mhurhangee/ep-ind-claims huggingface dataset:
A method for measuring a position of an object in an ambient space (22; 32) with an object position measuring system, said ambient space having a fluid connection with a reference pressure volume (20; 30), the method comprising: (a) measuring an absolute pressure in said reference pressure volume; (b) measuring a pressure difference between a pressure in said reference pressure volume and an ambient pressure in said ambient space; (c) adding said absolute pressure in said reference pressure volume and said pressure difference to determine a change of pressure in said ambient space; (d) determining said change of pressure in said ambient space, and (e) correcting a position measurement of said object position measuring system on the basis of said determined change of pressure in said ambient space. (a) measuring an absolute pressure in said reference pressure volume; (b) measuring a pressure difference between a pressure in said reference pressure volume and an ambient pressure in said ambient space; (c) adding said absolute pressure in said reference pressure volume and said pressure difference to determine a change of pressure in said ambient space; (d) determining said change of pressure in said ambient space, and (e) correcting a position measurement of said object position measuring system on the basis of said determined change of pressure in said ambient space.
An electrotype for attachment to the face cloth of a cylinder mould for forming an image during a paper making process, the electrotype comprising a mesh and at least one image forming element attached to the mesh.
A computer-implemented method of acquiring virtual object data in augmented reality (1203, 1210), the method comprising: identifying at least one component (301-305, 401-405) of a target device (300, 400) from three-dimensional image data corresponding to the target device (300, 400), the at least one component being exposed to a view from outside of the target device (300, 400); identifying a type of the target device (300, 400) from the three-dimensional image data corresponding to the target device (300, 400); identifying a plurality of directions of the target device (300, 400) based on the type of the target device (300, 400); obtaining at least one of a component weight corresponding to the at least one component or a direction weight of each of the plurality of directions, based on the type of the target device; and acquiring virtual object data for representing an appearance of the target device (300 400) by reducing the three-dimensional image data based on the at least one component, the plurality of directions, and the at least one of the component weight or the direction weight of each of the plurality of directions, while maintaining visual quality from the three-dimensional image data, by allocating more available data resources to visually important portions. identifying at least one component (301-305, 401-405) of a target device (300, 400) from three-dimensional image data corresponding to the target device (300, 400), the at least one component being exposed to a view from outside of the target device (300, 400); identifying a type of the target device (300, 400) from the three-dimensional image data corresponding to the target device (300, 400); identifying a plurality of directions of the target device (300, 400) based on the type of the target device (300, 400); obtaining at least one of a component weight corresponding to the at least one component or a direction weight of each of the plurality of directions, based on the type of the target device; and acquiring virtual object data for representing an appearance of the target device (300 400) by reducing the three-dimensional image data based on the at least one component, the plurality of directions, and the at least one of the component weight or the direction weight of each of the plurality of directions, while maintaining visual quality from the three-dimensional image data, by allocating more available data resources to visually important portions.
A method of manufacturing a touch panel, comprising: S1: forming a thin film layer on a first substrate; S2: forming a buffer layer on the thin film layer, wherein the thin film layer is located between the first substrate and the buffer layer; S3: forming a sensing layer on the buffer layer, wherein the buffer layer is located between the thin film layer and the sensing layer; S4: forming a second substrate on the sensing layer, wherein the sensing layer is located between the buffer layer and the second substrate; S5: removing the first substrate; S6: adhering a cover plate onto the thin film layer by a bonding layer, wherein the bonding layer is located between the cover plate and the thin film layer; and S7: removing the second substrate. S1: forming a thin film layer on a first substrate; S2: forming a buffer layer on the thin film layer, wherein the thin film layer is located between the first substrate and the buffer layer; S3: forming a sensing layer on the buffer layer, wherein the buffer layer is located between the thin film layer and the sensing layer; S4: forming a second substrate on the sensing layer, wherein the sensing layer is located between the buffer layer and the second substrate; S5: removing the first substrate; S6: adhering a cover plate onto the thin film layer by a bonding layer, wherein the bonding layer is located between the cover plate and the thin film layer; and S7: removing the second substrate.
A system, comprising: a turbine combustor, comprising: a fuel nozzle comprising an inner shell and an outer shell; and a feed cap disposed about the fuel nozzle comprising an outer wall and a back plate, wherein the back plate joins respective upstream ends of the outer shell of the fuel nozzle and the outer wall of the feed cap; wherein the turbine combustor is configured to flow a first pressurized air via a first air path extending along the outer wall of the feed cap, the back plate of the feed cap, and into the fuel nozzle. a fuel nozzle comprising an inner shell and an outer shell; and a feed cap disposed about the fuel nozzle comprising an outer wall and a back plate, wherein the back plate joins respective upstream ends of the outer shell of the fuel nozzle and the outer wall of the feed cap; wherein the turbine combustor is configured to flow a first pressurized air via a first air path extending along the outer wall of the feed cap, the back plate of the feed cap, and into the fuel nozzle.
