mhurhangee/patent-ind-claim-en huggingface dataset:
A cup impactor assembly comprising: a shaft ; a cup coupler at a cup end of the shaft adapted to releasably connect a cup in fixed relation for subsequent impacting; a handle at an impacting end of the shaft; an inertial sensor unit adapted to produce at least an orientation output related to an orientation of the cup impactor assembly and having a patient-specific file comprising: calibration data based on a planned geometric relation between an initial reference orientation of the cup impactor assembly and a reference, the calibration data for calibrating the inertial sensor unit relative to the pelvis for the inertial sensor unit to produce said orientation output; and a desired acetabular cup orientation data based on preoperative planning, characterised by a visual guide mounted to at least one of the shaft and the handle, the visual guide producing visual guidance toward at least one anatomical landmark of a pelvis, and in that the calibration data are based on a planned geometric relation between the initial reference orientation of the cup impactor assembly and the at least one anatomical landmark of the pelvis via the visual guidance of the visual guide. a shaft ; a cup coupler at a cup end of the shaft adapted to releasably connect a cup in fixed relation for subsequent impacting; a handle at an impacting end of the shaft; an inertial sensor unit adapted to produce at least an orientation output related to an orientation of the cup impactor assembly and having a patient-specific file comprising: calibration data based on a planned geometric relation between an initial reference orientation of the cup impactor assembly and a reference, the calibration data for calibrating the inertial sensor unit relative to the pelvis for the inertial sensor unit to produce said orientation output; and a desired acetabular cup orientation data based on preoperative planning, characterised by a visual guide mounted to at least one of the shaft and the handle, the visual guide producing visual guidance toward at least one anatomical landmark of a pelvis, and in that the calibration data are based on a planned geometric relation between the initial reference orientation of the cup impactor assembly and the at least one anatomical landmark of the pelvis via the visual guidance of the visual guide. calibration data based on a planned geometric relation between an initial reference orientation of the cup impactor assembly and a reference, the calibration data for calibrating the inertial sensor unit relative to the pelvis for the inertial sensor unit to produce said orientation output; and a desired acetabular cup orientation data based on preoperative planning, characterised by a visual guide mounted to at least one of the shaft and the handle, the visual guide producing visual guidance toward at least one anatomical landmark of a pelvis, and in that the calibration data are based on a planned geometric relation between the initial reference orientation of the cup impactor assembly and the at least one anatomical landmark of the pelvis via the visual guidance of the visual guide.
A method for sending a network packet, applied in a device comprising a network processor and an external storage space with which the network processor interacts through a bus, the method comprising: planning, in an initialization stage, header information stored in a memory of the network processor and header information stored in the external storage space respectively according to a frequency of the header information and traffic solution requirements in actual scenarios; in a case where the header information of the network packet is stored in the memory of the network processor, obtaining , by the network processor, the header information of the network packet from a mapping table stored in the memory of the network processor; and in a case where the header information of the network packet is stored in the external storage space, obtaining, by the network processor, the header information of the network packet from the external storage space, and storing the header information in a mapping table in a cache of the network processor; generating the network packet according to the header information and a payload; and sending , by the network processor, the network packet. planning, in an initialization stage, header information stored in a memory of the network processor and header information stored in the external storage space respectively according to a frequency of the header information and traffic solution requirements in actual scenarios; in a case where the header information of the network packet is stored in the memory of the network processor, obtaining , by the network processor, the header information of the network packet from a mapping table stored in the memory of the network processor; and in a case where the header information of the network packet is stored in the external storage space, obtaining, by the network processor, the header information of the network packet from the external storage space, and storing the header information in a mapping table in a cache of the network processor; generating the network packet according to the header information and a payload; and sending , by the network processor, the network packet.
A dual coil solenoid valve for a fuel gas control valve, comprising a stationary coil assembly and a moving coil assembly , wherein said stationary coil assembly comprises a stationary magnetic core and a stationary coil , said moving coil assembly comprises a moving magnetic core and a moving coil , a groove is provided on the inside of both said stationary magnetic core and said moving magnetic core , said stationary coil is arranged in the groove of said stationary magnetic core , said moving coil is arranged in the groove of said moving magnetic core , and said stationary coil assembly and said moving coil assembly have the same cross-sectional shape and area and are arranged oppositely with their axes coinciding with each other; characterized in that said stationary magnetic core and moving magnetic core are E-shaped.
