mhurhangee/ep-ind-claims huggingface dataset:
An information processing apparatus configured to create drawing data using print setting information and print data, the information processing apparatus comprising: a converting module configured to convert the print setting information to apparatus setting information; a control mode determining module configured to analyze the print setting information to determine a control mode applicable when the drawing data is created; a drawing data creating module configured to create drawing data using the apparatus setting information and the print data; and a creating module control module configured to control the drawing data creating module according to the control mode; wherein the control mode determining module is configured to analyze the print setting information to determine the creator of the print setting information and the print data and to determine the control mode according to the creator; wherein the converting module is configured to include conversion tables for different creators of the print setting information and the print data, each conversion table being created based on a correspondence between items of the print setting information and items of the apparatus setting information for the respective creator, and wherein the converting module is configured to select the conversion table for the creator detected from the descriptions of the print setting information and to create the apparatus setting information accordingly. a converting module configured to convert the print setting information to apparatus setting information; a control mode determining module configured to analyze the print setting information to determine a control mode applicable when the drawing data is created; a drawing data creating module configured to create drawing data using the apparatus setting information and the print data; and a creating module control module configured to control the drawing data creating module according to the control mode; wherein the control mode determining module is configured to analyze the print setting information to determine the creator of the print setting information and the print data and to determine the control mode according to the creator; wherein the converting module is configured to include conversion tables for different creators of the print setting information and the print data, each conversion table being created based on a correspondence between items of the print setting information and items of the apparatus setting information for the respective creator, and wherein the converting module is configured to select the conversion table for the creator detected from the descriptions of the print setting information and to create the apparatus setting information accordingly.
A computing device, comprising: a display; storage; and, a processor configured to execute computer readable instructions stored on the storage to perform operations comprising: managing the display as an original unit presenting at least one original graphical user interface,GUI,, and identifying a change in a current occlusion condition associated with the display, characterized by predicting a future occlusion condition associated with the display based at least on the change, the future occlusion condition being different from the current occlusion condition, computing a future unit presenting at least one updated GUI based at least on the future occlusion condition, the future unit being different from the original unit in at least one of a location, aspect ratio, or size, and presenting a transition unit with at least one transition GUI on the display, the transition unit having a location, aspect ratio and size in between those of the original unit and the future unit. a display; storage; and, a processor configured to execute computer readable instructions stored on the storage to perform operations comprising: managing the display as an original unit presenting at least one original graphical user interface,GUI,, and identifying a change in a current occlusion condition associated with the display, characterized by predicting a future occlusion condition associated with the display based at least on the change, the future occlusion condition being different from the current occlusion condition, computing a future unit presenting at least one updated GUI based at least on the future occlusion condition, the future unit being different from the original unit in at least one of a location, aspect ratio, or size, and presenting a transition unit with at least one transition GUI on the display, the transition unit having a location, aspect ratio and size in between those of the original unit and the future unit. managing the display as an original unit presenting at least one original graphical user interface,GUI,, and identifying a change in a current occlusion condition associated with the display, characterized by predicting a future occlusion condition associated with the display based at least on the change, the future occlusion condition being different from the current occlusion condition, computing a future unit presenting at least one updated GUI based at least on the future occlusion condition, the future unit being different from the original unit in at least one of a location, aspect ratio, or size, and presenting a transition unit with at least one transition GUI on the display, the transition unit having a location, aspect ratio and size in between those of the original unit and the future unit.
A method of servicing an auxiliary power unit, wherein an inlet duct is mounted to an aircraft skin and fastened thereon, the inlet duct having a seal which is seated on a housing flange of the auxiliary power unit without a fixed connection, the method comprising the steps of: removing the inlet duct from an opening in the aircraft skin, while keeping the aircraft skin in place; exposing the auxiliary power unit arranged within a cavity of the aircraft skin; and servicing a portion of the auxiliary power unit through the opening. removing the inlet duct from an opening in the aircraft skin, while keeping the aircraft skin in place; exposing the auxiliary power unit arranged within a cavity of the aircraft skin; and servicing a portion of the auxiliary power unit through the opening.