A clipping tool assembly for closing at least one closure means, like a closure clip, in a packaging machine, like a clipping machine, for closing tubular or bag-shaped packaging casings, comprising: a first closing tool and a second closing tool, wherein at least the first closing tool is reversibly movable towards the second closing tool, between an opened position and a closed position, for closing the at least one closure means; a drive means for reversibly moving at least the first closing tool towards the second closing tool in a closing direction; wherein a pusher means is provided in the region of the second closing tool for pushing the closure means just closed out of the second closing tool, and wherein the pusher means acts on that part of the closure means, which is supported by the second closure tool, characterized in that a pusher channel is a through hole extending through the second closing tool in the closing direction, wherein the second closing tool includes a pusher channel in which the pusher element is reversibly movable in the pushing direction. a first closing tool and a second closing tool, wherein at least the first closing tool is reversibly movable towards the second closing tool, between an opened position and a closed position, for closing the at least one closure means; a drive means for reversibly moving at least the first closing tool towards the second closing tool in a closing direction; wherein a pusher means is provided in the region of the second closing tool for pushing the closure means just closed out of the second closing tool, and wherein the pusher means acts on that part of the closure means, which is supported by the second closure tool, characterized in that a pusher channel is a through hole extending through the second closing tool in the closing direction, wherein the second closing tool includes a pusher channel in which the pusher element is reversibly movable in the pushing direction.
Coated substrate comprising a substrate made of an aluminium-silicon alloy or crystalline silicon to which a polishable layer is applied, which layer consists of amorphous silicon, microcrystalline silicon, silicon carbide, silicon nitride, titanium nitride, aluminium oxide, zirconium oxide, chromium and/or mixtures hereof, wherein an intermediate layer which acts as adhesive- or as barrier layer is disposed between the substrate and the polishable layer, and the intermediate layer consists of aluminium oxide, zirconium oxide, titanium or chromium.
A kayak with additional drive formed with a hull comprising a bottom and a deck in which is formed a crew chamber equipped with a seat and which is equipped not only with an electric engine, which is coupled with a screw-propeller, but also with a battery, which is electrically connected with the electric engine, wherein the electric engine is placed on a supporting frame, which is designed as a vertical flat element which is situated perpendicularly to the lengthwise axis of the kayak and is fixed in the back end part of the kayak, where the electric engine is on the supporting frame fixed by the help of a flat engine frame which is on the supporting frame fixed and it is parallel with its plane and also is, by the help of at least a drive element, which is by its end part waterproof way freely pivoted in the stern of the kayak in axial direction, coupled with the screw-propeller, whereas the battery is placed in a battery box which is placed in the front end part of the kayak.
A gas turbine engine comprising: a compressor portion; a combustor fluidly connected to the compressor portion; a turbine section fluidly connected to the combustor, wherein the turbine section includes at least a first turbine portion and a second turbine portion connected to the first turbine portion via a transition duct, fluid in the second turbine portion having a lower pressure than fluid in the first turbine portion; a fan drive gear system connecting the second turbine portion to a fan; wherein the first turbine portion (110; 210) drives a first shaft (130; 230) and the second turbine portion (120; 220) drives a second shaft (140; 240), and wherein the first shaft (130; 230) is supported relative to the second shaft (140; 240) via a piggyback intershaft bearing arrangement in which a bearing is supported radially between two revolving races relative to an axis of the engine; the gas turbine engine characterized in that the transition duct lacks flow correcting vanes, the first turbine portion and the second turbine portion are counter rotating turbine portions, and in that the second turbine portion includes exactly three turbine stages. a compressor portion; a combustor fluidly connected to the compressor portion; a turbine section fluidly connected to the combustor, wherein the turbine section includes at least a first turbine portion and a second turbine portion connected to the first turbine portion via a transition duct, fluid in the second turbine portion having a lower pressure than fluid in the first turbine portion; a fan drive gear system connecting the second turbine portion to a fan; wherein the first turbine portion (110; 210) drives a first shaft (130; 230) and the second turbine portion (120; 220) drives a second shaft (140; 240), and wherein the first shaft (130; 230) is supported relative to the second shaft (140; 240) via a piggyback intershaft bearing arrangement in which a bearing is supported radially between two revolving races relative to an axis of the engine; the gas turbine engine characterized in that the transition duct lacks flow correcting vanes, the first turbine portion and the second turbine portion are counter rotating turbine portions, and in that the second turbine portion includes exactly three turbine stages.
