mhurhangee/ep-ind-claims huggingface dataset:
A blood treatment device having an extracorporeal blood circuit which comprises an arterial line, a blood pump, a blood treatment unit and a venous line, wherein the arterial and venous lines can be connected to a blood vessel of a patient, and wherein the blood treatment device has an evaluation and control unit, wherein the evaluation and control unit is configured to carry out the following steps: determining the blood recirculation in a blood vessel of the patient connected to the extracorporeal blood circuit; and (b) calculating the blood flow in the blood vessel using the blood recirculation determined in accordance with and using a provided value or a value likewise previously determined for the cardiac output of the patient and characterized in that the evaluation and control unit is configured furthermore to take account of the extracorporeal blood flow and the outflow of fluid in the blood treatment apparatus, in addition to the blood recirculation and the cardiac output, when determining the blood flow in step (b). determining the blood recirculation in a blood vessel of the patient connected to the extracorporeal blood circuit; and (b) calculating the blood flow in the blood vessel using the blood recirculation determined in accordance with and using a provided value or a value likewise previously determined for the cardiac output of the patient
A hydrophobically-modified polymer or composition thereof, wherein the modified polymer is chitosan having saturated hydrocarbon hydrophobic groups of from 2 to about 10 different sizes attached to the polymer backbone; wherein the hydrophobic groups comprise C8 hydrocarbon groups, which are present along with at least one of C14, C16, or C18 hydrocarbon groups at a ratio of from 5:1 to 20:1; or wherein the hydrophobic groups comprise C10 or C12 hydrocarbon groups, which are present along with at least one of C14, C16, or C18 hydrocarbon groups at a ratio of 2:1 to 10:1. wherein the hydrophobic groups comprise C8 hydrocarbon groups, which are present along with at least one of C14, C16, or C18 hydrocarbon groups at a ratio of from 5:1 to 20:1; or wherein the hydrophobic groups comprise C10 or C12 hydrocarbon groups, which are present along with at least one of C14, C16, or C18 hydrocarbon groups at a ratio of 2:1 to 10:1.
Dry-piston railway compressor comprising a protective housing and an upstream fan and characterised in that the fan allows direct cooling of the compression heads, comprising cylinders and cylinder heads, with outside air not heated by a radiator, the railway compressor comprising a radiator installed at the cooling air outlet at the end of the housing so that ice plug formation due to the presence of condensates in the radiator is prevented.
A vertical axis turbine that includes: a rotatable hub assembly that is configured to be connected to an energy sink and rotatable about an axis of rotation; and at least two blades that are mounted on the hub assembly, each blade including a leading edge and a trailing edge, the blades being oriented so that the respective leading edges face in a common rotational direction, and each blade including: a straight section that is substantially parallel to the axis of rotation; and characterized in that each blade further includes two helical sections, the straight section being interposed between the helical sections, and the helical sections extending at least partially around the axis of rotation. a rotatable hub assembly that is configured to be connected to an energy sink and rotatable about an axis of rotation; and at least two blades that are mounted on the hub assembly, each blade including a leading edge and a trailing edge, the blades being oriented so that the respective leading edges face in a common rotational direction, and each blade including: a straight section that is substantially parallel to the axis of rotation; and characterized in that each blade further includes two helical sections, the straight section being interposed between the helical sections, and the helical sections extending at least partially around the axis of rotation. a straight section that is substantially parallel to the axis of rotation; and characterized in that each blade further includes two helical sections, the straight section being interposed between the helical sections, and the helical sections extending at least partially around the axis of rotation.
A control device for controlling tomosynthesis imaging for obtaining a tomosynthesis image from a projected image group captured by irradiating an object with X-rays from a plurality of different angles by using an X-ray generation unit and an X-ray detection unit, the control device comprising: a communication circuit that is adapted for transmitting at least either of the tomosynthesis image and the projected image group to an external device (113, 114, 115, 116, 117); setting means for setting at least one of the projected images of the projected image group as a reject; and output control means for limiting transmission of the data set as a reject to the external device (113, 114, 115, 116, 117), characterised in that the setting means is adapted to set the tomosynthesis image, generated by reconstruction using the projected image group including at least one of the projected images set as the reject, as a reject. a communication circuit that is adapted for transmitting at least either of the tomosynthesis image and the projected image group to an external device (113, 114, 115, 116, 117); setting means for setting at least one of the projected images of the projected image group as a reject; and output control means for limiting transmission of the data set as a reject to the external device (113, 114, 115, 116, 117), characterised in that the setting means is adapted to set the tomosynthesis image, generated by reconstruction using the projected image group including at least one of the projected images set as the reject, as a reject.
