mhurhangee/patent-ind-claim-en huggingface dataset:
A docking station comprising: a base housing comprising a first surface (F1) having a recessed portion formed in at least a region thereof, the recessed portion comprising a cradling recess and a receiving recess , a second surface (F2) directed in an opposite direction to the first surface (F1), and a side surface (F3) at least partially surrounding a space between the first surface (F1) and the second surface (F2); a slide housing slidably mounted on the recessed portion to open and close at least a part of the recessed portion ; and a connection member disposed on the cradling recess , wherein the receiving recess is provided at a side of the cradling recess, the receiving recess comprising a curved surface that guides sliding of the slide housing , wherein as the slide housing slides, the connection member is hidden or exposed, and in a state where a part of the recessed portion is opened, the slide housing is positioned inclined with respect to the first surface (F1) or the second surface (F2). a base housing comprising a first surface (F1) having a recessed portion formed in at least a region thereof, the recessed portion comprising a cradling recess and a receiving recess , a second surface (F2) directed in an opposite direction to the first surface (F1), and a side surface (F3) at least partially surrounding a space between the first surface (F1) and the second surface (F2); a slide housing slidably mounted on the recessed portion to open and close at least a part of the recessed portion ; and
A method, comprising: receiving , at a client in a distributed system, a transaction (T) to be committed to a server in communication with the client; computing , with one or more processors in a client library of the client, a tentative timestamp for the transaction, wherein the tentative timestamp is computed using a value for a current time plus a variable corresponding to bounds of uncertainty of clocks in the distributed system, the clocks including at least a client clock at the client and a server clock at the server; and initiating , with the one more processors, a commit for the transaction based on the computed tentative timestamp, wherein initiating the commit for the transaction is performed by the client outside of a lock-hold interval for the transaction and comprises sending a commit message to the server to execute the transaction using the computed tentative timestamp, and wherein the lock-hold interval begins when locks for the transaction have been acquired and ends when locks for the transaction are released . receiving , at a client in a distributed system, a transaction (T) to be committed to a server in communication with the client; computing , with one or more processors in a client library of the client, a tentative timestamp for the transaction, wherein the tentative timestamp is computed using a value for a current time plus a variable corresponding to bounds of uncertainty of clocks in the distributed system, the clocks including at least a client clock at the client and a server clock at the server; and initiating , with the one more processors, a commit for the transaction based on the computed tentative timestamp, wherein initiating the commit for the transaction is performed by the client outside of a lock-hold interval for the transaction and comprises sending a commit message to the server to execute the transaction using the computed tentative timestamp, and wherein the lock-hold interval begins when locks for the transaction have been acquired and ends when locks for the transaction are released .
An electric-field capacitive coupler module , comprising: a first processing unit ; a first communication interface coupled to the first processing unit; a second communication interface ; and an electric-field capacitive coupler that defines an isolation barrier coupled between the first communication interface and the second communication interface, wherein the second communication interface is coupled to a second processing unit , wherein the second processing unit is operably associated with an electrosurgical generator assembly , wherein: the electric-field capacitive coupler includes two transmit plates and two receive plates, a transmitter for transmitting data across the isolation barrier and coupled to the transmit plates and a receiver for receiving the data and coupled to the receive plates, and the transmit and receive plates are arranged in a stacked configuration. a first processing unit ; a first communication interface coupled to the first processing unit; a second communication interface ; and an electric-field capacitive coupler that defines an isolation barrier coupled between the first communication interface and the second communication interface, wherein the second communication interface is coupled to a second processing unit , wherein the second processing unit is operably associated with an electrosurgical generator assembly , wherein: the electric-field capacitive coupler includes two transmit plates and two receive plates, a transmitter for transmitting data across the isolation barrier and coupled to the transmit plates and a receiver for receiving the data and coupled to the receive plates, and the transmit and receive plates are arranged in a stacked configuration.
