mhurhangee/patent-ind-claim-en huggingface dataset:
Hip joint implant for fastening to a pelvic bone , with a support body which has a socket and whose convex outer face is designed to bear on the pelvic bone and which, on its concave inner face, has a receiving seat for a pelvis-side bearing that is designed to receive a joint head of a femoral component of a hip prosthesis, and with outwardly directed flat fastening brackets which are arranged at the edge region of the socket , are made of a reshapeable biocompatible material and are each provided with at least one receiving seat for a fastening means, wherein the socket is made of another, stiffer biocompatible material, wherein the fastening brackets are made in one piece with a fastening ring already prefabricated with an opening for receiving the socket and are connected to the socket by a non-releasable cohesive bond , wherein the socket is provided with a preferably circumferential support shoulder in the region where the fastening ring is received, such that the fastening brackets and the fastening ring are supported on the support shoulder .
A method for three-dimensional mapping of a geographical area comrpising capturing aerial images of a geographical area using a aircraft self-piloted according to a predetermined flight plan and an image capture apparatus mounted on the aircraft while being movable relative to the aircraft around a rotation axis to make it possible to modify the angular position of the image capture apparatus relative to the aircraft , the method comprising, during a single flyover of the geographical area by the aircraft: - capturing a first series of images by positioning the image capture apparatus relative to the aircraft iteratively according to a first sequence of angular position(s) including a first angular position or at least two distinct angular positions, a respective image being captured for each angular position of the first sequence upon each iteration of the sequence; then - capturing a second series of images by positioning the image capture apparatus relative to the aircraft iteratively according to a second sequence of angular position(s) including a first angular position or at least two distinct angular positions, a respective image being captured for each angular position of the second sequence upon each iteration of the sequence, the second sequence including at least one angular position distinct from each angular position of the first sequence, the method comprising calculating a three-dimensional map of the geographical area from the captured images. - capturing a first series of images by positioning the image capture apparatus relative to the aircraft iteratively according to a first sequence of angular position(s) including a first angular position or at least two distinct angular positions, a respective image being captured for each angular position of the first sequence upon each iteration of the sequence; then - capturing a second series of images by positioning the image capture apparatus relative to the aircraft iteratively according to a second sequence of angular position(s) including a first angular position or at least two distinct angular positions, a respective image being captured for each angular position of the second sequence upon each iteration of the sequence, the second sequence including at least one angular position distinct from each angular position of the first sequence,
A method of fabricating a printed circuit board, PCB, assembly , comprising: depositing a metal layer on a PCB substrate by laser-assisted deposition, LAD, in which jetting of metal droplets from a first donor substrate onto the PCB substrate and into one or more holes therein is effected using a laser to form the metal layer on the PCB substrate , the metal layer being subsequently dried and sintered; imaging, with an imaging unit , the metal layer so as to determine whether a desired thickness of the metal layer has been reached; repeating the jetting, drying, sintering, and imaging until the metal layer reaches the desired thickness; and thereafter forming at least one passivation layer over the metal layer . depositing a metal layer on a PCB substrate by laser-assisted deposition, LAD, in which jetting of metal droplets from a first donor substrate onto the PCB substrate and into one or more holes therein is effected using a laser to form the metal layer on the PCB substrate , the metal layer being subsequently dried and sintered; imaging, with an imaging unit , the metal layer so as to determine whether a desired thickness of the metal layer has been reached; repeating the jetting, drying, sintering, and imaging until the metal layer reaches the desired thickness; and thereafter forming at least one passivation layer over the metal layer .
