mhurhangee/patent-ind-claim-en huggingface dataset:
A computing device comprising: at least one master unit ; at least one slave unit (204-1); an interconnect structure configured to route transactions from the at least one master unit to the at least one slave unit (204-1); and a transaction logger device configured to intercept all communication between a master unit and the interconnect structure and receive transactions sent by the at least one master unit to the at least one slave unit (204-1) via the interconnect structure , extract a data set from each of the received transactions, save the extracted data set as a record of outstanding transactions, wherein the transaction logger device is further configured to receive a reset signal independent of the at least one master unit, when a reset is triggered and preserve the record of outstanding transactions when at least a part of the computing device is restarted. at least one master unit ; at least one slave unit (204-1); an interconnect structure configured to route transactions from the at least one master unit to the at least one slave unit (204-1); and a transaction logger device configured to intercept all communication between a master unit and the interconnect structure and receive transactions sent by the at least one master unit to the at least one slave unit (204-1) via the interconnect structure , extract a data set from each of the received transactions, save the extracted data set as a record of outstanding transactions, wherein the transaction logger device is further configured to receive a reset signal independent of the at least one master unit, when a reset is triggered and preserve the record of outstanding transactions when at least a part of the computing device is restarted.
A satellite deployment system comprising: a plurality of releasable dispenser modules attached to and stacked on top of each other, each releasable dispenser module configured to support a plurality of satellites to be deployed in orbit, wherein each releasable dispenser module is ring-shaped and comprises, on an outer surface , separation assemblies configured to releasably attach a plurality of satellites on an associated releasable ring-shaped dispenser module; and a controller comprising a dispenser module controller for each dispenser module, said controller being configured to: release each dispenser module from a launch vehicle; and for the each released module , to sequentially release into space, by the dispenser module controller , individual satellites of the plurality of satellites from the released dispenser module , with a time period chosen between two sequential releases to avoid collision of any two satellites of the plurality of satellites with each other. a plurality of releasable dispenser modules attached to and stacked on top of each other, each releasable dispenser module configured to support a plurality of satellites to be deployed in orbit, wherein each releasable dispenser module is ring-shaped and comprises, on an outer surface , separation assemblies configured to releasably attach a plurality of satellites on an associated releasable ring-shaped dispenser module; and a controller comprising a dispenser module controller for each dispenser module, said controller being configured to: release each dispenser module from a launch vehicle; and for the each released module , to sequentially release into space, by the dispenser module controller , individual satellites of the plurality of satellites from the released dispenser module , with a time period chosen between two sequential releases to avoid collision of any two satellites of the plurality of satellites with each other. release each dispenser module from a launch vehicle; and for the each released module , to sequentially release into space, by the dispenser module controller , individual satellites of the plurality of satellites from the released dispenser module , with a time period chosen between two sequential releases to avoid collision of any two satellites of the plurality of satellites with each other.
An active homing radar device mounted in a flying vehicle using a radar wave generated thereby, the radar device comprising: an antenna device to irradiate a target with the radar wave; a receiver to receive a reflected wave from the target through the antenna device ; and a signal processor to perform coherent integration processing on a reception signal from the receiver , to observe a clutter level by using a signal on which the coherent integration processing has been performed, and to control a transmission duty ratio such that a clutter level observed becomes equal to or closer to a receiver noise level, wherein the radar device determines whether a target to be handled is departing from the vehicle or approaching the vehicle , and when the target is departing from the vehicle , the radar device reduces the transmission duty ratio compared to when the target is approaching the vehicle . an antenna device to irradiate a target with the radar wave; a receiver to receive a reflected wave from the target through the antenna device ; and a signal processor to perform coherent integration processing on a reception signal from the receiver , to observe a clutter level by using a signal on which the coherent integration processing has been performed, and to control a transmission duty ratio such that a clutter level observed becomes equal to or closer to a receiver noise level, wherein the radar device determines whether a target to be handled is departing from the vehicle or approaching the vehicle , and when the target is departing from the vehicle , the radar device reduces the transmission duty ratio compared to when the target is approaching the vehicle .
