mhurhangee/ep-ind-claims huggingface dataset:
An airfoil component for a gas turbine engine comprising: at least one airfoil extending from a platform, the platform including a cooling passage defined by a surface; and a plurality of chevron-shaped trip strips extending from the surface into the cooling passage at a trip strip height along a length, the trip strip height varying along the length, wherein the airfoil component is a turbine vane having an inner and an outer platform (74, 76), the cooling passage is provided in the inner platform of the turbine vane, the turbine vane includes a pair of airfoils extending radially from the same inner platform, and the cooling passage is provided by first and second radially extending legs (98, 100) spaced circumferentially apart from one another and joined to one another by a circumferential passage, the circumferential passage including the trip strips, the first radially extending leg providing an inlet into the circumferential passage and the second radially extending leg being plugged with a plug weld. at least one airfoil extending from a platform, the platform including a cooling passage defined by a surface; and a plurality of chevron-shaped trip strips extending from the surface into the cooling passage at a trip strip height along a length, the trip strip height varying along the length, wherein the airfoil component is a turbine vane having an inner and an outer platform (74, 76), the cooling passage is provided in the inner platform of the turbine vane, the turbine vane includes a pair of airfoils extending radially from the same inner platform, and the cooling passage is provided by first and second radially extending legs (98, 100) spaced circumferentially apart from one another and joined to one another by a circumferential passage, the circumferential passage including the trip strips, the first radially extending leg providing an inlet into the circumferential passage and the second radially extending leg being plugged with a plug weld.
An oxide semiconductor sputtering target made of a composition including gallium oxide, tin oxide and indium oxide, characterized in that the content ratios of indium, gallium and tin being, by atomic percent, 60 to 70, 10 to 25 and 5 to 30, with respect to a total of indium, gallium and tin.
A method for monitoring the torsion of a cable comprising the steps of: providing a cable having an outer surface and extending along a longitudinal direction, the cable being provided with at least one identification tag arranged in a tag angular position in a cross-sectional plane taken transverse to the longitudinal direction, the at least one tag storing a tag identification code and being capable of transmitting a tag electromagnetic signal; interrogating the at least one identification tag to receive the tag electromagnetic signal, and detecting the tag electromagnetic signal, wherein the step of detecting the tag electromagnetic signal comprises the step of reading the tag identification code and determining the tag angular position of the at least one identification tag. providing a cable having an outer surface and extending along a longitudinal direction, the cable being provided with at least one identification tag arranged in a tag angular position in a cross-sectional plane taken transverse to the longitudinal direction, the at least one tag storing a tag identification code and being capable of transmitting a tag electromagnetic signal; interrogating the at least one identification tag to receive the tag electromagnetic signal, and detecting the tag electromagnetic signal, wherein the step of detecting the tag electromagnetic signal comprises the step of reading the tag identification code and determining the tag angular position of the at least one identification tag.
A method for obtaining location information by an electronic device including a first processor, being a low-power processor, operable at a first power level and a second processor operable at a second power level, the method comprising: receiving (601, 1603) first location information of the electronic device from at least one first sensor functionally connected with the first processor, the at least one first sensor identifying the first location information based on signals received from external electronic devices; determining (602, 1604) that reception of the first location information of the electronic device is failed; requesting location information to the second processor based on the determining that reception of the first location information is failed, wherein the second processor is in one of the deactivated state, a sleep mode or a low-power mode state to reduce power consumption; receiving (604, 606, 1607) second location information from at least one second sensor functionally connected with the second processor using the second processor; determining (1605, 1608) that the electronic device enters a geo-fence based on at least one of the first location information or the second location information; when it is determined that the electronic device enters the geo-fence using the first location information, determining that the geo-fence comprises an open zone; and when it is determined that the electronic device enters the geo-fence using the second location information, determining that the geo-fence comprises a shadow zone. receiving (601, 1603) first location information of the electronic device from at least one first sensor functionally connected with the first processor, the at least one first sensor identifying the first location information based on signals received from external electronic devices; determining (602, 1604) that reception of the first location information of the electronic device is failed; requesting location information to the second processor based on the determining that reception of the first location information is failed, wherein the second processor is in one of the deactivated state, a sleep mode or a low-power mode state to reduce power consumption; receiving (604, 606, 1607) second location information from at least one second sensor functionally connected with the second processor using the second processor; determining (1605, 1608) that the electronic device enters a geo-fence based on at least one of the first location information or the second location information; when it is determined that the electronic device enters the geo-fence using the first location information, determining that the geo-fence comprises an open zone; and when it is determined that the electronic device enters the geo-fence using the second location information, determining that the geo-fence comprises a shadow zone.
