mhurhangee/ep-ind-claims huggingface dataset:
A composition for sustained, targeted or sustained and targeted delivery of an active ingredient consisting of: • a complex formed between an uncrosslinked carboxyl substituted polymer chosen from a carboxyl substituted starch, a carboxyl substituted cellulose, a carboxyl substituted polyvinyl alcohol, a pectin, an alginate, or combinations thereof, and a lipid comprising a phospholipid chosen from phosphatidylcholine, phosphatidylethanolamine or combinations thereof. • a complex formed between an uncrosslinked carboxyl substituted polymer chosen from a carboxyl substituted starch, a carboxyl substituted cellulose, a carboxyl substituted polyvinyl alcohol, a pectin, an alginate, or combinations thereof, and a lipid comprising a phospholipid chosen from phosphatidylcholine, phosphatidylethanolamine or combinations thereof.
Light source assembly, comprising: a substrate comprising first and second substrate portions (14a, 14b) being arranged at a tilt angle (α) to each other forming a V-shaped structure, wherein, at the tip of the V-shaped structure, the first substrate portion comprises a first electrical terminal and the second substrate portion comprises a second electrical terminal; characterized in that, a light source is arranged to bridge a terminal gap between the first and second electrical terminals (16a, 16b) such that the light source is in electrical connection with the first and second electrical terminals (16a, 16b). a substrate comprising first and second substrate portions (14a, 14b) being arranged at a tilt angle (α) to each other forming a V-shaped structure, wherein, at the tip of the V-shaped structure, the first substrate portion comprises a first electrical terminal and the second substrate portion comprises a second electrical terminal; characterized in that, a light source is arranged to bridge a terminal gap between the first and second electrical terminals (16a, 16b) such that the light source is in electrical connection with the first and second electrical terminals (16a, 16b).
A crystalline form of Compound I having the formula wherein the crystalline form is: a. Form A 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 4.32, 6.07, 8.55, 12.07 and 15.37 ± 0.2 degrees 2-theta; or a. Form HC 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 8.36,8.71, 16.69, 17.39 and 24.59± 0.2 degrees 2-theta; or b. Form HD 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 7.60, 8.99 and 15.16 ± 0.2 degrees 2-theta; or a mixture thereof. a. Form A 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 4.32, 6.07, 8.55, 12.07 and 15.37 ± 0.2 degrees 2-theta; or a. Form A 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 4.32, 6.07, 8.55, 12.07 and 15.37 ± 0.2 degrees 2-theta; or a. Form HC 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 8.36,8.71, 16.69, 17.39 and 24.59± 0.2 degrees 2-theta; or b. Form HD 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 7.60, 8.99 and 15.16 ± 0.2 degrees 2-theta; or a mixture thereof. a. Form HC 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 8.36,8.71, 16.69, 17.39 and 24.59± 0.2 degrees 2-theta; or b. Form HD 0 which is characterized by an X-ray powder diffraction pattern comprising one or more of the following peaks: 7.60, 8.99 and 15.16 ± 0.2 degrees 2-theta; or a mixture thereof.
A method for preparing amorphous silibinin comprising the following steps: A.) extracting silibinin with a solvent having moderate polarity, B.) separating the solvent phase from solid residues, C.) concentrating the solvent phase at a temperature of less than 60 °C, D.) combining the concentrate obtained in step C.) with ethanol or a protic solvent having a dipole moment of less than 2 Debye and then combining it with hexane, concentrating the mixture, and removing the hexane phase, E.) concentrating the residue obtained in step D.), F.) separating the solid phase, G.) combining the solid phase obtained in step F.) with ethanol or a protic solvent having a dipole moment of less than 2 Debye, H.) adding activated charcoal, I.) separating the charcoal from the liquid phase, concentrating the liquid and crystallizing silibinin therefrom, J.) separating the crystals obtained in step I.) from the liquid phase, and if required, repeating steps G.), I.), J.) in order to enrich silibinin to a content of more than 95 % by weight, K.) optionally, filtrating, washing, drying and, if required, repeating these steps, L.) combining the material obtained in step K.) with anhydrous alcohol, refluxing, cooling and concentrating, M.) drying, milling, and homogenizing the obtained amorphous-like fine powder; wherein the starting material is milk thistle or a part thereof. A.) extracting silibinin with a solvent having moderate polarity, B.) separating the solvent phase from solid residues, C.) concentrating the solvent phase at a temperature of less than 60 °C, D.) combining the concentrate obtained in step C.) with ethanol or a protic solvent having a dipole moment of less than 2 Debye and then combining it with hexane, concentrating the mixture, and removing the hexane phase, E.) concentrating the residue obtained in step D.), F.) separating the solid phase, G.) combining the solid phase obtained in step F.) with ethanol or a protic solvent having a dipole moment of less than 2 Debye, H.) adding activated charcoal, I.) separating the charcoal from the liquid phase, concentrating the liquid and crystallizing silibinin therefrom, J.) separating the crystals obtained in step I.) from the liquid phase, and if required, repeating steps G.), I.), J.) in order to enrich silibinin to a content of more than 95 % by weight, K.) optionally, filtrating, washing, drying and, if required, repeating these steps, L.) combining the material obtained in step K.) with anhydrous alcohol, refluxing, cooling and concentrating, M.) drying, milling, and homogenizing the obtained amorphous-like fine powder; wherein the starting material is milk thistle or a part thereof.
