mhurhangee/patent-ind-claim-en huggingface dataset:
A method for positioning a centre point (M) of a second machine tool unit of a machine tool on a geometric axis of a first machine tool unit of the machine tool , wherein the second machine tool unit has a circular path (K) that is concentric with the centre point (M), is scannable and lies on a circular cylindrical surface , and wherein the first machine tool unit has a component that is rotatable about an axis of rotation coincident with the geometric axis, characterised in that a measuring unit is arranged on the first machine tool unit in a defined manner relative to the geometric axis and by means of the measuring unit the position of the circular path (K) in a geometric plane (KE), defined by the circular path (K), relative to the geometric axis is established in that the position of the circular path (K) is ascertained by means of the measuring unit by establishing the positions of three measurement points (P1, P2, P3) arranged at defined angular spacings from one another over the circular path (K) relative to the geometric axis , in that the position of the centre point (M) of the circular path (K) in the geometric plane (KE) relative to the geometric axis and a reference direction (E1, V) running through the geometric axis is calculated on the basis of the positions of the measurement points (P1, P2, P3) and the known radius (r) of the circular path (K), and in that , using machine tool-based adjustment directions (X, Y) of the machine tool units relative to one another, adjustment paths (dx, dy) in the geometric plane (KE), which are associated with the adjustment directions (X, Y), for positioning the centre point (M) on the geometric axis are calculated, and in that the machine tool units are moved relative to one another in accordance with these adjustment paths (dx, dy).
A method of seismic imaging, the method comprising: obtaining seismic data acquired by a seismic receiver comprising at least one of a geophone and a hydrophone deployed to a seismic medium, the seismic data responsive to seismic energy generated by at least one seismic source and propagating through the seismic medium by reflection from a subsurface geology; obtaining a set of seismic traces based on the acquired seismic data , each of the seismic traces including one or more samples of the seismic energy; generating a set of migrated gathers by performing reverse time migration on the seismic traces using a velocity model of the seismic energy propagating through the seismic medium, wherein the migrated gathers have amplitudes based at least in part on the reverse time migration and the velocity model ; generating amplitude compensated gathers from the migrated gathers ; and generating a seismic image of the subsurface geology, based on the amplitude compensated migrated gathers ; characterized in that the method further comprises: generating synthetic migrated gathers based on the velocity model and a source-receiver geometry representative of the at least one source and seismic receiver; and generating a filter based on the synthetic migrated gathers and a reflectivity model , wherein the filter is applied to the migrated gathers to correct the amplitudes. obtaining seismic data acquired by a seismic receiver comprising at least one of a geophone and a hydrophone deployed to a seismic medium, the seismic data responsive to seismic energy generated by at least one seismic source and propagating through the seismic medium by reflection from a subsurface geology; obtaining a set of seismic traces based on the acquired seismic data , each of the seismic traces including one or more samples of the seismic energy; generating a set of migrated gathers by performing reverse time migration on the seismic traces using a velocity model of the seismic energy propagating through the seismic medium, wherein the migrated gathers have amplitudes based at least in part on the reverse time migration and the velocity model ; generating amplitude compensated gathers from the migrated gathers ; and generating a seismic image of the subsurface geology, based on the amplitude compensated migrated gathers ; characterized in that the method further comprises: amplitude compensated migrated gathers ; characterized in that the method further comprises: generating synthetic migrated gathers based on the velocity model and a source-receiver geometry representative of the at least one source and seismic receiver; and generating a filter based on the synthetic migrated gathers and a reflectivity model , wherein the filter is applied to the migrated gathers to correct the amplitudes.