Pump for conveying a blood flow for cardiovascular support: comprising a rotor having an axis of rotation for conveying a liquid, the rotor having a second hollow-cylindrical permanent magnet which is rotatably mounted about an axis of rotation; and comprising a housing in which a first permanent magnet for transmitting a torque to the rotor is rotatably mounted about the axis of rotation, the first permanent magnet and the second permanent magnet at least partially axially overlapping, and the housing being located between the two permanent magnets (30, 40) in the axial overlapping region of the first permanent magnet and the second permanent magnet, comprising a first bearing for axially positioning the rotor and the housing relative to one another and comprising a second bearing and a third bearing for absorbing radial forces and for positioning the axis of rotation of the second permanent magnet, characterized in that the first permanent magnet is arranged axially offset with respect to the second permanent magnet in order to hold the rotor in the first bearing with a defined resulting force acting in the direction of the rotor axis of the rotor, which force is caused by an axial force caused by the axial offset arrangement of the first permanent magnet and the second permanent magnet and a hydraulic force acting in the direction of the axis of rotation of the rotor when the blood flow is conveyed. comprising a rotor having an axis of rotation for conveying a liquid, the rotor having a second hollow-cylindrical permanent magnet which is rotatably mounted about an axis of rotation; and comprising a housing in which a first permanent magnet for transmitting a torque to the rotor is rotatably mounted about the axis of rotation, the first permanent magnet and the second permanent magnet at least partially axially overlapping, and the housing being located between the two permanent magnets (30, 40) in the axial overlapping region of the first permanent magnet and the second permanent magnet, comprising a first bearing for axially positioning the rotor and the housing relative to one another and comprising a second bearing and a third bearing for absorbing radial forces and for positioning the axis of rotation of the second permanent magnet, characterized in that the first permanent magnet is arranged axially offset with respect to the second permanent magnet in order to hold the rotor in the first bearing with a defined resulting force acting in the direction of the rotor axis of the rotor, which force is caused by an axial force caused by the axial offset arrangement of the first permanent magnet and the second permanent magnet and a hydraulic force acting in the direction of the axis of rotation of the rotor when the blood flow is conveyed.
A blood processing apparatus comprising: a plurality of fluid chambers each having an internal space; a chamber pressurizing member compressing or expanding the internal spaces of the fluid chambers (51, 52, 53, 54, 55, 56, 57, 58); a chamber pressurizing member driver driving the chamber pressurizing member; and a flow control unit, wherein the plurality of fluid chambers (51, 52, 53, 54, 55, 56, 57, 58) includes n fluid chambers (where n is 2 or more and a positive integer), the n fluid chambers are each connected with a first flow tube through which a fluid is provided to the chamber and a second flow tube through which a fluid of the chamber is discharged therefrom, and the flow control unit controls a flow through the first and second flow tubes connected to the n chambers and characterized in that when the n is an even number, n/2 chambers are compressed and another n/2 chambers are expanded simultaneously, wherein when the n is an odd number, (n+1)/2 chambers are compressed and (n-1)/2 chambers are expanded simultaneously. a plurality of fluid chambers each having an internal space; a chamber pressurizing member compressing or expanding the internal spaces of the fluid chambers (51, 52, 53, 54, 55, 56, 57, 58); a chamber pressurizing member driver driving the chamber pressurizing member; and a flow control unit, wherein the plurality of fluid chambers (51, 52, 53, 54, 55, 56, 57, 58) includes n fluid chambers (where n is 2 or more and a positive integer), the n fluid chambers are each connected with a first flow tube through which a fluid is provided to the chamber and a second flow tube through which a fluid of the chamber is discharged therefrom, and the flow control unit controls a flow through the first and second flow tubes connected to the n chambers and characterized in that when the n is an even number, n/2 chambers are compressed and another n/2 chambers are expanded simultaneously, wherein when the n is an odd number, (n+1)/2 chambers are compressed and (n-1)/2 chambers are expanded simultaneously. a flow control unit, wherein the plurality of fluid chambers (51, 52, 53, 54, 55, 56, 57, 58) includes n fluid chambers (where n is 2 or more and a positive integer), the n fluid chambers are each connected with a first flow tube through which a fluid is provided to the chamber and a second flow tube through which a fluid of the chamber is discharged therefrom, and the flow control unit controls a flow through the first and second flow tubes connected to the n chambers and characterized in that when the n is an even number, n/2 chambers are compressed and another n/2 chambers are expanded simultaneously, wherein when the n is an odd number, (n+1)/2 chambers are compressed and (n-1)/2 chambers are expanded simultaneously.
