mhurhangee/patent-ind-claim-en huggingface dataset:
A telescoping wing system for an unmanned aerial vehicle, UAV, comprising: a first wing section comprising a substantially hollow interior; and a second wing section configured to be stowed within the interior of the first wing section such that an external surface of the second wing section is adjacent to an internal surface of the first wing section, wherein the second wing section is configured to be attached to a fuselage of the unmanned aerial vehicle, wherein the first wing section and the second wing section form a first wingspan in a first arrangement, the first arrangement comprising the second wing section stowed within the interior of the first wing section, wherein the first wing section and the second wing section form a second wingspan in a second arrangement, the second arrangement comprising the first wing section displaced along at least a portion of the second wing section, and wherein: a telescoping means extends the first wing section along the second wing section to increase a wingspan in the second arrangement; and further comprising: a control surface attached to a trailing-edge of the first wing section, wherein the control surface attaches to the first wing section via a hinge mounted on an external surface of the trailing-edge. a first wing section comprising a substantially hollow interior; and a second wing section configured to be stowed within the interior of the first wing section such that an external surface of the second wing section is adjacent to an internal surface of the first wing section, wherein the second wing section is configured to be attached to a fuselage of the unmanned aerial vehicle, wherein the first wing section and the second wing section form a first wingspan in a first arrangement, the first arrangement comprising the second wing section stowed within the interior of the first wing section, wherein the first wing section and the second wing section form a second wingspan in a second arrangement, the second arrangement comprising the first wing section displaced along at least a portion of the second wing section, and
A light-based dental treatment system comprising: a handle generator configured to generate therapeutic light, the handle generator including: a generator housing ; and at least one light element configured to generate the therapeutic light; at least one delivery shaft assembly selectively coupled with the handle generator, the at least one delivery shaft assembly including: a delivery shaft having a proximal shaft profile and a distal shaft profile ; a proximal light port aligned with the at least one light element ; and a distal light port configured to deliver light from the delivery shaft to a treatment location; a conductive heat sink coupled between the at least one light element and the generator housing , characterized in that the handle generator includes an alignment collet that surrounds at least a portion of the delivery shaft assembly and applies a clamping force with tightening of the alignment collet , the alignment collet having a light passage extending along an interior collet profile , wherein the interior collet profile of the alignment collet is configured to grasp the delivery shaft and align the proximal light port with the at least one light element , wherein the at least one delivery shaft includes a shaft fitting having a fitting profile coupled with the delivery shaft , and the fitting profile is complementary to the interior collet profile of the alignment collet . a handle generator configured to generate therapeutic light, the handle generator including: a generator housing ; and at least one light element configured to generate the therapeutic light; a generator housing ; and at least one light element configured to generate the therapeutic light; at least one delivery shaft assembly selectively coupled with the handle generator, the at least one delivery shaft assembly including: a delivery shaft having a proximal shaft profile and a distal shaft profile ; a proximal light port aligned with the at least one light element ; and a distal light port configured to deliver light from the delivery shaft to a treatment location; a delivery shaft having a proximal shaft profile and a distal shaft profile ; a proximal light port aligned with the at least one light element ; and a distal light port configured to deliver light from the delivery shaft to a treatment location; a conductive heat sink coupled between the at least one light element and the generator housing , characterized in that the handle generator includes an alignment collet that surrounds at least a portion of the delivery shaft assembly and applies a clamping force with tightening of the alignment collet , the alignment collet having a light passage extending along an interior collet profile , wherein the interior collet profile of the alignment collet is configured to grasp the delivery shaft and align the proximal light port with the at least one light element , wherein the at least one delivery shaft includes a shaft fitting having a fitting profile coupled with the delivery shaft , and the fitting profile is complementary to the interior collet profile of the alignment collet .
