mhurhangee/patent-ind-claim-en huggingface dataset:
An in-air sonar system for determining location and velocity information of objects (13-15) in an environment, the in-air sonar system comprising at least two emitters (111 1 -111 2 ) configured to emit respective sound signals (11 1 -11 2 ) into the environment, the respective sound signals having a low cross-correlation among each other; at least two receivers (112 1 ,112 2 ) configured to receive sound signals (12 1 ,12 2 ) from the environment; and a processing unit configured to perform: - obtaining, from the receivers (112 1 ,112 2 ), respective received sound signals (12 1 ,12 2 ) comprising the respective emitted sound signals reflected from objects (13-15) in the environment; - calculating , from the respective received sound signals (12 1 ,12 2 ), velocity-dependent range maps (211-218) for the respective emitted sound signals; the velocity-dependent range maps comprising information about the range and velocity of the respective objects; - deriving , from the calculated velocity-dependent range maps (211-218) and the spatial diversity of the at least two emitters and the at least two receivers, a velocity-dependent range-direction map comprising range information as a function of a received direction; - determining therefrom a location (321-323) of the respective objects (13-15); and - extracting , from the velocity-dependent range maps (211 - 218) and the spatial diversity of the at least two receivers, a velocity (341-343) of the respective objects based on the determined location (321-323). - obtaining, from the receivers (112 1 ,112 2 ), respective received sound signals (12 1 ,12 2 ) comprising the respective emitted sound signals reflected from objects (13-15) in the environment; - calculating , from the respective received sound signals (12 1 ,12 2 ), velocity-dependent range maps (211-218) for the respective emitted sound signals; the velocity-dependent range maps comprising information about the range and velocity of the respective objects; - deriving , from the calculated velocity-dependent range maps (211-218) and the spatial diversity of the at least two emitters and the at least two receivers, a velocity-dependent range-direction map comprising range information as a function of a received direction; - determining therefrom a location (321-323) of the respective objects (13-15); and - extracting , from the velocity-dependent range maps (211 - 218) and the spatial diversity of the at least two receivers, a velocity (341-343) of the respective objects based on the determined location (321-323).
A method for encoding audio signals and related spatial information into a reproduction layout-independent format, the method comprising: generating two groups of tracks comprising: assigning a first set of the audio signals containing audio needing highly directional localization into a first group and encoding the first group as a set of mono audio tracks with associated metadata describing the direction of origin of the signal of each track with respect to a recording position, and its initial playback time; assigning a second set of the audio signals containing audio for which localization provided by low order Ambisonics suffices into a second group and encoding the second group as at least one set of Ambisonics tracks of a given order and mixture of orders; wherein localization is a perceived spatial audio localization when the audio signals are reproduced, and characterized in that the method further comprises: encoding a direction angle accompanied with an angular width of a perceived sound image of a corresponding audio source associated to the tracks in the set of mono audio tracks. assigning a first set of the audio signals containing audio needing highly directional localization into a first group and encoding the first group as a set of mono audio tracks with associated metadata describing the direction of origin of the signal of each track with respect to a recording position, and its initial playback time; assigning a second set of the audio signals containing audio for which localization provided by low order Ambisonics suffices into a second group and encoding the second group as at least one set of Ambisonics tracks of a given order and mixture of orders; wherein localization is a perceived spatial audio localization when the audio signals are reproduced, and characterized in that the method further comprises: encoding a direction angle accompanied with an angular width of a perceived sound image of a corresponding audio source associated to the tracks in the set of mono audio tracks.
A cargo system for cargo platform, cargo cabinet or container, comprising a compartment for goods in liquid form, wherein the compartment has bellows sides , and wherein the compartment is arranged, so that due to the bellows sides it has a maximum height in the case of filled compartments and a minimum height in the case of empty compartments, wherein the arrangement further comprises a rectangular cargo-receiving surface horizontally arranged on top of the compartment in such a manner that the height of the cargo-receiving surface follows the state of fullness in the compartment with a maximum height in the case of filled compartments and a minimum height in the case of empty compartments, characterized in that the bellows sides comprise rubber and graphene.
A cell structure for use in a treatment of a lysosomal storage disease, comprising a plurality of biocompatible polymer blocks and a plurality of cells of at least one type, wherein the plurality of polymer blocks are three-dimensionally disposed in a mosaic pattern in the gaps between the plurality of cells, wherein the cells include at least a mesenchymal stem cell or a fibroblast, and wherein the treatment is transplantation of the cell structure. wherein the cells include at least a mesenchymal stem cell or a fibroblast, and wherein the treatment is transplantation of the cell structure.