A method for modifying a template double stranded polynucleotide, comprising: (a) contacting the template polynucleotide with a MuA transposase and a population of double stranded MuA substrates each comprising at least one overhang of universal nucleotides such that the transposase fragments the template polynucleotide and ligates a substrate to one or both ends of the double stranded fragments and thereby producing a plurality of fragment/substrate constructs in which the overhang of universal nucleotides is hybridised to the fragment to close a gap left by the action of the transposase; and (b) ligating the overhang to the fragments in the constructs, thereby producing a plurality of modified double stranded polynucleotides. (a) contacting the template polynucleotide with a MuA transposase and a population of double stranded MuA substrates each comprising at least one overhang of universal nucleotides such that the transposase fragments the template polynucleotide and ligates a substrate to one or both ends of the double stranded fragments and thereby producing a plurality of fragment/substrate constructs in which the overhang of universal nucleotides is hybridised to the fragment to close a gap left by the action of the transposase; and (b) ligating the overhang to the fragments in the constructs, thereby producing a plurality of modified double stranded polynucleotides.
A control method of an internal combustion engine including an in-cylinder injection fuel injection valve arranged to inject a fuel to a combustion chamber, and a port injection fuel injection valve arranged to inject the fuel to an intake port, the control method comprising: sensing or estimating a fuel temperature at a tip end portion of the in-cylinder injection fuel injection valve; sensing an intake pressure; judging whether or not a flash boiling condition in which a flash boiling condition may be generated is satisfied, based on the fuel temperature and the intake pressure; setting the in-cylinder fuel injection valve to a default fuel injection valve; and injecting an entire or a part of the fuel from the port injection fuel injection valve by decreasing an injection amount ratio of the in-cylinder injection fuel injection valve when the flash boiling condition is satisfied. sensing or estimating a fuel temperature at a tip end portion of the in-cylinder injection fuel injection valve; sensing an intake pressure; judging whether or not a flash boiling condition in which a flash boiling condition may be generated is satisfied, based on the fuel temperature and the intake pressure; setting the in-cylinder fuel injection valve to a default fuel injection valve; and injecting an entire or a part of the fuel from the port injection fuel injection valve by decreasing an injection amount ratio of the in-cylinder injection fuel injection valve when the flash boiling condition is satisfied.
Method for inspecting a surface area with a known position for material defects using a camera configuration arranged on an unmanned and autonomously navigating aircraft, comprising: automatically approaching the surface area starting from a take-off site, wherein obstacles can be avoided by using methods for automatically detecting obstacles and avoiding them; continuously measuring a relative position of the aircraft with respect to the surface area with the help of a position sensor; recording a sequence of images (121, 122) of the surface area, wherein between the individual images (121, 122) the aircraft is moved along a flight path in relation to the surface area in such a way that the images (121, 122) of the sequence have at least partially overlapping image details of the surface area in overlap regions; compiling the images (121, 122) of the sequence to form an overall image of the surface area, in order to allow for an inspection of the surface area for defects and a localization of defects using the overall image, the method is characterized in that the relative position of the aircraft is regulated continuously so that the aircraft maintains a predefined distance (d) and a predefined orientation in relation to the surface area, and the flight path runs essentially parallel to the surface area. automatically approaching the surface area starting from a take-off site, wherein obstacles can be avoided by using methods for automatically detecting obstacles and avoiding them; continuously measuring a relative position of the aircraft with respect to the surface area with the help of a position sensor; recording a sequence of images (121, 122) of the surface area, wherein between the individual images (121, 122) the aircraft is moved along a flight path in relation to the surface area in such a way that the images (121, 122) of the sequence have at least partially overlapping image details of the surface area in overlap regions; compiling the images (121, 122) of the sequence to form an overall image of the surface area, in order to allow for an inspection of the surface area for defects and a localization of defects using the overall image, the method is characterized in that the relative position of the aircraft is regulated continuously so that the aircraft maintains a predefined distance (d) and a predefined orientation in relation to the surface area, and the flight path runs essentially parallel to the surface area.