An RFeB system magnet production method for producing an R L 2 Fe 14 B system magnet which is a sintered magnet or a hot-deformed magnet containing, as a main rare-earth element, a light rare-earth element R L which is one of two elements of Nd and Pr, the method comprising steps of: preparing a coating material by mixing a silicone grease and an R H -containing powder containing a heavy rare-earth element R H composed of one element selected from a group of Dy, Tb and Ho, wherein a dispersant for enhancing dispersibility of the R H -containing powder is added to the coating material, the dispersant containing fatty ester as a main component; applying, to a surface of a base material of the R L 2 Fe 14 B system magnet, the coating material; and heating the base material together with the coating material. preparing a coating material by mixing a silicone grease and an R H -containing powder containing a heavy rare-earth element R H composed of one element selected from a group of Dy, Tb and Ho, wherein a dispersant for enhancing dispersibility of the R H -containing powder is added to the coating material, the dispersant containing fatty ester as a main component; applying, to a surface of a base material of the R L 2 Fe 14 B system magnet, the coating material; and heating the base material together with the coating material.
A FoxMl gene splicing modifier selected from a compound of formula or of formula or of formula (VIII): wherein X is -O- or -N(CH 3)-; R' is cyano, pyrazolyl optionally substituted with methyl, or pyridinyl substituted with methyl and hydroxy; R" is hydrogen, methyl or methoxy; R′′′ is pyrazolyl optionally substituted with methyl, or pyridinyl substituted with methyl and hydroxy; R u is hydrogen, chloro or fluoro; R v is hydrogen, chloro or fluoro; or a pharmaceutically acceptable salt thereof; for use in the treatment, prevention and/or delay of progression of cancer.
Pressure controlled multistage cooling plant having at least a high stage comprising at least a set of first compressors, a set of first condensers, at least a first receiver means and a first duct of an intermediate heat exchanger means mutually connected to form the high stage refrigeration circuit; said plant being further provided with at least a low stage comprising at least a set of second compressors, a second duct of the intermediate heat exchanger means, at least a second receiver means, a set of low stage user apparatus mutually connected to form the low stage refrigeration circuit, a control means for controlling various elements of the plant, feeding means to feed the intermediate heat exchanger means with a cooling fluid; said plant comprises pressure sensor means assigned to detect the pressure of the fluid of the low stage and connected to the control means configured to activate the feeding means when said pressure of the fluid of the idle low stage reaches or exceeds a predetermined threshold value; said feeding means are activated and connected to a duct of the intermediate heat exchanger means to feed in said duct a cooling fluid for cooling the fluid of the low stage in a condition of activation of said feeding means; said duct of the intermediate heat exchanger means that can be connected to the feeding means consists of the first duct of the intermediate heat exchanger means and the cooling fluid feed by the feeding means consists of the fluid of the high stage; said plant is characterized in that the feeding means comprising at least a safety compressor, at least one safety condenser, a first cut-off valve and a first expansion means; the inlet of the safety compressor is connected to a first inlet of the first duct of the intermediate heat exchanger means and the outlet of said safety compressor is connected to an inlet of the at least one safety condenser whose outlet is connected to the inlet of the first receiver means whose outlet is connectable, by means of the first cut-off valve and of the first expansion means operated by the control means, to the second inlet of the first duct, where said first duct, safety compressor, safety condenser, first receiver means, first cut-off valve and first expansion means, in the condition of activation operated by the control means, carry out the circuit of the feeding means for cooling the fluid of the low stage.
A computer-implemented method for generating a building automation project of a building automation system, BAS, comprising the steps: receiving, via an interface, structural information (31, 32, 33, 34, 35) regarding building equipment, wherein the structural information comprises input data available during a planning stage of a building automation process; generating a semantic model of the building automation system, comprising the step of automatically extracting equipment information from the structural information (31, 32, 33, 34, 35) regarding the building equipment, wherein the step of automatically extracting equipment information from the structural information (31, 32, 33, 34, 35) regarding the building equipment comprises specifying a type of building equipment and/or relations of the building equipment; extending the semantic model of the building automation system by providing application information, wherein the step of providing application information comprises specifying a type of applications corresponding to the type of building equipment and/or the relations of the building equipment; and generating, based on the equipment information and application information of the extended semantic model of the building automation system, a building automation project adapted for loading on a building automation device which presents the building automation project to a user. receiving, via an interface, structural information (31, 32, 33, 34, 35) regarding building equipment, wherein the structural information comprises input data available during a planning stage of a building automation process; generating a semantic model of the building automation system, comprising the step of automatically extracting equipment information from the structural information (31, 32, 33, 34, 35) regarding the building equipment, wherein the step of automatically extracting equipment information from the structural information (31, 32, 33, 34, 35) regarding the building equipment comprises specifying a type of building equipment and/or relations of the building equipment; extending the semantic model of the building automation system by providing application information, wherein the step of providing application information comprises specifying a type of applications corresponding to the type of building equipment and/or the relations of the building equipment; and generating, based on the equipment information and application information of the extended semantic model of the building automation system, a building automation project adapted for loading on a building automation device which presents the building automation project to a user.
