mhurhangee/patent-ind-claim-en huggingface dataset:
A computer-implemented method of modeling a geological body, the method comprising: building, for a volume of interest, a contemporary structural model comprising a plurality of block units ; generating a paleo-space model by transforming the plurality of block units from contemporary space to paleo-space; constructing a geological body in the paleo-space model using data acquired from a contemporary formation; determining a set of block units containing the geological body in the paleo-space model; constructing, for each block unit of the set of block units, a copy of the closed bounding surface of the geological body ; generating a plurality of inverse transformed boundary surfaces by applying an inverse paleo-transform to each copy of the closed bounding surface; trimming the plurality of inverse transformed boundary surfaces to fit the plurality of block units in the contemporary structural model to generate a plurality of clipped pieces; collecting the plurality of clipped pieces in one geometry feature that represents the geological body in a contemporary structural model. building, for a volume of interest, a contemporary structural model comprising a plurality of block units ; generating a paleo-space model by transforming the plurality of block units from contemporary space to paleo-space; constructing a geological body in the paleo-space model using data acquired from a contemporary formation; determining a set of block units containing the geological body in the paleo-space model; constructing, for each block unit of the set of block units, a copy of the closed bounding surface of the geological body ; generating a plurality of inverse transformed boundary surfaces by applying an inverse paleo-transform to each copy of the closed bounding surface; trimming the plurality of inverse transformed boundary surfaces to fit the plurality of block units in the contemporary structural model to generate a plurality of clipped pieces; collecting the plurality of clipped pieces in one geometry feature that represents the geological body in a contemporary structural model.
A method of transmitting channel state information (CSI) for a hybrid beamforming from a user equipment in a wireless communication system, the method comprising: measuring a gain of a directional beam formed with reference to a first direction and a gain of an omni-directional beam formed equivalently in all directions respectively; and transmitting the CSI including a gain difference between the directional beam and the omni-directional beam to a base station, wherein a direction of a digital beamforming in the hybrid beamforming is determined in accordance with the gain difference between the directional beam and the omni-directional beam and wherein a direction of an analog beamforming in the hybrid beamforming is determined in accordance with the first direction. measuring a gain of a directional beam formed with reference to a first direction and a gain of an omni-directional beam formed equivalently in all directions respectively; and transmitting the CSI including a gain difference between the directional beam and the omni-directional beam to a base station, wherein a direction of a digital beamforming in the hybrid beamforming is determined in accordance with the gain difference between the directional beam and the omni-directional beam and wherein a direction of an analog beamforming in the hybrid beamforming is determined in accordance with the first direction.
A computer-implemented method for displaying aircraft engine information, the method comprising: acquiring a value of an engine control parameter during operation of an aircraft engine, wherein the engine control parameter has a nonlinear relationship with thrust and wherein the engine control parameter is a fan speed 'N1'; displaying a scale on a display unit ; displaying first symbology having a position relative to the scale using a nonlinear scaling function in the region from a zero fan speed to a maximum rated fan speed 'N1 Max ', whereby sensitivity is reduced at the zero fan speed and sensitivity is increased at the maximum rated fan speed, the first symbology representing the acquired value of the fan speed; and displaying second symbology representing a target fan speed 'N1 Targ '. acquiring a value of an engine control parameter during operation of an aircraft engine, wherein the engine control parameter has a nonlinear relationship with thrust and wherein the engine control parameter is a fan speed 'N1'; displaying a scale on a display unit ; displaying first symbology having a position relative to the scale using a nonlinear scaling function in the region from a zero fan speed to a maximum rated fan speed 'N1 Max ', whereby sensitivity is reduced at the zero fan speed and sensitivity is increased at the maximum rated fan speed, the first symbology representing the acquired value of the fan speed; and displaying second symbology representing a target fan speed 'N1 Targ '.
A pushing device for pushing a sliding door (12; 13; 14) in a pushing direction relative to a furniture body , having a housing and having an entrainer that can be moved relative to this housing , wherein the entrainer is part of a piston unit which is guided in the housing and which is loaded against the pushing direction by means of a spring , and wherein the spring can be loaded by means of a Bowden cable having a shape-memory element , characterized in that the entrainer has a stop surface pointing in the pushing direction , the Bowden cable traverses the piston unit , the spring and the housing , and the Bowden cable has a piston-unit-side end arranged outside of the piston unit and a housing-side end movable relative to this piston-unit-side end and arranged outside of the housing , which ends can be connected to two poles of a current source .