Cargo location device , configured to be disposed at, especially hidden in a cargo item or a group of cargo items, the cargo location device comprising means for wirelessly transmitting and receiving signals, a central processing unit and at least one energy source , and being configured to be operated in a monitoring mode in which it transmits a monitoring signal, which is receivable by monitoring means and a tracking mode in which it transmits a tracking signal which is traceable by tracking means , wherein the means for wirelessly transmitting and receiving the signals comprise a GSM module and a GPS module and a radio module , preferably a VHF radio module, characterized in that the means for wirelessly transmitting and receiving the signals also comprise a LPWAN module and in that the cargo location device is configured to switch from monitoring mode to tracking mode in response to receiving a tracking activation message that can be sent via a GSM network, a LPWAN and a radio network, preferably a VHF radio network, wherein the cargo location device is configured such that the GPS module intermittently provides coordinates, in particular LAT/LONG coordinates, at least when the cargo location device is in tracking mode, and in that it transmits the coordinates provided by the GPS module .
A crosslinkable elastomer composition including at least a hydrogen-free fluorine oligomer (a) and a crosslinkable elastomer, wherein the crosslinkable elastomer includes at least: one elastomer (B) selected from vinylidene fluoride/hexafluoropropene-based copolymers, vinylidene fluoride/hexafluoropropene/tetrafluoroethylene-based copolymers, tetrafluoroethylene/propylene-based copolymers; copolymers obtained by copolymerizing ethylene or perfluoroalkylvinyl ether to any of the aforementioned copolymers; block copolymers of fluorine rubber comprising vinylidene fluoride/hexafluoropropene/tetrafluoroethylene-based copolymers and fluorine resin comprising tetrafluoroethylene/ethylene alternating copolymers or polyvinylidene fluoride; and silicone rubber, and a perfluoroelastomer (A) containing as copolymer units a perfluoroolefin, a perfluorovinyl ether selected from the group consisting of perfluoro(alkylvinyl) ethers, perfluoro(alkoxyvinyl) ethers, and mixtures thereof, and a curing site monomer. including at least a hydrogen-free fluorine oligomer (a) and a crosslinkable elastomer, wherein the crosslinkable elastomer includes at least: one elastomer (B) selected from vinylidene fluoride/hexafluoropropene-based copolymers, vinylidene fluoride/hexafluoropropene/tetrafluoroethylene-based copolymers, tetrafluoroethylene/propylene-based copolymers; copolymers obtained by copolymerizing ethylene or perfluoroalkylvinyl ether to any of the aforementioned copolymers; block copolymers of fluorine rubber comprising vinylidene fluoride/hexafluoropropene/tetrafluoroethylene-based copolymers and fluorine resin comprising tetrafluoroethylene/ethylene alternating copolymers or polyvinylidene fluoride; and silicone rubber, and a perfluoroelastomer (A) containing as copolymer units a perfluoroolefin, a perfluorovinyl ether selected from the group consisting of perfluoro(alkylvinyl) ethers, perfluoro(alkoxyvinyl) ethers, and mixtures thereof, and a curing site monomer.
Whey protein micelles for use in the treatment and/or prevention of a condition linked to a reduced concentration of plasma amino acids in a patient in need thereof, wherein the treatment or prevention does not include an additional exercise regimen, wherein the condition is muscle atrophy or sarcopenia and wherein the whey protein micelles are administered to the patient in combination with a meal, wherein the meal comprises whey protein isolates, hydrolyzed milk proteins or any combination thereof; and wherein the whey protein micelles are administered to the patient in a daily dose of at least 20 g dry weight.
