mhurhangee/ep-ind-claims huggingface dataset:
An additive manufacturing system for printing a three-dimensional part, the additive manufacturing system comprising: one or more imaging engines (12p, 12s) configured to develop layers of the three-dimensional part; a build platform; one or more gantry mechanisms (82, 84) configured to move the build platform; a rotatable transfer medium configured to receive the developed layers from the one or more imaging engines (12p, 12s), and to transfer the developed layers onto intermediate build surfaces of the three-dimensional part on the build platform in a layer-by-layer manner; one or more imaging sensors (74, 76, 78) configured to scan the developed layers on the rotatable transfer medium and on the three-dimensional part, and to transmit data relating to the scans; and a controller assembly configured to receive the transmitted data from the one or more imaging sensors(74, 76, 78), to detect overlay errors from the scans, and to adjust the one or more gantry mechanisms (82, 84) to reduce the overlay errors. one or more imaging engines (12p, 12s) configured to develop layers of the three-dimensional part; a build platform; one or more gantry mechanisms (82, 84) configured to move the build platform; a rotatable transfer medium configured to receive the developed layers from the one or more imaging engines (12p, 12s), and to transfer the developed layers onto intermediate build surfaces of the three-dimensional part on the build platform in a layer-by-layer manner; one or more imaging sensors (74, 76, 78) configured to scan the developed layers on the rotatable transfer medium and on the three-dimensional part, and to transmit data relating to the scans; and a controller assembly configured to receive the transmitted data from the one or more imaging sensors(74, 76, 78), to detect overlay errors from the scans, and to adjust the one or more gantry mechanisms (82, 84) to reduce the overlay errors.
A pellicle frame, comprising: an aluminum frame material formed of aluminum or an aluminum alloy; and an anodic oxide film on a surface of the aluminum frame material, wherein the anodic oxide film comprises a film formed by using an alkaline anodic oxidation solution and a film formed by using an acid anodic oxidation solution. an aluminum frame material formed of aluminum or an aluminum alloy; and an anodic oxide film on a surface of the aluminum frame material, wherein the anodic oxide film comprises a film formed by using an alkaline anodic oxidation solution and a film formed by using an acid anodic oxidation solution.
Transmission device for an electric drive of a motor vehicle, having a housing, having three planetary gear sets (32, 34, 36), which are arranged in the housing and which each comprise a sun gear (38, 46, 54), a planet carrier (40, 48, 56) and a ring gear (42, 50, 58), having an input shaft, which can be driven by a rotor of an electric machine, and having an output shaft, by means of which at least one wheel of the motor vehicle can be driven, wherein: - at least one first shifting element is provided, by means of which the ring gear of a first of the planetary gear sets (32, 34, 36) can be secured to the housing, - the ring gear of the first planetary gear set is permanently coupled to the sun gear of a second of the planetary gear sets (32, 34, 36) for conjoint rotation therewith; and - the ring gear of the second planetary gear set is permanently coupled to the planet carrier of the first planetary gear set for conjoint rotation therewith; characterised in that - the sun gear of the third planetary gear set is permanently coupled to the ring gear of the second planetary gear set for conjoint rotation therewith and permanently coupled to the output shaft for conjoint rotation therewith, - a second shifting element is provided, by means of which the planet carrier of the second planetary gear set can be secured to the housing, - the sun gear of the first planetary gear set is permanently coupled to the input shaft for conjoint rotation therewith, - the planet carrier of the third planetary gear set is or can be permanently coupled to the planet carrier of the second planetary gear set for conjoint rotation therewith. - at least one first shifting element is provided, by means of which the ring gear of a first of the planetary gear sets (32, 34, 36) can be secured to the housing, - the ring gear of the first planetary gear set is permanently coupled to the sun gear of a second of the planetary gear sets (32, 34, 36) for conjoint rotation therewith; and - the ring gear of the second planetary gear set is permanently coupled to the planet carrier of the first planetary gear set for conjoint rotation therewith; characterised in that - the sun gear of the third planetary gear set is permanently coupled to the ring gear of the second planetary gear set for conjoint rotation therewith and permanently coupled to the output shaft for conjoint rotation therewith, - a second shifting element is provided, by means of which the planet carrier of the second planetary gear set can be secured to the housing, - the sun gear of the first planetary gear set is permanently coupled to the input shaft for conjoint rotation therewith, - the planet carrier of the third planetary gear set is or can be permanently coupled to the planet carrier of the second planetary gear set for conjoint rotation therewith.
