mhurhangee/patent-ind-claim-en huggingface dataset:
An X-ray apparatus comprising: an X-ray source for emitting X-ray radiation; and a beam chopping apparatus coupled to said X-ray source , wherein said beam chopping apparatus comprises a hollow cylinder with a first end and a second end defining a length of said cylinder and at least two helical apertures extending substantially along said length, wherein said cylinder is adapted to receive said X-ray radiation and to form a moving beam spot having a frequency, wherein said beam frequency is substantially constant; and wherein the hollow cylinder comprises a tungsten cylinder with a carbon fiber fabric wrapped around the tungsten cylinder , and with an epoxy shield around the cylinder . an X-ray source for emitting X-ray radiation; and a beam chopping apparatus coupled to said X-ray source , wherein said beam chopping apparatus comprises a hollow cylinder with a first end and a second end defining a length of said cylinder and at least two helical apertures extending substantially along said length, wherein said cylinder is adapted to receive said X-ray radiation and to form a moving beam spot having a frequency, wherein said beam frequency is substantially constant; and wherein the hollow cylinder comprises a tungsten cylinder with a carbon fiber fabric wrapped around the tungsten cylinder , and with an epoxy shield around the cylinder .
A compound of formula: wherein an alkoxymethylene group, =CHOR, is present at position 1, 2 or 3; and wherein R represents a C 1-3 alkyl group. wherein an alkoxymethylene group, =CHOR, is present at position 1, 2 or 3; and wherein R represents a C 1-3 alkyl group.
A microwave filter , comprising at least one resonant filter element (F, F1-F6) resonating at a resonant frequency (F0), the at least one resonant filter element (F, F1-F6) comprising: a housing ; a resonant filter cavity (C, C1-C6) arranged in the housing ; and a resonator element in the shape of a resonator rod arranged in the housing and extending into the cavity (C, C1-C6), wherein at least two tuning elements are arranged on the housing of the resonant filter element (F, F1-F6) and each extends into the cavity (C, C1-C6) with a shaft portion , wherein the at least two tuning elements are movable with respect to the housing to adjust the length (L1, L2) of the shaft portion extending into the cavity (C, C1-C6) and wherein the at least two tuning elements are constituted and designed such that by adjusting the length (L1, L2) of the shaft portion of each tuning element extending into the housing a temperature drift of the resonant frequency (F0) is adjustable, wherein the at least two tuning elements are arranged symmetrically with respect to a plane of symmetry extending along a longitudinal axis of the resonator element such that they are symmetrically placed at either side of the plane of symmetry, characterized in that the at least two tuning elements differ in material and/or shape. a housing ; a resonant filter cavity (C, C1-C6) arranged in the housing ; and a resonator element in the shape of a resonator rod arranged in the housing and extending into the cavity (C, C1-C6), wherein at least two tuning elements are arranged on the housing of the resonant filter element (F, F1-F6) and each extends into the cavity (C, C1-C6) with a shaft portion , wherein the at least two tuning elements are movable with respect to the housing to adjust the length (L1, L2) of the shaft portion extending into the cavity (C, C1-C6) and wherein the at least two tuning elements are constituted and designed such that by adjusting the length (L1, L2) of the shaft portion of each tuning element extending into the housing a temperature drift of the resonant frequency (F0) is adjustable, wherein the at least two tuning elements are arranged symmetrically with respect to a plane of symmetry extending along a longitudinal axis of the resonator element such that they are symmetrically placed at either side of the plane of symmetry, characterized in that the at least two tuning elements differ in material and/or shape.