A computing node in a distributed information security system, wherein the computing node is adapted to communicate with a subset of clients of the distributed information security system, wherein the computing node is adapted to provide at least one cryptographic service relating to transactions for the subset of clients, wherein the computing node is provisioned with a plurality of keys for use by said at least one cryptographic service wherein the plurality of keys are provided in a key list with a limited period of validity, wherein the computing node is adapted to perform a deterministic process based on data identifying a transaction for a client in the subset of clients to associate a key from the plurality of keys to a service request for the client relating to the transaction, wherein the same key is to be used for further service requests relating to the same transaction, and wherein the computing node is further adapted to carry out the same deterministic process reusing the plurality of keys in the key list for further cryptographic services for further transactions for the subset of clients during the limited period of validity of the key list, wherein the key list is replaced with a further key list when the key list is no longer valid.
A combustor wall comprising: a hot side panel (96") having a first face defining at least in-part a combustion chamber (64"); a second face defining at least in-part a cooling air plenum (68"); and a vascular lattice structure (108") located between the first and second faces for distributing cooling air from the plenum (68") and to the chamber (64"), wherein the combustor wall further comprises a cold side panel (94") spaced from the vascular lattice structure (108") and having the second face, wherein a plurality of inlet holes (110") are in the second face and a plurality of outlet holes (114") are in the first face for flowing cooling air from the plenum (68"), through the lattice structure (108") and into the combustion chamber (64"), wherein the plurality of outlet holes (114") are film cooling holes, characterized in that the plurality of film cooling holes are multi-lobed cooling holes. a hot side panel (96") having a first face defining at least in-part a combustion chamber (64"); a second face defining at least in-part a cooling air plenum (68"); and a vascular lattice structure (108") located between the first and second faces for distributing cooling air from the plenum (68") and to the chamber (64"), wherein the combustor wall further comprises a cold side panel (94") spaced from the vascular lattice structure (108") and having the second face, wherein a plurality of inlet holes (110") are in the second face and a plurality of outlet holes (114") are in the first face for flowing cooling air from the plenum (68"), through the lattice structure (108") and into the combustion chamber (64"), wherein the plurality of outlet holes (114") are film cooling holes, characterized in that the plurality of film cooling holes are multi-lobed cooling holes.
A modular motor and magnetic bearing assembly comprising a positioning casing comprising a first end portion presenting a plane reference surface perpendicular to a longitudinal axis X-X', a second end portion forming the support of an axial magnetic abutment , a cylindrical wall presenting a first end having an outer cylindrical reference surface , a second end secured to said second end portion , a central portion provided on an outer face with channels for a flow of cooling liquid, a first intermediate portion provided with openings for entry of gaseous fluid, and a second intermediate portion provided with openings for exit of gaseous fluid; characterized in that it further comprises: a rotor having said longitudinal axis X-X' as its axis and presenting a first end provided with an inner cylindrical reference surface and a plane reference surface perpendicular to said longitudinal axis X-X'; an electric motor comprising a stator mounted on an inner face of the central portion of said cylindrical wall of the positioning casing and an armature mounted on an outer surface of the rotor ; a first radial magnetic bearing comprising a stator mounted on an inner face of the first intermediate portion of said cylindrical wall of the positioning casing and an armature mounted on an outer surface of the rotor ; a second radial magnetic bearing comprising a stator mounted on an inner face of the second intermediate portion of said cylindrical wall of the positioning casing and an armature mounted on an outer surface of the rotor ; an axial abutment comprising a rotor armature mounted at the second end of the rotor perpendicularly to said longitudinal axis X-X' and two stator subassemblies (31, 33; 32, 34) mounted on said axial abutment support ; a first auxiliary mechanical bearing arranged between said first end portion of the positioning casing and said first end of the rotor ; and a second auxiliary mechanical bearing arranged between said second end portion of the positioning casing and said second end of the rotor .
A power supply device , including a plurality of battery modules having secondary batteries , wherein the battery modules are configured to be mutually connected in series according to a gate signal, characterised in that each battery module includes disconnection means for forcibly disconnecting the battery module from the series connection regardless of provision of the gate signal, and the disconnection means are configured to, at the time of powering by power supply output, forcibly disconnect one or more of the battery modules from the series connection to make accumulated discharge current amounts thereof per unit time become smaller than those of other battery modules included in the power supply device . the battery modules are configured to be mutually connected in series according to a gate signal, characterised in that each battery module includes disconnection means for forcibly disconnecting the battery module from the series connection regardless of provision of the gate signal, and the disconnection means are configured to, at the time of powering by power supply output, forcibly disconnect one or more of the battery modules from the series connection to make accumulated discharge current amounts thereof per unit time become smaller than those of other battery modules included in the power supply device .