A method for forming a single-header filtration module, comprising: inserting a first end of a braid-reinforced hollow fiber membrane in a low-viscosity light-curable adhesive having a viscosity less than 5 Pa·s (5000 cps) removing said first end from said adhesive to form a coating of said adhesive on said first end and a plug of said adhesive in the internal bore of said first end; after removing said first end from said adhesive, exposing said first end to a light source to cure said adhesive; wherein the membrane has a diameter of between 0.5 mm and 3.9 mm and the total diameter of said first end after said exposing step is less than 4 mm, and the thickness ( t) of said adhesive on the exterior of said first end after said exposing step is between 0.05 mm and 0.8 mm; wherein the method further comprises the step of securing a second unsealed end of said membrane in a header and wherein said method does not comprise the step of inserting said sealed end of said membrane in a header; wherein a plurality of said membranes are secured in said header such that a density of greater than 99,000 membranes per square meter (64 membranes per square inch) is achieved. inserting a first end of a braid-reinforced hollow fiber membrane in a low-viscosity light-curable adhesive having a viscosity less than 5 Pa·s (5000 cps) removing said first end from said adhesive to form a coating of said adhesive on said first end and a plug of said adhesive in the internal bore of said first end; after removing said first end from said adhesive, exposing said first end to a light source to cure said adhesive; wherein the membrane has a diameter of between 0.5 mm and 3.9 mm and the total diameter of said first end after said exposing step is less than 4 mm, and the thickness ( t) of said adhesive on the exterior of said first end after said exposing step is between 0.05 mm and 0.8 mm; wherein the method further comprises the step of securing a second unsealed end of said membrane in a header and wherein said method does not comprise the step of inserting said sealed end of said membrane in a header; wherein a plurality of said membranes are secured in said header such that a density of greater than 99,000 membranes per square meter (64 membranes per square inch) is achieved.
A glycosylated polypeptide selected from the group of polypeptides consisting of SEQ ID NOs: 2-50 and polypeptides having at least 75% sequence identity to the full length sequence of SEQ ID Nos: 2-50, wherein the glycosylated polypeptide comprises an O-linked glycosylation in at least one position.
A system for a gas turbine engine, comprising: a fuel nozzle, comprising: a fuel injector (61, 70) configured to output a fuel flow; and a premixer tube disposed about the fuel flow output from the fuel injector (61, 70), wherein the premixer tube comprises a perforated portion and a non-perforated portion, and the non-perforated portion is downstream of the perforated portion; characterized in that the fuel nozzle further comprises: a cap enclosing the fuel injector (61, 70) and the premixer tube, wherein the cap is configured to receive air, direct air to a downstream portion of the cap to facilitate cooling of a downstream portion of the fuel nozzle, and direct air to the premixer tube. a fuel nozzle, comprising: a fuel injector (61, 70) configured to output a fuel flow; and a premixer tube disposed about the fuel flow output from the fuel injector (61, 70), wherein the premixer tube comprises a perforated portion and a non-perforated portion, and the non-perforated portion is downstream of the perforated portion; characterized in that the fuel nozzle further comprises: a cap enclosing the fuel injector (61, 70) and the premixer tube, wherein the cap is configured to receive air, direct air to a downstream portion of the cap to facilitate cooling of a downstream portion of the fuel nozzle, and direct air to the premixer tube. a fuel injector (61, 70) configured to output a fuel flow; and a premixer tube disposed about the fuel flow output from the fuel injector (61, 70), wherein the premixer tube comprises a perforated portion and a non-perforated portion, and the non-perforated portion is downstream of the perforated portion; characterized in that the fuel nozzle further comprises: a cap enclosing the fuel injector (61, 70) and the premixer tube, wherein the cap is configured to receive air, direct air to a downstream portion of the cap to facilitate cooling of a downstream portion of the fuel nozzle, and direct air to the premixer tube. a cap enclosing the fuel injector (61, 70) and the premixer tube, wherein the cap is configured to receive air, direct air to a downstream portion of the cap to facilitate cooling of a downstream portion of the fuel nozzle, and direct air to the premixer tube.