A reference signal sending method, comprising: determining (S320), by a network device, a plurality of resource elements, REs used to carry a first CSI-RS of one CSI-RS port, wherein the plurality of REs are distributed in a plurality of resource units, wherein in each resource unit, a plurality of REs used to carry the first CSI-RS are located on a plurality of subcarriers in a same symbol, values of the first CSI-RS carried on at least two REs are different and are from one first pilot sequence, and values of the first CSI-RS are loaded to the plurality of REs in the resource unit by using a first multiplex code; and sending (S330), by the network device, the first CSI-RS to a terminal device by using the plurality of REs. determining (S320), by a network device, a plurality of resource elements, REs used to carry a first CSI-RS of one CSI-RS port, wherein the plurality of REs are distributed in a plurality of resource units, wherein in each resource unit, a plurality of REs used to carry the first CSI-RS are located on a plurality of subcarriers in a same symbol, values of the first CSI-RS carried on at least two REs are different and are from one first pilot sequence, and values of the first CSI-RS are loaded to the plurality of REs in the resource unit by using a first multiplex code; and sending (S330), by the network device, the first CSI-RS to a terminal device by using the plurality of REs.
Motor vehicle latch , in particular an electrically operated motor vehicle latch, for a movable part of a vehicle , comprising a locking mechanism having at least one catch and at least one pawl for locking the catch in at least one ratchet position (I), an opening drive comprising at least one motor and at least one gear for electromechanically unlocking the locking mechanism , further comprising a load opening drive for electromechanically unlocking the locking mechanism in a load case, wherein the load opening drive can be activated by a user from at least outside the vehicle , wherein at least one energy source , in the form of a battery or a supercapacitor, is provided for supplying energy to the load opening drive , wherein a switching means for activating the load opening drive is provided, wherein the switching means can be arranged at a location on the movable part that is accessible to the user outside the vehicle , wherein the load opening drive is signal-connected to a control unit and the control unit interacts with a detection unit so that the load opening drive can be activated in the event of a load detection by the detection unit , wherein the switching means , the energy source and the load opening drive are connected in series so that the load opening drive can be activated only when the control unit receives a signal from the detection unit that a load case exists, so that a switch of the control unit is closed, wherein the load opening drive is activated only when the switch of the switching means is also operated and an opening request from a user of the vehicle is implemented.
A method for transmitting a random access preamble to a base station in a wireless access system, the method performed by a user equipment and comprising: transmitting the random access preamble to the base station, wherein the random access preamble is defined based on a cyclic shift 'C v ' of a Zadoff-Chu, ZC, sequence having a length N, wherein the cyclic shift 'C v ' satisfies following Equation 1: C v = S ⋅ ⌊ v / P ⌋ + v mod P ⋅ N CS , v = 0,1 , ... , P ⋅ G + R − 1 , wherein the parameters 'G', 'P', 'R', and 'S' satisfy following Equation 2 under condition of Ncs ≤ du < (N/3): P = ⌊ d u / N CS ⌋ , S = 2 ⋅ d u + P ⋅ N CS , R = max ⌊ N − 2 ⋅ d u − G ⋅ S / N CS ⌋ 0 , G = ⌊ N / S ⌋ , or and wherein the parameters 'G', 'P', 'R' and 'S' satisfy following Equation 3 under condition of (N/3) ≤ d u ≤ (N-Ncs)/2: P = ⌊ N − 2 ⋅ d u / N CS ⌋ , S = N − 2 ⋅ d u + P ⋅ N CS , R = min max ⌊ d u − G ⋅ S / N CS ⌋ 0 , P G = ⌊ d u / S ⌋ , and and wherein 'd u ' represents a variable for Doppler Shift and determined based on 'u', 'u' represent a root index of ZC sequence, and 'Ncs' represents a cyclic shift unit. transmitting the random access preamble to the base station, wherein the random access preamble is defined based on a cyclic shift 'C v ' of a Zadoff-Chu, ZC, sequence having a length N, wherein the cyclic shift 'C v ' satisfies following Equation 1: C v = S ⋅ ⌊ v / P ⌋ + v mod P ⋅ N CS , v = 0,1 , ... , P ⋅ G + R − 1 , wherein the parameters 'G', 'P', 'R', and 'S' satisfy following Equation 2 under condition of Ncs ≤ du < (N/3): P = ⌊ d u / N CS ⌋ , S = 2 ⋅ d u + P ⋅ N CS , R = max ⌊ N − 2 ⋅ d u − G ⋅ S / N CS ⌋ 0 , G = ⌊ N / S ⌋ , or and wherein the parameters 'G', 'P', 'R' and 'S' satisfy following Equation 3 under condition of (N/3) ≤ d u ≤ (N-Ncs)/2: P = ⌊ N − 2 ⋅ d u / N CS ⌋ , S = N − 2 ⋅ d u + P ⋅ N CS , R = min max ⌊ d u − G ⋅ S / N CS ⌋ 0 , P G = ⌊ d u / S ⌋ , and and wherein 'd u ' represents a variable for Doppler Shift and determined based on 'u', 'u' represent a root index of ZC sequence, and 'Ncs' represents a cyclic shift unit.