Two-component polyurea composition, comprising a polyisocyanate component C1 and a hardener component C2, wherein the polyisocyanate component C1 comprises at least a polyisocyanate PI ; the hardener component C2 comprises at least a compound of formula (I) wherein R 1 represents a n-valent organic radical; R 2 and R 3 represent independently of one another an aliphatic or cycloaliphatic or aromatic radical; n is an integer with a value of 2 to 6, particularly 2 or 3; characterized in that the hardener component C2 comprises at least one salt hydrate SH with a decomposition temperature of between 30 °C and 80 °C. R 1 represents a n-valent organic radical; R 2 and R 3 represent independently of one another an aliphatic or cycloaliphatic or aromatic radical; n is an integer with a value of 2 to 6, particularly 2 or 3;
A method for wireless communication at a device , comprising: determining at least one resource reserved for transmitting a demodulation reference signal, DM-RS; transmitting a sounding reference signal, SRS, over the at least one resource by multiplexing the SRS with the DM-RS for each unutilized antenna port and for each antenna port that communicates a same signal as another antenna port. determining at least one resource reserved for transmitting a demodulation reference signal, DM-RS; transmitting a sounding reference signal, SRS, over the at least one resource by multiplexing the SRS with the DM-RS for each unutilized antenna port and for each antenna port that communicates a same signal as another antenna port.
A polypropylene composition (PC) comprising: i) from 95.0 to 99.99 wt.-%, based on the total weight of the composition, of a polypropylene (PP), preferably a propylene homopolymer (HPP); and ii) from 0.01 to 5.0 wt.-%, based on the total weight of the composition, of a compound according to Formula (I) wherein each R is independently selected from C 1 to C 6 alkylene, C 2 to C 6 alkenylene and a single bond, each R' is independently selected from H and C 1 to C 6 alkyl, each R" is independently selected from H and C 1 to C 22 alkyl, wherein each alkylene, alkenylene and alkyl group may optionally be substituted by deuterium or fluorine, and the two substituents on the central benzene ring may be either positioned in an ortho, meta or para relationship; wherein the individual content of the polypropylene (PP), more preferably the propylene homopolymer (HPP), and the compound according to Formula (I) add up to at least 98.0 wt.-%, more preferably at least 99.0 wt.-%, based on the total weight of the composition, and wherein the polypropylene (PP), more preferably the propylene homopolymer (HPP), has a melt flow rate MFR 2 , determined according to ISO 1133 at 230 °C at a load of 2.16 kg, in the range from 400 to 5000 g/10 min and a melting temperature Tm, determined by differential scanning calorimetry (DSC) according to ISO 11357, in the range from 140 to 170 °C. i) from 95.0 to 99.99 wt.-%, based on the total weight of the composition, of a polypropylene (PP), preferably a propylene homopolymer (HPP); and ii) from 0.01 to 5.0 wt.-%, based on the total weight of the composition, of a compound according to Formula (I) wherein each R is independently selected from C 1 to C 6 alkylene, C 2 to C 6 alkenylene and a single bond, each R' is independently selected from H and C 1 to C 6 alkyl, each R" is independently selected from H and C 1 to C 22 alkyl, wherein each alkylene, alkenylene and alkyl group may optionally be substituted by deuterium or fluorine, and the two substituents on the central benzene ring may be either positioned in an ortho, meta or para relationship; wherein the individual content of the polypropylene (PP), more preferably the propylene homopolymer (HPP), and the compound according to Formula (I) add up to at least 98.0 wt.-%, more preferably at least 99.0 wt.-%, based on the total weight of the composition, and wherein the polypropylene (PP), more preferably the propylene homopolymer (HPP), has a melt flow rate MFR 2 , determined according to ISO 1133 at 230 °C at a load of 2.16 kg, in the range from 400 to 5000 g/10 min and a melting temperature Tm, determined by differential scanning calorimetry (DSC) according to ISO 11357, in the range from 140 to 170 °C.
