mhurhangee/patent-ind-claim-en huggingface dataset:
Device for transmission of a torque from drive equipment to a roll in a roll stand for the rolling of rolling material, comprising: a spindle ; a drive-side rotary bearing for rotational coupling of the spindle with the drive output shaft of the drive equipment ; a roll-side rotary bearing for rotational coupling of the spindle with a pin of the roll, wherein a lubricant chamber is formed in the roll-side rotary bearing ; and at least one pump device , which is incorporated in a circuit for liquid lubricant, for conveying the liquid lubricant in the circuit; wherein a forward run channel and a return run channel for the lubricant are formed in the region of the spindle and are fluid-conductively connected with the lubricant chamber in the roll-side rotary bearing; characterised in that a lubricant chamber is formed in the drive-side rotary bearing ; and the lubricant chambers in the roll-side and drive-side rotary bearings are fluid-conductively connected together by way of the forward run channel and the return run channel , whereby the circuit for the lubricant is formed to be closed. a spindle ; a drive-side rotary bearing for rotational coupling of the spindle with the drive output shaft of the drive equipment ; a roll-side rotary bearing for rotational coupling of the spindle with a pin of the roll, wherein a lubricant chamber is formed in the roll-side rotary bearing ; and at least one pump device , which is incorporated in a circuit for liquid lubricant, for conveying the liquid lubricant in the circuit; wherein a forward run channel and a return run channel for the lubricant are formed in the region of the spindle and are fluid-conductively connected with the lubricant chamber in the roll-side rotary bearing; characterised in that a lubricant chamber is formed in the drive-side rotary bearing ; and the lubricant chambers in the roll-side and drive-side rotary bearings are fluid-conductively connected together by way of the forward run channel and the return run channel , whereby the circuit for the lubricant is formed to be closed.
Slow-release solid oral nutraceutical and/or pharmaceutical composition comprising: a) a core containing a donor of methyl groups characterised in that said donor of methyl groups is selected from SAMe or a pharmaceutically acceptable salt thereof, a folate, a reduced folate or a mixture thereof, and at least one pharmaceutically acceptable excipient, and b) an outer coating containing shellac and/or a pharmaceutically acceptable salt thereof, magnesium stearate and at least one pharmaceutically acceptable excipient, characterised in that the shellac and/or a pharmaceutically acceptable salt thereof is present in the composition in an amount ranging between 0.5% and 10% by weight based on the total weight of the composition, and characterised in that the magnesium stearate is present in the outer coating in an amount ranging between 10% and 20% by weight based on the outer coating; and characterised in that said solid oral form is a tablet. a) a core containing a donor of methyl groups characterised in that said donor of methyl groups is selected from SAMe or a pharmaceutically acceptable salt thereof, a folate, a reduced folate or a mixture thereof, and at least one pharmaceutically acceptable excipient, and b) an outer coating containing shellac and/or a pharmaceutically acceptable salt thereof, magnesium stearate and at least one pharmaceutically acceptable excipient, characterised in that the shellac and/or a pharmaceutically acceptable salt thereof is present in the composition in an amount ranging between 0.5% and 10% by weight based on the total weight of the composition, and characterised in that the magnesium stearate is present in the outer coating in an amount ranging between 10% and 20% by weight based on the outer coating;
An exhaust-air guide of a fuel cell stack, especially in a motor vehicle, with a cooling device, in which air is conveyed in accordance with the jet pump principle, characterised in that the cooling device is a cooler structure belonging to the functional environment of the fuel cell stack and is passed through by ambient air , in that a heat carrier medium is guided through the cooler structure , the heat carrier medium exchanging heat with the ambient air , and in that the exhaust air of the fuel cell stack is guided to a point upstream of, or into, said cooler structure in such a way that the exhaust air flows through the cooler structure in the flow direction (D) and in so doing entrains ambient air in accordance with the jet pump principle.
