mhurhangee/ep-ind-claims huggingface dataset:
A liquid nanoemulsion concentrate, comprising: a) a mixture of one or more sucrose fatty acid esters or a mixture of the sucrose fatty acid esters and a PEG-derivative of Vitamin E, wherein: the total amount of sucrose fatty acids esters or mixture of the sucrose fatty acid esters and a PEG-derivative of Vitamin E is between 16 % and 30 %, by weight, or 17 % and 29 %, by weight, of the concentrate; a nanoemulsion is an emulsion in which the particle size of the dispersed droplets is less than 1000 nm; and the concentrate contains at least 1% sucrose fatty acid ester or mixtures thereof, which increases miscibility with the polar solvent compared to the absence of the sucrose fatty acid ester; b) a polar solvent in an amount between 60 % and 79 % by weight, of the concentrate; and c) a non-polar active ingredient selected from among any one or more of polyunsaturated fatty acids, omega-3 fatty acids, omega-6 fatty acids, conjugated fatty acids, Coenzyme Q10 compounds, vitamin D3 and phytosterols in an amount between 5 % and 10 %, by weight, of the concentrate a) a mixture of one or more sucrose fatty acid esters or a mixture of the sucrose fatty acid esters and a PEG-derivative of Vitamin E, wherein: the total amount of sucrose fatty acids esters or mixture of the sucrose fatty acid esters and a PEG-derivative of Vitamin E is between 16 % and 30 %, by weight, or 17 % and 29 %, by weight, of the concentrate; a nanoemulsion is an emulsion in which the particle size of the dispersed droplets is less than 1000 nm; and the concentrate contains at least 1% sucrose fatty acid ester or mixtures thereof, which increases miscibility with the polar solvent compared to the absence of the sucrose fatty acid ester; the total amount of sucrose fatty acids esters or mixture of the sucrose fatty acid esters and a PEG-derivative of Vitamin E is between 16 % and 30 %, by weight, or 17 % and 29 %, by weight, of the concentrate; a nanoemulsion is an emulsion in which the particle size of the dispersed droplets is less than 1000 nm; and the concentrate contains at least 1% sucrose fatty acid ester or mixtures thereof, which increases miscibility with the polar solvent compared to the absence of the sucrose fatty acid ester; b) a polar solvent in an amount between 60 % and 79 % by weight, of the concentrate; and c) a non-polar active ingredient selected from among any one or more of polyunsaturated fatty acids, omega-3 fatty acids, omega-6 fatty acids, conjugated fatty acids, Coenzyme Q10 compounds, vitamin D3 and phytosterols in an amount between 5 % and 10 %, by weight, of the concentrate
A continuous mixer for continuously mixing a material, comprising: a barrel with a hollow interior; and a pair of mixing rotors which are housed in the barrel and rotate in mutually different directions, each of the mixing rotors including a mixing portion with a plurality of mixing flights formed about an axial center of the mixing rotor and projecting radially outward, wherein: both of the mixing rotors (2, 2) are arranged so as to make a center distance therebetween smaller than a rotation outer diameter of each of the mixing flights; and the continuous mixer has an inter-rotor clearance which is a smallest clearance between the mixing portions at each rotation phase of the mixing rotors in a cross section perpendicular to axial directions of both of the mixing rotors, characterized in that the inter-rotor clearance has a size equal to or smaller than 0.16-fold of an inner diameter (Db) of the barrel over a rotation region of 85% or more of one rotation of each of the mixing rotors. a barrel with a hollow interior; and a pair of mixing rotors which are housed in the barrel and rotate in mutually different directions, each of the mixing rotors including a mixing portion with a plurality of mixing flights formed about an axial center of the mixing rotor and projecting radially outward, wherein: both of the mixing rotors (2, 2) are arranged so as to make a center distance therebetween smaller than a rotation outer diameter of each of the mixing flights; and the continuous mixer has an inter-rotor clearance which is a smallest clearance between the mixing portions at each rotation phase of the mixing rotors in a cross section perpendicular to axial directions of both of the mixing rotors, characterized in that the inter-rotor clearance has a size equal to or smaller than 0.16-fold of an inner diameter (Db) of the barrel over a rotation region of 85% or more of one rotation of each of the mixing rotors. both of the mixing rotors (2, 2) are arranged so as to make a center distance therebetween smaller than a rotation outer diameter of each of the mixing flights; and the continuous mixer has an inter-rotor clearance which is a smallest clearance between the mixing portions at each rotation phase of the mixing rotors in a cross section perpendicular to axial directions of both of the mixing rotors, characterized in that the inter-rotor clearance has a size equal to or smaller than 0.16-fold of an inner diameter (Db) of the barrel over a rotation region of 85% or more of one rotation of each of the mixing rotors.