A manufacturing method of a carbon-coated lithium iron phosphate material, characterized by comprising steps of: (a) providing a first slurry, a carbon source and a lithium source, wherein the first slurry is formed from an iron source and a phosphorus source; (b) mixing the first slurry, the carbon source and the lithium source to form a second slurry, and grinding the second slurry in a tank at a first temperature to form a third slurry, wherein the first temperature is ranged from 25 °C to 40 °C; and (c) drying and sintering the third slurry to form the carbon-coated lithium iron phosphate material including a core layer and a coating layer coated on the core layer, wherein the core layer comprises lithium, iron, and phosphorus, wherein the coating layer comprises carbon. (a) providing a first slurry, a carbon source and a lithium source, wherein the first slurry is formed from an iron source and a phosphorus source; (b) mixing the first slurry, the carbon source and the lithium source to form a second slurry, and grinding the second slurry in a tank at a first temperature to form a third slurry, wherein the first temperature is ranged from 25 °C to 40 °C; and (c) drying and sintering the third slurry to form the carbon-coated lithium iron phosphate material including a core layer and a coating layer coated on the core layer, wherein the core layer comprises lithium, iron, and phosphorus, wherein the coating layer comprises carbon.
A high voltage electrical system for a vehicle, the system comprising: a high voltage battery unit having a first high voltage battery connected in series with a second high voltage battery such that a nominal operating voltage of the battery unit is the sum of a voltage of the first high voltage battery and a voltage of the second high voltage battery , characterized in that the high voltage electrical system further comprises: a bi-directional high voltage DC/DC-converter connected in parallel with the first high voltage battery and with the second high voltage battery , the DC/DC-converter being arranged to receive a charging voltage from a high voltage inlet or from a propulsion converter connected to an electrical machine ; wherein the DC/DC converter is configured to control charging of the first and second high voltage battery to balance a state of charge of the first and second high voltage battery when receiving the charging voltage from either the high voltage inlet or from the propulsion converter . a bi-directional high voltage DC/DC-converter connected in parallel with the first high voltage battery and with the second high voltage battery , the DC/DC-converter being arranged to receive a charging voltage from a high voltage inlet or from a propulsion converter connected to an electrical machine ; wherein the DC/DC converter is configured to control charging of the first and second high voltage battery to balance a state of charge of the first and second high voltage battery when receiving the charging voltage from either the high voltage inlet or from the propulsion converter .
Cosmetic composition, comprising: - one or more amino silicones of formula (K): in which: - x ranges from 10 to 2000 and especially from 100 to 1000; - y ranges from 1 to 100; - A comprises 3 to 6 carbon atoms; and more particularly A is chosen from the following divalent radicals: -CH 2 CH 2 CH 2 and -CH 2 CH(CH 3 )CH 2 -; and - R1 and R2, which may be identical or different, are saturated linear alkyl radicals comprising 6 to 30 carbon atoms, preferably 8 to 24 carbon atoms and especially 12 to 20 carbon atoms; chosen in particular from dodecyl, tetradecyl, pentadecyl, hexadecyl, heptadecyl, octadecyl, nonadecyl and eicosyl radicals; preferentially, R1 and R2, which may be identical or different, is chosen from hexadecyl (cetyl) and octadecyl (stearyl) radicals. - one or more cationic surfactants, - at least 3% by weight of one or more fatty alcohols comprising 8 to 30 carbon atoms, and - one or more hydrocarbon-based oils chosen from linear or branched C6-C32 and especially C8-C24 alkanes. - one or more amino silicones of formula (K): in which: - x ranges from 10 to 2000 and especially from 100 to 1000; - y ranges from 1 to 100; - A comprises 3 to 6 carbon atoms; and more particularly A is chosen from the following divalent radicals: -CH 2 CH 2 CH 2 and -CH 2 CH(CH 3 )CH 2 -; and - R1 and R2, which may be identical or different, are saturated linear alkyl radicals comprising 6 to 30 carbon atoms, preferably 8 to 24 carbon atoms and especially 12 to 20 carbon atoms; chosen in particular from dodecyl, tetradecyl, pentadecyl, hexadecyl, heptadecyl, octadecyl, nonadecyl and eicosyl radicals; preferentially, R1 and R2, which may be identical or different, is chosen from hexadecyl (cetyl) and octadecyl (stearyl) radicals. - one or more cationic surfactants, - at least 3% by weight of one or more fatty alcohols comprising 8 to 30 carbon atoms, and - one or more hydrocarbon-based oils chosen from linear or branched C6-C32 and especially C8-C24 alkanes. - x ranges from 10 to 2000 and especially from 100 to 1000; - y ranges from 1 to 100; - A comprises 3 to 6 carbon atoms; and more particularly A is chosen from the following divalent radicals: -CH 2 CH 2 CH 2 and -CH 2 CH(CH 3 )CH 2 -; and - R1 and R2, which may be identical or different, are saturated linear alkyl radicals comprising 6 to 30 carbon atoms, preferably 8 to 24 carbon atoms and especially 12 to 20 carbon atoms; chosen in particular from dodecyl, tetradecyl, pentadecyl, hexadecyl, heptadecyl, octadecyl, nonadecyl and eicosyl radicals; preferentially, R1 and R2, which may be identical or different, is chosen from hexadecyl (cetyl) and octadecyl (stearyl) radicals. - one or more cationic surfactants, - at least 3% by weight of one or more fatty alcohols comprising 8 to 30 carbon atoms, and - one or more hydrocarbon-based oils chosen from linear or branched C6-C32 and especially C8-C24 alkanes.
