mhurhangee/ep-ind-claims huggingface dataset:
Filter element for filtering a fluid, in particular fuel or oil, in particular for the internal combustion engine of a motor vehicle, having a closure member for closing a drainage channel of a filter head provided for the connection of the filter element, which closing member is eccentrically disposed on a front face of the filter element relative to the longitudinal axis of the filter element and extends away from the front face of the filter element in the axial direction, characterized in that the filter element features an annular standing aid snap-connected to the filter element, which standing aid extends away from the front face of the filter element in the axial direction up to the level of the free end of the closure member or beyond the free end of the closure member so that, thanks to the standing aid, the filter element can be positioned on its front face provided with the closure member without falling over and the closure member is protected against damages. having a closure member for closing a drainage channel of a filter head provided for the connection of the filter element, which closing member is eccentrically disposed on a front face of the filter element relative to the longitudinal axis of the filter element and extends away from the front face of the filter element in the axial direction, characterized in that the filter element features an annular standing aid snap-connected to the filter element, which standing aid extends away from the front face of the filter element in the axial direction up to the level of the free end of the closure member or beyond the free end of the closure member so that, thanks to the standing aid, the filter element can be positioned on its front face provided with the closure member without falling over and the closure member is protected against damages.
A control device for varying the transmittance of an electrochromic device, the control device comprising: a power source configured to be electrically coupled to the electrochromic device, the power source configured to supply power to the electrochromic device; an electrical load sensing circuit configured to be coupled to the electrochromic device, the electrical load sensing circuit configured to measure at least one of a voltage and a current supplied to the electrochromic device; and a processor electrically coupled to the electrical load sensing circuit and the power source, the processor configured to receive a measured electrical load value from the electrical load sensing circuit indicating an electrical property of the electrochromic device, and to control one or more properties of the electrochromic device by controlling the amount of current or voltage supplied from the power source to the electrochromic device; wherein the processor is configured to vary a property of the electrochromic device while maintaining the electrochromic device at a consistent transmittance such that a first transmission state has a transmittance within 5% of the transmittance of a second transmission state, wherein the property of the electrochromic device to be varied is selected from - a color of the electrochromic device, or - an amount of infrared radiation transmitted through the electrochromic device. a power source configured to be electrically coupled to the electrochromic device, the power source configured to supply power to the electrochromic device; an electrical load sensing circuit configured to be coupled to the electrochromic device, the electrical load sensing circuit configured to measure at least one of a voltage and a current supplied to the electrochromic device; and a processor electrically coupled to the electrical load sensing circuit and the power source, the processor configured to receive a measured electrical load value from the electrical load sensing circuit indicating an electrical property of the electrochromic device, and to control one or more properties of the electrochromic device by controlling the amount of current or voltage supplied from the power source to the electrochromic device; wherein the processor is configured to vary a property of the electrochromic device while maintaining the electrochromic device at a consistent transmittance such that a first transmission state has a transmittance within 5% of the transmittance of a second transmission state, wherein the property of the electrochromic device to be varied is selected from - a color of the electrochromic device, or - an amount of infrared radiation transmitted through the electrochromic device. - a color of the electrochromic device, or - an amount of infrared radiation transmitted through the electrochromic device.
A method of manufacturing a sintered body, the method comprising: a debindering process of carrying out a debindering to an injection molded body produced by a primary shaping by injecting into an injection mold a shaping material in which a metal powder and a binder are mixed, to produce an intermediate shaped body; a sintering process of carrying out a sintering to the intermediate shaped body to produce a sintered body; and a secondary shaping process of transforming the injection molded body or the intermediate shaped body before the sintered body is produced, characterized in that the secondary shaping process includes a process of grasping a first part and a second part of the injection molded body or the intermediate shaped body, and rotating the first part and the second part relatively to apply torsion transformation to the injection molded body or the intermediate shaped body. a debindering process of carrying out a debindering to an injection molded body produced by a primary shaping by injecting into an injection mold a shaping material in which a metal powder and a binder are mixed, to produce an intermediate shaped body; a sintering process of carrying out a sintering to the intermediate shaped body to produce a sintered body; and a secondary shaping process of transforming the injection molded body or the intermediate shaped body before the sintered body is produced, characterized in that the secondary shaping process includes a process of grasping a first part and a second part of the injection molded body or the intermediate shaped body, and rotating the first part and the second part relatively to apply torsion transformation to the injection molded body or the intermediate shaped body.