A beverage preparation device, comprising an extraction head (100/100a), the extraction head (100/100a) comprises a frame, a capsule holder (20/20a), a push plate (30/30a) and a closing mechanism (40/40a), the capsule holder (20/20a) is disposed on the frame, the push plate (30/30a) covers the capsule holder ((20/20a), a brewing chamber is formed between the push plate (30/30a) and the capsule holder (20/20a), and the closing mechanism (40/40a) is connected to the push plate (30/30a), wherein the closing mechanism (40/40a) comprises a flap, a crank, a connecting assembly, and a push shaft fixedly connected to the push plate (30/30a), the crank is disposed on the flap, the connecting assembly is rotatably connected to the crank, and when the flap is moved, the push shaft moves relative to the capsule holder (20/20a), to seal or open the brewing chamber; characterized in that the push plate (30/30a) comprises at least one lancet (32/32a) extending into the brewing chamber, and the at least one lancet (32/32a) is configured to pierce a capsule located in the brewing chamber; the extraction head (100/100a) further comprises a propulsion compensation mechanism, the propulsion compensation mechanism is configured to push the push plate (30/30a) on the capsule holder (20/20a), the propulsion compensation mechanism comprises a first housing and a second housing, the first housing is extended upward from a side of the push plate (30/30a) which is away from the capsule holder (20/20a), the second housing covers the first housing and is connected to the push plate (30/30a), the first housing and the second housing form a sealed chamber, a water inlet is disposed on the second housing and configured for connecting to a water injection pipe, the at least one lancet (32/32a) passes through the first housing and extends towards the capsule holder (20/20a), the first housing further comprises an unidirectional pressure-holding seal assembly which is disposed in a connecting passage between the lancet (32/32a) and the sealed chamber, and the unidirectional pressure-maintaining seal assembly is configured for one-way water injection to the connecting passage and maintaining pressure
A data processing apparatus for communicating data bits via a predetermined number of sub-carrier signals of an Orthogonal Frequency Division Multiplexed OFDM symbol, the data processing apparatus comprising a parity interleaver (22, 23) operable to perform parity interleaving on a Low Density Parity Check LDPC encoded data bits obtained by LDPC encoding the data bits according to a parity check matrix of an LDPC code, which includes a parity matrix corresponding to parity bits of an LDPC code, the parity matrix having a stepwise structure, so that a parity bit of the LDPC encoded data bits is interleaved to a different parity bit position, a mapping unit for mapping the parity interleaved bits onto data symbols corresponding to modulation symbols of a modulation scheme of the OFDM sub-carrier signals, a symbol interleaver arranged in operation to read-into a symbol interleaver memory the predetermined number of data symbols for mapping onto the OFDM sub-carrier signals, and to read-out of the symbol interleaver memory the data symbols for the OFDM sub-carriers to effect the mapping, the read-out being in a different order than the read-in, the order being determined from a set of addresses, with the effect that the data symbols are interleaved on the sub-carriers signals of the OFDM symbol, an address generator operable to generate the set of addresses, an address being generated for each of the input symbols to indicate one of the sub-carrier signals onto which the data symbol is to be mapped, the address generator comprising a linear feedback shift register including a predetermined number of register stages and being operable to generate a pseudo-random bit sequence in accordance with a generator polynomial, a permutation circuit operable to receive the content of the shift register stages and to permute the bits present in the register stages in accordance with a permutation code to form an address of one of the OFDM sub-carriers, and a control unit operable in combination with an address check circuit to re-generate an address when a generated address exceeds a predetermined maximum valid address, wherein the predetermined maximum valid address is substantially four thousand and ninety six, the linear feedback shift register has eleven register stages with a generator polynomial for the linear feedback shift register of R i ʹ 10 = R i − 1 ʹ 0 ⊕ R i − 1 ʹ 2, and the permutation order forms an eleven bit address R i [ n] for the i-th data symbol from the bit present in the n-th register stage R i ʹ n in accordance with the table: R i ʹ n for n = 10 9 8 7 6 5 4 3 2 1 0 R ¡ [n]for n = 7 10 5 8 1 2 4 9 0 3 6