A package formed of a resin film including a sealant film with a three-dimensionally shaped portion that protrudes outward, characterized in that the sealant film has a thinnest part at the three-dimensionally shaped portion that protrudes outward with a thickness of 50 to 95% of a thickness of the sealant film at a part other than the three-dimensionally shaped portion .
A method of air-to-air refueling, the method comprising: receiving a video frame; generating, from the video frame, a plurality of images having differing decreasing resolutions comprising blurring and downsampling the video frame; detecting, within each of the plurality of images, a set of aircraft keypoints for an aircraft to be refueled; merging the sets of aircraft keypoints into a set of merged aircraft keypoints; based on at least the merged aircraft keypoints, determining a position of a fuel receptacle on the aircraft; and determining a position of a boom tip of an aerial refueling boom. receiving a video frame; generating, from the video frame, a plurality of images having differing decreasing resolutions comprising blurring and downsampling the video frame; detecting, within each of the plurality of images, a set of aircraft keypoints for an aircraft to be refueled; merging the sets of aircraft keypoints into a set of merged aircraft keypoints; based on at least the merged aircraft keypoints, determining a position of a fuel receptacle on the aircraft; and determining a position of a boom tip of an aerial refueling boom.
A timepiece shaft (1; 1'; 1"), especially a balance shaft , comprising a first functional portion (2a; 2b) including at least one part (221a; 221b) of a pivot-shank (22a; 22b) and/or at least one part (211a; 211b) of a pivot (21a; 21b; 21'; 21"; 21*), wherein the first functional portion is made entirely of ceramic and a first outer diameter (D1) of the first functional portion is less than 0.5 mm, or less than 0.4 mm, or less than 0.2 mm, or less than 0.1 mm.
Assembly of an installation box and electric installation material with electric wirings, wherein the installation box comprises a housing with a first bottom wall and a first circumferential wall upright from the first bottom wall, wherein the first bottom wall and the first circumferential wall together enclose an installation space for electric installation material, wherein an upper edge of the first circumferential wall facing away from the first bottom wall confines an installation opening for providing access to the installation space, wherein the first circumferential wall is provided with at least one pair of slide couplings , such that the installation box is couplable with a further installation box, and with a passage below each of the at least one pair of slide couplings for electric wirings to pass through the first circumferential wall, characterized in that the installation box further comprises a separate airtight insert in the installation space, wherein the airtight insert comprises a second bottom wall and a second circumferential wall upright from the second bottom wall and an upper edge facing away from the second bottom wall , wherein the second circumferential wall is provided with at least one first membrane adjacent to the passage below the at least one pair of slide couplings , wherein the outer side of the second bottom wall and the second circumferential wall are beyond the installation opening and the passage complementary to the inner side of the first bottom wall and the first circumferential wall , wherein the airtight insert comprises an inner layer manufactured from a rigid material, such as polyolefin, preferably polypropylene, and an outer layer manufactured from an elastic material, such as a thermoplastic elastomer, wherein the at least one first membrane is provided by the outer layer of the airtight insert , and the first membrane is framed by an aperture in the inner layer of the airtight insert , and wherein the second circumferential wall has a second membrane with one or more target fractures that may be closed off with a membrane, through which the electric wirings can pass, wherein the electric wirings passing through the one or more target fractures are enclosed in an airtight manner.
A sliding member comprising: a lining layer formed from an alloy having a predetermined shape; and an overlay layer formed on an inner circumferential surface of the lining layer , the overlay layer being formed of resin, the overlay layer sliding with a shaft , the overlay layer including a raised portion a height of which in a predetermined area that includes each of an edge in an axial direction of the shaft is greater than a height of another area of the overlay layer ; wherein a surface of the lining layer is flat along the axial direction; and in a cross section parallel to the axial direction, the height of the overlay layer gradually increases from a starting point of the raised portion to a top point of the raised portion , and gradually decreases from the top point of the raised portion to the axial edge. a lining layer formed from an alloy having a predetermined shape; and an overlay layer formed on an inner circumferential surface of the lining layer , the overlay layer being formed of resin, the overlay layer sliding with a shaft , the overlay layer including a raised portion a height of which in a predetermined area that includes each of an edge in an axial direction of the shaft is greater than a height of another area of the overlay layer ; wherein a surface of the lining layer is flat along the axial direction; and in a cross section parallel to the axial direction, the height of the overlay layer gradually increases from a starting point of the raised portion to a top point of the raised portion , and gradually decreases from the top point of the raised portion to the axial edge.