Frame for a prefabricated element for a building, comprising: - a plurality of support structures , each support structure consisting of a plurality of main beams connected together, wherein each support structure is arranged on a respective level of at least two levels which are parallel and spaced apart from each other in a thickness direction of the frame (X-X), said plurality of support structures defining at least one pair of homologous support structures including two support structures arranged on distinct levels and facing each other in said thickness direction (X-X), wherein the support structures are configured to support a panel of the prefabricated element for each level, - a plurality of connecting members , each connecting member connecting two of said homologous support structures facing each other, and - a plurality of tensioning cables , each cable being arranged between two distinct levels and having two ends , the two ends of each cable being secured to two distinct connecting members to make the frame work as a tensile structure. - a plurality of support structures , each support structure consisting of a plurality of main beams connected together, wherein each support structure is arranged on a respective level of at least two levels which are parallel and spaced apart from each other in a thickness direction of the frame (X-X), said plurality of support structures defining at least one pair of homologous support structures including two support structures arranged on distinct levels and facing each other in said thickness direction (X-X), wherein the support structures are configured to support a panel of the prefabricated element for each level, wherein each support structure is arranged on a respective level of at least two levels which are parallel and spaced apart from each other in a thickness direction of the frame (X-X), said plurality of support structures defining at least one pair of homologous support structures including two support structures arranged on distinct levels and facing each other in said thickness direction (X-X), wherein the support structures are configured to support a panel of the prefabricated element for each level, - a plurality of connecting members , each connecting member connecting two of said homologous support structures facing each other, and - a plurality of tensioning cables , each cable being arranged between two distinct levels and having two ends , the two ends of each cable being secured to two distinct connecting members to make the frame work as a tensile structure.
A gas turbine engine comprising: an oil tank assembly comprising: an oil tank defining an interior; and a heat exchanger integrated with the oil tank and having a cooling conduit defined at least in part by a fuel line of a fuel circuit ; wherein the oil tank has a wall with an internal passage , which forms a portion of the fuel line; and wherein the fuel line passes through the interior; and an engine core with a combustion section ; the fuel circuit fluidly coupled to the combustion section ; and an oil circuit fluidly coupled to the engine core , the oil circuit comprising the oil tank . an oil tank assembly comprising: an oil tank defining an interior; and a heat exchanger integrated with the oil tank and having a cooling conduit defined at least in part by a fuel line of a fuel circuit ; wherein the oil tank has a wall with an internal passage , which forms a portion of the fuel line; and wherein the fuel line passes through the interior; and an oil tank defining an interior; and a heat exchanger integrated with the oil tank and having a cooling conduit defined at least in part by a fuel line of a fuel circuit ; wherein the oil tank has a wall with an internal passage , which forms a portion of the fuel line; and wherein the fuel line passes through the interior; and an engine core with a combustion section ; the fuel circuit fluidly coupled to the combustion section ; and an oil circuit fluidly coupled to the engine core , the oil circuit comprising the oil tank .
A crystalline composite comprising ■ sodium bicarbonate (NaHCO 3 ), ■ anhydrous sodium carbonate (Na 2 CO 3 ) or sodium carbonate in hydrated form (Na2CO 3 .nH 2 O), ■ at least one ammonium salt, characterised in that the composite comprises o 50 to 65% by weight of bicarbonate ion, o 2 to 9% by weight of carbonate ion, o 0.5 to 5% by weight of ammonia equivalent from ammonium ion. ■ sodium bicarbonate (NaHCO 3 ), ■ anhydrous sodium carbonate (Na 2 CO 3 ) or sodium carbonate in hydrated form (Na2CO 3 .nH 2 O), ■ at least one ammonium salt, o 50 to 65% by weight of bicarbonate ion, o 2 to 9% by weight of carbonate ion, o 0.5 to 5% by weight of ammonia equivalent from ammonium ion.
A surface enhanced Raman scattering unit , comprising: a support that includes a cavity provided with an opening ; an optical functional portion that is disposed in the cavity to face the opening and causes surface enhanced Raman scattering; and a package that accommodates the support and is evacuated, wherein: the package is flexible and formed in a bag shape; the package is in contact with at least an edge of the opening , characterized in that the package is bent toward the optical functional portion in a state in which the package is spaced apart from the optical functional portion in the opening ; and the package is bent toward the optical functional portion due to evacuation. a support that includes a cavity provided with an opening ; an optical functional portion that is disposed in the cavity to face the opening and causes surface enhanced Raman scattering; and a package that accommodates the support and is evacuated, wherein: the package is flexible and formed in a bag shape; the package is in contact with at least an edge of the opening , characterized in that the package is bent toward the optical functional portion in a state in which the package is spaced apart from the optical functional portion in the opening ; and the package is bent toward the optical functional portion due to evacuation. the package is flexible and formed in a bag shape; the package is in contact with at least an edge of the opening , characterized in that the package is bent toward the optical functional portion in a state in which the package is spaced apart from the optical functional portion in the opening ; and the package is bent toward the optical functional portion due to evacuation.