A gas turbine engine comprising: a core; a variable pitch fan arranged in flow communication with said core, said variable pitch fan comprising a disk and at least nine fan blades coupled to said disk for rotation together with said disk; a trunnion mechanism coupling each of said fan blades to said disk such that said fan blades are rotatable relative to said disk about a pitch axis, wherein each of said trunnion mechanisms comprises a line contact bearing (146, 162); an actuation mechanism for varying a pitch of said fan blades; a pitch correction device operatively coupled to said fan blades via said actuation mechanism such that the pitch correction device is remote from said fan blades; and a rotatable nacelle covering said disk such that said engine has a fan hub radius ratio of between about.1 and about.4. a core; a variable pitch fan arranged in flow communication with said core, said variable pitch fan comprising a disk and at least nine fan blades coupled to said disk for rotation together with said disk; a trunnion mechanism coupling each of said fan blades to said disk such that said fan blades are rotatable relative to said disk about a pitch axis, wherein each of said trunnion mechanisms comprises a line contact bearing (146, 162); an actuation mechanism for varying a pitch of said fan blades; a pitch correction device operatively coupled to said fan blades via said actuation mechanism such that the pitch correction device is remote from said fan blades; and a rotatable nacelle covering said disk such that said engine has a fan hub radius ratio of between about.1 and about.4.
A method of forming a wind turbine blade, comprising: providing a first blade half; providing a second blade half; providing a shear web, the shear web including at least one aperture formed therein; providing at least one bulkhead, the at least one bulkhead attached to the shear web; placing the shear web and at least one bulkhead on the first blade half; disposing the second blade half on the first blade half to define a blade interior therebetween, the shear web and at least one bulkhead disposed within the blade interior, characterized in that the bulkhead includes a frame and a removable lid. providing a first blade half; providing a second blade half; providing a shear web, the shear web including at least one aperture formed therein; providing at least one bulkhead, the at least one bulkhead attached to the shear web; placing the shear web and at least one bulkhead on the first blade half; disposing the second blade half on the first blade half to define a blade interior therebetween, the shear web and at least one bulkhead disposed within the blade interior, characterized in that the bulkhead includes a frame and a removable lid.
A sensing unit for monitoring the condition of a liquid, said sensing unit comprising at least one sensor interface (101, 102) and an evaluation unit, where - said sensor interface (101, 102) is adapted to measure two or more raw signals, the raw signals corresponding to at least two different parameters of the liquid, where said parameters relate to at least liquid degradation or wear debris particle generation (411, 412), and each signal providing a mean value and a variance different from zero over,a course of at least two measurements, - the sensor interface (101, 102) is further adapted to transmit said raw signals as transmission signals to said evaluation unit, each transmission signal equalling a raw signal, characterised by each transmission signal having a variance equal to the variance of its corresponding raw signal, and - the evaluation unit is adapted to evaluate the condition of the liquid by inter-correlating the at least two transmission signals, thereby inter-correlating the at least two parameters. - said sensor interface (101, 102) is adapted to measure two or more raw signals, the raw signals corresponding to at least two different parameters of the liquid, where said parameters relate to at least liquid degradation or wear debris particle generation (411, 412), and each signal providing a mean value and a variance different from zero over,a course of at least two measurements, - the sensor interface (101, 102) is further adapted to transmit said raw signals as transmission signals to said evaluation unit, each transmission signal equalling a raw signal, characterised by each transmission signal having a variance equal to the variance of its corresponding raw signal, and - the evaluation unit is adapted to evaluate the condition of the liquid by inter-correlating the at least two transmission signals, thereby inter-correlating the at least two parameters.
A phenyl triazole derivative which is 6-[[5-(difluoromethyl)-3-(4-fluorophenyl)triazol-4-yl]methoxy]pyridazine-3-carboxamide; or a pharmaceutically acceptable salt, a polymorph, or a hydrate thereof.
