mhurhangee/patent-ind-claim-en huggingface dataset:
A RAID controller configured to control one of a plurality of data storage clusters configured to store a plurality of data symbols in a plurality of data storage devices, wherein the RAID controller is configured to determine from a configuration matrix which data storage devices from the plurality of data storage devices are assigned to said one of the plurality of data storage clusters, the RAID controller comprising: a calculator configured to compute a first intermediate checksum of the data symbols stored in said one of the plurality of data storage clusters and to compute a complete checksum based on the computed first intermediate checksum and further intermediate checksums; wherein the RAID controller is further configured to distribute the first intermediate checksum via a communication fabric and to receive the further checksums via the communication fabric, wherein each of the further intermediate checksums corresponds to one of the plurality of data storage clusters, and wherein the RAID controller is further configured to store the calculated complete checksum in at least one of the plurality of storage devices. a calculator configured to compute a first intermediate checksum of the data symbols stored in said one of the plurality of data storage clusters and to compute a complete checksum based on the computed first intermediate checksum and further intermediate checksums; wherein the RAID controller is further configured to distribute the first intermediate checksum via a communication fabric and to receive the further checksums via the communication fabric, wherein each of the further intermediate checksums corresponds to one of the plurality of data storage clusters, and wherein the RAID controller is further configured to store the calculated complete checksum in at least one of the plurality of storage devices.
A method of producing multiple batches of objects by stereolithography, comprising the steps of: (a) dispensing an initial or subsequent batch of dual cure resin into a stereolithography apparatus , said resin comprising a light polymerizable component and a heat polymerizable component; (b) producing an intermediate object by light polymerization of said resin in said apparatus , wherein said intermediate object retains excess resin on a surface thereof, and wherein said stereolithography apparatus is a bottom up stereolithography apparatus ; then (c) separating excess resin from said intermediate object, wherein said separating step is carried out by centrifugal separation; (d) blending said excess resin with additional dual cure resin to produce a subsequent batch of dual cure resin; (e) repeating steps (a) through (c), and optionally repeating step (d), to produce additional object(s); and (f) baking said objects, together or separately, to produce multiple batches of objects. (a) dispensing an initial or subsequent batch of dual cure resin into a stereolithography apparatus , said resin comprising a light polymerizable component and a heat polymerizable component; (b) producing an intermediate object by light polymerization of said resin in said apparatus , wherein said intermediate object retains excess resin on a surface thereof, and wherein said stereolithography apparatus is a bottom up stereolithography apparatus ; then (c) separating excess resin from said intermediate object, wherein said separating step is carried out by centrifugal separation; (d) blending said excess resin with additional dual cure resin to produce a subsequent batch of dual cure resin; (e) repeating steps (a) through (c), and optionally repeating step (d), to produce additional object(s); and (f) baking said objects, together or separately, to produce multiple batches of objects.
Laminated cellulose-based, liquid food packaging material (10a;10b), comprising a bulk material layer (11a; 11b) with through-going holes, openings or slits , each defining an opening area, further comprising an outermost, transparent and protective thermoplastic polymer layer (19a;19b) arranged on the outside of the bulk material layer, i.e. on the side to be directed outwards from a packaging container made from the laminated material, and an innermost, heat sealable and liquid-tight thermoplastic polymer layer (17a;17b), which is intended to be in direct contact with the packed food product, an aluminium metal foil (12a;12b) for providing gas barrier properties, which is laminated between the bulk material layer and the innermost thermoplastic polymer layer, wherein a thermo-mechanically stable polymer layer (15a;15b) is also laminated between the bulk material layer and the innermost thermoplastic layer, the thermomechanically stable polymer layer being of a polymer composition having a melting point higher than 150°C and comprising at least 70 wt-% of a polymer selected from the group consisting of ethylene vinyl alcohol copolymer (EVOH) and polyamide (PA) resulting from polymerization of monomers selected from the group consisting of Caprolactam, Laurolactam, Undecanolactam, Adipic Acid, Azelaic Acid, Sebacic Acid, Dodecanedioic Acid, Terephatalic Acid, Isophathalic Acid, Butanediamine, Hexamethylene diamine, Trimethylhexamethylene diamine and Metaxyxylene diamine (MXDA) monomer, or of a blend of two or more polyamidesobtained from different such monomer combinations, the amount of MXDA monomer included in the polyamide being in total 80 mol% or less, wherein the thermo-mechanically stable layer (15a;15b) is laminated between the aluminium metal foil (12a;12b) and the bulk material layer (11a; 11b), together with at least one intermediate bonding layer (13a, 14a,b, 16a,b) of a thermoplastic polymer and wherein the aluminium metal foil, the inner- and outermost thermoplastic polymer layers and the thermo-mechanically stable polymer layer, all extend throughout the areas of the holes, openings or slits of the bulk material layer, such that they are laminated and sealed to each other to form a laminated opening membrane material, not containing the bulk material layer, within the opening areas.