Architecture of a propulsion system of a multi-engine helicopter, comprising turboshaft engines that are connected to a power transmission gearbox , and comprising a low DC voltage onboard network for supplying power to helicopter equipment during flight, characterised in that it comprises: - only one turboshaft engine among said turboshaft engines, referred to as a hybrid turboshaft engine , which is capable of operating in at least one standby mode during a stable flight of the helicopter, the other turboshaft engines operating alone during this stable flight, - an electrotechnical pack for quickly restarting said hybrid turboshaft engine in order bring said engine out of said standby mode and to reach a mode referred to as the nominal mode, in which it provides mechanical power to said power transmission gearbox, said restart pack being connected to said onboard network , said electrotechnical pack for quick restart being a high-voltage pack, - at least two sources of electrical power for said onboard network , and - a low voltage-high voltage converter is arranged between said onboard network and said rapid restart pack - only one turboshaft engine among said turboshaft engines, referred to as a hybrid turboshaft engine , which is capable of operating in at least one standby mode during a stable flight of the helicopter, the other turboshaft engines operating alone during this stable flight, - an electrotechnical pack for quickly restarting said hybrid turboshaft engine in order bring said engine out of said standby mode and to reach a mode referred to as the nominal mode, in which it provides mechanical power to said power transmission gearbox, said restart pack being connected to said onboard network , said electrotechnical pack for quick restart being a high-voltage pack, - at least two sources of electrical power for said onboard network , and - a low voltage-high voltage converter is arranged between said onboard network and said rapid restart pack
A component for Higher Order Ambisonic, HOA, composition for an HOA decoder, the component for HOA composition being configured to: - receive an HOA representation of predominant sound components ĉ PS, n ( k - 1 ) obtained from a compressed HOA signal, wherein n denotes an index of coefficient channels with n = 1, ... , O , wherein O = ( N +1) 2 with N being the order of the compressed HOA signal and wherein k is a frame index; - receive a further HOA representation AMB , n ( k - 1 ) obtained from the compressed HOA Signal, wherein n denotes the index of coefficient channels and k the frame index; - receive a layered mode indication LMF D indicating whether the compressed HOA signal comprises at least two layers; - add the HOA representation of predominant sound components to the further HOA representation, wherein coefficients of the HOA representation of the predominant sound signals and corresponding coefficients of the further HOA representation are added, to obtain a decompressed HOA signal ĉ ( k - 1 ), wherein, if the layered mode indication LMF D indicates a layered mode with at least two layers, the component for HOA composition adds the HOA representations according to: c ^ n k − 1 = { c ̃ ^ AMB , n k − 1 for 1 ≤ n ≤ O MIN c ^ n k − 1 = c ^ PS , n k − 1 + c ̃ ^ AMB , n k − 1 , for O MIN + 1 ≤ n ≤ O , wherein O MIN = ( N MIN + 1) 2 and N MIN is a predefined integer value, wherein, if the layered mode indication LMF D indicates a single-layer mode, the component for HOA composition adds the HOA representations according to: c ^ n k − 1 = c ^ PS , n k − 1 + c ^ AMB , n k − 1 for 1 ≤ n ≤ O . - receive an HOA representation of predominant sound components ĉ PS, n ( k - 1 ) obtained from a compressed HOA signal, wherein n denotes an index of coefficient channels with n = 1, ... , O , wherein O = ( N +1) 2 with N being the order of the compressed HOA signal and wherein k is a frame index; - receive a further HOA representation AMB , n ( k - 1 ) obtained from the compressed HOA Signal, wherein n denotes the index of coefficient channels and k the frame index; - receive a layered mode indication LMF D indicating whether the compressed HOA signal comprises at least two layers; - add the HOA representation of predominant sound components to the further HOA representation, wherein coefficients of the HOA representation of the predominant sound signals and corresponding coefficients of the further HOA representation are added, to obtain a decompressed HOA signal ĉ ( k - 1 ), wherein, if the layered mode indication LMF D indicates a layered mode with at least two layers, the component for HOA composition adds the HOA representations according to: c ^ n k − 1 = { c ̃ ^ AMB , n k − 1 for 1 ≤ n ≤ O MIN c ^ n k − 1 = c ^ PS , n k − 1 + c ̃ ^ AMB , n k − 1 , for O MIN + 1 ≤ n ≤ O , wherein O MIN = ( N MIN + 1) 2 and N MIN is a predefined integer value, wherein, if the layered mode indication LMF D indicates a single-layer mode, the component for HOA composition adds the HOA representations according to: c ^ n k − 1 = c ^ PS , n k − 1 + c ^ AMB , n k − 1 for 1 ≤ n ≤ O .