An ink conditioner for an inkjet printer, comprising a main body with an ink damping cavity , the ink conditioner further comprising a heat transfer element , at least one ink inlet and at least one ink outlet , characterised in that the main body , the heat transfer element , the at least one ink inlet and the at least one ink outlet consist of the same material and form a single piece.
A system arrangement for lifting mechanisms comprising at least one drive motor , at least one cable drum connected thereto, a reduction transmission arranged between the drive motor and the cable drum , an automatic overrun shutdown means, and at least one safety brake , characterised in that instead of at least one passive operating brake there is provided at least one active motor locking means for holding the load when the drive motor is slowed down to the rotary speed '0'.
An airfoil comprising: an airfoil wall defining a leading end , a trailing end , and first and second sides joining the leading end and the trailing end ; first and second ribs each connecting the first and second sides of the airfoil wall , each of the first and second ribs defining a tube portion circumscribing a rib passage and including cooling apertures , and first and second connector arms solely joining the tube portion to, respectively, the first and second sides of the airfoil wall , the airfoil wall and the first and second ribs bounding a cooling channel there between, characterized by the cooling apertures of the first and second ribs opening at the cooling channel such that there is a cooling circuit in which the rib passage of the first rib is fluidly connected to the rib passage of the second rib through the cooling apertures of the first rib , then from the cooling apertures of the first rib to the cooling channel , and then from the cooling channel to the cooling apertures of the second rib . an airfoil wall defining a leading end , a trailing end , and first and second sides joining the leading end and the trailing end ; first and second ribs each connecting the first and second sides of the airfoil wall , each of the first and second ribs defining a tube portion circumscribing a rib passage and including cooling apertures , and first and second connector arms solely joining the tube portion to, respectively, the first and second sides of the airfoil wall , a tube portion circumscribing a rib passage and including cooling apertures , and first and second connector arms solely joining the tube portion to, respectively, the first and second sides of the airfoil wall , the airfoil wall and the first and second ribs bounding a cooling channel there between, characterized by the cooling apertures of the first and second ribs opening at the cooling channel such that there is a cooling circuit in which the rib passage of the first rib is fluidly connected to the rib passage of the second rib through the cooling apertures of the first rib , then from the cooling apertures of the first rib to the cooling channel , and then from the cooling channel to the cooling apertures of the second rib .
A cover article comprising: a glass sleeve structure having an internal cavity, a first index of refraction, and a non-circular cross section; a second glass structure between at least part of the glass sleeve structure and the internal cavity, disposed on at least part of the interior of the glass sleeve structure, and having a second index of refraction; and an index-matching material present between the glass sleeve and second glass structure, wherein the index-matching material is disposed on at least part of the interior of the glass sleeve and has a third refractive index, wherein the third refractive index is within ±10% of the first or the second index of refraction; wherein the glass sleeve has been thermally or chemically tempered and has a thickness from 0.3 mm to 2.0 mm and the second glass structure has a thickness from 30 μm to 0.5 mm; and wherein the index-matching material comprises a polymer, liquid, cement, adhesive, or gel; and wherein the second index of refraction is within ±10% of the first index of refraction and the third refractive index is within ±10% of the first index of refraction. a glass sleeve structure having an internal cavity, a first index of refraction, and a non-circular cross section; a second glass structure between at least part of the glass sleeve structure and the internal cavity, disposed on at least part of the interior of the glass sleeve structure, and having a second index of refraction; and an index-matching material present between the glass sleeve and second glass structure, wherein the index-matching material is disposed on at least part of the interior of the glass sleeve and has a third refractive index, wherein the third refractive index is within ±10% of the first or the second index of refraction;
A tube filter for smoking a smokable substance, the tube filter comprising: a receiving section having a receiving chamber dimensioned to receive the smokable substance; a smoke section having a smoke chamber to output smoke produced while the smokable substance is ignited, wherein the smoke section has a first open end into the smoke chamber and the receiving section has a second open end into the receiving chamber that is opposite to the first end ; characterized in that the tube filter further comprises: a first indentation and a second indentation that separates the receiving chamber from the smoke chamber , the first indentation formed from a first concave portion of a wall of the tube filter and the second indentation formed from a second concave portion of the wall of the tube filter , wherein the first concave portion and the second concave portion are at least partially disposed within a cross-section