A system, comprising: a delivery device comprising a proximal portion , distal portion and lumen extending therebetween; a first injectable composition disposed within the distal portion of the delivery device; and a second injectable composition disposed within the proximal portion of the delivery device; wherein a viscosity of the first injectable composition is less than a viscosity of the second injectable composition, wherein the second injectable composition comprises a gellan gum and the first injectable composition comprises a lower concentration of the gellan gum of the second injectable composition, dissolved in a same or different aqueous isotonic solution, or the first injectable composition does not include any amount of the gellan gum, wherein the first and second injectable compositions are separated by a barrier member which is configured to rupture above a threshold level of force after the first injectable composition has been discharged from the distal portion of the delivery device. a delivery device comprising a proximal portion , distal portion and lumen extending therebetween; a first injectable composition disposed within the distal portion of the delivery device; and a second injectable composition disposed within the proximal portion of the delivery device; wherein a viscosity of the first injectable composition is less than a viscosity of the second injectable composition, wherein the second injectable composition comprises a gellan gum and the first injectable composition comprises a lower concentration of the gellan gum of the second injectable composition, dissolved in a same or different aqueous isotonic solution, or the first injectable composition does not include any amount of the gellan gum, wherein the first and second injectable compositions are separated by a barrier member which is configured to rupture above a threshold level of force after the first injectable composition has been discharged from the distal portion of the delivery device.
A trapping catheter for insertion into a guide catheter assembly, said guide catheter assembly comprising a guide catheter and a valve fitting mounted to a proximal end of the guide catheter , wherein the trapping catheter comprises: - a balloon , and - a trapping catheter body bounding an inflation lumen extending longitudinally within the trapping catheter , the inflation lumen having a distal end opening into an internal space bounded by the balloon , characterized in that the trapping catheter further comprises: - a stopper for abutting against an abutment at a proximal end of the guide catheter assembly so as to determine a maximum insertion depth of the trapping catheter into the guide catheter assembly, wherein the stopper projects to one radial side of the trapping catheter body only, and wherein the stopper comprises a curved section of the trapping catheter body . wherein the trapping catheter comprises: - a balloon , and - a trapping catheter body bounding an inflation lumen extending longitudinally within the trapping catheter , the inflation lumen having a distal end opening into an internal space bounded by the balloon , - a balloon , and - a trapping catheter body bounding an inflation lumen extending longitudinally within the trapping catheter , the inflation lumen having a distal end opening into an internal space bounded by the balloon , characterized in that the trapping catheter further comprises: - a stopper for abutting against an abutment at a proximal end of the guide catheter assembly so as to determine a maximum insertion depth of the trapping catheter into the guide catheter assembly, - a stopper for abutting against an abutment at a proximal end of the guide catheter assembly so as to determine a maximum insertion depth of the trapping catheter into the guide catheter assembly, wherein the stopper projects to one radial side of the trapping catheter body only, and wherein the stopper comprises a curved section of the trapping catheter body .
