mhurhangee/ep-ind-claims huggingface dataset:
A computer-implemented method for layered storage of enterprise data of one or more virtual machines (227, 228; 311, 312, 314) running on a host machine and managed by a hypervisor, said method comprising: - a local cache memory in a storage accelerator (102, 103, 104, 105) receiving from said one or more virtual machines (227, 228; 311, 312, 314) data blocks having a fixed length block size in the range from 4 kilobyte to 64 kilobyte; - said local cache memory de-duplicating said data blocks for said one or more virtual machines (227, 228; 311, 312, 314); - storing de-duplicated data blocks in said local cache memory as a first tier caching in a first storage layer; - a container generator in said storage accelerator (102, 103, 104, 105) time-based grouping said de-duplicated data blocks into data containers (151, 152) having a configurable maximum container size in the range from 1 megabyte to 16 megabyte as a second tier caching in said first storage layer; - a storage distributor dividing each data container (151, 152) in X fixed length mega-blocks, X being a first integer number; - said storage distributor for each data container (151, 152) applying erasure encoding to said X fixed length mega-blocks; - said storage distributor dividing each data container in Y fixed length mega-blocks with redundant data, Y being a second integer number larger than X; and - said storage distributor distributed storing said Y fixed length mega-blocks over multiple backend storage systems (226; 403; 503) as a second storage layer. - a local cache memory in a storage accelerator (102, 103, 104, 105) receiving from said one or more virtual machines (227, 228; 311, 312, 314) data blocks having a fixed length block size in the range from 4 kilobyte to 64 kilobyte; - said local cache memory de-duplicating said data blocks for said one or more virtual machines (227, 228; 311, 312, 314); - storing de-duplicated data blocks in said local cache memory as a first tier caching in a first storage layer; - a container generator in said storage accelerator (102, 103, 104, 105) time-based grouping said de-duplicated data blocks into data containers (151, 152) having a configurable maximum container size in the range from 1 megabyte to 16 megabyte as a second tier caching in said first storage layer; - a storage distributor dividing each data container (151, 152) in X fixed length mega-blocks, X being a first integer number; - said storage distributor for each data container (151, 152) applying erasure encoding to said X fixed length mega-blocks; - said storage distributor dividing each data container in Y fixed length mega-blocks with redundant data, Y being a second integer number larger than X; and - said storage distributor distributed storing said Y fixed length mega-blocks over multiple backend storage systems (226; 403; 503) as a second storage layer.
Phosphate-based ceramic coating comprising porous particles obtainable by reacting a component mixture A with a component mixture B, wherein (a) component mixture A comprises water and acidic phosphate; and (b) component mixture B comprises water and alkaline earth metal oxide and/or hydroxide; characterized in that component mixtures A and/or B comprise(s) porous particles which are selected from expanded perlite particles or a mixture of expanded perlite particles and aerogel particles and which have a mean particle size of from 2 μm up to 700 μm, wherein the phosphate-based ceramic coating comprising porous particles has been sprayed and is in the form of a layer having a layer thickness of from 2 μm up to 5 mm. (a) component mixture A comprises water and acidic phosphate; and (b) component mixture B comprises water and alkaline earth metal oxide and/or hydroxide; characterized in that component mixtures A and/or B comprise(s) porous particles which are selected from expanded perlite particles or a mixture of expanded perlite particles and aerogel particles and which have a mean particle size of from 2 μm up to 700 μm, wherein the phosphate-based ceramic coating comprising porous particles has been sprayed and is in the form of a layer having a layer thickness of from 2 μm up to 5 mm. characterized in that component mixtures A and/or B comprise(s) porous particles which are selected from expanded perlite particles or a mixture of expanded perlite particles and aerogel particles and which have a mean particle size of from 2 μm up to 700 μm, wherein the phosphate-based ceramic coating comprising porous particles has been sprayed and is in the form of a layer having a layer thickness of from 2 μm up to 5 mm.