A Pt vs. RhPt thermocouple, wherein the thermocouple comprises a Pt limb and a RhPt limb, characterised in that the Pt limb of the thermocouple is doped platinum comprising: (a) platinum; and (b) ≤ 0.01 wt% of zirconium; wherein the platinum to which the dopant is added is ≥ 99.997 wt% pure. (a) platinum; and (b) ≤ 0.01 wt% of zirconium;
A lubricating grease supply device of a wind energy installation , which comprises a lubricating grease conveying device and a lubricating grease cleaning device , wherein the lubricating grease conveying device is set up to convey lubricating grease in a direction of conveyance in a closed circuit for lubricating grease, wherein a bearing of the wind energy installation , which bearing is to be lubricated, and the lubricating grease cleaning device each form a section of the closed circuit for lubricating grease, characterised in that the lubricating grease cleaning device comprises a magnetic separator and at least one gravity separator .
An implantable connector assembly for communicating an element from a source exterior of a patient or implanted within the patient to an implantable device within the patient, comprising a plug configured to operatively connect to one of the source and the implantable device , the plug including a plunger body ; a receptacle configured to operatively connect to the other of the source and the implantable device , the receptacle including a sleeve and a stopper , the sleeve defining an opening sized for receiving the plunger body , the stopper resiliently mounted within the sleeve and biased toward the opening to cover and fluidly seal the opening for inhibiting contamination from entering within the sleeve when the plunger body is withdrawn from the sleeve , and characterized in that it further comprises a pair of communication structures positioned respectively on the plunger body and the sleeve , one of the pair of communication structures is configured to operatively connect to the source for receiving the element from the source and the other of the pair of communication structures is configured to operatively connect to the implantable device for directing the element to the implantable device , wherein inserting the plunger body into the sleeve displaces the stopper and removably couples the pair of communication structures for communication of the element therebetween, and wherein the element is electrical power, and the pair of communication structures are a pair of annular electrical conduits positioned respectively about the plunger body and the sleeve , the pair of annular electrical conduits configured to removably connect for communicating the electrical power therebetween.
A method of producing a whey protein nanogel composition, the method comprising: a) providing a whey protein solution having: - a content of native beta-lactoglobulin (BLG) in an amount of at least 3% w/w, - a pH in the range of 5.8-7.5, - a weight ratio between the total amount calcium and native BLG which is - at most 0.0041*pH-0.0209, and - at least 0.0037*pH-0.0234 but larger than zero, and - a total concentration of monovalent metal cations of - at most 25 mM if the content of native BLG of the whey protein solution is less than 10% w/w, or - at most 20 mM if the content of native BLG of the whey protein solution is at least 10% w/w, b) heating the whey protein solution to a temperature of at least 68 degrees C for a duration sufficient to form a suspension of whey protein nanogels having a z-average diameter, when measured by dynamic light scattering, of 150-1000 nm, c) optionally, concentrating the suspension of whey protein nanogels to obtain a concentrated suspension of whey protein nanogels, d) optionally, drying a dryer feed comprising whey protein nanogels derived from step b) or c). a) providing a whey protein solution having: - a content of native beta-lactoglobulin (BLG) in an amount of at least 3% w/w, - a pH in the range of 5.8-7.5, - a weight ratio between the total amount calcium and native BLG which is - at most 0.0041*pH-0.0209, and - at least 0.0037*pH-0.0234 but larger than zero, and - a total concentration of monovalent metal cations of - at most 25 mM if the content of native BLG of the whey protein solution is less than 10% w/w, or - at most 20 mM if the content of native BLG of the whey protein solution is at least 10% w/w, - a content of native beta-lactoglobulin (BLG) in an amount of at least 3% w/w, - a pH in the range of 5.8-7.5, - a weight ratio between the total amount calcium and native BLG which is - at most 0.0041*pH-0.0209, and - at least 0.0037*pH-0.0234 but larger than zero, and - at most 0.0041*pH-0.0209, and - at least 0.0037*pH-0.0234 but larger than zero, and - a total concentration of monovalent metal cations of - at most 25 mM if the content of native BLG of the whey protein solution is less than 10% w/w, or - at most 20 mM if the content of native BLG of the whey protein solution is at least 10% w/w, - at most 25 mM if the content of native BLG of the whey protein solution is less than 10% w/w, or - at most 20 mM if the content of native BLG of the whey protein solution is at least 10% w/w, b) heating the whey protein solution to a temperature of at least 68 degrees C for a duration sufficient to form a suspension of whey protein nanogels having a z-average diameter, when measured by dynamic light scattering, of 150-1000 nm, c) optionally, concentrating the suspension of whey protein nanogels to obtain a concentrated suspension of whey protein nanogels, d) optionally, drying a dryer feed comprising whey protein nanogels derived from step b) or c).