An aircraft comprising an internal combustion engine and a wing comprising a hollow structural member (74, 76, 78) comprising any of a wing leading edge box, a wing centre box, and a wing trailing edge box, wherein the aircraft comprises an electrical network comprising: at least one alternating current electrical generator configured to be driven by the internal combustion engine; an electrical motor configured to drive an aircraft propulsor; at least one conductor (80, 82) configured to electrically couple the electrical motor and the electrical generator, the conductor (80, 82) comprising at least two conducting elements (80a-c) carrying a separate electrical phase, and each current carrying element (80a-c) being arranged concentrically; wherein the electrical conductor (80, 82) is formed of the hollow structural member (74, 76, 78) of the aircraft wing. at least one alternating current electrical generator configured to be driven by the internal combustion engine; an electrical motor configured to drive an aircraft propulsor; at least one conductor (80, 82) configured to electrically couple the electrical motor and the electrical generator, the conductor (80, 82) comprising at least two conducting elements (80a-c) carrying a separate electrical phase, and each current carrying element (80a-c) being arranged concentrically; wherein the electrical conductor (80, 82) is formed of the hollow structural member (74, 76, 78) of the aircraft wing.
An apparatus comprising: - a switching power converter configured to transfer energy from an input of the power converter to a load coupled to the power converter in conformity with a regulated current, the switching power converter comprising a switch and an energy storage device, wherein the regulated current is a function of a switching period of the switching power converter and a peak current of the energy storage device during the switching period; wherein the switching power converter comprises one of a buck converter, a buck-boost converter, and a flyback converter., and - a controller configured to generate a control signal (Cs) to activate and deactivate the switch in order to control the switching period and the peak current to maintain the regulated current at a desired current level such that: if the switching period decreases below a minimum switching period, the controller increases the switching period by a ringing period of a voltage of the switch and increases the peak current to compensate for the increase of the switching period in order to maintain the regulated current; and if the peak current increases above a maximum peak current, the controller decreases the switching period by a ringing period of the voltage of the switch and decreases the peak current to compensate for the decrease of the switching period in order to maintain the regulated current. - a switching power converter configured to transfer energy from an input of the power converter to a load coupled to the power converter in conformity with a regulated current, the switching power converter comprising a switch and an energy storage device, wherein the regulated current is a function of a switching period of the switching power converter and a peak current of the energy storage device during the switching period; wherein the switching power converter comprises one of a buck converter, a buck-boost converter, and a flyback converter., and - a controller configured to generate a control signal (Cs) to activate and deactivate the switch in order to control the switching period and the peak current to maintain the regulated current at a desired current level such that: if the switching period decreases below a minimum switching period, the controller increases the switching period by a ringing period of a voltage of the switch and increases the peak current to compensate for the increase of the switching period in order to maintain the regulated current; and if the peak current increases above a maximum peak current, the controller decreases the switching period by a ringing period of the voltage of the switch and decreases the peak current to compensate for the decrease of the switching period in order to maintain the regulated current.
A calibration index for use in calibration of an onboard camera, comprising: a curved graphic formed of a curved line surrounding a predetermined region; a linear graphic comprising at least two straight lines forming an intersection point within said region surrounded by the curved graphic, said curved graphic and said linear graphic being formed in a same plane and being surrounded by a quadrangle; and a plurality of segments separated by the curved line forming the curved graphic and the straight lines forming the linear graphic being colored in a checkered pattern; characterized in that the straight lines forming the linear graphic are provided with an inclination relative to the horizontal plane in the field of view of the onboard camera and a vertical plane vertical relative to said horizontal plane and relative to sides of the quadrangle. a curved graphic formed of a curved line surrounding a predetermined region; a linear graphic comprising at least two straight lines forming an intersection point within said region surrounded by the curved graphic, said curved graphic and said linear graphic being formed in a same plane and being surrounded by a quadrangle; and a plurality of segments separated by the curved line forming the curved graphic and the straight lines forming the linear graphic being colored in a checkered pattern; characterized in that the straight lines forming the linear graphic are provided with an inclination relative to the horizontal plane in the field of view of the onboard camera and a vertical plane vertical relative to said horizontal plane and relative to sides of the quadrangle.