An aluminum alloy brazing sheet for a heat exchanger, the aluminum alloy brazing sheet comprising a four-layer material in which an air-side surface of a core material is cladded with an intermediate layer and an air-side brazing material layer in this order from the core material side and an internal side surface of the core material is cladded and stacked with an internal brazing material layer, wherein the intermediate layer is formed of an aluminum alloy including Mn of 0.2 mass % or more and less than 0.35 mass %, Si of 0.6 mass % or less, Fe of 0.7 mass % or less, and Cu of 0.1 mass % or less, and optionally one or two or more of Ti of 0.3 mass % or less, Zr of 0.3 mass % or less, and Cr of 0.3 mass % or less, with the balance being A1 and inevitable impurities, the core material is formed of an aluminum alloy including Si of 1.2 mass % or less, Fe of 1.0 mass % or less, Cu of 0.3 mass % or more and 1.0 mass % or less, and Mn of 0.5 mass % or more and 2.0 mass % or less, and optionally one or two or more of Ti of 0.3 mass % or less, Zr of 0.3 mass % or less, and Cr of 0.3 mass % or less, with the balance being Al and inevitable impurities, each of the air-side brazing material layer and the internal brazing material layer is formed of an aluminum alloy including Si of 4 mass % or more and 13 mass % or less, wherein one or both of the aluminum alloy forming the air-side brazing material layer and the aluminum alloy forming the internal brazing material layer optionally includes Sr of 0.1 mass % or less, with the balance being A1 and inevitable impurities, and the intermediate layer has a clad ratio of 5 to 30%, the air-side brazing material layer has a clad ratio of 5 to 20%, and the internal brazing material layer has a clad ratio of 5 to 20%. the intermediate layer is formed of an aluminum alloy including Mn of 0.2 mass % or more and less than 0.35 mass %, Si of 0.6 mass % or less, Fe of 0.7 mass % or less, and Cu of 0.1 mass % or less, and optionally one or two or more of Ti of 0.3 mass % or less, Zr of 0.3 mass % or less, and Cr of 0.3 mass % or less, with the balance being A1 and inevitable impurities, the core material is formed of an aluminum alloy including Si of 1.2 mass % or less, Fe of 1.0 mass % or less, Cu of 0.3 mass % or more and 1.0 mass % or less, and Mn of 0.5 mass % or more and 2.0 mass % or less, and optionally one or two or more of Ti of 0.3 mass % or less, Zr of 0.3 mass % or less, and Cr of 0.3 mass % or less, with the balance being Al and inevitable impurities, each of the air-side brazing material layer and the internal brazing material layer is formed of an aluminum alloy including Si of 4 mass % or more and 13 mass % or less, wherein one or both of the aluminum alloy forming the air-side brazing material layer and the aluminum alloy forming the internal brazing material layer optionally includes Sr of 0.1 mass % or less, with the balance being A1 and inevitable impurities, and the intermediate layer has a clad ratio of 5 to 30%, the air-side brazing material layer has a clad ratio of 5 to 20%, and the internal brazing material layer has a clad ratio of 5 to 20%.
Connecting device for connecting a floor element to a support , comprising - a latching element with a latching projection (4.2) and - a receiving element with a receptacle (6.3.1) for at least partially receiving the latching projection (4.2) in a positive-locking manner, characterised - in that the receiving element has a vibration damper (6.3) for reducing the transmission of vibrations to the floor element , and - in that the receiving element is designed for levelling height deviations and comprises a continuously adjustable levelling mechanism for levelling height deviations. - a latching element with a latching projection (4.2) and - a receiving element with a receptacle (6.3.1) for at least partially receiving the latching projection (4.2) in a positive-locking manner, characterised - in that the receiving element has a vibration damper (6.3) for reducing the transmission of vibrations to the floor element , and - in that the receiving element is designed for levelling height deviations and comprises a continuously adjustable levelling mechanism for levelling height deviations.
A biological model for training, comprising: an artificial tube shaped tissue which is constituted by a tube shaped body , which includes a diameter-reduction portion whose mid portion in the longitudinal direction thereof is diameter-reduced and which simulates a tube shaped tissue; a reinforcement member provided on the outer circumference side of the diameter-reduction portion for reinforcing the diameter-reduction portion ; and a restriction member which is installed on the outer circumference side of the reinforcement member and which restricts the deformation thereof when the reinforcement member is deformed, wherein an artificial narrow portion is constituted by the diameter-reduction portion , the reinforcement member and the restriction member , which simulates a narrow portion occurring at a tube shaped tissue, and the artificial narrow portion is for use in an expansion training for carrying out expansion with respect to the narrow portion, characterized in that the reinforcement member is constituted by a plastically deformable material including at least one kind within a silicone clay, a rubber clay, a resin clay and an oil clay, and a compressive elastic modulus of the plastically deformable material is 0.001 MPa to 0.5 MPa. an artificial tube shaped tissue which is constituted by a tube shaped body , which includes a diameter-reduction portion whose mid portion in the longitudinal direction thereof is diameter-reduced and which simulates a tube shaped tissue; a reinforcement member provided on the outer circumference side of the diameter-reduction portion for reinforcing the diameter-reduction portion ; and a restriction member which is installed on the outer circumference side of the reinforcement member and which restricts the deformation thereof when the reinforcement member is deformed, wherein an artificial narrow portion is constituted by the diameter-reduction portion , the reinforcement member and the restriction member , which simulates a narrow portion occurring at a tube shaped tissue, and the artificial narrow portion is for use in an expansion training for carrying out expansion with respect to the narrow portion, characterized in that the reinforcement member is constituted by a plastically deformable material including at least one kind within a silicone clay, a rubber clay, a resin clay and an oil clay, and a compressive elastic modulus of the plastically deformable material is 0.001 MPa to 0.5 MPa.