A method for exchanging wheels of a wheel carriage resting in a sliding track, said wheel carriage comprising one wheel holder, at least two wheels, one door carrier and a height adjustment means; wherein the wheel holder comprises at least two wheel connection means each comprising two connection points connected to opposite sides of one of the wheels, wherein the connection points are recesses in the lower side of the wheel holder and wherein the door carrier is attached to a door panel, comprising the steps: - lowering the door panel in a vertical direction by means of the height adjustment means, increasing the distance between the wheel holder and the door carrier to such an extent that the bottom of the door panel rests at a foundation when the wheel carriage is still arranged in the sliding track, whereby the wheels are removable from the wheel holder, - replacing at least one wheel and - elevating the door panel so that the weight of the door panel rests on the sliding track. - lowering the door panel in a vertical direction by means of the height adjustment means, increasing the distance between the wheel holder and the door carrier to such an extent that the bottom of the door panel rests at a foundation when the wheel carriage is still arranged in the sliding track, whereby the wheels are removable from the wheel holder, - replacing at least one wheel and - elevating the door panel so that the weight of the door panel rests on the sliding track.
An aircraft cabin comprising a system (100, 200) of passenger seats, each passenger seat (10, 20) comprising: - a seat body, - a passenger seat electrical net (50,60) - an energy harvesting system (30,40) comprising an energy harvesting device (31, 41) adapted for capturing from the seat body ambient energy, wherein the energy harvesting device (31, 41) is provided to the seat body, the energy harvesting system (30, 40) being connected to the passenger seat electrical net (50, 60), the cabin further comprising - load consumers (L1,..Ln), - an aircraft electrical net, wherein the aircraft electrical net connects a number of passenger seat electrical nets (50,60.1. 60.2.. 60.n) of a predetermined number (n) of passenger seats and their energy harvesting systems (40.1... 40.n) to the load consumers (L1... Ln), the load consumers being connected by load wiring to the aircraft electrical net, wherein - each energy harvesting system (30, 40) is adapted for providing electrical energy into the passenger seat electrical net (50, 60) and the aircraft electrical net. - a seat body, - a passenger seat electrical net (50,60) - an energy harvesting system (30,40) comprising an energy harvesting device (31, 41) adapted for capturing from the seat body ambient energy, wherein the energy harvesting device (31, 41) is provided to the seat body, the energy harvesting system (30, 40) being connected to the passenger seat electrical net (50, 60), - load consumers (L1,..Ln), - an aircraft electrical net, wherein the aircraft electrical net connects a number of passenger seat electrical nets (50,60.1. 60.2.. 60.n) of a predetermined number (n) of passenger seats and their energy harvesting systems (40.1... 40.n) to the load consumers (L1... Ln), the load consumers being connected by load wiring to the aircraft electrical net, wherein - each energy harvesting system (30, 40) is adapted for providing electrical energy into the passenger seat electrical net (50, 60) and the aircraft electrical net.
A method for transmitting a signal, comprising steps of: generating a control signal; generating modulation symbols by binary phase shift keying, BPSK modulating bits of the control signal; code division multiplexing the modulation symbols based on an orthogonal sequence with a spreading length of 4; mapping, repeatedly for a predetermined number of times, the code division multiplexed modulation symbols to resource units spread in a frequency domain and two antennas based on a space frequency block coding, SFBC, scheme, each of the resource units including a pair of neighboring subcarriers in the frequency domain and two subsequent orthogonal frequency division multiplexing, OFDM, symbols in a time domain; and transmitting the symbols mapped on the resource units through the two antennas based on a result of the mapping. wherein the control signal includes one of an acknowledgement, ACK, signal and a negative acknowledgement, NACK, signal, wherein the code division multiplexed modulation symbols are divided into a first pair consisting of two leading symbols of the code division multiplexed symbols and a second pair of two ending symbols of the code division multiplexed symbols, and wherein the first pair and the second pair are mapped alternately to the two subsequent OFDM symbols in different transmissions in the frequency domain. generating a control signal; generating modulation symbols by binary phase shift keying, BPSK modulating bits of the control signal; code division multiplexing the modulation symbols based on an orthogonal sequence with a spreading length of 4; mapping, repeatedly for a predetermined number of times, the code division multiplexed modulation symbols to resource units spread in a frequency domain and two antennas based on a space frequency block coding, SFBC, scheme, each of the resource units including a pair of neighboring subcarriers in the frequency domain and two subsequent orthogonal frequency division multiplexing, OFDM, symbols in a time domain; and transmitting the symbols mapped on the resource units through the two antennas based on a result of the mapping. wherein the control signal includes one of an acknowledgement, ACK, signal and a negative acknowledgement, NACK, signal, wherein the code division multiplexed modulation symbols are divided into a first pair consisting of two leading symbols of the code division multiplexed symbols and a second pair of two ending symbols of the code division multiplexed symbols, and wherein the first pair and the second pair are mapped alternately to the two subsequent OFDM symbols in different transmissions in the frequency domain.