Drone for searching and marking a target, comprising: - an aerial vehicle provided with at least one rotor participating in the lift and/or propulsion of said drone, - a mission system, and - a device for fixing said mission system to said aerial vehicle said mission system comprising: - a structure, fixed with respect to said aerial vehicle, - a calculator, - at least one detection device for detecting a target, and - a distribution device for distributing at least one marking element, said distribution device being provided with at least one compartment designed to contain a marking element, said distribution device being configured so as to release said marking element contained in a compartment so as to mark a location of a detected target, characterised in that said distribution device comprises a rotary engine, a distributor provided with multiple compartments and a base provided with an opening, said rotary engine allowing a relative rotation of said distributor with respect to said base so that said opening is disposed below a compartment so as to release said marking element contained in said compartment. - an aerial vehicle provided with at least one rotor participating in the lift and/or propulsion of said drone, - a mission system, and - a device for fixing said mission system to said aerial vehicle - a structure, fixed with respect to said aerial vehicle, - a calculator, - at least one detection device for detecting a target, and - a distribution device for distributing at least one marking element, said distribution device being provided with at least one compartment designed to contain a marking element, said distribution device being configured so as to release said marking element contained in a compartment so as to mark a location of a detected target,
Cooking appliance comprising a cooking enclosure, a support configured to directly or indirectly receive food to cook and a mechanism configured to guide the support towards the outside of the enclosure according to a rectilinear path and, conversely, towards the inside of the enclosure, characterised in that the mechanism comprises: - at least one first articulated arm (6, 7) of which a first end (6a, 7a) is mounted in pivot connection about a first axis (X1, X'1) opposite the enclosure and a second end (6b, 7b) is mounted in pivot connection about a second axis (X2, X'2) opposite the support, said first and second axes being parallel to one another and defined respectively in first and second planes (P1, P2) perpendicular to said rectilinear path, - at least one second articulated arm of which a first end is mounted in pivot connection about a third axis opposite the enclosure and a second end is mounted in pivot connection about a fourth axis opposite the support, said third and fourth axes being parallel to one another and defined respectively in third and fourth planes (P3, P4) perpendicular to said rectilinear path, - the first and second axes (X1, X2, X'1, X'2) being inclined with respect to the third and fourth axes (X3, X4). - at least one first articulated arm (6, 7) of which a first end (6a, 7a) is mounted in pivot connection about a first axis (X1, X'1) opposite the enclosure and a second end (6b, 7b) is mounted in pivot connection about a second axis (X2, X'2) opposite the support, said first and second axes being parallel to one another and defined respectively in first and second planes (P1, P2) perpendicular to said rectilinear path, - at least one second articulated arm of which a first end is mounted in pivot connection about a third axis opposite the enclosure and a second end is mounted in pivot connection about a fourth axis opposite the support, said third and fourth axes being parallel to one another and defined respectively in third and fourth planes (P3, P4) perpendicular to said rectilinear path, - the first and second axes (X1, X2, X'1, X'2) being inclined with respect to the third and fourth axes (X3, X4).
A gas bearing comprising: a bearing housing having a shaft bore defined by a radially inward facing bearing surface, and a plurality of laser-drilled capillaries extending radially into the bearing housing through the bearing surface to provide fluid communication between the bearing surface and a pressurisable space contained within and radially enclosed by the bearing housing, wherein the pressurisable space comprises a plurality of chambers in fluid communication with each other along a common channel, wherein one or more of the chambers has an inlet conduit extending thereto from the outside of the bearing housing, characterised in that: the plurality of chambers comprises a plurality of separate axially extending bores arranged regularly on a ring around the shaft bore, the bearing housing is a one-piece bearing housing, and each laser-drilled capillary includes a gas-outlet at the bearing surface which narrows as it extends away from the bearing surface, each gas-outlet including an indented pocket formed in the bearing surface. a bearing housing having a shaft bore defined by a radially inward facing bearing surface, and a plurality of laser-drilled capillaries extending radially into the bearing housing through the bearing surface to provide fluid communication between the bearing surface and a pressurisable space contained within and radially enclosed by the bearing housing, wherein the pressurisable space comprises a plurality of chambers in fluid communication with each other along a common channel, wherein one or more of the chambers has an inlet conduit extending thereto from the outside of the bearing housing, a shaft bore defined by a radially inward facing bearing surface, and a plurality of laser-drilled capillaries extending radially into the bearing housing through the bearing surface to provide fluid communication between the bearing surface and a pressurisable space contained within and radially enclosed by the bearing housing, wherein the pressurisable space comprises a plurality of chambers in fluid communication with each other along a common channel, wherein one or more of the chambers has an inlet conduit extending thereto from the outside of the bearing housing, the plurality of chambers comprises a plurality of separate axially extending bores arranged regularly on a ring around the shaft bore, the bearing housing is a one-piece bearing housing, and each laser-drilled capillary includes a gas-outlet at the bearing surface which narrows as it extends away from the bearing surface, each gas-outlet including an indented pocket formed in the bearing surface.