A method for homogenizing a start-up behavior, in particular of a liquid discharge temperature, of a continuous-flow heater, in particular comprising a bare heating wire system in a beverage machine, in the case of which - a liquid flows through a heating channel section, which can be heated by a heating device of the continuous-flow heater and a drain line (7, 8), which is connected thereto up to a removal device and which comprises a first drain line section, - the heating device of the continuous-flow heater heats the liquid to a desired set-point temperature, and - a residual quantity of liquid, which remains in the heating channel and in the drain line (7, 8) after each liquid removal, is considered in a subsequent heating process, characterized in - that the first drain line section is flushed after each liquid removal, in particular with non-heated liquid, so that a temperature level, which is always the same, can be used in response to a subsequent heating process, - that the liquid, which flows through the continuous-flow heater, is introduced into an outlet via a valve until the desired set-point temperature is reached, or - that the liquid, which flows through the continuous-flow heater, is supplied again to the continuous-flow heater via the valve and a return line until the desired set-point temperature is reached. - a liquid flows through a heating channel section, which can be heated by a heating device of the continuous-flow heater and a drain line (7, 8), which is connected thereto up to a removal device and which comprises a first drain line section, - the heating device of the continuous-flow heater heats the liquid to a desired set-point temperature, and - a residual quantity of liquid, which remains in the heating channel and in the drain line (7, 8) after each liquid removal, is considered in a subsequent heating process, - that the first drain line section is flushed after each liquid removal, in particular with non-heated liquid, so that a temperature level, which is always the same, can be used in response to a subsequent heating process, - that the liquid, which flows through the continuous-flow heater, is introduced into an outlet via a valve until the desired set-point temperature is reached, or - that the liquid, which flows through the continuous-flow heater, is supplied again to the continuous-flow heater via the valve and a return line until the desired set-point temperature is reached.
A turbine engine component comprising: an airfoil portion having an airfoil mean line, a pressure side, and a suction side; a first region on said pressure side having a first array of cooling microcircuits embedded in a wall forming said pressure side; a second region on said pressure side having a second array of cooling microcircuits embedded in said wall; said first region being located on a first side of said mean line and said second region being located on a second side of said mean line; and a trailing edge internal circuit within said airfoil portion; said first array having a first cooling circuit with a first inlet located on said first side of said mean line, said first inlet receiving cooling fluid from said trailing edge internal circuit; said second array having a second cooling circuit with a second inlet located on said second side of said mean line, said second inlet receiving cooling fluid from said trailing edge internal circuit; characterised in that: said second cooling circuit has a first passageway oriented along a span of said airfoil portion, a second passageway at an angle with respect to said first passageway, and a third passageway at an angle with respect to said second passageway and wherein said third passageway has a plurality of film cooling holes for allowing cooling fluid to flow over the pressure side of said airfoil portion. an airfoil portion having an airfoil mean line, a pressure side, and a suction side; a first region on said pressure side having a first array of cooling microcircuits embedded in a wall forming said pressure side; a second region on said pressure side having a second array of cooling microcircuits embedded in said wall; said first region being located on a first side of said mean line and said second region being located on a second side of said mean line; and a trailing edge internal circuit within said airfoil portion; said first array having a first cooling circuit with a first inlet located on said first side of said mean line, said first inlet receiving cooling fluid from said trailing edge internal circuit; said second array having a second cooling circuit with a second inlet located on said second side of said mean line, said second inlet receiving cooling fluid from said trailing edge internal circuit; characterised in that: said second cooling circuit has a first passageway oriented along a span of said airfoil portion, a second passageway at an angle with respect to said first passageway, and a third passageway at an angle with respect to said second passageway and wherein said third passageway has a plurality of film cooling holes for allowing cooling fluid to flow over the pressure side of said airfoil portion. said second cooling circuit has a first passageway oriented along a span of said airfoil portion, a second passageway at an angle with respect to said first passageway, and a third passageway at an angle with respect to said second passageway and wherein said third passageway has a plurality of film cooling holes for allowing cooling fluid to flow over the pressure side of said airfoil portion.