Wet clutch (K0, E1, E2) for a powertrain system comprising, about an axis, at least: - a multi-disc assembly (K0, E1, E2) composed of flanges (6, 11, 21) and friction discs (7, 12, 22); - a torque-transmitting disc carrier supporting the multi-disc assembly of the wet clutch, comprising: • a cylindrical portion, • a flange extending radially from the cylindrical portion, • an annular cavity (103, 101, 102) of axis positioned on one side of the flange and designed to receive an actuating piston (5, 15, 25) for actuation of the multi-disc assembly (K0, E1, E2), - a radial guide bearing attached to the torque-transmitting disc carrier on the other side of the flange and arranged to guide the wet clutch in rotation relative to the powertrain system, wherein the torque-transmitting disc carrier comprises at least one outlet portion of a lubrication channel for lubricating the radial guide bearing which opens out radially below the radial guide bearing, characterized in that the outlet portion of the lubrication channel is oriented in the opposite direction to the direction of the annular cavity (103, 101, 102) and inclined relative to the axis by an angle (Δ) of between 0 and 60 degrees. - a multi-disc assembly (K0, E1, E2) composed of flanges (6, 11, 21) and friction discs (7, 12, 22); - a torque-transmitting disc carrier supporting the multi-disc assembly of the wet clutch, comprising: • a cylindrical portion, • a flange extending radially from the cylindrical portion, • an annular cavity (103, 101, 102) of axis positioned on one side of the flange and designed to receive an actuating piston (5, 15, 25) for actuation of the multi-disc assembly (K0, E1, E2), • a cylindrical portion, • a flange extending radially from the cylindrical portion, • an annular cavity (103, 101, 102) of axis positioned on one side of the flange and designed to receive an actuating piston (5, 15, 25) for actuation of the multi-disc assembly (K0, E1, E2), - a radial guide bearing attached to the torque-transmitting disc carrier on the other side of the flange and arranged to guide the wet clutch in rotation relative to the powertrain system, wherein the torque-transmitting disc carrier comprises at least one outlet portion of a lubrication channel for lubricating the radial guide bearing which opens out radially below the radial guide bearing, characterized in that the outlet portion of the lubrication channel is oriented in the opposite direction to the direction of the annular cavity (103, 101, 102) and inclined relative to the axis by an angle (Δ) of between 0 and 60 degrees.
A combination of i) interleukin-2 (IL-2) and ii) an interleukin 1 (IL-1) inhibitor, for use in treating an auto-immune and/or inflammatory disorder in a subject, preferably a human subject, wherein the IL-1 inhibitor is selected from the group consisting of i) a soluble form of an IL-1 receptor, ii) an anti-IL-1R antibody or a fragment thereof, and iii) an anti-IL-1 antibody or a fragment thereof.
A coating composition comprising a cold water soluble starch and one or more binders, thickeners and/or pigments characterized in that said cold water soluble starch is derived from a starch selected from the group consisting of wheat starch, corn starch and mixtures thereof, and has a DE of less than 5 and has: - a number of average molecular weight (Mn) of 3500 to 20000 Daltons; - a granular structure before solubilisation; - a solubility at pH7 and 20°C of 30 to 90%; and - a solubility at pH10 and 35°C which is at least 10% greater than S1. - a number of average molecular weight (Mn) of 3500 to 20000 Daltons; - a granular structure before solubilisation; - a solubility at pH7 and 20°C of 30 to 90%; and - a solubility at pH10 and 35°C which is at least 10% greater than S1.