An arrangement provided for determining the weight of an animal , characterized in that said arrangement comprises: - a three-dimensional camera , directable towards the animal, wherein the three-dimensional camera is provided to record a three-dimensional image of the animal; and - image processing means provided for digitally processing the recorded three-dimensional image and for determining the weight of the animal based on the digitally processed three-dimensional image and a table which correlates dimensions or volumes with weights for the species or breed, to which the animal belongs. - a three-dimensional camera , directable towards the animal, wherein the three-dimensional camera is provided to record a three-dimensional image of the animal; and - image processing means provided for digitally processing the recorded three-dimensional image and for determining the weight of the animal based on the digitally processed three-dimensional image and a table which correlates dimensions or volumes with weights for the species or breed, to which the animal belongs.
An interior permanent magnet synchronous motor having a stator with a cylindrical core with stator coils installed in the stator core, said motor further having an internal rotor rotatably disposed inside the stator and having embedded arc-shaped permanent magnets wherein the stator core comprises stator teeth having flange portions extending in opposite circumferential directions along an air gap between said stator and rotor, the rotor comprises rotor cavities on outer circumferential portions facing said air gap between said stator and rotor and, the stator teeth comprise stator cavities in the middle of said two flange portions of each stator tooth facing said air gap between said stator and rotor characterized in that; the rotor cavities are positioned at equal distance from closest parts of two neighboring arc-shaped permanent magnets on opposite sides, the stator and rotor cavities are arranged such that the stator cavity is associated with a first length in the form of a first radius of curvature of an elliptic cross-section stator cavity and the rotor cavity is associated with a second length in the form of a second radius of curvature of an elliptic cross-section rotor cavity wherein said first radius of curvature is greater than said second radius of curvature .
A data processing method, comprising: parsing , by a user plane data processing network element, a received packet and determining first service type information of a data flow to which the packet belongs; obtaining , by the user plane data processing network element, second service type information of the data flow from a data analysis network element; and processing , by the user plane data processing network element, the data flow based on the first service type information and the second service type information, wherein the processing , by the user plane data processing network element, the data flow based on the first service type information and the second service type information comprises: adjusting, by the user plane data processing network element, a priority of the data flow when the first service type information is inconsistent with the second service type information. parsing , by a user plane data processing network element, a received packet and determining first service type information of a data flow to which the packet belongs; obtaining , by the user plane data processing network element, second service type information of the data flow from a data analysis network element; and processing , by the user plane data processing network element, the data flow based on the first service type information and the second service type information, wherein the processing , by the user plane data processing network element, the data flow based on the first service type information and the second service type information comprises: adjusting, by the user plane data processing network element, a priority of the data flow when the first service type information is inconsistent with the second service type information.
A method of monitoring turbine blade creep in a gas turbine engine , the method including: receiving stereo images of a turbine blade of a row of turbine blades, the stereo images being over the whole radial length of the blade, and having been obtained using a stereo borescope located in the engine adjacent the row of turbine blades; identifying a trailing edge , platform edge , and shroud edge of the blade in each of the stereo images; mapping each of the trailing edge , platform edge , and shroud edge by triangulation onto a 3D space; measuring in the 3D space a distance (D) between a radially inner landmark at the corner of the platform edge closest to the trailing edge on the blade, and a radially outer landmark at the corner of the shroud edge closest to the trailing edge on the blade; and comparing the measured distance (D) with the distance between the radially inner and radially outer landmarks for a turbine blade which has not experienced creep to determine an amount of creep-induced distortion of the blade. receiving stereo images of a turbine blade of a row of turbine blades, the stereo images being over the whole radial length of the blade, and having been obtained using a stereo borescope located in the engine adjacent the row of turbine blades; identifying a trailing edge , platform edge , and shroud edge of the blade in each of the stereo images; mapping each of the trailing edge , platform edge , and shroud edge by triangulation onto a 3D space; measuring in the 3D space a distance (D) between a radially inner landmark at the corner of the platform edge closest to the trailing edge on the blade, and a radially outer landmark at the corner of the shroud edge closest to the trailing edge on the blade; and comparing the measured distance (D) with the distance between the radially inner and radially outer landmarks for a turbine blade which has not experienced creep to determine an amount of creep-induced distortion of the blade.