A method of producing an elastomer composite, comprising: - providing a carbon black slurry; and - providing a latex blend comprising skim latex and at least one of field latex and latex concentrate, wherein when the latex blend comprises field latex blended with skim latex, the latex blend comprises field latex at a ratio from 20:1 to 1:1 by volume with respect to skim latex, and when the latex blend comprises latex concentrate blended with skim latex, the latex blend comprises latex concentrate at a ratio from 20:1 to 1:2 by volume with respect to skim latex; and wherein the dry rubber content of the latex blend is at least 15% by weight; and - combining the carbon black slurry and the latex blend to form a mixture under conditions in which the mixture coagulates, wherein combining comprises feeding a continuous flow of carbon black slurry under pressure to a mixing zone of a coagulum reactor to form a mixture with the latex blend, the carbon black being effective to coagulate the latex within the latex blend and the feeding of the latex blend and the carbon black slurry within the mixing zone being sufficiently energetic to substantially completely coagulate the latex with the carbon black in the coagulum reactor. - providing a carbon black slurry; and - providing a latex blend comprising skim latex and at least one of field latex and latex concentrate, wherein when the latex blend comprises field latex blended with skim latex, the latex blend comprises field latex at a ratio from 20:1 to 1:1 by volume with respect to skim latex, and when the latex blend comprises latex concentrate blended with skim latex, the latex blend comprises latex concentrate at a ratio from 20:1 to 1:2 by volume with respect to skim latex; and wherein the dry rubber content of the latex blend is at least 15% by weight; and - combining the carbon black slurry and the latex blend to form a mixture under conditions in which the mixture coagulates,
A composition comprising magnesium, potassium and citrate for use in the inhibition of crystallization and/or biofilm formation on an indwelling urinary catheter, wherein magnesium, potassium and citrate are present as ion(s), wherein the molar ratio of potassium ions to magnesium ions to citrate ions in the composition is 4:1:2, wherein the tripotassium citrate monohydrate constitutes 70-80 weight % of the citrate salts in the composition, wherein anhydrous trimagnesium citrate constitutes 20-30 weight % of the citrate salts in the composition, and wherein the administration of the composition to a subject is to begin within 1 hour of the catheterization of said subject. wherein the tripotassium citrate monohydrate constitutes 70-80 weight % of the citrate salts in the composition, wherein anhydrous trimagnesium citrate constitutes 20-30 weight % of the citrate salts in the composition, and wherein the administration of the composition to a subject is to begin within 1 hour of the catheterization of said subject.
An accommodating intraocular lens, comprising: a bulk polymeric material; and a silicone oil having a mean molecular weight number average of between 5000 Daltons to 6500 Daltons and a polydispersity index less than 1.5, wherein the silicone oil comprises diphenyl siloxane and dimethyl siloxane and the components of the silicone oil are fully miscible with each other. a bulk polymeric material; and a silicone oil having a mean molecular weight number average of between 5000 Daltons to 6500 Daltons and a polydispersity index less than 1.5, wherein the silicone oil comprises diphenyl siloxane and dimethyl siloxane and the components of the silicone oil are fully miscible with each other.
A light-transmitting gasket intended in particular to be inserted at the bottom of a stopper or cap, in the form of a support on at least one of the faces of which a light-transmitting coating is applied, characterized in that the coating presents a watermark, that is to say an image visible in transmitted light and not visible in reflection.
A device comprising: a processor operative to provide pixel data and audio data; and a plurality of differential lane transmission circuits (19a,.., 19n), operatively coupled to the processor, and operative to provide, across respective differential lines (20a,.., 20n), non-redundant data and at least one of redundant control symbols or redundant control data and operative to skew the at least one of respective redundant control symbols or redundant control data in time across the plurality of differential lane transmission circuits. a processor operative to provide pixel data and audio data; and a plurality of differential lane transmission circuits (19a,.., 19n), operatively coupled to the processor, and operative to provide, across respective differential lines (20a,.., 20n), non-redundant data and at least one of redundant control symbols or redundant control data and operative to skew the at least one of respective redundant control symbols or redundant control data in time across the plurality of differential lane transmission circuits.