A method for data processing, applied to a first device, the first device comprising a Packet Data Convergence Protocol, PDCP,-layer entity and a first Radio Link Control, RLC,-layer entity, the method comprising: receiving, by the PDCP-layer entity, a PDCP Service Data Unit, SDU; encapsulating and processing, by the PDCP-layer entity, the PDCP SDU to obtain a PDCP Protocol Data Unit, PDU, and a duplicate PDCP PDU, in a case that a data duplication and transmission function of the PDCP-layer entity is in an active state; transmitting, by the PDCP-layer entity, the PDCP PDU and the duplicate PDCP PDU to the first RLC-layer entity and a second RLC-layer entity respectively; characterized by interrupting processing , by the second RLC-layer entity, a second RLC SDU which is incompletely processed in the second RLC-layer entity, responsive to detecting by the first RLC-layer entity that a first RLC Protocol Data Unit, PDU, which is associated with a first RLC Service Data Unit, SDU, and processed by the first RLC-layer entity is completely delivered, wherein the first RLC PDU is an RLC PDU in at least one RLC PDU corresponding to the first RLC SDU, the first RLC SDU corresponds to the PDCP PDU, the second RLC SDU corresponds to the duplicate PDCP PDU, and the first RLC SDU is the same as the second RLC SDU. receiving, by the PDCP-layer entity, a PDCP Service Data Unit, SDU; encapsulating and processing, by the PDCP-layer entity, the PDCP SDU to obtain a PDCP Protocol Data Unit, PDU, and a duplicate PDCP PDU, in a case that a data duplication and transmission function of the PDCP-layer entity is in an active state; transmitting, by the PDCP-layer entity, the PDCP PDU and the duplicate PDCP PDU to the first RLC-layer entity and a second RLC-layer entity respectively; characterized by interrupting processing , by the second RLC-layer entity, a second RLC SDU which is incompletely processed in the second RLC-layer entity, responsive to detecting by the first RLC-layer entity that a first RLC Protocol Data Unit, PDU, which is associated with a first RLC Service Data Unit, SDU, and processed by the first RLC-layer entity is completely delivered, wherein the first RLC PDU is an RLC PDU in at least one RLC PDU corresponding to the first RLC SDU, the first RLC SDU corresponds to the PDCP PDU, the second RLC SDU corresponds to the duplicate PDCP PDU, and the first RLC SDU is the same as the second RLC SDU.
A method of operating an agricultural harvester having a drive motor which is controlled by a control device and which is operatively connected by a switchable clutch to a main drive train for transmitting a drive speed, by which at least one working assembly of the harvester is driven, characterised in that before switching of the clutch an automatic reduction in the drive speed of the drive motor to a limit speed (n Grenz ) which ensures operation of the harvester is initiated.
A method of measuring a fluid parameter of a fluid within a fluid containment vessel , the method including: mounting a first multi-sensor assembly to a fluid containment vessel, the first multi-sensor assembly having two or more multi-sensor pairs located at consecutive heights of the fluid containment vessel, wherein each of the two or more multi-sensor pairs are stacked above each other and spaced apart at successive elevations along the height of the fluid containment vessel, each of the two or more multi-sensor pairs having a first ultrasonic sensor and an opposite second ultrasonic sensor , each of the two or more multi-sensor pairs being in communication with a single transmitter assembly ; sending a signal from the first ultrasonic sensor towards the second ultrasonic sensor of the two or more multi-sensor pairs; measuring a transit time for the signal to pass between the first ultrasonic sensor and the second ultrasonic sensor; and comparing the transit time of adjacent multi-sensor pairs to identify a fluid boundary within the fluid containment vessel. mounting a first multi-sensor assembly to a fluid containment vessel, the first multi-sensor assembly having two or more multi-sensor pairs located at consecutive heights of the fluid containment vessel, wherein each of the two or more multi-sensor pairs are stacked above each other and spaced apart at successive elevations along the height of the fluid containment vessel, each of the two or more multi-sensor pairs having a first ultrasonic sensor and an opposite second ultrasonic sensor , each of the two or more multi-sensor pairs being in communication with a single transmitter assembly ; sending a signal from the first ultrasonic sensor towards the second ultrasonic sensor of the two or more multi-sensor pairs; measuring a transit time for the signal to pass between the first ultrasonic sensor and the second ultrasonic sensor; and comparing the transit time of adjacent multi-sensor pairs to identify a fluid boundary within the fluid containment vessel.
A shear wave elastography method for imaging an observation field in an anisotropic medium , the method comprising a) an initial ultrasonic acquisition step during which at least one initial physical parameter is acquired in at least one region of interest in the anisotropic medium ; b) a spatial characterization step during which a set of spatial characteristics of the anisotropic medium is determined on the basis of the initial physical parameter, said set of spatial characteristics comprising a direction or a spatial angle of anisotropic features in the at least one region of interest ; and c) a shear wave imaging step comprising: c1) an excitation substep during which a shear wave is generated inside the anisotropic medium on the basis of said set of spatial characteristics; and c2) an observation substep during which the propagation of said shear wave is observed simultaneously at a multitude of points in the observation field . a) an initial ultrasonic acquisition step during which at least one initial physical parameter is acquired in at least one region of interest in the anisotropic medium ; b) a spatial characterization step during which a set of spatial characteristics of the anisotropic medium is determined on the basis of the initial physical parameter, said set of spatial characteristics comprising a direction or a spatial angle of anisotropic features in the at least one region of interest ; and c) a shear wave imaging step comprising: c1) an excitation substep during which a shear wave is generated inside the anisotropic medium on the basis of said set of spatial characteristics; and c2) an observation substep during which the propagation of said shear wave is observed simultaneously at a multitude of points in the observation field . c1) an excitation substep during which a shear wave is generated inside the anisotropic medium on the basis of said set of spatial characteristics; and c2) an observation substep during which the propagation of said shear wave is observed simultaneously at a multitude of points in the observation field .