A fiber reinforced, cementitious armor panel comprising: a cementitious core comprising reinforcing fiber within a continuous phase resulting from the curing of an aqueous mixture of: a) 25-45 weight % inorganic cement binder; b) filler, wherein the filler in the cementitious aqueous mixture consists of i) silica sand filler having a median particle size of 150-450 microns, the silica sand filler being in an amount of at least 35 weight %, and ii) pozzolanic filler having a median particle size of less than or equal to 50 microns, the pozzolanic filler being 5-15 weight % of the cementitious aqueous mixture, and wherein the pozzolanic filler is silica fume; c) 0.25-5.0 weight % polycarboxylate based self-levelling agent; d) 6-12 weight % water; and e) reinforcing fiber, and a fiber-reinforced skin layer attached to at least one surface of the cured continuous phase. a cementitious core comprising reinforcing fiber within a continuous phase resulting from the curing of an aqueous mixture of: a) 25-45 weight % inorganic cement binder; b) filler, wherein the filler in the cementitious aqueous mixture consists of i) silica sand filler having a median particle size of 150-450 microns, the silica sand filler being in an amount of at least 35 weight %, and ii) pozzolanic filler having a median particle size of less than or equal to 50 microns, the pozzolanic filler being 5-15 weight % of the cementitious aqueous mixture, and wherein the pozzolanic filler is silica fume; c) 0.25-5.0 weight % polycarboxylate based self-levelling agent; d) 6-12 weight % water; and e) reinforcing fiber, and a) 25-45 weight % inorganic cement binder; b) filler, wherein the filler in the cementitious aqueous mixture consists of i) silica sand filler having a median particle size of 150-450 microns, the silica sand filler being in an amount of at least 35 weight %, and ii) pozzolanic filler having a median particle size of less than or equal to 50 microns, the pozzolanic filler being 5-15 weight % of the cementitious aqueous mixture, and wherein the pozzolanic filler is silica fume; c) 0.25-5.0 weight % polycarboxylate based self-levelling agent; d) 6-12 weight % water; and e) reinforcing fiber, and a fiber-reinforced skin layer attached to at least one surface of the cured continuous phase.
Method for maintaining the functionality of a field device using in automation engineering, said method involving the following steps: - Monitoring of the field device for at least one performed parameter change (Δn x ), wherein an old parameter set (n x-1 ) is changed to a new parameter set (n x ) by the parameter change (Δn x ), - Saving of all the parameter changes performed on the field device (Δn x in a parameter change history (PH), - Continuous monitoring of the field device to detect a malfunction (F), - Performance of a corrective measure (BM), wherein the parameter change history (PH) and a parameter error link element (VE) are accessed to rectify the malfunction (F) occurring at the field device, wherein, in order to perform the corrective measure (BM), at least one parameter change determined automatically (Δn"' x ) is reset, wherein the parameter error link element (VE) is accessed to determine the at least one parameter change determined automatically (Δn"' x ) and wherein this at least one parameter change determined automatically (Δn"' x ) is offered to the operator (B) for selection, and if this is selected by the operator (B), the field device resets this at least one parameter change determined automatically (Δn"' x ). - Monitoring of the field device for at least one performed parameter change (Δn x ), wherein an old parameter set (n x-1 ) is changed to a new parameter set (n x ) by the parameter change (Δn x ), - Saving of all the parameter changes performed on the field device (Δn x in a parameter change history (PH), - Continuous monitoring of the field device to detect a malfunction (F), - Performance of a corrective measure (BM), wherein the parameter change history (PH) and a parameter error link element (VE) are accessed to rectify the malfunction (F) occurring at the field device, wherein, in order to perform the corrective measure (BM), at least one parameter change determined automatically (Δn"' x ) is reset, wherein the parameter error link element (VE) is accessed to determine the at least one parameter change determined automatically (Δn"' x ) and wherein this at least one parameter change determined automatically (Δn"' x ) is offered to the operator (B) for selection, and if this is selected by the operator (B), the field device resets this at least one parameter change determined automatically (Δn"' x ).