A method for forecasting aircraft engine deterioration comprising: creating a first fused data set corresponding to a first actual aircraft engine , the first fused data set including at least one as manufactured parameter of the actual aircraft engine, expected operating parameters of the first actual aircraft engine, and actual operating parameters of the actual aircraft engine, the actual operating parameters of the actual aircraft engine including internal aircraft sensor data , and external flight tracking data ; and predicting an expected engine deterioration of the first actual engine based on the expected operating parameters and the actual operating parameters of the first actual aircraft engine by applying the first fused data set to a forecasting model, wherein the forecasting model is a recurrent neural network based algorithm, and the recurrent neural network based algorithm is trained via a plurality of second fused data sets corresponding to actual aircraft engines. creating a first fused data set corresponding to a first actual aircraft engine , the first fused data set including at least one as manufactured parameter of the actual aircraft engine, expected operating parameters of the first actual aircraft engine, and actual operating parameters of the actual aircraft engine, the actual operating parameters of the actual aircraft engine including internal aircraft sensor data , and external flight tracking data ; and predicting an expected engine deterioration of the first actual engine based on the expected operating parameters and the actual operating parameters of the first actual aircraft engine by applying the first fused data set to a forecasting model, wherein the forecasting model is a recurrent neural network based algorithm, and the recurrent neural network based algorithm is trained via a plurality of second fused data sets corresponding to actual aircraft engines.
An electrolytic cell for the production of ammonia (NH 3 ), the electrolytic cell comprising (i) an electrolytic cell unit comprising a first electrode , a second electrode , and an electrolyte , (ii) a voltage generator , (iii) a supply of a dinitrogen (N 2 ) comprising fluid , and (iv) a supply of a water comprising fluid , wherein the voltage generator is configured to apply a negative potential to the first electrode and a positive potential to the second electrode , wherein the electrolyte is configured to allow transport of protons, wherein the first electrode is permeable for protons and non-permeable for O 2 , N 2 , NH 3 and H 2 O, wherein the first electrode is at first side in contact with the electrolyte and at second side is in fluid contact with the supply of the dinitrogen comprising fluid , and wherein the second electrode is permeable for protons, and non-permeable for O 2 and H 2 O, wherein the second electrode is at first side also in contact with the electrolyte , and at second side in fluid contact with the supply of the water comprising fluid , wherein the first electrode comprises one or more of Ni and Fe, and wherein the second electrode comprises nickel metal or an alloy of nickel, and wherein the first electrode has a thickness d1 in the range of 0.5-250 μm.
Shaft for a rotating electrical machine comprising at least one housing element extending in an axial direction (B) and leading to the outside in a radial direction, one side of the housing element leading to the outside in an axial direction, the housing element being able to receive at least one insulated electrical conductor and a spacer , wherein the housing element is in the form of a groove whose cross-section perpendicular to the axial direction comprises a first portion that is substantially rectangular in shape leading to a second portion that is substantially trapezoidal in shape, the second portion leading to the outside in a radial direction, the second portion that is substantially trapezoidal in shape including a radially outer small base and a large base, the small base being disposed outside the large base in the radial direction such that an insulated electrical conductor can be inserted into the first portion in a radial direction of the shaft through the second portion , characterised in that the first portion is configured to receive a plurality of insulated electrical conductors so as to fill the first portion, the size of the small base being determined such that a single insulated electrical conductor can be inserted into the first portion in a radial direction of the shaft through the second portion .
A delivery device comprising: a housing having a hollow cavity formed therein; an inlet in fluid communication with the cavity and structured to deliver a stream of a fluid to the cavity; an outlet in fluid communication with the cavity and structured to deliver a flow of the fluid out of the cavity, and a delivery mechanism structured to deliver a beam of electromagnetic energy out of the outlet and within the flow, characterized in that the outlet comprises a straight section of a substantially unvarying diameter and further comprises a curved entryway and an adjacent tapered region situated upstream of the straight section, wherein the curved entryway is situated upstream of the tapered region. a housing having a hollow cavity formed therein; an inlet in fluid communication with the cavity and structured to deliver a stream of a fluid to the cavity; an outlet in fluid communication with the cavity and structured to deliver a flow of the fluid out of the cavity, and a delivery mechanism structured to deliver a beam of electromagnetic energy out of the outlet and within the flow, characterized in that the outlet comprises a straight section of a substantially unvarying diameter and further comprises a curved entryway and an adjacent tapered region situated upstream of the straight section, wherein the curved entryway is situated upstream of the tapered region.