Method for manufacturing an optical component of curable material, comprising: molding and curing a first structure of a first curable material on a substrate ; molding and curing a second structure of a second curable material on a first surface of the first structure facing away from the substrate , so that at the first surface of the first structure a boundary surface between the first structure and the second structure forms and so that the first structure is not covered by the second structure in a passage area , wherein the first curable material is soluble for the solvent after curing and the second curable material is insoluble for the solvent after curing; molding and curing a third structure of a third curable material on a first surface of the second structure facing away from the substrate, so that at the first surface of the second structure a boundary surface forms between the second structure and the third structure and so that the passage area through the third structure is not blocked, wherein the third curable material is insoluble for the solvent after curing; introducing a solvent into the passage area after molding and curing the second structure in order to dissolve the first curable material of the first structure so that a cavity is formed between the second structure and a surface of the substrate . molding and curing a first structure of a first curable material on a substrate ; molding and curing a second structure of a second curable material on a first surface of the first structure facing away from the substrate , so that at the first surface of the first structure a boundary surface between the first structure and the second structure forms and so that the first structure is not covered by the second structure in a passage area , wherein the first curable material is soluble for the solvent after curing and the second curable material is insoluble for the solvent after curing; molding and curing a third structure of a third curable material on a first surface of the second structure facing away from the substrate, so that at the first surface of the second structure a boundary surface forms between the second structure and the third structure and so that the passage area through the third structure is not blocked, wherein the third curable material is insoluble for the solvent after curing; introducing a solvent into the passage area after molding and curing the second structure in order to dissolve the first curable material of the first structure so that a cavity is formed between the second structure and a surface of the substrate .
A packet , comprising: a front panel and a back panel defining an internal volume therebetween, wherein the front panel and the back panel comprise a first edge having a plurality of first recesses formed therein, and wherein a nozzle provides a path of fluid communication from the internal volume, through the first edge , to an exterior of the packet , wherein the first edge further includes a second recess formed therein, and wherein an end of the nozzle is positioned within the second recess ; a consumer product disposed within the internal volume; and a cap configured to prevent the consumer product from flowing from the internal volume, through the nozzle , and to the exterior of the packet , characterized in that the second recess is deeper than the first recesses . a front panel and a back panel defining an internal volume therebetween, wherein the front panel and the back panel comprise a first edge having a plurality of first recesses formed therein, and wherein a nozzle provides a path of fluid communication from the internal volume, through the first edge , to an exterior of the packet , wherein the first edge further includes a second recess formed therein, and wherein an end of the nozzle is positioned within the second recess ; a consumer product disposed within the internal volume; and a cap configured to prevent the consumer product from flowing from the internal volume, through the nozzle , and to the exterior of the packet , characterized in that the second recess is deeper than the first recesses .
A method for controlling fluid flow within a chromatography system , the method comprising: activating a makeup pump configured to pump a makeup fluid into the chromatography system downstream of a column ; determining a flow rate through a first restrictor , wherein the first restrictor is located upstream of a detector and downstream of both the makeup pump and the column ; decreasing an output volume of the makeup pump in order to direct a portion of an output from the column through the first restrictor and to the detector ; increasing an output volume of the makeup pump in order to direct the output from the column to a second restrictor , located downstream of the makeup pump and the column and in parallel with the first restrictor and the detector ; and controlling a ratio of the output from the column directed to the first restrictor and the second restrictor by adjusting the output volume of the makeup pump . activating a makeup pump configured to pump a makeup fluid into the chromatography system downstream of a column ; determining a flow rate through a first restrictor , wherein the first restrictor is located upstream of a detector and downstream of both the makeup pump and the column ; decreasing an output volume of the makeup pump in order to direct a portion of an output from the column through the first restrictor and to the detector ; increasing an output volume of the makeup pump in order to direct the output from the column to a second restrictor , located downstream of the makeup pump and the column and in parallel with the first restrictor and the detector ; and controlling a ratio of the output from the column directed to the first restrictor and the second restrictor by adjusting the output volume of the makeup pump .