A method for screening genomic DNA fragments capable of providing plants with an agriculturally advantageous phenotypic variation of a quantitative trait, comprising the steps of: 1) preparing genomic DNA from a plant, which is then cloned into a cloning vector to form a genomic DNA library with the proviso that a preliminary selection step of the genomic DNA fragments before introducing the genomic DNA fragments into the plant is excluded; 2) introducing the genomic DNA fragment from each of the genomic clones constituting the genomic DNA library randomly and separately into a plant to produce transgenic plants; 3) cultivating the transgenic plants or progeny thereof to select a plant exhibiting an agriculturally advantageous phenotypic variation of the quantitative trait; 4) selecting the genomic DNA fragment, which was introduced in step into the plant selected in step, as a purposed genomic DNA fragment, wherein the selection is independent of the characteristics of the plant which is a donor of the genomic DNA fragments and the genomic DNA fragments that are introduced; and 5) optionally introducing the genomic DNA fragment selected in step or a part thereof into a plant to repeat steps 3 and 4, and selecting a genomic DNA fragment which produces a plant exhibiting an agriculturally advantageous phenotypic variation of the quantitative trait as a purposed genomic DNA fragment in each repetition. 1) preparing genomic DNA from a plant, which is then cloned into a cloning vector to form a genomic DNA library with the proviso that a preliminary selection step of the genomic DNA fragments before introducing the genomic DNA fragments into the plant is excluded; 2) introducing the genomic DNA fragment from each of the genomic clones constituting the genomic DNA library randomly and separately into a plant to produce transgenic plants; 3) cultivating the transgenic plants or progeny thereof to select a plant exhibiting an agriculturally advantageous phenotypic variation of the quantitative trait; 4) selecting the genomic DNA fragment, which was introduced in step into the plant selected in step, as a purposed genomic DNA fragment, wherein the selection is independent of the characteristics of the plant which is a donor of the genomic DNA fragments and the genomic DNA fragments that are introduced; and 5) optionally introducing the genomic DNA fragment selected in step or a part thereof into a plant to repeat steps 3 and 4, and selecting a genomic DNA fragment which produces a plant exhibiting an agriculturally advantageous phenotypic variation of the quantitative trait as a purposed genomic DNA fragment in each repetition.
Filter system for filtering a fluid, comprising - a filter element, - a filter housing, comprising a first housing component and a second housing component in which the filter element is disposed, - a sealing apparatus disposed between the first housing component and the second housing component for sealing a housing interior area against an environment, which sealing apparatus features a seal disposed on a seal carrier, wherein the seal with at least one radially inside-lying inner face rests on the radially outside-lying contact face of the seal carrier and is radially inwardly supported by the contact face, and wherein the seal carrier features coupling elements (36, 46) for connecting to the first housing component and/or to the second housing component, wherein the coupling elements (36, 46) feature snap or locking elements, wherein the coupling elements (36, 46) engage in a coupling receptacle on the interior side of the first housing component and/or of the second housing component. - a filter element, - a filter housing, comprising a first housing component and a second housing component in which the filter element is disposed, - a sealing apparatus disposed between the first housing component and the second housing component for sealing a housing interior area against an environment, which sealing apparatus features a seal disposed on a seal carrier, wherein the seal with at least one radially inside-lying inner face rests on the radially outside-lying contact face of the seal carrier and is radially inwardly supported by the contact face, and wherein the seal carrier features coupling elements (36, 46) for connecting to the first housing component and/or to the second housing component, wherein the coupling elements (36, 46) feature snap or locking elements, wherein the coupling elements (36, 46) engage in a coupling receptacle on the interior side of the first housing component and/or of the second housing component.
A method in a receiving node, for determining whether received data is encoded with a certain channel code candidate, said method comprising: - obtaining data encoded with an unknown channel code, said method being characterized in that it comprises: - calculating the respective posterior probabilities that a set of syndrome checks are satisfied, given the obtained data, which syndrome checks are associated with the channel code candidate, - combining the posterior probabilities, and - determining whether the channel code candidate was used for encoding the obtained data, based on the combined posterior probabilities, wherein the combining and determining involves a statistical test which is a Generalized Likelihood Ratio Test (GLRT). - obtaining data encoded with an unknown channel code, said method being characterized in that it comprises: - calculating the respective posterior probabilities that a set of syndrome checks are satisfied, given the obtained data, which syndrome checks are associated with the channel code candidate, - combining the posterior probabilities, and - determining whether the channel code candidate was used for encoding the obtained data, based on the combined posterior probabilities, wherein the combining and determining involves a statistical test which is a Generalized Likelihood Ratio Test (GLRT).
An aqueous fabric softener composition [composition, herein after] comprising: - from 0.01 to 10.0 wt.% of at least one fragrance fixative comprising at least one carbohydrate ester; - from 0.01 to 10 wt.% of at least one fragrance; - from 0.01 to 50 wt.% of at least one cationic surfactant; - at least 45.0 wt.% of water; wherein the fragrance fixative is characterized by a cLogP value of equal to or greater than 1.5 and a boiling point from 200°C to 350°C; and wherein the carbohydrate ester comprises at least one ester group of formula -O-(C=O)-R 1 wherein R 1 is selected from C1-C6 alkyl or C1-C6 alkoxy groups; and whereby the weight percentages are expressed relative to the total weight of the composition. - from 0.01 to 10.0 wt.% of at least one fragrance fixative comprising at least one carbohydrate ester; - from 0.01 to 10 wt.% of at least one fragrance; - from 0.01 to 50 wt.% of at least one cationic surfactant; - at least 45.0 wt.% of water; wherein the fragrance fixative is characterized by a cLogP value of equal to or greater than 1.5 and a boiling point from 200°C to 350°C; and wherein the carbohydrate ester comprises at least one ester group of formula -O-(C=O)-R 1 wherein R 1 is selected from C1-C6 alkyl or C1-C6 alkoxy groups; and whereby the weight percentages are expressed relative to the total weight of the composition.