A vibration mitigation coating for an integrally bladed rotor , wherein the integrally bladed rotor comprises a disk including an interior radius proximate an axis and an exterior radius distal from said axis , said disk including a substrate with an external surface , said external surface extending from said interior radius to said exterior radius ; wherein the vibration mitigation coating comprises a damping material disposed directly onto the external surface of the substrate ; characterized in that the thickness of the damping material varies across a width of the damping material to create a shaped cross-section. wherein the vibration mitigation coating comprises a damping material disposed directly onto the external surface of the substrate ; characterized in that the thickness of the damping material varies across a width of the damping material to create a shaped cross-section.
Valve device , in particular a wiper liquid valve, with a housing which comprises an inlet connection , an outlet connection and a media channel connecting the inlet connection to the outlet connection , and with a displaceable valve element , which is urged against a valve seat formed in the housing by a first spring element in order to close the media channel , and which is urged away from the valve seat in order to open the media channel by a second spring element , wherein the first spring element is made of a thermally activatable material and comprises, in a deactivated state, a first spring force which is smaller than that of the second spring element , and, in an activated state, a second spring force which is greater than that of the second spring element such that the valve element is displaced to close the media channel , wherein the first spring element is held at least partially in a hollow cylindrical housing projection protruding outwards from the housing , characterised in that an in particular annular sealing element is arranged on the valve element which is designed to interact with the valve seat in the activated state of the first spring element, and in that the valve element comprises, axially spaced apart from the sealing element in the direction of the housing projection , at least one radial projection which is designed to interact with at least one axial stop formed in the housing axially spaced apart from the valve seat in the direction of the valve seat in order to limit maximum deformation of the sealing element .
A composition comprising an effective amount of a hydroxypropyl-beta-cyclodextrin for use in the treatment of Alzheimer's disease in a human patient suffering from Alzheimer's disease, wherein the hydroxypropyl-beta-cyclodextrin composition is administered in a monthly dose amount of about 500 mg/kg to about 1500 mg/kg.
A process for producing a coextruded multilayer structure comprising coextruding a poly(hydroxyalkanoic acid) polymer composition, a tie layer composition, and a sealant layer composition to produce a multilayer structure; cooling the multilayer film structure in a first bubble to produce a tubular multilayer structure; orienting the tubular multilayer structure under heating in a second bubble to produce an oriented tubular multilayer structure; and relaxing the oriented tubular multilayer structure under heating in a third bubble; wherein the tie layer composition comprises one or more olefin homopolymers and/or copolymers, and wherein the sealant layer composition comprises one or more olefin homopolymers and/or copolymers capable of fusion bonding on another layer by conventional means of heat sealing. coextruding a poly(hydroxyalkanoic acid) polymer composition, a tie layer composition, and a sealant layer composition to produce a multilayer structure; cooling the multilayer film structure in a first bubble to produce a tubular multilayer structure; orienting the tubular multilayer structure under heating in a second bubble to produce an oriented tubular multilayer structure; and relaxing the oriented tubular multilayer structure under heating in a third bubble; wherein the tie layer composition comprises one or more olefin homopolymers and/or copolymers, and wherein the sealant layer composition comprises one or more olefin homopolymers and/or copolymers capable of fusion bonding on another layer by conventional means of heat sealing.
A finless heat exchanger comprising: - two headers ; and - a plurality of heat transfer tubes spaced apart from each other and arranged side by side, - the two headers each having a plurality of insertion holes , to which both ends of the plurality of heat transfer tubes are fitted and connected, - the plurality of heat transfer tubes each including - straight portions extending in a direction orthogonal to an arrangement direction in which the plurality of heat transfer tubes are arranged and turning portions , - the straight portions and the turning portions being alternately and continuously arranged, the finless heat exchanger further comprising a positioning structure maintaining intervals between the straight portions , wherein the positioning structure includes recesses supporting the turning portions , characterised in that the recesses are arranged in one or each of the two headers . - two headers ; and - a plurality of heat transfer tubes spaced apart from each other and arranged side by side, - the two headers each having a plurality of insertion holes , to which both ends of the plurality of heat transfer tubes are fitted and connected, - the plurality of heat transfer tubes each including - straight portions extending in a direction orthogonal to an arrangement direction in which the plurality of heat transfer tubes are arranged and turning portions , - the straight portions and the turning portions being alternately and continuously arranged, the finless heat exchanger further comprising a positioning structure maintaining intervals between the straight portions , wherein the positioning structure includes recesses supporting the turning portions , characterised in that the recesses are arranged in one or each of the two headers .