A method for preparing cabazitaxel comprising the steps of: 1) reacting 10-deacetylbaccatin III of Chemical Formula 2 with a silylating agent in polar or nonpolar organic solvent in the presence of N,N-dimethylaminopyridine to obtain an intermediate of Chemical Formula 3 in which hydroxy group at the 7 position is protected by a silylated radical; 2) methylating hydroxy group at the 10 position of the intermediate of Chemical Formula 3 by the use of dimethyl sulfate to obtain an intermediate of Chemical Formula 4; 3) deprotecting hydroxy group at the 7 position of the intermediate of Chemical Formula 4 by the use of hydrochloric acid to obtain an intermediate of Chemical Formula 5; 4) methylating hydroxy group at the 7 position of the intermediate of Chemical Formula 5 by the use of dimethyl sulfate to obtain an intermediate of Chemical Formula 6; 5) esterifying hydroxy group at the 13 position of the intermediate of Chemical Formula 6 in the presence of oxazolidine acid derivative of Chemical Formula 8 to obtain an intermediate of Chemical Formula 7; and 6) treating the intermediate of Chemical Formula 7 with an acid to obtain cabazitaxel of Chemical Formula 1: wherein Ac represents acetyl group; Me represents methyl group; Ph represents phenyl group; and M represents a silylated radical. 1) reacting 10-deacetylbaccatin III of Chemical Formula 2 with a silylating agent in polar or nonpolar organic solvent in the presence of N,N-dimethylaminopyridine to obtain an intermediate of Chemical Formula 3 in which hydroxy group at the 7 position is protected by a silylated radical; 2) methylating hydroxy group at the 10 position of the intermediate of Chemical Formula 3 by the use of dimethyl sulfate to obtain an intermediate of Chemical Formula 4; 3) deprotecting hydroxy group at the 7 position of the intermediate of Chemical Formula 4 by the use of hydrochloric acid to obtain an intermediate of Chemical Formula 5; 4) methylating hydroxy group at the 7 position of the intermediate of Chemical Formula 5 by the use of dimethyl sulfate to obtain an intermediate of Chemical Formula 6; 5) esterifying hydroxy group at the 13 position of the intermediate of Chemical Formula 6 in the presence of oxazolidine acid derivative of Chemical Formula 8 to obtain an intermediate of Chemical Formula 7; and 6) treating the intermediate of Chemical Formula 7 with an acid to obtain cabazitaxel of Chemical Formula 1: wherein Ac represents acetyl group; Me represents methyl group; Ph represents phenyl group; and M represents a silylated radical. Ac represents acetyl group; Me represents methyl group; Ph represents phenyl group; and M represents a silylated radical.
A proximity warning system for a helicopter, the helicopter comprising a roof top structure, a main rotor and a main rotor head, and the proximity warning system comprising a standard torus-shaped housing and at least two radar units arranged to transmit microwaves and receive reflections of said microwaves from obstacles, wherein the at least two radar units are integrated into the standard torus-shaped housing, said standard torus-shaped housing being mountable on a non-rotating standpipe on top of the main rotor head or, alternatively, fixable below the main rotor head on the roof top structure of the helicopter for horizontally scanning an entire environment of 360° around the helicopter, the standard torus-shaped housing being able to open and being constructed with a joint and a closure for easy installation or de-installation of the radar units
A speaker system comprising: a speaker housing having a first set of at least one primary radial X axis, a second set of at least one primary radial Y axis perpendicular to a respective primary X axis of the first set, and a primary longitudinal Z axis perpendicular to the first set of at least one primary radial X axis and the second set of at least one primary radial Y axis, wherein a cross-section of the housing along a single plane is one of: a circular shape and an ellipsoidal shape with a distinct length along the primary X axis than along the primary Y axis; and a microphone array contained within the speaker housing, the microphone array having a set of microphones positioned in said, single plane.wherein said single plane is perpendicular to the primary Z axis and axially asymmetric with respect to all the primary X axes of the first set and the primary Y axes of the second set. a speaker housing having a first set of at least one primary radial X axis, a second set of at least one primary radial Y axis perpendicular to a respective primary X axis of the first set, and a primary longitudinal Z axis perpendicular to the first set of at least one primary radial X axis and the second set of at least one primary radial Y axis, wherein a cross-section of the housing along a single plane is one of: a circular shape and an ellipsoidal shape with a distinct length along the primary X axis than along the primary Y axis; and a microphone array contained within the speaker housing, the microphone array having a set of microphones positioned in said, single plane.wherein said single plane is perpendicular to the primary Z axis and axially asymmetric with respect to all the primary X axes of the first set and the primary Y axes of the second set.