A robotic surgery system, comprising: a controller configured to control actuation of at least one servo motor; and a surgical instrument coupled distally to a mechanical tracker linkage (16, 18, 20, 34, 36, 38, 40) and proximally to a robotic arm coupled to the at least one servo motor, such that the surgical instrument is configured to be movable in a workspace controlled, at least in part, by actuation of the at least one servo motor; wherein the mechanical tracker linkage (16, 18, 20, 34, 36, 38, 40) is adapted to be coupled between the surgical instrument and a portion of skeletal anatomy of a patient, the tracker linkage comprising one or more joints associated with one or more joint rotation sensors and being configured to send joint signals to the controller; wherein the controller controls the positioning of the instrument by selectively activating the at least one servo motor coupled to the robotic arm to enforce motion limitations upon the surgical instrument based at least in part upon the joint signals received from the mechanical tracker linkage (16, 18, 20, 34, 36, 38, 40). a controller configured to control actuation of at least one servo motor; and a surgical instrument coupled distally to a mechanical tracker linkage (16, 18, 20, 34, 36, 38, 40) and proximally to a robotic arm coupled to the at least one servo motor, such that the surgical instrument is configured to be movable in a workspace controlled, at least in part, by actuation of the at least one servo motor; wherein the mechanical tracker linkage (16, 18, 20, 34, 36, 38, 40) is adapted to be coupled between the surgical instrument and a portion of skeletal anatomy of a patient, the tracker linkage comprising one or more joints associated with one or more joint rotation sensors and being configured to send joint signals to the controller; wherein the controller controls the positioning of the instrument by selectively activating the at least one servo motor coupled to the robotic arm to enforce motion limitations upon the surgical instrument based at least in part upon the joint signals received from the mechanical tracker linkage (16, 18, 20, 34, 36, 38, 40).
A cell-protecting pharmaceutical composition for use in inhibiting apoptosis of liver cells, comprising a cyclo histidine-proline (Cyclo His-Pro, CHP) or a pharmaceutically acceptable salt thereof as an active ingredient, wherein the cell protecting pharmaceutical composition is used in prevention or treatment of diseases selected from the group consisting of hepatic failure, acute hepatitis, chronic hepatitis, liver cirrhosis, hepatic coma and alcoholic liver disease, or wherein the composition is used in inhibiting a drug-induced liver cell damage.
Aircraft turbine casing designed to carry a set of ring sectors that partly delimits a conduit inside which a gas flow passes through the turbine, the casing comprising dynamic means of adjusting the radial position of ring sectors by the controlled injection of an air flow on portions of an annular wall of the casing, the casing comprising an upstream radial lug that connects an upstream end of each ring sector, along the direction of the gas flow to the casing, and a downstream radial lug that connects a downstream end of each ring sector to the casing, and at least the upstream radial lug is made as a single piece with the casing and is directly connected to the upstream end of each ring sector, characterised in that the casing comprises an air flow guide conduit along an inner annular face of the annular wall of the casing, that opens up towards the direction of the ring sectors and in that at least the upstream radial lug comprises air passage orifices for ventilation of the ring sectors, that open up into said guide conduit.
A light-emitting diode device, comprising: a light-emitting diode; and an optical component positioned so that light exiting the light-emitting diode passes through the optical component, the optical component including: a matrix material; and a plurality of coated color-converting particles disposed in the matrix material such that the matrix material surrounds the coated color-converting particles individually, with individual coated color-converting particles of the plurality of coated color-converting particles having a particle core and a coating generally surrounding the particle core, wherein individual particle cores of the plurality of coated color-converting particles include a solid mass of a color-converting material, and individual coatings of the plurality of coated color-converting particles include a parylene. a light-emitting diode; and an optical component positioned so that light exiting the light-emitting diode passes through the optical component, the optical component including: a matrix material; and a plurality of coated color-converting particles disposed in the matrix material such that the matrix material surrounds the coated color-converting particles individually, a matrix material; and a plurality of coated color-converting particles disposed in the matrix material such that the matrix material surrounds the coated color-converting particles individually, with individual coated color-converting particles of the plurality of coated color-converting particles having a particle core and a coating generally surrounding the particle core, wherein individual particle cores of the plurality of coated color-converting particles include a solid mass of a color-converting material, and individual coatings of the plurality of coated color-converting particles include a parylene.
Floor panel (1, 40, 51), comprising a laminate of: - a magnesium oxide based core layer (34, 44, 56); - at least one magnesium oxide based upper crust layer (35, 46, 58) positioned on top of said core layer (34, 44, 56), wherein the density of said upper crust layer (35, 46, 58) is larger than the density of the core layer (34, 44, 56); characterized in that said laminate of the floor panel (1, 40, 51) further comprises: - at least one upper reinforcing layer situated in between said core layer (34, 44, 56) and said at least one upper crust layer (35, 46, 58), wherein the upper reinforcing layer comprises a fiberglass mesh (45, 57), wherein the fiberglass mesh (45, 57) is provided with a coating. - a magnesium oxide based core layer (34, 44, 56); - at least one magnesium oxide based upper crust layer (35, 46, 58) positioned on top of said core layer (34, 44, 56), wherein the density of said upper crust layer (35, 46, 58) is larger than the density of the core layer (34, 44, 56); characterized in that said laminate of the floor panel (1, 40, 51) further comprises: - at least one upper reinforcing layer situated in between said core layer (34, 44, 56) and said at least one upper crust layer (35, 46, 58),
Device for cleaning a container treating machine comprising a media outlet opening, comprising a closing element that is able to be applied in a sealing manner to the media outlet opening, wherein the device has at least one spray opening for deflecting cleaning medium present at the media outlet opening onto surrounding plant regions, wherein the spray opening is in fluid communication with the media outlet opening and the fluid communication is able to be interrupted or throttled via a valve, characterized in that the closing element contains the at least one spray opening, and in that the valve is provided in the closing element.