An integrated circuit device comprising at least one cut-through forwarding module being adapted to forward a data frame before the whole frame has been received, the cut-through forwarding module comprising: at least one receiver component arranged to receive data to be forwarded, and to generate a request for transmission of a block of data upon receipt thereof; and at least one controller unit arranged to execute at least one thread (225, 310, 320, 330, 340, 350) for processing requests generated by the at least one receiver component, characterised in that the at least one controller unit is arranged to set a priority context for the at least one thread (225, 310, 320, 330, 340, 350), and to schedule an execution of the at least one thread based at least partly on the priority context therefor. at least one receiver component arranged to receive data to be forwarded, and to generate a request for transmission of a block of data upon receipt thereof; and at least one controller unit arranged to execute at least one thread (225, 310, 320, 330, 340, 350) for processing requests generated by the at least one receiver component, characterised in that the at least one controller unit is arranged to set a priority context for the at least one thread (225, 310, 320, 330, 340, 350), and to schedule an execution of the at least one thread based at least partly on the priority context therefor.
A spherical assembly for vehicle propulsion, comprising: a spherical encasing; a first motor connected to a first weight and the spherical encasing; a second motor connected to a second weight and the spherical encasing; and a controller, operatively coupled to the first motor and to the second motor, and configured to: cause the first motor to rotate the first weight in a first direction at a first rotational speed based on a rotational speed of the spherical assembly; and cause the second motor to rotate the second weight in a second direction at a second rotational speed based on the rotational speed of the spherical assembly; wherein the spherical assembly is configured to be propelled by a moment of gravitational force due to the rotation of the first weight and/or the second weight; characterized in that each of the first weight and the second weight includes a planar surface, and the planar surfaces are tilted and mirrored with respect to a vertical center axial line of the spherical assembly. a spherical encasing; a first motor connected to a first weight and the spherical encasing; a second motor connected to a second weight and the spherical encasing; and a controller, operatively coupled to the first motor and to the second motor, and configured to: cause the first motor to rotate the first weight in a first direction at a first rotational speed based on a rotational speed of the spherical assembly; and cause the second motor to rotate the second weight in a second direction at a second rotational speed based on the rotational speed of the spherical assembly; cause the first motor to rotate the first weight in a first direction at a first rotational speed based on a rotational speed of the spherical assembly; and cause the second motor to rotate the second weight in a second direction at a second rotational speed based on the rotational speed of the spherical assembly; wherein the spherical assembly is configured to be propelled by a moment of gravitational force due to the rotation of the first weight and/or the second weight; characterized in that each of the first weight and the second weight includes a planar surface, and the planar surfaces are tilted and mirrored with respect to a vertical center axial line of the spherical assembly.
A rotor system of an aircraft, which is drivable to rotate to thereby generate lift and thrust for the aircraft, the rotor system comprising: a hub; rotor blades extending outwardly from the hub; an actuation system comprising electro-mechanical actuators respectively disposed between the hub and each of the rotor blades, each electro-mechanical actuator comprising a rotary inductive device; a gear train associated with each electro-mechanical actuator and the corresponding rotary inductive device to convert linear displacements of a piston responsive to rotor blade lead/lag into rotation of the rotary inductive device; and a controller that is configured to control the rotary inductive device to operate, in a first mode, as a motor which drives the gear train, and, in a second mode, as a generator which is driven by the gear train. a hub; rotor blades extending outwardly from the hub; an actuation system comprising electro-mechanical actuators respectively disposed between the hub and each of the rotor blades, each electro-mechanical actuator comprising a rotary inductive device; a gear train associated with each electro-mechanical actuator and the corresponding rotary inductive device to convert linear displacements of a piston responsive to rotor blade lead/lag into rotation of the rotary inductive device; and a controller that is configured to control the rotary inductive device to operate, in a first mode, as a motor which drives the gear train, and, in a second mode, as a generator which is driven by the gear train.