An engine block comprising: a cylinder ; a piston slidably received within the cylinder ; a liner positioned between the cylinder and the piston ; at least two oil nozzles arranged spaced apart from each other, wherein one of the oil nozzles is provided on a first side of the piston and another of the oil nozzles is provided on a second side of the piston such that the first and second sides oppose each other, the oil nozzles configured to spray oil on the piston ; an oil channel located on the first side ; a passage provided on the first side as being provided in the engine block to fluidly connect the oil channel with one of the oil nozzles (124; 126) provided on the first side ; and a passage provided on the second side as being provided in the engine block to fluidly connect the groove with one of the oil nozzles provided on the second side , characterized in that a groove is disposed about and provided in communication with the liner and the cylinder , and the oil channel is configured to supply oil to at least one of the at least two oil nozzles via the groove , wherein the groove is in fluid communication with the oil nozzles . a cylinder ; a piston slidably received within the cylinder ; a liner positioned between the cylinder and the piston ; at least two oil nozzles arranged spaced apart from each other, wherein one of the oil nozzles is provided on a first side of the piston and another of the oil nozzles is provided on a second side of the piston such that the first and second sides oppose each other, the oil nozzles configured to spray oil on the piston ; an oil channel located on the first side ; a passage provided on the first side as being provided in the engine block to fluidly connect the oil channel with one of the oil nozzles (124; 126) provided on the first side ; and a passage provided on the second side as being provided in the engine block to fluidly connect the groove with one of the oil nozzles provided on the second side , characterized in that a groove is disposed about and provided in communication with the liner and the cylinder , and the oil channel is configured to supply oil to at least one of the at least two oil nozzles via the groove , wherein the groove is in fluid communication with the oil nozzles .
A photonics integrated system , the photonics integrated system being configured for cooperating with a radiation source having a bandwidth and for cooperating with a detector, the photonics integrated system comprising - a substrate , - an integrated interferometer integrated in the substrate and being configured for receiving radiation from a radiation source having a bandwidth, and - an integrated spectral filter integrated in the substrate and being configured for receiving radiation from the interferometer , wherein the integrated interferometer has a period (P ii ) and the integrated spectral filter has a bandwidth (BW sa ) such that the period (P ii ) of the integrated interferometer is smaller than the bandwidth (BW sa ) of the integrated spectral filter , characterised in that the integrated spectral filter has a periodic transfer characteristic with a period (P sa ) and the photonics integrated system has a bandwidth (BW system ) determined by the bandwidth of the components of the photonics integrated system, such that the period (P sa ) of the periodic transfer characteristic of the integrated spectral filter is larger than the bandwidth (BW system ) of the system . - a substrate , - an integrated interferometer integrated in the substrate and being configured for receiving radiation from a radiation source having a bandwidth, and - an integrated spectral filter integrated in the substrate and being configured for receiving radiation from the interferometer ,
A hollow-fiber membrane element for forward osmosis comprising a porous distribution pipe and a wound hollow-fiber membrane body which is a both open-ended hollow-fiber membrane arranged in an intersecting manner by winding the hollow-fiber membranes around the porous distribution pipe in a helical manner, wherein a) the number of winds per element length in a region from an outermost layer of the wound hollow-fiber membrane body to one eighth to three quarter of the thickness of the wound hollow-fiber membrane body is 0.33 to 1.75, b) the number of winds per element length in a region from an innermost layer of the wound hollow-fiber membrane body to one fourth of the thickness of the wound hollow-fiber membrane body is greater than 1.75, and the wound hollow-fiber membrane body has a length of 0.2 to 1.6 m. a) the number of winds per element length in a region from an outermost layer of the wound hollow-fiber membrane body to one eighth to three quarter of the thickness of the wound hollow-fiber membrane body is 0.33 to 1.75, b) the number of winds per element length in a region from an innermost layer of the wound hollow-fiber membrane body to one fourth of the thickness of the wound hollow-fiber membrane body is greater than 1.75, and the wound hollow-fiber membrane body has a length of 0.2 to 1.6 m.
A drug-releasing biodegradable stent , comprising: a first stent structure configured to have a plurality of cells by means of a wire crossing pattern of a woven structure by weaving a metal wire made of a shape-memory alloy in a specific pattern on a jig and be provided in a hollow cylindrical shape; a second stent structure formed as a 3D print that is provided to have a plurality of cells by means of a wire crossing pattern of a printed structure by performing 3D printing using a printing material including a biodegradable polymer and a drug and also have a hollow cylindrical shape; and a third stent structure configured to have a plurality of cells by means of a wire crossing pattern of a woven structure by weaving a metal wire made of a shape-memory alloy in a specific pattern on a jig and be provided in a hollow cylindrical shape, and disposed such that it covers an outer circumferential surface of the first stent structure or an outer circumferential surface thereof is covered with the first stent structure ; characterized in that the second stent structure is inserted into and disposed in a space between the first stent structure and the third stent structure . a first stent structure configured to have a plurality of cells by means of a wire crossing pattern of a woven structure by weaving a metal wire made of a shape-memory alloy in a specific pattern on a jig and be provided in a hollow cylindrical shape; a second stent structure formed as a 3D print that is provided to have a plurality of cells by means of a wire crossing pattern of a printed structure by performing 3D printing using a printing material including a biodegradable polymer and a drug and also have a hollow cylindrical shape; and a third stent structure configured to have a plurality of cells by means of a wire crossing pattern of a woven structure by weaving a metal wire made of a shape-memory alloy in a specific pattern on a jig and be provided in a hollow cylindrical shape, and disposed such that it covers an outer circumferential surface of the first stent structure or an outer circumferential surface thereof is covered with the first stent structure ; characterized in that the second stent structure is inserted into and disposed in a space between the first stent structure and the third stent structure .