A method for environmental parameter mapping, comprising adding at least one entry to a mapping data structure and sending at least one command to a robotic device wherein the method further comprises determining a likelihood of observing a plurality of first measurements based on a plurality of second measurements at corresponding locations of a robotic device, wherein each of the plurality of first measurements is determined based on sensor signals captured by the robotic device, wherein each of the plurality of second measurements is stored in a mapping data structure with respect to the corresponding location of one of the plurality of first measurements; and determining whether each of the plurality of first measurements has a likelihood above a threshold; wherein each entry includes a position of a robotic device and at least one corresponding environmental parameter for the respective position of the robotic device, wherein each environmental parameter of each entry indicates an attribute of an environment at the corresponding position and is based on at least one sensor signal captured at the corresponding position, wherein the at least one entry is determined based on each first measurement having a likelihood above a threshold; and wherein the at least one command is determined based on the mapping data structure and includes at least one command to navigate. wherein the method further comprises determining a likelihood of observing a plurality of first measurements based on a plurality of second measurements at corresponding locations of a robotic device, wherein each of the plurality of first measurements is determined based on sensor signals captured by the robotic device, wherein each of the plurality of second measurements is stored in a mapping data structure with respect to the corresponding location of one of the plurality of first measurements; and determining whether each of the plurality of first measurements has a likelihood above a threshold; wherein each entry includes a position of a robotic device and at least one corresponding environmental parameter for the respective position of the robotic device, wherein each environmental parameter of each entry indicates an attribute of an environment at the corresponding position and is based on at least one sensor signal captured at the corresponding position, wherein the at least one entry is determined based on each first measurement having a likelihood above a threshold; and wherein the at least one command is determined based on the mapping data structure and includes at least one command to navigate.
A method of making a filling, the method comprising: heating the fat component to a temperature of 5.56 °C (10°F) to 11.11 °C (20°F) above the melting point of the fat component; combining the fat component with a sugar source and continuously mixing the fat component and the sugar source while maintaining the temperature 5.56 °C (10°F) to 11.11 °C (20°F) above the melting point of the fat component to form a slurry; introducing the slurry at a temperature 5.56 °C (10°F) to 11.11 °C (20°F) above the melting point of the fat component into a scraped-surface heat exchanger; cooling the slurry in the scraped surface heat exchanger at a cooling rate of about 3.89 °C/minute to about 40 °C/minute (about 7°F/minute to about 72°F/minute); and dispensing the slurry from the heat exchanger at a temperature effective to provide the filling, wherein the slurry includes about 20 to about 50 percent fat component and about 50 to about 80 percent sugar. heating the fat component to a temperature of 5.56 °C (10°F) to 11.11 °C (20°F) above the melting point of the fat component; combining the fat component with a sugar source and continuously mixing the fat component and the sugar source while maintaining the temperature 5.56 °C (10°F) to 11.11 °C (20°F) above the melting point of the fat component to form a slurry; introducing the slurry at a temperature 5.56 °C (10°F) to 11.11 °C (20°F) above the melting point of the fat component into a scraped-surface heat exchanger; cooling the slurry in the scraped surface heat exchanger at a cooling rate of about 3.89 °C/minute to about 40 °C/minute (about 7°F/minute to about 72°F/minute); and dispensing the slurry from the heat exchanger at a temperature effective to provide the filling, wherein the slurry includes about 20 to about 50 percent fat component and about 50 to about 80 percent sugar.
A shroud comprising a plenum and an opening to secure an area for airflow by rotation of an axial fan, wherein the plenum constitutes a frame of the shroud and is configured to be large enough to cover the fan, wherein that said shroud further comprises a slot formed on said plenum and wherein said opening is provided in a circular shape and said slot comprises an arc slot formed along a part of a circumference of said opening and wherein said shroud further comprises a rib formed on said plenum, and said slot further comprises a rib slot formed along said rib, characterized in that said slot comprises said arc slot and said rib slot such that one end of said arc slot is connected to one end of said rib slot.
A closing device for a door having an activatable privacy function for blocking access from a first side, including a controller on the first side that has a magnetic field sensor, including at least one permanent magnet (22, 23) on a second side facing away from the first side, and including a ferromagnetic securing element extending from the first side to the second side, wherein the permanent magnet (22, 23) is shiftable by means of a handle between a locking position that activates the privacy function and a release position that deactivates the privacy function, and wherein the securing element serves to transmit the magnetic field of the permanent magnet (22, 23) to the magnetic field sensor, so that the controller enables or blocks an actuation of the closing device from the first side as a function of the position of the permanent magnet (22, 23).