A stereolithography apparatus, having: - an exposure arrangement comprising: - a radiative element configured to emit optical radiation, and - a masking element configured to form an exposure pattern by partially masking optical radiation from the radiative element, - a table having a horizontal upper surface on which is placeable a vat for holding resin to be photopolymerized in a stereolithographic 3D printing process by optical radiation, wherein the masking element is arranged in thermal connection with the horizontal upper surface, and the apparatus further comprises a controller, the controller being coupled i) to said radiative element for emitting optical radiation from the radiative element to the masking element, wherein the controller is configured to execute a resin pre-heating process to heat the resin in the vat, characterised in that the controller is coupled ii) to said masking element for keeping the masking element closed, wherein the controller is configured to execute the resin pre-heating process to heat the resin in the vat by emitting optical radiation from the radiative element to the closed masking element, whereby the masking element is heated by the optical radiation absorbed in the masking element and thermal energy is further transferred to the resin in the vat. - an exposure arrangement comprising: - a radiative element configured to emit optical radiation, and - a masking element configured to form an exposure pattern by partially masking optical radiation from the radiative element, - a radiative element configured to emit optical radiation, and - a masking element configured to form an exposure pattern by partially masking optical radiation from the radiative element, - a table having a horizontal upper surface on which is placeable a vat for holding resin to be photopolymerized in a stereolithographic 3D printing process by optical radiation, the masking element is arranged in thermal connection with the horizontal upper surface, and the apparatus further comprises a controller, the controller being coupled i) to said radiative element for emitting optical radiation from the radiative element to the masking element, wherein the controller is configured to execute a resin pre-heating process to heat the resin in the vat, characterised in that the controller is coupled ii) to said masking element for keeping the masking element closed, wherein the controller is configured to execute the resin pre-heating process to heat the resin in the vat by emitting optical radiation from the radiative element to the closed masking element, whereby the masking element is heated by the optical radiation absorbed in the masking element and thermal energy is further transferred to the resin in the vat.
Implant having a surface comprising a coating on at least a portion of the surface of the implant, wherein the coating comprises at least two coating layers consisting of bioactive compounds and optionally an antioxidative agent adjacent to each other, wherein the first coating layer is a patch-like, non-continuous powder coating layer, and the second coating layer is a continuous coating layer concealing or agglutinating the first coating layer, and wherein the first and second bioactive compounds are selected from a group consisting of pain reliever, blood thinning substances, hormones, cytostatic substances, growth factors, inflammation inhibitors and antibiotics, obtainable in a process comprising the following steps: - providing an implant with a surface, - providing a first suspension comprising at least one first bioactive compound in a first solvent, wherein the first bioactive compound is non-soluble or partially soluble in the first solvent, - applying said first suspension comprising the at least one first bioactive compound onto at least a part of the implant surface forming a first coating layer, - drying the first coating layer, - providing a second solution comprising at least one second bioactive compound in a second solvent, wherein the second bioactive compound is soluble or readily soluble in the second solvent; - applying said second solution comprising the at least one second bioactive compound onto the first coating layer forming a second coating layer, and - drying the second coating layer. - providing an implant with a surface, - providing a first suspension comprising at least one first bioactive compound in a first solvent, wherein the first bioactive compound is non-soluble or partially soluble in the first solvent, - applying said first suspension comprising the at least one first bioactive compound onto at least a part of the implant surface forming a first coating layer, - drying the first coating layer, - providing a second solution comprising at least one second bioactive compound in a second solvent, wherein the second bioactive compound is soluble or readily soluble in the second solvent; - applying said second solution comprising the at least one second bioactive compound onto the first coating layer forming a second coating layer, and - drying the second coating layer.
A method for preparing a dry-strength agent of glyoxylated polyacrylamide, in which an aqueous solution of polyacrylamide is supplemented with ethanediol (glyoxal) under stirring by means of a circulation pump, the reaction is started by the addition of a base, in particular a strong base, at a pH value above 8, and is allowed to react under stirring or circulating, whereupon the reaction is stopped by the addition of an acid under stirring or circulating after completion of a predetermined reaction time, characterized in that the reaction of polyacrylamide and ethandial is a ratio of 3:1 to 10:1 is performed over a predetermined constant time of 6 to 20 minutes, in particular 12 to 18 minutes, that the method is performed as a discontinuous method in which the quantitative reaction of ethanedial with an excess amount of polyacrylamide in an aqueous basic medium is controlled and/or regulated by d) drop of pH value and at least one of the following factors, selected from: a) turbidity measurement b) pH adaptation as a function of the temperature c) pH adaptation as a function of the reaction time or e) current consumption of the circulation pump. a) turbidity measurement b) pH adaptation as a function of the temperature c) pH adaptation as a function of the reaction time or e) current consumption of the circulation pump.
A cell holder, having form of a plate, in which there are provided cylindrical cavities for cells, ending with a bottom, wherein the bottom has a through hole, shifted from the side wall of the cavity, while from the side of the cavity the bottom is at least partially covered with a soft gasket, wherein the gasket is integrated with and permanently connected to the cell holder, and wherein the thickness of the gasket near the side wall of the cavity is greater than the thickness of the gasket near the through hole.