Antenna arrangement for a vehicle , having at least one second electronic circuit for operating at least one first antenna structure , at least one third electronic circuit for operating at least one second antenna structure and at least one impedance converter , wherein the impedance converter has at least one first electronic circuit introduced into a housing of the impedance converter for the passive or active adjustment of an impedance and for amplifying a signal of a radio antenna with at least one electric input and at least one electric output , characterised in that in the housing the at least one second electronic circuit is arranged, which is connected to the at least one first antenna structure for sending and receiving data, wherein the at least one first antenna structure is attached onto or into the housing , and in the housing the at least one third electronic circuit is arranged, which is connected to the at least one second antenna structure for sending and receiving data via at least one electric line , wherein the second antenna structure is arranged outside the housing .
A nonwoven web comprising: a plurality of fibers produced by melt spinning a composition comprising an intimate admixture of a thermoplastic polymer, and characterized in that the composition comprises 8-40 wt.% of an oil, based on the weight of the total composition, the oil having a melting point of 25°C or less and a boiling point greater than 160°C, and wherein the oil is dispersed within the thermoplastic polymer. a plurality of fibers produced by melt spinning a composition comprising an intimate admixture of a thermoplastic polymer, and characterized in that the composition comprises 8-40 wt.% of an oil, based on the weight of the total composition, the oil having a melting point of 25°C or less and a boiling point greater than 160°C, and wherein the oil is dispersed within the thermoplastic polymer.
A turbine engine system (20;200), comprising: at least one hydrogen fuel tank ; a core flow path heat exchanger in a core flow path (C); and a compressor section , a combustor section having a burner, and a turbine section , each section located in the core flow path (C), wherein the core flow path heat exchanger is arranged in the core flow path (C) downstream of the combustor section , wherein hydrogen fuel is supplied from the at least one hydrogen fuel tank through a hydrogen fuel supply line , passing through the core flow path heat exchanger and then supplied into the burner for combustion, characterised in that the core flow path heat exchanger comprises: a radially outward plenum assembly ; a radially inward plenum assembly ; and a plurality of heat transfer tubes extending from the radially inward plenum assembly to the radially outward plenum assembly across the core flow path (C). at least one hydrogen fuel tank ; a core flow path heat exchanger in a core flow path (C); and a compressor section , a combustor section having a burner, and a turbine section , each section located in the core flow path (C), wherein the core flow path heat exchanger is arranged in the core flow path (C) downstream of the combustor section , wherein hydrogen fuel is supplied from the at least one hydrogen fuel tank through a hydrogen fuel supply line , passing through the core flow path heat exchanger and then supplied into the burner for combustion, a radially outward plenum assembly ; a radially inward plenum assembly ; and a plurality of heat transfer tubes extending from the radially inward plenum assembly to the radially outward plenum assembly across the core flow path (C).
An exterior panel for a transport vehicle , the exterior panel comprising: an exterior skin configured for atmospheric exposure; an intermediate skin spaced below the exterior skin; an interior skin spaced below the intermediate skin, and configured for attachment to a structural frame member of the transport vehicle ; and a first superplastic formed multicellular core sandwiched between the exterior skin and the intermediate skin , and a second superplastic formed multicellular core sandwiched between the intermediate skin and the interior skin ; and wherein the first superplastic formed multicellular core and the second superplastic formed multicellular core are superplastic formed and diffusion bonded respectively to the exterior skin and the intermediate skin , and to the intermediate skin and the interior skin , and wherein at least one of the first superplastic formed multicellular core and the second superplastic formed multicellular core comprises an air flow channel . an exterior skin configured for atmospheric exposure; an intermediate skin spaced below the exterior skin; an interior skin spaced below the intermediate skin, and configured for attachment to a structural frame member of the transport vehicle ; and a first superplastic formed multicellular core sandwiched between the exterior skin and the intermediate skin , and a second superplastic formed multicellular core sandwiched between the intermediate skin and the interior skin ; and wherein the first superplastic formed multicellular core and the second superplastic formed multicellular core are superplastic formed and diffusion bonded respectively to the exterior skin and the intermediate skin , and to the intermediate skin and the interior skin , and wherein at least one of the first superplastic formed multicellular core and the second superplastic formed multicellular core comprises an air flow channel .