Hot-blast lance for use in metallurgical processes, such as for example steel production, with which hot air can be blown in above a molten bath of a steel converter, which consists of an outer shell and at least one inner shell and an innermost shell, and arranged between the outer shell and an inner shell is at least one intermediate space or cooling channel through which coolant flows, characterized in that the innermost shell is defined by an innermost lance tube through which hot air can flow, and the inner shell or the innermost shell consists at least partially of a thermally insulating further shell , or a thermally insulating shell, or is provided with such a shell, or is coated with a thermally insulating layer, and the innermost shell is mounted in the hot-blast lance in a floating manner.
A method of producing an aqueous solution comprising an N-C 8-22 acyl acidic amino acid and/or a salt thereof and having pH 8.4 - 9.5, comprising the first step for reacting an acidic amino acid and/or a salt thereof with a C 8-22 fatty acid chloride in a water solvent at pH 10 - 12.0 to form an N-C 8-22 acyl acidic amino acid and/or a salt thereof, and the second step for adjusting the pH of the aqueous solution after the first step to 8.4 - 9.5. the first step for reacting an acidic amino acid and/or a salt thereof with a C 8-22 fatty acid chloride in a water solvent at pH 10 - 12.0 to form an N-C 8-22 acyl acidic amino acid and/or a salt thereof, and the second step for adjusting the pH of the aqueous solution after the first step to 8.4 - 9.5.
A method in a page-wide array printing apparatus comprising at least first and second printing dies that overlap in a page width direction , the method comprising the steps of: calibrating the printing apparatus in a media advance direction to a higher resolution than the resolution of calibration in the page width direction , the media advance direction being perpendicular to the page width direction ; and using printing masks to control the operation of a plurality of nozzles in an overlap area between the first and second printing dies , wherein each printing die prints alternating columns of the printing mask, the size of each column randomly variable to reduce any visible defects caused by dot placement errors in the page width direction . calibrating the printing apparatus in a media advance direction to a higher resolution than the resolution of calibration in the page width direction , the media advance direction being perpendicular to the page width direction ; and using printing masks to control the operation of a plurality of nozzles in an overlap area between the first and second printing dies , wherein each printing die prints alternating columns of the printing mask, the size of each column randomly variable to reduce any visible defects caused by dot placement errors in the page width direction .
Industrial installation for cleaning workpieces, in particular for cleaning components of engines and transmission components using a cleaning liquid, the installation including a filter arrangement comprising: a first filter which is a backwash filter for receiving contaminated cleaning liquid, a second filter arranged for receiving backwashed contaminated cleaning liquid from the backwash filter , and for removing solid matter from the contaminated cleaning liquid, and an oil separator arranged for receiving contaminated cleaning liquid and for removing oil from the contaminated cleaning liquid, wherein the oil separator is fluidly connected to the second filter ; characterised in that the oil separator is arranged for receiving the contaminated cleaning liquid directly from the second filter without a pump in the fluid path from the second filter to the oil separator , the second filter being arranged above, in particular on top of, the oil separator . a first filter which is a backwash filter for receiving contaminated cleaning liquid, a second filter arranged for receiving backwashed contaminated cleaning liquid from the backwash filter , and for removing solid matter from the contaminated cleaning liquid, and an oil separator arranged for receiving contaminated cleaning liquid and for removing oil from the contaminated cleaning liquid, wherein the oil separator is fluidly connected to the second filter ;