A large scale process for producing high purity samples of low copy number plasmids from bacterial cells, comprising the steps of: a) producing a lysate solution by contacting a cell suspension of said bacterial cells comprising said low copy number plasmids with lysis solution; b) neutralizing said lysate solution with a neutralizing solution to produce a dispersion that comprises neutralized lysate solution and debris and wherein the dispersion fluid is held for less than one hour to separate the neutralized lysate solution; c) filtering the dispersion through at least one filter; d) performing ion exchange separation on said neutralized lysate solution to produce an ion exchange eluate; and e) performing hydrophobic interaction separation on said ion exchange eluate to produce a hydrophobic interaction solution; wherein step a) comprises mixing said cell suspension with lysis solution in a high shear, in-line mixer; wherein step b) comprises mixing said lysate solution with said neutralizing solution in a bubble mixer; and wherein step e) comprises performing hydrophobic interaction separation using a hydrophobic interaction column or a hydrophobic interaction membrane to form a hydrophobic interaction solution; wherein the method comprises transitioning from one step to a subsequent step substantially continuously. a) producing a lysate solution by contacting a cell suspension of said bacterial cells comprising said low copy number plasmids with lysis solution; b) neutralizing said lysate solution with a neutralizing solution to produce a dispersion that comprises neutralized lysate solution and debris and wherein the dispersion fluid is held for less than one hour to separate the neutralized lysate solution; c) filtering the dispersion through at least one filter; d) performing ion exchange separation on said neutralized lysate solution to produce an ion exchange eluate; and e) performing hydrophobic interaction separation on said ion exchange eluate to produce a hydrophobic interaction solution;
A method for analyzing diffraction data obtained using a crystal structure analysis sample, the crystal structure analysis sample comprising a single crystal of a porous compound, and a compound for which a structure is to be determined, the single crystal of the porous compound having a three-dimensional framework, and either or both of pores and voids that are defined by the three-dimensional framework, and are three-dimensionally arranged in an ordered manner, the three-dimensional framework having been determined by crystal structure analysis, and molecules of the compound for which the structure is to be determined being arranged in either or both of the pores and the voids in an ordered manner to such an extent that they can be observed by crystal structure analysis, the method comprising: a step of providing the crystal structure analysis sample including the single crystal of the porous compound whose space group is already known; a step of providing a diffraction data of a crystal structure of the porous compound previously analyzed; a step that selects a space group that is identical to a space group of the single crystal of the porous compound, or a space group that has a symmetry lower than that of the space group of the single crystal of the porous compound; a step that determines an initial structure of the crystal structure analysis sample using the space group determined by the step by analyzing diffraction data of the crystal structure analysis sample using the diffraction data of a crystal structure of the porous compound previously analyzed as initial values; and a step that refines the initial structure determined by the step using a Fourier method, a least-square method, or a maximum likelihood method, thereby obtaining a crystal structure of the compound for which the structure is to be determined, wherein the single crystal of the porous compound is a single crystal of a polynuclear metal complex, and the compound for which the structure is to be determined is a compound having a molecular weight of 20 to 3,000. a step of providing the crystal structure analysis sample including the single crystal of the porous compound whose space group is already known; a step of providing a diffraction data of a crystal structure of the porous compound previously analyzed; a step that selects a space group that is identical to a space group of the single crystal of the porous compound, or a space group that has a symmetry lower than that of the space group of the single crystal of the porous compound; a step that determines an initial structure of the crystal structure analysis sample using the space group determined by the step by analyzing diffraction data of the crystal structure analysis sample using the diffraction data of a crystal structure of the porous compound previously analyzed as initial values; and a step that refines the initial structure determined by the step using a Fourier method, a least-square method, or a maximum likelihood method, thereby obtaining a crystal structure of the compound for which the structure is to be determined,