A method for performing an earthmoving operation with a work vehicle , the work vehicle having an articulable implement , the method comprising: receiving, with a computing device , an input associated with a target profile of a worksite; receiving, with the computing device , data indicative of a soil composition of a worksite below a surface of the worksite; generating, with the computing device , an earthmoving prescription map based at least in part on the target profile of the worksite and the soil composition of the worksite, the earthmoving prescription map indicating soil composition layers between the surface of the worksite and the target profile of the worksite; and controlling, with the computing device , an operation of the work vehicle based at least in part on the earthmoving prescription map to automatically perform an earthmoving operation to separate the different soil composition layers based on the earthmoving prescription map; the method is characterized in that controlling the operation of the work vehicle comprises controlling the operation of the work vehicle to perform an earthmoving operation with the implement at the worksite based at least in part on the earthmoving prescription map , wherein the earthmoving prescription map identifies the depth range across which each soil composition layer extends for each position within the worksite. receiving, with a computing device , an input associated with a target profile of a worksite; receiving, with the computing device , data indicative of a soil composition of a worksite below a surface of the worksite; generating, with the computing device , an earthmoving prescription map based at least in part on the target profile of the worksite and the soil composition of the worksite, the earthmoving prescription map indicating soil composition layers between the surface of the worksite and the target profile of the worksite; and controlling, with the computing device , an operation of the work vehicle based at least in part on the earthmoving prescription map to automatically perform an earthmoving operation to separate the different soil composition layers based on the earthmoving prescription map; the method is characterized in that controlling the operation of the work vehicle comprises controlling the operation of the work vehicle to perform an earthmoving operation with the implement at the worksite based at least in part on the earthmoving prescription map , wherein the earthmoving prescription map identifies the depth range across which each soil composition layer extends for each position within the worksite.
A downhole antenna tool comprising: a substrate comprising a plurality of antenna bars that are releasably coupled to the substrate ; coils wound on individual ones of the plurality of antenna bars through associated coil carriers of the individual ones of the plurality of antenna bars ; and characterised by a protective coating over the coils; wherein the plurality of antenna bars are mechanically decoupled from the substrate . a substrate comprising a plurality of antenna bars that are releasably coupled to the substrate ; coils wound on individual ones of the plurality of antenna bars through associated coil carriers of the individual ones of the plurality of antenna bars ; and characterised by a protective coating over the coils; wherein the plurality of antenna bars are mechanically decoupled from the substrate .
A modular and autonomous assembly for detecting the angular position of the blades of a turbine engine , the modular assembly being configured to be mounted in a reversible way on a turbine engine including a first impeller comprising a first number of blades (111 to 115) and a second impeller comprising a second number of blades (121 to 127), each of the two impellers having an air flow passing through it and being coupled directly or indirectly to one another, and the first number of blades of the first impeller and the second number of blades of the second impeller being distinct and mutually prime, the assembly comprising: - at least one electrical power source allowing the operation of the elements of the detection assembly independently of the turbine engine on which it is intended to be carried, - at least one first sensor configured to be associated with the first impeller , - at least one second sensor configured to be associated with the second impeller , - and a main housing including a main processing unit and storage means , each of said sensors being configured to generate a signal (S 1 , S 2 ) at each passage of a blade of an impeller in front of the sensor, and the main processing unit being configured to determine the time interval separating the detection of a blade (111 to 115) of the first impeller with the detection of each of the blades (121 to 127) of the second impeller . the assembly comprising: - at least one electrical power source allowing the operation of the elements of the detection assembly independently of the turbine engine on which it is intended to be carried, - at least one first sensor configured to be associated with the first impeller , - at least one second sensor configured to be associated with the second impeller , - and a main housing including a main processing unit and storage means , - at least one electrical power source allowing the operation of the elements of the detection assembly independently of the turbine engine on which it is intended to be carried, - at least one first sensor configured to be associated with the first impeller , - at least one second sensor configured to be associated with the second impeller , - and a main housing including a main processing unit and storage means , each of said sensors being configured to generate a signal (S 1 , S 2 ) at each passage of a blade of an impeller in front of the sensor, and the main processing unit being configured to determine the time interval separating the detection of a blade (111 to 115) of the first impeller with the detection of each of the blades (121 to 127) of the second impeller .
