions are determined in a first segmentation method using a method of classical image processing without machine learning, characterized in that second candidates for code image regions are determined in a second segmentation method using machine learning, and in that the first and second candidates are combined to find the code image regions.
A method for determining a connection status of a device to a cable that transmits data within a network environment, the method comprising: obtaining a signal from a power-carrying wire in the cable by a detector that is digitally isolated from data transmitted by the cable within the network environment, wherein the signal is a power signal, wherein the digitally isolated detector is unable to access unfiltered data transmitted by the cable; and evaluating the signal to determine a connection status of the device to the cable, wherein evaluating the signal to determine the connection status of the device comprises: comparing the signal to a pre-determined power characteristic associated to the device; and determining a connection status on the basis of the comparison, wherein the connection status comprises an indication whether the device is connected or not connected to the cable. obtaining a signal from a power-carrying wire in the cable by a detector that is digitally isolated from data transmitted by the cable within the network environment, wherein the signal is a power signal, wherein the digitally isolated detector is unable to access unfiltered data transmitted by the cable; and evaluating the signal to determine a connection status of the device to the cable, wherein evaluating the signal to determine the connection status of the device comprises: comparing the signal to a pre-determined power characteristic associated to the device; and determining a connection status on the basis of the comparison, wherein the connection status comprises an indication whether the device is connected or not connected to the cable. comparing the signal to a pre-determined power characteristic associated to the device; and determining a connection status on the basis of the comparison, wherein the connection status comprises an indication whether the device is connected or not connected to the cable.
Method for the continuous production of hydrocarbons from synthesis gas in the presence of a catalyst comprising a synthesis step in which a synthesis gas is reacted in the presence of a catalyst in a Fischer-Tropsch synthesis reactor, characterised in that, at the same time as the synthesis step and at the actual site of the Fischer-Tropsch synthesis unit, the following successive steps are carried out: a) charging a catalyst precursor comprising cobalt oxide in a dedicated reduction reactor; b) reducing the catalyst precursor charged in step a) by placing it in contact with a reduction gas comprising hydrogen (H 2) or carbon monoxide, the reduction being carried out at a temperature between 200 and 500°C, at a total pressure between 0.1 and 5 MPa and under a gas flow between 0.1 and 20 NI/h/g of catalyst to be processed, during 1 to 24 hours; c) at least one step for conditioning the catalyst reduced in step b), the conditioning operation being carried out by placing the reduced catalyst in contact with a reduction gas which comprises carbon monoxide alone or an admixture of hydrogen and carbon monoxide wherein the molar ratio H 2 /CO is between 0.01 and 10, the conditioning operation being carried out at a temperature between 200 and 500°C, at a total pressure between 0.1 and 5 MPa and under a gas flow between 0.1 and 20 Nl/h/g of catalyst to be processed, during 1 to 48 hours; and d) introducing the catalyst reduced in step c) into the synthesis reactor in semi-continuous mode or in continuous mode. a) charging a catalyst precursor comprising cobalt oxide in a dedicated reduction reactor; b) reducing the catalyst precursor charged in step a) by placing it in contact with a reduction gas comprising hydrogen (H 2) or carbon monoxide, the reduction being carried out at a temperature between 200 and 500°C, at a total pressure between 0.1 and 5 MPa and under a gas flow between 0.1 and 20 NI/h/g of catalyst to be processed, during 1 to 24 hours; c) at least one step for conditioning the catalyst reduced in step b), the conditioning operation being carried out by placing the reduced catalyst in contact with a reduction gas which comprises carbon monoxide alone or an admixture of hydrogen and carbon monoxide wherein the molar ratio H 2 /CO is between 0.01 and 10, the conditioning operation being carried out at a temperature between 200 and 500°C, at a total pressure between 0.1 and 5 MPa and under a gas flow between 0.1 and 20 Nl/h/g of catalyst to be processed, during 1 to 48 hours; and d) introducing the catalyst reduced in step c) into the synthesis reactor in semi-continuous mode or in continuous mode.
A method of charging coolant in a cooling system for a vehicle, the method comprising: determining when a diagnostic apparatus configured for charging the coolant has been connected to a vehicle; starting an engine of the vehicle in a predetermined operation state; in a response that the diagnostic apparatus configured for charging the coolant is determined to be connected to the vehicle, starting a coolant charging mode for charging the coolant by the diagnostic apparatus after starting the engine; and determining, by the diagnostic apparatus, when a coolant charging mode release condition has been satisfied after starting the coolant charging mode, wherein in a response that the coolant charging mode is determined to have entered, a drive of an Exhaust Gas Recirculation device is turned off (S14; S25). determining when a diagnostic apparatus configured for charging the coolant has been connected to a vehicle; starting an engine of the vehicle in a predetermined operation state; in a response that the diagnostic apparatus configured for charging the coolant is determined to be connected to the vehicle, starting a coolant charging mode for charging the coolant by the diagnostic apparatus after starting the engine; and determining, by the diagnostic apparatus, when a coolant charging mode release condition has been satisfied after starting the coolant charging mode, wherein in a response that the coolant charging mode is determined to have entered, a drive of an Exhaust Gas Recirculation device is turned off (S14; S25).