A polymer, containing a hydrocarbon-containing block A and a polyether carbonate-containing block B, characterized in that the polymer is a mixture of compounds with the structure AB, ABA and possibly B, wherein starter represents the rest of an H-functional starter substance without the reacted OH group and includes no further OH group, R a' , R b' , R c' , R d' , R e' , R f' independently each represent an aliphatic hydrocarbon radical with 2 to 8 carbon atoms, a, b, c, d, e, f independently each represent a number of 1 to 20, wherein the amount of compounds with the structure AB is at least 80 wt-% and with the structure ABA is 1.20 to 20.00 wt-%, each based on the total weight of the compounds with the structures AB, ABA and B. starter represents the rest of an H-functional starter substance without the reacted OH group and includes no further OH group, R a' , R b' , R c' , R d' , R e' , R f' independently each represent an aliphatic hydrocarbon radical with 2 to 8 carbon atoms, a, b, c, d, e, f independently each represent a number of 1 to 20, wherein the amount of compounds with the structure AB is at least 80 wt-% and with the structure ABA is 1.20 to 20.00 wt-%, each based on the total weight of the compounds with the structures AB, ABA and B.
An OPEP device , comprising: a housing enclosing at least one chamber ; a chamber inlet configured to receive exhaled air into the at least one chamber ; a first chamber outlet and a second chamber outlet configured to permit exhaled air to exit the at least one chamber ; an exhalation flow path defined between the chamber inlet and the first chamber outlet ; a restrictor member positioned in the exhalation flow path , the restrictor member moveable in response to a flow of exhaled air along the exhalation flow path between a closed position, where the flow of exhaled air along the exhalation flow path through the chamber inlet is restricted and the flow of exhaled air is directed toward the first chamber outlet , and an open position, where the flow of exhaled air along the exhalation flow path through the chamber inlet is less restricted and the flow of exhaled air is directed toward the second chamber outlet ; a variable nozzle positioned in the exhalation flow path such that the exhalation flow path passes through an orifice of the variable nozzle ; and a vane positioned adjacent the orifice , the vane being operatively connected to the restrictor member and configured to move the restrictor member between the closed position and the open position in response to an increased pressure adjacent the vane , wherein a size of the orifice is configured to increase in response to the flow of exhaled air through the orifice . a housing enclosing at least one chamber ; a chamber inlet configured to receive exhaled air into the at least one chamber ; a first chamber outlet and a second chamber outlet configured to permit exhaled air to exit the at least one chamber ; an exhalation flow path defined between the chamber inlet and the first chamber outlet ; a restrictor member positioned in the exhalation flow path , the restrictor member moveable in response to a flow of exhaled air along the exhalation flow path between a closed position, where the flow of exhaled air along the exhalation flow path through the chamber inlet is restricted and the flow of exhaled air is directed toward the first chamber outlet , and an open position, where the flow of exhaled air along the exhalation flow path through the chamber inlet is less restricted and the flow of exhaled air is directed toward the second chamber outlet ; a variable nozzle positioned in the exhalation flow path such that the exhalation flow path passes through an orifice of the variable nozzle ; and a vane positioned adjacent the orifice , the vane being operatively connected to the restrictor member and configured to move the restrictor member between the closed position and the open position in response to an increased pressure adjacent the vane , wherein a size of the orifice is configured to increase in response to the flow of exhaled air through the orifice .