A single crystal thin film on a substrate for nonlinear optical applications, wherein the single crystal thin film consisting of a configurationally locked polyene compound with phenolic electron donor, wherein the compound is represented by the formula (I)
Modular passenger compartment for a means of locomotion , comprising: - a first passenger compartment part having a first edge , - a second passenger compartment part having a second edge , - a third passenger compartment part having a third edge , wherein the first edge is designed to correspond - to the second edge and - to the third edge in order to selectively close off a volume of the passenger compartment to the outside by means of the second passenger compartment part or by means of the third passenger compartment part , and wherein the second passenger compartment part further has a fourth edge which is designed to correspond to the third edge in order to close off the volume of the passenger compartment to the outside by means of the third passenger compartment part , wherein the passenger compartment parts have a respective interface for temporary connection to a common driving mount , characterized in that at least one passenger compartment part has a service counter with an automatic accepting and dispensing mechanism, designed in the manner of a package station, via which a customer standing in front of the passenger compartment part can introduce a transport container into the passenger compartment . - a first passenger compartment part having a first edge , - a second passenger compartment part having a second edge , - a third passenger compartment part having a third edge , wherein the first edge is designed to correspond - to the second edge and - to the third edge in order to selectively close off a volume of the passenger compartment to the outside by means of the second passenger compartment part or by means of the third passenger compartment part , and wherein the second passenger compartment part further has a fourth edge which is designed to correspond to the third edge in order to close off the volume of the passenger compartment to the outside by means of the third passenger compartment part , wherein the passenger compartment parts have a respective interface for temporary connection to a common driving mount ,
A method for wireless communication between a router in a moving vehicle , such as a train, and a stationary communication server outside the moving vehicle through at least one external mobile network on at least one link, the method, performed in at least one of the stationary communication server and the router , comprising: receiving data packets of a data stream to be transferred on said at least one link; and determining whether said data stream is of a data type belonging to a set of prioritized data types; characterized in that the method comprises: providing a first output buffer and a second output buffer ; selecting, in case it has been determined that the data stream is of a data type belonging to the set of prioritized data types, the first output buffer for said data packets; selecting, in case it has been determined that the data stream is of a data type not belonging to the set of prioritized data types, the second output buffer for said data packets; and transferring the data packets to the selected output buffer, for subsequent transmission of the data packets on said at least one link, wherein data packets are transmitted from the first and second output buffers (26a, 96a; 26b, 96b) with essentially the same output rate. receiving data packets of a data stream to be transferred on said at least one link; and determining whether said data stream is of a data type belonging to a set of prioritized data types; characterized in that the method comprises: providing a first output buffer and a second output buffer ; selecting, in case it has been determined that the data stream is of a data type belonging to the set of prioritized data types, the first output buffer for said data packets; selecting, in case it has been determined that the data stream is of a data type not belonging to the set of prioritized data types, the second output buffer for said data packets; and transferring the data packets to the selected output buffer, for subsequent transmission of the data packets on said at least one link, wherein data packets are transmitted from the first and second output buffers (26a, 96a; 26b, 96b) with essentially the same output rate. providing a first output buffer and a second output buffer ; selecting, in case it has been determined that the data stream is of a data type belonging to the set of prioritized data types, the first output buffer for said data packets; selecting, in case it has been determined that the data stream is of a data type not belonging to the set of prioritized data types, the second output buffer for said data packets; and transferring the data packets to the selected output buffer, for subsequent transmission of the data packets on said at least one link, wherein data packets are transmitted from the first and second output buffers (26a, 96a; 26b, 96b) with essentially the same output rate.
A vane assembly , comprising: a plurality of airfoils each extending between an inner platform and an outer platform , characterised by the plurality of airfoils comprising a nominal airfoil , a thickened airfoil (400; 416; 428), and a first thinned airfoil (406; 422) circumferentially adjacent to the thickened airfoil (400; 416; 428), wherein each of the thickened airfoil (400; 416; 428) and the first thinned airfoil (406; 422) comprise a similar chord length and/or camber to the nominal airfoil ; wherein the nominal airfoil has a first chord thickness (W1); the thickened airfoil (400; 416; 428) has a thickened region relative to the nominal airfoil and a second chord thickness (W2); and the first thinned airfoil (406; 422) is thinned relative to the nominal airfoil and has a third chord thickness (W3); wherein the second chord thickness (W2) is greater than the first chord thickness (W1) and the third chord thickness (W3) is less than the first chord thickness (W1); and a probe disposed within the thickened airfoil (400; 416; 428), wherein a throat area between the thickened airfoil (400; 416; 428) and the first thinned airfoil (406; 422) is within ± 5% of a throat area between the nominal airfoil and a circumferentially adjacent nominal airfoil of the plurality of airfoils , and wherein the thickened airfoil (400; 416; 428) and the adjacent first thinned airfoil (406; 422) are configured to turn a gas path flow therebetween to within ± 20% of a trailing edge exit angle as the nominal airfoil . a plurality of airfoils each extending between an inner platform and an outer platform , characterised by the plurality of airfoils comprising a nominal airfoil , a thickened airfoil (400; 416; 428), and a first thinned airfoil (406; 422) circumferentially adjacent to the thickened airfoil (400; 416; 428), wherein each of the thickened airfoil (400; 416; 428) and the first thinned airfoil (406; 422) comprise a similar chord length and/or camber to the nominal airfoil ; wherein the nominal airfoil has a first chord thickness (W1); the thickened airfoil (400; 416; 428) has a thickened region relative to the nominal airfoil and a second chord thickness (W2); and the first thinned airfoil (406; 422) is thinned relative to the nominal airfoil and has a third chord thickness (W3); wherein the second chord thickness (W2) is greater than the first chord thickness (W1) and the third chord thickness (W3) is less than the first chord thickness (W1); and a probe disposed within the thickened airfoil (400; 416; 428), wherein a throat area between the thickened airfoil (400; 416; 428) and the first thinned airfoil (406; 422) is within ± 5% of a throat area between the nominal airfoil and a circumferentially adjacent nominal airfoil of the plurality of airfoils , and wherein the thickened airfoil (400; 416; 428) and the adjacent first thinned airfoil (406; 422) are configured to turn a gas path flow therebetween to within ± 20% of a trailing edge exit angle as the nominal airfoil .