Cooking machine of the type comprising an outer casing, within which there is housed a container for foodstuffs to be cooked and a source of hot air transportable in the direction of said foodstuffs, such casing being closed at its upper part by a lid, associated with such lid there are provided means for the generation of a hot airflow in the direction of the foodstuffs arranged in the container comprising at least an upper heating element, at least a fan actuated by a motor adapted to generate an airflow heated by said heating element, and a duct for conveying air, adapted to direct the hot airflow downwards in a direction substantially perpendicular to the plane on which the foodstuffs are arranged in the container, a duct for distributing the cooling air which surrounds such motor adapted to collect cold air from outside through holes obtained on such lid and to direct it downwards around such motor and to distribute it radially and to eject it towards an edge through air intakes provided laterally on the lid, characterised in that such distribution duct has a variable diameter and in particular it has an upper frustoconical portion whose opening faces a central dome in the area having such holes, beneath such frustoconical portion the duct has a substantially cylindrical-shaped central portion, the diameter of such portion being selected so as to create a suitable space between it and the body of the motor for the descending air flow, the duct further comprising a lower portion which has a flaring directed upwards so as to facilitate the upward radial ejection of the cooling airflow.
A latent heat storage unit for an exhaust system of a combustion engine, in particular of a motor vehicle, - with at least one storage plate having two plate bodies (3, 4) lying on top of one another, enclosing a storage space filled with heat storage material, each comprising a wave structure (5, 6), - wherein the wave structure of the one plate body runs inclined relative to the wave structure of the other plate body, - wherein at least two storage plates are provided, which for forming a plate stack are arranged on top of each other, - wherein between adjacent storage plates a flow path is formed, - wherein the respective flow path is laterally delimited through side walls, which extend along the plate stack, - wherein the side walls each extend from an open inlet of the flow path as far as to an open outlet of the flow path, characterized in - that inlet and outlet are opposing each other in a longitudinal axis, - that the side walls extend parallel to the longitudinal axis and are opposing each other transversly to the longitudinal axis, and - that the side walls are formed through angled-off lateral rims of the storage plates overlapping one another. - with at least one storage plate having two plate bodies (3, 4) lying on top of one another, enclosing a storage space filled with heat storage material, each comprising a wave structure (5, 6), - wherein the wave structure of the one plate body runs inclined relative to the wave structure of the other plate body, - wherein at least two storage plates are provided, which for forming a plate stack are arranged on top of each other, - wherein between adjacent storage plates a flow path is formed, - wherein the respective flow path is laterally delimited through side walls, which extend along the plate stack, - wherein the side walls each extend from an open inlet of the flow path as far as to an open outlet of the flow path, - that inlet and outlet are opposing each other in a longitudinal axis, - that the side walls extend parallel to the longitudinal axis and are opposing each other transversly to the longitudinal axis, and - that the side walls are formed through angled-off lateral rims of the storage plates overlapping one another.
Packaging unit for the transport and/or storage of at least one organic peroxide comprising (i) a transport and/or storage container consisting of an outer container and at least one inner container filled with the at least one organic peroxide; and (ii) at least one bag and/or bottle filled with an extinguishing agent, wherein the at least one bag and/or the at least one bottle is separately introduced into the receiving area of the outer container and/or into the at least one inner container of the transport and/or storage container and is detachably connected or not connected to the outer container and to the inner container filled with peroxide. (i) a transport and/or storage container consisting of an outer container and at least one inner container filled with the at least one organic peroxide; and (ii) at least one bag and/or bottle filled with an extinguishing agent,
A cell transplantation kit comprising: a first sac-shaped structure consisting of a membrane having pores of an average pore diameter of 0.2 mm or less; a plurality of second sac-shaped structures having an average long diameter larger than the average pore diameter of the pores of the first sac-shaped structure; and a cell structure including a polymer block having biocompatibility and cells, wherein the plurality of second sac-shaped structures are provided for incorporation into the first sac-shaped structure, at least a part of the plurality of second sac-shaped structures contain cells, in the cell structure, a plurality of the polymer blocks is arranged in a gap between a plurality of the cells, and the cell structure is provided inside of the first sac-shaped structure. a first sac-shaped structure consisting of a membrane having pores of an average pore diameter of 0.2 mm or less; a plurality of second sac-shaped structures having an average long diameter larger than the average pore diameter of the pores of the first sac-shaped structure; and a cell structure including a polymer block having biocompatibility and cells, wherein the plurality of second sac-shaped structures are provided for incorporation into the first sac-shaped structure, at least a part of the plurality of second sac-shaped structures contain cells, in the cell structure, a plurality of the polymer blocks is arranged in a gap between a plurality of the cells, and the cell structure is provided inside of the first sac-shaped structure.