A pneumatic tire comprising: a pair of sidewall portions, wherein a first region having a first surface, and a second region having a second surface that projects or is recessed relative to the first surface in a sidewall portion thickness direction, are formed on a surface of at least one of the pair of sidewall portions, a projection-recess portion is formed on the second surface, a height of the projection-recess portion is less than a relative distance in the sidewall portion thickness direction between the first surface and the second surface, the first surface is smoother than the second surface, and the first region and the second region alternate in a tire circumferential direction and a tire radial direction, characterized in that the second region includes a first edge extending in the tire circumferential direction, and a second edge extending in the tire circumferential direction in a portion located outward of the first edge in the tire radial direction, and the second region has a rectangular shape or the second region has a trapezoidal shape in which the first edge and the second edge are parallel to each other and a length of the second edge is greater than a length of the first edge. a pair of sidewall portions, wherein a first region having a first surface, and a second region having a second surface that projects or is recessed relative to the first surface in a sidewall portion thickness direction, are formed on a surface of at least one of the pair of sidewall portions, a projection-recess portion is formed on the second surface, a height of the projection-recess portion is less than a relative distance in the sidewall portion thickness direction between the first surface and the second surface, the first surface is smoother than the second surface, and the first region and the second region alternate in a tire circumferential direction and a tire radial direction, characterized in that the second region includes a first edge extending in the tire circumferential direction, and a second edge extending in the tire circumferential direction in a portion located outward of the first edge in the tire radial direction, and the second region has a rectangular shape or the second region has a trapezoidal shape in which the first edge and the second edge are parallel to each other and a length of the second edge is greater than a length of the first edge.
A control for a liquid heating vessel comprising a moulded plastics unit which houses at least one switch for controlling a supply of electrical power to the liquid heating vessel, and a generally planar metal mount plate attached to the moulded plastics unit, wherein the metal mount plate comprises one or more holes (16a, 16b, 16c) allowing the metal mount plate to be fastened to a base of a liquid heating vessel, wherein the metal mount plate further comprises a metal tab arranged to attach the mount plate to the moulded plastics unit, characterised in that the metal tab comprising a pillar that is bent at its base out of the plane of the mount plate and the pillar comprising an arm (24a, 24b) extending substantially parallel to the mount plate in the same plane as the pillar, and in that the moulded plastics unit comprises a rest (26a, 26b) positioned to receive the arm (24a, 24b) of the metal tab, and in that the mount plate is plastically deformed next to the metal tab so as to form a stiffened shape at the base of the pillar that creates a tensile force acting along the pillar so that the arm (24a, 24b) pulls down on the rest (26a, 26b) in the plane of the pillar and the metal tab is therefore held in tension to attach the mount plate to the moulded plastics unit.
A method for operating a communication system comprising at least one speech or multimodal controlled dialogue system, the method comprising the steps of: using a classifier for determining the level of expertise of a specific user accessing the dialogue system, based on user specific data remotely retrieved from a storage area, said storage area being accessible by a plurality of different speech or multimodal controlled dialogue systems, adapting a dialogue of said dialogue system with said specific user to said level of expertise, characterized in that said classifier uses Hidden Markov Models for determining said level of expertise, said Hidden Markov Models comprise some visible states that correspond to said levels of expertise and some hidden states that are used internally only. using a classifier for determining the level of expertise of a specific user accessing the dialogue system, based on user specific data remotely retrieved from a storage area, said storage area being accessible by a plurality of different speech or multimodal controlled dialogue systems, adapting a dialogue of said dialogue system with said specific user to said level of expertise, characterized in that said classifier uses Hidden Markov Models for determining said level of expertise, said Hidden Markov Models comprise some visible states that correspond to said levels of expertise and some hidden states that are used internally only.
A curable precursor of a structural adhesive composition, comprising: a) a cationically self-polymerizable monomer; b) a polymerization initiator of the cationically self-polymerizable monomer which is initiated at a temperature T1; c) a curable monomer which is different from the cationically self-polymerizable monomer; and d) a curing initiator of the curable monomer which is initiated at a temperature T2 and which is different from the polymerization initiator of the cationically self-polymerizable monomer; wherein the cationically self-polymerizable monomer is a polyfunctional compound comprising at least one cyclic amine; and wherein the curable monomer which is different from the cationically self-polymerizable monomer comprises at least one functional group selected from the group consisting of epoxy groups. a) a cationically self-polymerizable monomer; b) a polymerization initiator of the cationically self-polymerizable monomer which is initiated at a temperature T1; c) a curable monomer which is different from the cationically self-polymerizable monomer; and d) a curing initiator of the curable monomer which is initiated at a temperature T2 and which is different from the polymerization initiator of the cationically self-polymerizable monomer;
An in vitro method of inducing the differentiation of stem cells into erythroid cells, said method comprising the step of contacting stem cells with Wnt3A, Activin A, a GSK3 inhibitor and a phosphodiesterase inhibitor, wherein the stem cells are induced pluripotent stem cells (iPS) and/or stem cells obtained without destruction of a human embryo.