A system, comprising: a rotatable magnet; a first set of one or more Hall sensors; a second set of one or more Hall sensors; a third set of one or more Hall sensors; a processor configured to: receive, from the first set of one or more Hall sensors in a first component, a first measurement of the magnet; receive, from the second set of one or more Hall sensors in a second component, a second measurement associated with the magnet, wherein the first component and the second component are in a plane that is parallel to an axis of rotation associated with the magnet; receive, from the third set of one or more Hall sensors in a third component, a third measurement associated with the magnet, wherein the third component is in the same plane as the first component and the second component; generate (304, 802) an alpha value, a beta value, and a gamma value using a Clarke transform, the first measurement, the second measurement, and the third measurement; and determine (304, 804) an angle associated with the magnet, including by performing an atan2 function on the alpha value and the beta value. a rotatable magnet; a first set of one or more Hall sensors; a second set of one or more Hall sensors; a third set of one or more Hall sensors; a processor configured to: receive, from the first set of one or more Hall sensors in a first component, a first measurement of the magnet; receive, from the second set of one or more Hall sensors in a second component, a second measurement associated with the magnet, wherein the first component and the second component are in a plane that is parallel to an axis of rotation associated with the magnet; receive, from the third set of one or more Hall sensors in a third component, a third measurement associated with the magnet, wherein the third component is in the same plane as the first component and the second component; generate (304, 802) an alpha value, a beta value, and a gamma value using a Clarke transform, the first measurement, the second measurement, and the third measurement; and determine (304, 804) an angle associated with the magnet, including by performing an atan2 function on the alpha value and the beta value. receive, from the first set of one or more Hall sensors in a first component, a first measurement of the magnet; receive, from the second set of one or more Hall sensors in a second component, a second measurement associated with the magnet, wherein the first component and the second component are in a plane that is parallel to an axis of rotation associated with the magnet; receive, from the third set of one or more Hall sensors in a third component, a third measurement associated with the magnet, wherein the third component is in the same plane as the first component and the second component; generate (304, 802) an alpha value, a beta value, and a gamma value using a Clarke transform, the first measurement, the second measurement, and the third measurement; and determine (304, 804) an angle associated with the magnet, including by performing an atan2 function on the alpha value and the beta value.
One-piece door arrester made of plastics material, having a stop block and an attaching means for attaching the door arrester to a leaf of a door, the stop block being movably connected to the attaching means such that said attaching means can be brought into a stopping position in a gap between the door leaf and a floor in order to secure the door against pivoting in an opening or closing direction, the door arrester having a holder for releasably holding the stop block in an inoperative position in which the stop block does not enter the gap between the door leaf and the floor, characterised in that the door arrester has a living hinge as a joint, which hinge hingedly connects the stop block to the attaching means, such that the stop block can be moved from the stopping position into an inoperative position and vice versa.
An environmental defense shield for a turbine engine on an aircraft, the environmental defense shield comprising a plurality of aerodynamic vanes, wherein each of the aerodynamic vanes comprises a leading edge and a trailing edge wherein the leading edge and trailing edge are not equidistant at all points along the length of each of the plurality of aerodynamic vanes, and further wherein each of the plurality of aerodynamic vanes comprises a symmetrical airfoil cross-sectional shape, wherein the plurality of aerodynamic vanes are spaced apart sufficiently to allow air to enter the engine while mitigating the ingestion of objects into the engine, and wherein the arrangement of the plurality of aerodynamic vanes defines an internal plenum space upstream of the engine, each of the plurality of aerodynamic vanes further comprises: a. a forward end; b. a rearward end; c. a first section at the forward end wherein the trailing edge at the first section comprises an arcuate, concave shape wherein a perpendicular distance between the leading edge and the trailing edge of each of the plurality of aerodynamic vanes at the forward end is larger than at any other position on the first section; d. a second section between the forward end and the rearward end, wherein a perpendicular distance between the leading edge and the trailing edge at the first section is larger than a perpendicular distance between the leading edge and the trailing edge at the second section; and, e. a third section nearer the rearward end than the first and second sections wherein the trailing edge at the third section comprises an arcuate, convex shape wherein a perpendicular distance between the leading edge and the trailing edge at the rearward end is larger than a perpendicular distance at at least one other position on the third section. a. a forward end; b. a rearward end; c. a first section at the forward end wherein the trailing edge at the first section comprises an arcuate, concave shape wherein a perpendicular distance between the leading edge and the trailing edge of each of the plurality of aerodynamic vanes at the forward end is larger than at any other position on the first section; d. a second section between the forward end and the rearward end, wherein a perpendicular distance between the leading edge and the trailing edge at the first section is larger than a perpendicular distance between the leading edge and the trailing edge at the second section; and, e. a third section nearer the rearward end than the first and second sections wherein the trailing edge at the third section comprises an arcuate, convex shape wherein a perpendicular distance between the leading edge and the trailing edge at the rearward end is larger than a perpendicular distance at at least one other position on the third section.