of the tube filter , wherein the first indentation and the second indentation form a path inside the tube filter that fluidly couples the receiving chamber to the smoke chamber and that runs diagonally through a center longitudinal axis of the tube filter , and wherein the first indentation is radially separated from the second indentation about the center longitudinal axis by 180°. a receiving section having a receiving chamber dimensioned to receive the smokable substance; a smoke section having a smoke chamber to output smoke produced while the smokable substance is ignited, wherein the smoke section has a first open end into the smoke chamber and the receiving section has a second open end into the receiving chamber that is opposite to the first end ; characterized in that the tube filter further comprises: a first indentation and a second indentation that separates the receiving chamber from the smoke chamber , the first indentation formed from a first concave portion of a wall of the tube filter and the second indentation formed from a second concave portion of the wall of the tube filter , wherein the first concave portion and the second concave portion are at least partially disposed within a cross-section of the tube filter , wherein the first indentation and the second indentation form a path inside the tube filter that fluidly couples the receiving chamber to the smoke chamber and that runs diagonally through a center longitudinal axis of the tube filter , and wherein the first indentation is radially separated from the second indentation about the center longitudinal axis by 180°.
A hybrid loader boom arm assembly kit for a loader work vehicle, the kit comprising: a hollow first beam formed from a first material having a weight lighter than steel, and having a first end for coupling to a work vehicle and a first through bore at the first end; a first block formed from a second material having a weight lighter than steel, the first block having a central cross bore , the first block configured to be received within the first end of the hollow first beam ; at least one first steel reinforcing plate configured to couple to the hollow first beam at a second end of the hollow first beam ; and at least one connecting plate configured to couple to the at least one first steel reinforcing plate and to connect the hollow first beam to a hollow second beam formed from the first material. a hollow first beam formed from a first material having a weight lighter than steel, and having a first end for coupling to a work vehicle and a first through bore at the first end; a first block formed from a second material having a weight lighter than steel, the first block having a central cross bore , the first block configured to be received within the first end of the hollow first beam ; at least one first steel reinforcing plate configured to couple to the hollow first beam at a second end of the hollow first beam ; and at least one connecting plate configured to couple to the at least one first steel reinforcing plate and to connect the hollow first beam to a hollow second beam formed from the first material.
A method of operating a communication network device for coordinating communication between devices in a network, comprising: generating, by the communication network device, a first identification code; assigning, by the communication network device, the first identification code to a first application executing on a first device, wherein the first identification code is unique to the first application executing on the first device; receiving, by the communication network device, a transmission of data from a sending device, wherein the transmission specifies a recipient of the data using the first identification code, the recipient being different from the sending device; determining, by the communication network device, that the transmission of data is incompatible with the first application based on compatibility information of the first application; modifying, by the communication network device, the data to generate a version of the data that is compatible with the first application; determining, by the communication network device, that the transmission is incompatible with the first device based on compatibility information of the first device; modifying, by the communication network device, the data to generate a version of the data compatible with the first device; and transmitting, by the communication network device, the transmission of data to the recipient. generating, by the communication network device, a first identification code; assigning, by the communication network device, the first identification code to a first application executing on a first device, wherein the first identification code is unique to the first application executing on the first device; receiving, by the communication network device, a transmission of data from a sending device, wherein the transmission specifies a recipient of the data using the first identification code, the recipient being different from the sending device; determining, by the communication network device, that the transmission of data is incompatible with the first application based on compatibility information of the first application; modifying, by the communication network device, the data to generate a version of the data that is compatible with the first application; determining, by the communication network device, that the transmission is incompatible with the first device based on compatibility information of the first device; modifying, by the communication network device, the data to generate a version of the data compatible with the first device; and transmitting, by the communication network device, the transmission of data to the recipient.