A method for communication in a wireless network, comprising the following steps performed by a station: receiving (S500) a trigger frame, wherein the trigger frame comprises an identifier of a target resource unit, RU, allocated to the station, and the target RU is in a frequency domain; sending (S501) an uplink orthogonal frequency division multiple access physical layer protocol data unit, OFDMA PPDU, wherein a data part of the uplink OFDMA PPDU is sent on the target RU, and a common physical layer preamble of the uplink OFDMA PPDU is sent on one or more channel units in which the target RU is located; and receiving (S502) a downlink OFDMA PPDU in response to the uplink OFDMA PPDU, wherein the downlink OFDMA PPDU comprises an acknowledgement frame for the station, the acknowledgement frame for the station is received on a selected RU, the selected RU is in the frequency domain and in the one or more channel units, and the selected RU in the frequency domain is different from the target RU in the frequency domain. receiving (S500) a trigger frame, wherein the trigger frame comprises an identifier of a target resource unit, RU, allocated to the station, and the target RU is in a frequency domain; sending (S501) an uplink orthogonal frequency division multiple access physical layer protocol data unit, OFDMA PPDU, wherein a data part of the uplink OFDMA PPDU is sent on the target RU, and a common physical layer preamble of the uplink OFDMA PPDU is sent on one or more channel units in which the target RU is located; and receiving (S502) a downlink OFDMA PPDU in response to the uplink OFDMA PPDU, wherein the downlink OFDMA PPDU comprises an acknowledgement frame for the station, the acknowledgement frame for the station is received on a selected RU, the selected RU is in the frequency domain and in the one or more channel units, and the selected RU in the frequency domain is different from the target RU in the frequency domain.
A conductive hook-and-loop fastener comprising a base cloth containing a woven fabric, having existing on one surface thereof plural loop engagement elements including a multifilament yarn including as at least a part thereof a conductive filament, wherein the multifilament yarn constituting the loop engagement elements is inwoven in a warp direction of the woven fabric, wherein the conductive hook-and-loop fastener is a hook-and-loop coexistence type fastener including plural hook engagement elements including a monofilament yarn and the plural loop engagement elements, coexisting on one surface of the base cloth containing the woven fabric, and wherein the monofilament yarn constituting the hook engagement elements is a non-conductive monofilament yarn. wherein the multifilament yarn constituting the loop engagement elements is inwoven in a warp direction of the woven fabric, wherein the conductive hook-and-loop fastener is a hook-and-loop coexistence type fastener including plural hook engagement elements including a monofilament yarn and the plural loop engagement elements, coexisting on one surface of the base cloth containing the woven fabric, and wherein the monofilament yarn constituting the hook engagement elements is a non-conductive monofilament yarn.
An orthopedic implant extraction tool comprising: a handle ; a gripping handle pivotably connected to the handle; a movable jaw connected to the gripping handle; and a modular jaw adapted to be connected to the handle, the modular jaw including: an elongated body , a claw about a distal end of the elongated body for engaging an object, and a locking mechanism about a posterior end of the elongated body for engaging the orthopedic implant extraction tool, characterised in that the locking mechanism includes: a dovetail lock , a detent mounted to the dovetail lock, and a distally facing surface about a proximal end of the elongated body; wherein the orthopedic implant extraction tool further comprises a shaft adapted to be connected to the handle for locking the modular jaw in position. a handle ; a gripping handle pivotably connected to the handle; a movable jaw connected to the gripping handle; and a modular jaw adapted to be connected to the handle, the modular jaw including: an elongated body , a claw about a distal end of the elongated body for engaging an object, and a locking mechanism about a posterior end of the elongated body for engaging the orthopedic implant extraction tool, characterised in that the locking mechanism includes: a dovetail lock , a detent mounted to the dovetail lock, and a distally facing surface about a proximal end of the elongated body; wherein the orthopedic implant extraction tool further comprises a shaft adapted to be connected to the handle for locking the modular jaw in position. a modular jaw adapted to be connected to the handle, the modular jaw including: an elongated body , a claw about a distal end of the elongated body for engaging an object, and a locking mechanism about a posterior end of the elongated body for engaging the orthopedic implant extraction tool, characterised in that the locking mechanism includes: a dovetail lock , a detent mounted to the dovetail lock, and a distally facing surface about a proximal end of the elongated body; wherein the orthopedic implant extraction tool further comprises an elongated body , a claw about a distal end of the elongated body for engaging an object, and a locking mechanism about a posterior end of the elongated body for engaging the orthopedic implant extraction tool, characterised in that the locking mechanism includes: a dovetail lock , a detent mounted to the dovetail lock, and a distally facing surface about a proximal end of the elongated body; wherein the orthopedic implant extraction tool further comprises a dovetail lock , a detent mounted to the dovetail lock, and a distally facing surface about a proximal end of the elongated body; wherein the orthopedic implant extraction tool further comprises a shaft adapted to be connected to the handle for locking the modular jaw in position.