Light-emitting diode module which is suitable as an LED light source for on-board electrical systems in the aeronautical field, comprising a housing (31, 41), at least one light-emitting diode, and at least one printed circuit board (10a, 10b), wherein the printed circuit board is connected to the at least one light-emitting diode and comprises an LED driver, a control module and a circuit arrangement, wherein the LED driver provides a constant operating point in V-I characteristics for operation of the light-emitting diode controlled by the control module, and wherein the circuit arrangement comprises a DC/DC converter, characterised in that the DC/DC converter is an integrated down-converter module, wherein the circuit arrangement further comprises a bypass connected in parallel with the integrated down-converter module, the bypass being activatable by a comparator circuit, wherein the comparator circuit is configured to detect the level of an input voltage applied to the circuit arrangement, to activate the bypass when the level is below a threshold value, and to deactivate the bypass when the level exceeds the threshold value.
A spindle drive, in particular for a linear actuator, comprising - a spindle, - a spindle nut which interacts with the spindle, and - a lubricating channel outlet for lubricating the spindle and the spindle nut the spindle drive further comprising - a stationary channel system, - a rotatable channel system connected to the stationary channel system for feeding lubricant to the lubricating channel outlet, wherein the rotatable channel system is arranged at least partially in the spindle or in a hollow-shaft rotor of the spindle drive and comprises a longitudinal channel arranged in the spindle or in the hollow-shaft rotor, at least one radial lubricating channel connected to the longitudinal channel for supplying the longitudinal channel with lubricant, and second radial lubricating channels comprising lubricating channel outlets, and - a transfer space arranged between the stationary channel system and the rotatable channel system, wherein the transfer space is of annular configuration and is sealed by shaft seals. - a spindle, - a spindle nut which interacts with the spindle, and - a lubricating channel outlet for lubricating the spindle and the spindle nut the spindle drive further comprising - a stationary channel system, - a rotatable channel system connected to the stationary channel system for feeding lubricant to the lubricating channel outlet, wherein the rotatable channel system is arranged at least partially in the spindle or in a hollow-shaft rotor of the spindle drive and comprises a longitudinal channel arranged in the spindle or in the hollow-shaft rotor, at least one radial lubricating channel connected to the longitudinal channel for supplying the longitudinal channel with lubricant, and second radial lubricating channels comprising lubricating channel outlets, and - a transfer space arranged between the stationary channel system and the rotatable channel system, wherein the transfer space is of annular configuration and is sealed by shaft seals.
Device for heating a heat transfer medium for in particular laundry machines, with a burner which is assigned a heating pipe fired from the inside, and at least one heat exchanger (20, 40, 44, 48, 55, 56, 63) which has at least one flow channel (34, 41, 45, 49) for the heat transfer medium, wherein the heating pipe generates thermal radiation which acts on the heat exchanger (20, 40, 44, 48, 56, 63), wherein the heating pipe which is arranged in a cylinder space enclosed by the at least one cylindrically designed heat exchanger (20, 40, 44, 48, 55, 56, 63), and is fired from the inside by the burner is designed for outputting infrared radiation which is directed radially outwards to the at least one heat exchanger (20, 40, 44, 48, 56, 63), characterized in that the at least one heat exchanger is double-walled, in that the heating pipe has a perforated or lattice-like supporting pipe and at least one incandescent mantle composed of a heat-resistant woven fabric, braided fabric and/or mesh, wherein the at least one incandescent mantle surrounds the supporting pipe from the outside, and in that the at least one heat exchanger (20, 40, 44, 48, 55, 56) has a cylindrical inner wall and a cylindrical outer wall, which form heat exchanger surfaces for supply energy on both sides to the at least one heat exchanger (20, 40, 44, 48, 55, 56), wherein longitudinal edges of the two walls of the at least one cylindrical heat exchanger (20, 40, 44, 48, 55, 56) are connected by at least one longitudinal weld seam (39, 61) in order to form part of the at least one flow channel (34, 41, 45, 49) by means of the at least one longitudinal weld seam (39, 61).