An industrial process temperature transmitter for measuring a temperature of a process medium contained in a process vessel comprising an isolation wall , the industrial process temperature transmitter comprising: a thermally conductive stem portion having a first end, configured to be brought into contact with or in close proximity to the isolation wall , and a second end; and a housing attached to the second end of the stem portion ; a process temperature sensor configured to perform a temperature measurement of the process medium through the isolation wall ; a secondary temperature sensor configured to produce a secondary temperature signal based on a sensed temperature, wherein the secondary temperature sensor is within the housing ; wherein the industrial process temperature transmitter is configured to produce a temperature signal that is indicative of the temperature of the process medium in the process vessel , based on a process temperature signal output from the process temperature sensor and the secondary temperature signal during a temperature measurement; a compensation circuit configured to provide a dynamic compensation to the temperature signal for a response time of the temperature measurement to a change in the temperature of the process medium and a rate of change of the temperature measurement, and output a compensated temperature signal ; an output circuit configured to produce a temperature output as a function of the compensated temperature signal . a thermally conductive stem portion having a first end, configured to be brought into contact with or in close proximity to the isolation wall , and a second end; and a housing attached to the second end of the stem portion ; a process temperature sensor configured to perform a temperature measurement of the process medium through the isolation wall ; a secondary temperature sensor configured to produce a secondary temperature signal based on a sensed temperature, wherein the secondary temperature sensor is within the housing ; wherein the industrial process temperature transmitter is configured to produce a temperature signal that is indicative of the temperature of the process medium in the process vessel , based on a process temperature signal output from the process temperature sensor and the secondary temperature signal during a temperature measurement; a compensation circuit configured to provide a dynamic compensation to the temperature signal for a response time of the temperature measurement to a change in the temperature of the process medium and a rate of change of the temperature measurement, and output a compensated temperature signal ; an output circuit configured to produce a temperature output as a function of the compensated temperature signal .
A system for treating pulmonary hypertension, the system comprising: a balloon (202, 202', 202", 202"') adapted to be implanted in a pulmonary artery; a reservoir in fluid communication with the balloon (202, 202', 202", 202'") via a conduit (206, 206', 206", 206'", 206""): and a first anchor adapted to be implanted in a pulmonary artery and configured to transition between a contracted state and an expanded state, the first anchor sized and shaped to contact a wall of the pulmonary artery in the expanded state; characterized by a second anchor (208, 208'. 208") coupled to the balloon (202, 202', 202", 202'"), the second anchor (208, 208', 208") configured, after implantation of the first anchor within the pulmonary artery, to be coupled to the first anchor in the pulmonary artery to secure the balloon (202, 202', 202", 202'") within the pulmonary artery, characterised in that the balloon (202, 202', 202", 202'") is configured to be detachable from the first anchor in vivo such that the balloon (202, 202', 202", 202"') is replaceable while the first anchor remains implanted. a balloon (202, 202', 202", 202"') adapted to be implanted in a pulmonary artery; a reservoir in fluid communication with the balloon (202, 202', 202", 202'") via a conduit (206, 206', 206", 206'", 206""): and a first anchor adapted to be implanted in a pulmonary artery and configured to transition between a contracted state and an expanded state, the first anchor sized and shaped to contact a wall of the pulmonary artery in the expanded state; characterized by a second anchor (208, 208'. 208") coupled to the balloon (202, 202', 202", 202'"), the second anchor (208, 208', 208") configured, after implantation of the first anchor within the pulmonary artery, to be coupled to the first anchor in the pulmonary artery to secure the balloon (202, 202', 202", 202'") within the pulmonary artery, characterised in that the balloon (202, 202', 202", 202'") is configured to be detachable from the first anchor in vivo such that the balloon (202, 202', 202", 202"') is replaceable while the first anchor remains implanted.