An aircraft monitoring system comprising: an aircraft; a fiber optic mesh ; optical transmitter system connected to the fiber optic mesh , wherein the optical transmitter system is operable to send optical signals into the fiber optic mesh ; optical receiver system connected to fiber optic mesh , wherein the optical receiver system is operable to detect response optical signals occurring in response to the optical signals sent into the fiber optic mesh by the optical transmitter system and generate sensor data from the response optical signals detected; and a computer system in communication with the optical transmitter system and the optical receiver system , wherein the computer system is operable to control the optical transmitter system to send the optical signals into the fiber optic mesh ; is operable to receive sensor data from the optical receiver system during operation of the aircraft , and is operable to determine whether a group of nonconformances is present in the aircraft using the sensor data , wherein: fiber optic mesh comprises a film and optical fibers attached or adhered to one side of the film or embedded or integrated within the film ; and the optical fibers comprise first optical fibers parallel to each other and second optical fibers parallel to each other, wherein the first optical fibers intersect the second optical fibers , characterized in that : the film is a tape; and the fiber optic mesh covers an exterior surface of the aircraft. an aircraft; a fiber optic mesh ; optical transmitter system connected to the fiber optic mesh , wherein the optical transmitter system is operable to send optical signals into the fiber optic mesh ; optical receiver system connected to fiber optic mesh , wherein the optical receiver system is operable to detect response optical signals occurring in response to the optical signals sent into the fiber optic mesh by the optical transmitter system and generate sensor data from the response optical signals detected; and a computer system in communication with the optical transmitter system and the optical receiver system , wherein the computer system is operable to control the optical transmitter system to send the optical signals into the fiber optic mesh ; is operable to receive sensor data from the optical receiver system during operation of the aircraft , and is operable to determine whether a group of nonconformances is present in the aircraft using the sensor data , wherein: fiber optic mesh comprises a film and optical fibers attached or adhered to one side of the film or embedded or integrated within the film ; and the optical fibers comprise first optical fibers parallel to each other and second optical fibers parallel to each other, wherein the first optical fibers intersect the second optical fibers , characterized in that : the film is a tape; and the fiber optic mesh covers an exterior surface of the aircraft. the film is a tape; and the fiber optic mesh covers an exterior surface of the aircraft.
A device for capturing vibrations produced by an object, the device comprising: a first sensor in contact with a surface of the object; a second sensor being a coil sensor and spaced apart from the first sensor ; characterized by a clamping mechanism configured to fix the device and thus both, the first sensor and the second sensor , to the object, wherein the first sensor is placed in contact with the object by the clamping mechanism , wherein the second sensor is spaced apart from the object, suspended above the object, and located at a fixed location relative to the object by the clamping mechanism , and wherein the first sensor is a sensor element which captures vibration in the object at the clamping mechanism . a first sensor in contact with a surface of the object; a second sensor being a coil sensor and spaced apart from the first sensor ; characterized by a clamping mechanism configured to fix the device and thus both, the first sensor and the second sensor , to the object, wherein the first sensor is placed in contact with the object by the clamping mechanism , wherein the second sensor is spaced apart from the object, suspended above the object, and located at a fixed location relative to the object by the clamping mechanism , and wherein the first sensor is a sensor element which captures vibration in the object at the clamping mechanism .
A liquid concentrated neutralized vinegar with a total dry matter content of at least 50% (w/w) and with a total acidity based on acetic acid of at least 500 mmol per 100 g and comprising potassium cations in an amount of at least 50 (mol) % of the total amount of cations present.