A tobacco composition comprising a tobacco component in an amount of from 60 to 90% by weight of the tobacco composition, a filler in an amount of 0 to 20% by weight of the tobacco composition, and an aerosol generating agent in an amount of from 10 to 20% by weight of the tobacco composition; wherein the tobacco composition has a nicotine content of from 0.5 to 1.5% by weight of the tobacco composition; and wherein the tobacco component comprises paper reconstituted tobacco in an amount of from 70 to 100% by weight of the tobacco component. wherein the tobacco composition has a nicotine content of from 0.5 to 1.5% by weight of the tobacco composition; and wherein the tobacco component comprises paper reconstituted tobacco in an amount of from 70 to 100% by weight of the tobacco component.
A two-stroke uniflow engine comprising: a cylinder; a piston that slides inside the cylinder; an exhaust valve that is provided at one end portion in a stroke direction of the cylinder, and is opened and closed in order to discharge exhaust gas that is generated inside the cylinder; a scavenging port that is provided in an internal circumferential surface at an end portion on the other side in the stroke direction of the cylinder, and takes active gas into the interior of the cylinder in accordance with the sliding movement of the piston; a fuel injection port that is provided in the internal circumferential surface of the cylinder; a fuel injection valve that injects fuel gas into the fuel injection port; and a fuel injection control unit that executes control of the injection of the fuel gas in the fuel injection valve, wherein the fuel injection control unit decides at least one of an injection pressure and an injection time of the fuel injection valve based on changes in pressure inside the cylinder that are caused by a reciprocating movement of the piston, characterized in that the fuel injection control unit predicts the changes in the internal pressure in the cylinder based on the internal pressure in the cylinder when an angle of a crank that converts the reciprocating movement of the piston into an axial rotation movement reaches a predetermined angle, and the predetermined angle is an optional angle between a point when the exhaust valve changes to a closed state and a point when the fuel injection port changes to a closed state. a cylinder; a piston that slides inside the cylinder; an exhaust valve that is provided at one end portion in a stroke direction of the cylinder, and is opened and closed in order to discharge exhaust gas that is generated inside the cylinder; a scavenging port that is provided in an internal circumferential surface at an end portion on the other side in the stroke direction of the cylinder, and takes active gas into the interior of the cylinder in accordance with the sliding movement of the piston; a fuel injection port that is provided in the internal circumferential surface of the cylinder; a fuel injection valve that injects fuel gas into the fuel injection port; and a fuel injection control unit that executes control of the injection of the fuel gas in the fuel injection valve, wherein the fuel injection control unit decides at least one of an injection pressure and an injection time of the fuel injection valve based on changes in pressure inside the cylinder that are caused by a reciprocating movement of the piston, characterized in that the fuel injection control unit predicts the changes in the internal pressure in the cylinder based on the internal pressure in the cylinder when an angle of a crank that converts the reciprocating movement of the piston into an axial rotation movement reaches a predetermined angle, and the predetermined angle is an optional angle between a point when the exhaust valve changes to a closed state and a point when the fuel injection port changes to a closed state.
Boat of the outboard type comprising a hydrodynamic rear bearing assembly navigating on a hull cooperating with a set of front wings (11a, 11b), the outboard is driven by an underwater propeller motor assembly propelled by a shaft direct engine actuated by an indirect engine shaft, on an engine propulsion hull comprising anti-stack and anti-cavitation plates positioned above the propeller intended to be positioned at water level, hydrodynamic assembly in which the manufacturer's engine position is lowered under water, the engine hull is fitted with a supporting wing attached at the front to the direct shaft hull ogive, a deflection ring attached above the anti-stacking and anti-cavitation plates and at the front and the hull of the indirect drive shaft, a reported hydrodynamic penetration profile nested at the front of the hull of the indirect drive shaft, occupying the space at the front of the engine between the top of the anti-stacking and anti-cavitation plates and the bottom of the deflection ring, the rear of the hull is equipped at the height of the placement of the ring deflection of a deflection plate.