A gas turbine engine comprising: a compressor section which includes a high pressure compressor and a low pressure compressor; a low spool; a fan, said fan is driven with said low pressure compressor by said low spool, and there being a gear reduction between said fan and said low spool; said fan delivering air into said compressor section and into a bypass duct having a variable area nozzle, and said compressor section compressing air and delivering it into a combustion section; the combustion section mixing air with fuel, igniting the fuel, and driving the products of the combustion across turbine rotors, said turbine rotors including a low turbine rotor driving said low spool and said low pressure compressor; a control for said gas turbine engine, programmed to position said nozzle at startup of the engine to increase airflow across said fan; characterized in that: said control includes stored desired positions for said nozzle to provide increased airflow into the compressor section at startup at various conditions, said various conditions including the altitude of an aircraft carrying the gas turbine engine, an air speed of the aircraft and a speed of the low spool. a compressor section which includes a high pressure compressor and a low pressure compressor; a low spool; a fan, said fan is driven with said low pressure compressor by said low spool, and there being a gear reduction between said fan and said low spool; said fan delivering air into said compressor section and into a bypass duct having a variable area nozzle, and said compressor section compressing air and delivering it into a combustion section; the combustion section mixing air with fuel, igniting the fuel, and driving the products of the combustion across turbine rotors, said turbine rotors including a low turbine rotor driving said low spool and said low pressure compressor; a control for said gas turbine engine, programmed to position said nozzle at startup of the engine to increase airflow across said fan; characterized in that: said control includes stored desired positions for said nozzle to provide increased airflow into the compressor section at startup at various conditions, said various conditions including the altitude of an aircraft carrying the gas turbine engine, an air speed of the aircraft and a speed of the low spool.
Household appliance comprising a mist circuit for conducting an ozone-containing mist with mist droplets and an ozone chamber, which comprises an ozone converter for generating ozone, wherein the household appliance comprises a duct for connecting the mist circuit to the ozone chamber, characterised in that the duct comprises a separation facility for separating the mist droplets.
A method for estimating a center of mass of an aircraft via a shock strut system comprising: receiving, by a processor, a first gas pressure of a first shock strut from a takeoff phase to a landing phase of the aircraft from a first gas pressure sensor; receiving, by the processor, a second gas pressure of a second shock strut from the takeoff phase to the landing phase of the aircraft from a second gas pressure sensor; receiving, by the processor, a third gas pressure of a third shock strut from the takeoff phase to the landing phase of the aircraft from a third gas pressure sensor; determining, by the processor, the center of mass of the aircraft based on the first gas pressure, the second gas pressure, the third gas pressure, a wheel tread distance along a wheel tread axis, and a wheelbase distance along a wheelbase axis; and transmitting, by the processor, the center of mass of the aircraft to a device; and wherein the takeoff phase includes a vertical takeoff, the landing phase includes a vertical landing, and the takeoff phase to landing phase occurs within a predetermined period of time. receiving, by a processor, a first gas pressure of a first shock strut from a takeoff phase to a landing phase of the aircraft from a first gas pressure sensor; receiving, by the processor, a second gas pressure of a second shock strut from the takeoff phase to the landing phase of the aircraft from a second gas pressure sensor; receiving, by the processor, a third gas pressure of a third shock strut from the takeoff phase to the landing phase of the aircraft from a third gas pressure sensor; determining, by the processor, the center of mass of the aircraft based on the first gas pressure, the second gas pressure, the third gas pressure, a wheel tread distance along a wheel tread axis, and a wheelbase distance along a wheelbase axis; and transmitting, by the processor, the center of mass of the aircraft to a device; and wherein the takeoff phase includes a vertical takeoff, the landing phase includes a vertical landing, and the takeoff phase to landing phase occurs within a predetermined period of time.