A system for an aircraft , the system comprising: a low profile pneumatic sensing system comprising: a first pneumatic sensor (30; 52a, 52b) configured to be positioned to sense first sensed data of an airflow about an exterior of the aircraft , wherein the first pneumatic sensor (30; 52a, 52b) comprises a low profile bump that is configured to protrude from the aircraft exterior and to not extend beyond a boundary layer of the aircraft and a first port for sensing a total pressure, and wherein the first sensed data is used to determine first air data parameters; and the system further comprising an acoustic sensing system configured to emit acoustic signals about the exterior of the aircraft and sense the acoustic signals as second sensed data, wherein the second sensed data is used to determine second air data parameters. a first pneumatic sensor (30; 52a, 52b) configured to be positioned to sense first sensed data of an airflow about an exterior of the aircraft , wherein the first pneumatic sensor (30; 52a, 52b) comprises a low profile bump that is configured to protrude from the aircraft exterior and to not extend beyond a boundary layer of the aircraft and a first port for sensing a total pressure, and wherein the first sensed data is used to determine first air data parameters; and the system further comprising an acoustic sensing system configured to emit acoustic signals about the exterior of the aircraft and sense the acoustic signals as second sensed data, wherein the second sensed data is used to determine second air data parameters.
A refrigerator , comprising: a cabinet having a cabinet liner ; a partition plate assembly disposed in the cabinet liner and configured to partition an inner space of the cabinet liner into a plurality of compartments spaced apart from one another; and a door having a door liner , mounted to the cabinet , and configured to open or close the plurality of compartments simultaneously, wherein the door liner is configured to be sealingly fitted with the partition plate assembly so as to isolate the plurality of compartments hermetically, wherein a first sealing member is provided at a front surface of the partition plate assembly ; and a second sealing member is provided at a rear surface of the door liner , and the first sealing member is configured to be fitted with the second sealing member , characterized in that the door is further provided with a plurality of third sealing members , the plurality of third sealing members are in one-to-one correspondence with the plurality of compartments , and each third sealing member is configured to be sealingly fitted with a corresponding compartment , wherein each third sealing member is configured to be a sealing boss having a frame shape, and the sealing boss is configured to be tightly fitted with a part of an inner peripheral wall of the corresponding compartment , wherein the second sealing member is disposed between the third sealing members . a cabinet having a cabinet liner ; a partition plate assembly disposed in the cabinet liner and configured to partition an inner space of the cabinet liner into a plurality of compartments spaced apart from one another; and a door having a door liner , mounted to the cabinet , and configured to open or close the plurality of compartments simultaneously, wherein the door liner is configured to be sealingly fitted with the partition plate assembly so as to isolate the plurality of compartments hermetically, wherein a first sealing member is provided at a front surface of the partition plate assembly ; and a second sealing member is provided at a rear surface of the door liner , and the first sealing member is configured to be fitted with the second sealing member , characterized in that the door is further provided with a plurality of third sealing members , the plurality of third sealing members are in one-to-one correspondence with the plurality of compartments , and each third sealing member is configured to be sealingly fitted with a corresponding compartment , wherein each third sealing member is configured to be a sealing boss having a frame shape, and the sealing boss is configured to be tightly fitted with a part of an inner peripheral wall of the corresponding compartment , wherein the second sealing member is disposed between the third sealing members .
Side channel compressor for a fuel cell system for conveying and/or compressing a gas, in particular hydrogen, having a housing and a drive , wherein the housing has a housing upper portion and a housing lower portion , having a compressor chamber which extends in the housing circumferentially around a rotation axis and which has at least one circumferential side channel , having a compressor wheel which is located in the housing and which is arranged so as to be able to rotate about the rotation axis and which is driven by the drive , wherein the compressor wheel has on the circumference thereof blades which are arranged in the region of the compressor chamber , and having in each case a gas inlet opening and a gas outlet opening which are formed in the housing and which are connected to each other in fluid terms by means of the compressor chamber , in particular the at least one side channel , wherein the drive is constructed as an axial field electric motor , which has a stator and a rotor , wherein the stator and the rotor are constructed so as to extend in a disc-like manner around the rotation axis and wherein the stator is arranged in the direction of the rotation axis beside the rotor , characterized in that the disc-like rotor has a cylindrical attachment which extends in the direction of the rotation axis , wherein the cylindrical attachment is arranged at the side of the rotor facing away from the stator and wherein the covering face of the outer diameter of the cylindrical attachment extends circumferentially around the rotation axis , and wherein the cylindrical attachment at the inner diameter thereof is in contact with an outer diameter of a bearing and at the outer diameter thereof with the inner diameter of the compressor wheel , in particular with the hub disc of the compressor wheel , wherein the contact of the cylindrical attachment with respect to the bearing and/or the compressor wheel is carried out in particular in a non-positive-locking manner by means of an interference fit.