A method for implementing a generic routing encapsulation, GRE, tunnel, comprising: obtaining , by an access device, an address of an aggregation gateway group, wherein the aggregation gateway group comprises at least one aggregation gateway; sending , by the access device and by using the address of the aggregation gateway group as a destination address, a GRE tunnel setup request in which an address of the access device is encapsulated, wherein the GRE tunnel setup request is used to request for setting up a first GRE tunnel; receiving , by the access device, a GRE tunnel setup accept response sent back by a first aggregation gateway, wherein an address of a line card in the first aggregation gateway is encapsulated in the GRE tunnel setup accept response, and obtaining the address of the line card in the first aggregation gateway from the GRE tunnel setup accept response, wherein the first aggregation gateway belongs to the aggregation gateway group; and configuring , by the access device, the address of the line card as a network side destination address of the first GRE tunnel. obtaining , by an access device, an address of an aggregation gateway group, wherein the aggregation gateway group comprises at least one aggregation gateway; sending , by the access device and by using the address of the aggregation gateway group as a destination address, a GRE tunnel setup request in which an address of the access device is encapsulated, wherein the GRE tunnel setup request is used to request for setting up a first GRE tunnel; receiving , by the access device, a GRE tunnel setup accept response sent back by a first aggregation gateway, wherein an address of a line card in the first aggregation gateway is encapsulated in the GRE tunnel setup accept response, and obtaining the address of the line card in the first aggregation gateway from the GRE tunnel setup accept response, wherein the first aggregation gateway belongs to the aggregation gateway group; and configuring , by the access device, the address of the line card as a network side destination address of the first GRE tunnel.
A process for formulating buffer products for feeding to a bioprocess comprising: combining multiple buffer solutions to form a final buffer product, the multiple buffer solutions including at least a first buffer solution and a second buffer solution; measuring a conductivity of the final buffer product; measuring a refractive index of the final buffer product; comparing the measured conductivity to a preset conductivity range and comparing the measured refractive index to a preset refractive index range; and selectively adjusting a flow rate of at least one of the first buffer solution in relation to a flow rate of the second buffer solution in order to maintain the conductivity and the refractive index of the final buffer product within the preset ranges. combining multiple buffer solutions to form a final buffer product, the multiple buffer solutions including at least a first buffer solution and a second buffer solution; measuring a conductivity of the final buffer product; measuring a refractive index of the final buffer product; comparing the measured conductivity to a preset conductivity range and comparing the measured refractive index to a preset refractive index range; and selectively adjusting a flow rate of at least one of the first buffer solution in relation to a flow rate of the second buffer solution in order to maintain the conductivity and the refractive index of the final buffer product within the preset ranges.
Assembly for material processing using a laser beam, in particular for laser drilling, with - a dynamic deflection device (AE) for the laser beam (LS), which is designed to deflect the laser beam (LS) into two directions extending perpendicularly to each other, and - an optical assembly, with which a laser beam exiting the deflection device (AE) is focussed onto a processing plane (W), - wherein the optical assembly includes a first optical system (OS1) and a second optical system (OS2) along an optical axis of the optical assembly, which are designed and arranged such that the laser beam (LS) forms a intermediate focus (ZF) between the first and second optical systems (OS1, OS2), characterized in that the laser beam when entering the first optical system (OS1) at an angle to the optical axis and at a distance therefrom intersects the optical axis between the second optical system (OS2) and the processing plane (W). - a dynamic deflection device (AE) for the laser beam (LS), which is designed to deflect the laser beam (LS) into two directions extending perpendicularly to each other, and - an optical assembly, with which a laser beam exiting the deflection device (AE) is focussed onto a processing plane (W), - wherein the optical assembly includes a first optical system (OS1) and a second optical system (OS2) along an optical axis of the optical assembly, which are designed and arranged such that the laser beam (LS) forms a intermediate focus (ZF) between the first and second optical systems (OS1, OS2), characterized in that the laser beam when entering the first optical system (OS1) at an angle to the optical axis and at a distance therefrom intersects the optical axis between the second optical system (OS2) and the processing plane (W).