Procedure to determine the flow of a gas mixture - wherein at least one component i of the gas mixture is a hydrocarbon - through a circular cylindrical measuring tube with a straight longitudinal axis of the measuring tube and an inner diameter D I , with the following procedural steps: Determination of a first average flow velocity v L using the measurement of the runtime difference of acoustic signals along a signal path; Determination of the kinematic viscosity v kin of the gas mixture by determining or specifying the molar fraction x i of the different components i of the gas mixture; Determination of a modified Reynolds number Re mod according to the formula Re mod = (v L ∗ D I )/v kin , Determination of a second average flow velocity v A using a known function v A = f(Re mod ) ∗ v L depending on the modified Reynolds number Re mod and the determined first average flow velocity v L , wherein the step involving the determination of the kinematic viscosity v kin of the gas mixture precedes the step involving the determination of the modified Reynolds number Re mod , wherein f/(Re mod ) is determined by analyzing a ratio v L / v A in a calibration rig. Determination of a first average flow velocity v L using the measurement of the runtime difference of acoustic signals along a signal path; Determination of the kinematic viscosity v kin of the gas mixture by determining or specifying the molar fraction x i of the different components i of the gas mixture; Determination of a modified Reynolds number Re mod according to the formula Re mod = (v L ∗ D I )/v kin , Determination of a second average flow velocity v A using a known function v A = f(Re mod ) ∗ v L depending on the modified Reynolds number Re mod and the determined first average flow velocity v L , wherein the step involving the determination of the kinematic viscosity v kin of the gas mixture precedes the step involving the determination of the modified Reynolds number Re mod , wherein f/(Re mod ) is determined by analyzing a ratio v L / v A in a calibration rig.
A liner for a teat cup of a milking device , the liner having a cylindrical shape and comprising: a bore part disposed in a cylindrical shell such that a space (S) is formed between an inner surface of the shell and the bore part , the bore part being elastically deformable between an open state and a closed state; a mouthpiece part disposed at one end of the bore part and closing one end of the shell , the mouthpiece part being configured to allow a teat to be inserted therethrough and being provided with a vent which opens to an outside; a short milk tube part disposed at the other end of the bore part and closing the other end of the shell , the short milk tube part allowing milk (m) sucked from the teat on the bore part to flow therethrough; and a vent line provided as a groove on an inner surface of the liner , characterized in that the vent line extends on the bore part continuously from the vent . a bore part disposed in a cylindrical shell such that a space (S) is formed between an inner surface of the shell and the bore part , the bore part being elastically deformable between an open state and a closed state; a mouthpiece part disposed at one end of the bore part and closing one end of the shell , the mouthpiece part being configured to allow a teat to be inserted therethrough and being provided with a vent which opens to an outside; a short milk tube part disposed at the other end of the bore part and closing the other end of the shell , the short milk tube part allowing milk (m) sucked from the teat on the bore part to flow therethrough; and a vent line provided as a groove on an inner surface of the liner , characterized in that the vent line extends on the bore part continuously from the vent .
A method of preparing a compound of formula (Ia): comprising reacting a compound of formula (IIa): with in the presence of a dehydrating reagent to provide the compound of formula (Ia), wherein the dehydrating reagent comprises (i) trimethyl orthoformate and a catalytic amount of trifluoroacetic acid or (ii) titanium(IV) ethoxide.
Data and/or command device for vehicles , comprising at least one communication unit for receiving at least one item of non-charging-related object information pertaining to at least one electrical unit , in particular a hand-held power tool, which the electrical unit itself provides, and at least one item of vehicle information pertaining to at least one vehicle in which the electrical unit is arranged, and having at least one control or regulating unit which is configured to take an evaluation of the item of non-charging-related object information and the item of vehicle information as a basis for controlling or regulating the electrical unit , characterized in that the control or regulating unit is configured to take an evaluation of the item of non-charging-related object information and the item of vehicle information as a basis for controlling or regulating a charging operation of the electrical unit and enabling or disabling the electrical unit for use.