Procedure for providing measured values for end customers, said procedure comprising the following steps: Recording of a measured value of a process variable using a sensor S1, S2, S3, Transmission of the measured value to a process control system PCS, Counting of the number A of transmission processes, Calculation of the costs for the end customer depending on the number A of the transmission processes, characterized in that the number A of the transmission processes is recorded in the sensor S1, S2, S3. Recording of a measured value of a process variable using a sensor S1, S2, S3, Transmission of the measured value to a process control system PCS, Counting of the number A of transmission processes, Calculation of the costs for the end customer depending on the number A of the transmission processes, characterized in that the number A of the transmission processes is recorded in the sensor S1, S2, S3.
An isolated anti-Cadherin-17 antibody comprising: a heavy chain variable region CDR1 comprising SEQ ID NO: 4; a heavy chain variable region CDR2 comprising SEQ ID NO: 8; a heavy chain variable region CDR3 comprising SEQ ID NO: 17; a light chain variable region CDR1 comprising SEQ ID NO: 24; a light chain variable region CDR2 comprising SEQ ID NO: 30; and a light chain variable region CDR3 comprising SEQ ID NO: 34, optionally wherein any of SEQ ID NOs: 4, 8, 17, 24, 30 or 34 independently comprises one, two, three, four or five konservative amino acid substitutions, wherein the antibody is capable of being internalised into a cell expressing Cadherin-17. a heavy chain variable region CDR1 comprising SEQ ID NO: 4; a heavy chain variable region CDR2 comprising SEQ ID NO: 8; a heavy chain variable region CDR3 comprising SEQ ID NO: 17; a light chain variable region CDR1 comprising SEQ ID NO: 24; a light chain variable region CDR2 comprising SEQ ID NO: 30; and a light chain variable region CDR3 comprising SEQ ID NO: 34, optionally wherein any of SEQ ID NOs: 4, 8, 17, 24, 30 or 34 independently comprises one, two, three, four or five konservative amino acid substitutions, wherein the antibody is capable of being internalised into a cell expressing Cadherin-17.
Continuously variable power split transmission for powering vehicles and/or work machines by a combustion engine, comprising a variator, a summing gear train and a number of couplings, the variator delivering a fraction of the power of the combustion engine with a speed that is continuously variably controlled between maximum speeds in both directions to the summing gear train, where it is added to the other fraction of the power, and where the transition between a plurality of ranges occurs in points of synchronism, the summing gear train being a planetary gear train with four shafts including a sun gear as a first central gear wheel, a second central gear wheel (S2; H2), a ring gear and a number of planetary gears (P1, P2) journalled on a planet carrier, wherein: a. The couplings (C0, C1, B0, B1) are united in one common entry unit, which is arranged in the flux of power between the combustion engine and the summing gear train (SG1; SG2), b. The summing gear train (SG1; SG2) includes first planetary gears and second planetary gears jounalled on a common planet carrier, the first and the second planetary gears meshing with each other, c. The first sun gear or the first ring gear are driven by the combustion engine and the second central gear wheel (S2; H2) is driven by the variator, the first sun gear or the first ring gear, for the transition from one range to the next range in a point of synchronism (1,2,3), being in turn drivingly connected with the combustion engine, d. The planet carrier is drinvingly connected with the output shaft of the transmission. a. The couplings (C0, C1, B0, B1) are united in one common entry unit, which is arranged in the flux of power between the combustion engine and the summing gear train (SG1; SG2), b. The summing gear train (SG1; SG2) includes first planetary gears and second planetary gears jounalled on a common planet carrier, the first and the second planetary gears meshing with each other, c. The first sun gear or the first ring gear are driven by the combustion engine and the second central gear wheel (S2; H2) is driven by the variator, the first sun gear or the first ring gear, for the transition from one range to the next range in a point of synchronism (1,2,3), being in turn drivingly connected with the combustion engine, d. The planet carrier is drinvingly connected with the output shaft of the transmission.