A laser medium unit comprising: a plate-shaped laser gain medium which includes a first surface (S1) and a second surface (S2) opposite to the first surface (S1), a distance between the first surface (S1) and the second surface (S2) defining a thickness of the laser gain medium, and said laser gain medium being configured to generate emission light by irradiation of excitation light from the first surface (S1); a reflection member that is provided on the second surface (S2) so as to reflect the excitation light and the emission light; and a cooling member that cools the laser gain medium , wherein the laser gain medium includes an irradiation area (IR) which is irradiated with the excitation light and an outer area (OR) which is located outside the irradiation area (IR) when viewed from a thickness direction intersecting the first surface (S1) and the second surface (S2), wherein the cooling member is thermally connected to the second surface (S2) through the reflection member so that a cooling area (CA) of the laser gain medium is formed on the second surface (S2), characterized in that an outer edge of the cooling area (CA) is located inside an outer edge of the irradiation area (IR) when viewed from the thickness direction. a plate-shaped laser gain medium which includes a first surface (S1) and a second surface (S2) opposite to the first surface (S1), a distance between the first surface (S1) and the second surface (S2) defining a thickness of the laser gain medium, and said laser gain medium being configured to generate emission light by irradiation of excitation light from the first surface (S1); a reflection member that is provided on the second surface (S2) so as to reflect the excitation light and the emission light; and a cooling member that cools the laser gain medium , wherein the laser gain medium includes an irradiation area (IR) which is irradiated with the excitation light and an outer area (OR) which is located outside the irradiation area (IR) when viewed from a thickness direction intersecting the first surface (S1) and the second surface (S2), wherein the cooling member is thermally connected to the second surface (S2) through the reflection member so that a cooling area (CA) of the laser gain medium is formed on the second surface (S2), characterized in that an outer edge of the cooling area (CA) is located inside an outer edge of the irradiation area (IR) when viewed from the thickness direction.
A heat dissipation substrate on which an electronic component (EC) is mounted, comprising: a substrate including a mounting surface on which the electronic component (EC) is mounted, and a rear surface of the mounting surface; and a plurality of thermal vias which passes through the heat dissipation substrate between the mounting surface and the rear surface, wherein at least the plurality of thermal vias is disposed in an electronic component projection region projected to the mounting surface in a direction in which a region of a bottom surface portion of the electronic component (EC) is perpendicular to the mounting surface, a surface density of the thermal vias which occupies the mounting surface per unit area is at least partially different, and the plurality of thermal vias is disposed so that the surface density of the thermal vias becomes the greatest at a dense portion (MD) on an inner side of an edge portion of the electronic component projection region, characterized in that an interval between the thermal vias adjacent to each other becomes gradually wider from an inner side of the electronic component projection region to an outer side of the electronic component projection region. a substrate including a mounting surface on which the electronic component (EC) is mounted, and a rear surface of the mounting surface; and a plurality of thermal vias which passes through the heat dissipation substrate between the mounting surface and the rear surface, wherein at least the plurality of thermal vias is disposed in an electronic component projection region projected to the mounting surface in a direction in which a region of a bottom surface portion of the electronic component (EC) is perpendicular to the mounting surface, a surface density of the thermal vias which occupies the mounting surface per unit area is at least partially different, and the plurality of thermal vias is disposed so that the surface density of the thermal vias becomes the greatest at a dense portion (MD) on an inner side of an edge portion of the electronic component projection region, characterized in that an interval between the thermal vias adjacent to each other becomes gradually wider from an inner side of the electronic component projection region to an outer side of the electronic component projection region.
A method for determining a misalignment of a the wind orientation sensor attached to a wind turbine with respect to an axis of a rotor of said wind turbine; the method comprising the steps of: (i) inputting a plurality of data points , each data point relating the wind turbine performance versus wind orientation as measured by said wind orientation sensor itself or via an extra equipment ; (ii) classifying said data points in a plurality of data sets to thereby determining a classification; (iii) applying to each of said data sets a method for determining the misalignment of the wind orientation sensor attached to the wind turbine with respect to the axis of the rotor of said wind turbine, the method comprising the steps of: (a) inputting the data points of one of said data sets; (b) computing a characteristic of a curve defined by said data points of the data set; (c) determining said misalignment from said characteristic; and (iv) combining the results thereof to determine said misalignment , characterised in that said classification is based on the time of measurement of said data points.