Plug strip for a control device, comprising a contact carrier in which a plurality of contact elements are embedded and mounted over a partial length of the said contact carrier, wherein the contact elements have contact sections (5.1) which exit from the contact carrier at a front side (20.1) and are arranged in an exposed manner in at least one plug module which is open on one side and which is suitable for receiving a mating plug, wherein the contact carrier and the at least one plug module are produced as a monolithic plastic component, characterized in that a cavity structure with at least one duct is formed on the contact carrier , which cavity structure reinforces the contact carrier .
A one-piece egg pack produced by plastic injection moulding comprising a lower part which has a plurality of egg holders in an interior (I) and a lid which is moulded on integrally via a hinge strip and has an at least partially planar lid wall, wherein the lid is configured to be foldable over the lower part by means of hinge strips and a releasable closed position of the lid on the lower part can be achieved by engagement of lid fastening means into lower part fastening means and a lower part edge engaging in a lid edge , characterized in that furthermore at least one latch-in means is moulded on a lid inner surface of the at least partially planar lid wall such that said at least one latch-in means projects away in the direction of a lid plane (D) and at least one open hollow stub is moulded on the lower part between adjacent egg holders such that said at least one open hollow stub projects away from the egg holders and a lower part plane (U) out of the interior (I) with a stub opening edge in such a manner that in the closed position of the lid the at least one open hollow stub projects from the interior (I) as far as the lid inner surface of the at least partially planar lid wall, wherein the stub opening edge can be operatively connected to the latch-in means and the lid inner surface and thus a guided latching-in and a local fixing of the hollow stub can be achieved.
A device (EMU) for emulating a bimetallic strip, the emulating device (EMU) comprising a current sensor (CC) capable of measuring a line current ( I P ) flowing through the emulating device (EMU), the emulating device (EMU) being capable of providing a value representative of a cumulative thermal state (E th_n ) over time t, which is referred to as cumulative thermal state (E th_n ), by recursively adding a value representative of an initial thermal state (E th_i ), which is referred to as initial thermal state (E th_i ), and a value representative of a present thermal state (E th_on , E th _ off ), which is referred to as present thermal state (E th_on , E th_off ), which is determined depending on the line current ( I P ), the emulating device (EMU) comprising a squaring operator (CAR) configured to square a value representative of the line current ( I P ), which is output by the current sensor (CC), the value representative of the line current ( I P ) being an image voltage (Vinc) of the line current ( I P ), the emulating device (EMU) comprising at least one series RC circuit (CIRC_RC), and comprising at least one capacitor (Cm), at the terminals of which the cumulative thermal state (E th_n ) is measured, the series RC circuit (CIRC_RC) being connected to the squaring operator (CAR), the initial thermal state (E th_i ) being determined by the initial state of charge of the capacitor (Cm) at the end of a charging or discharging cycle, the present thermal state (E th_on , E th _ off ) being determined by the evolution of the state of charge of the capacitor (Cm), characterised in that the squaring operator (CAR) comprises: - a comparator (COMP1) configured to compare the image voltage (Vinc) with a ramp signal and to reset the periodic ramp signal as soon as it is equal to the image voltage (Vine), thus generating a variable period ramp signal (t ramp ) having, for each variable period (t ramp ), a maximum amplitude equal to the image voltage (Vinc) at the same instant; - an integrator (INTG) connected to the output of the comparator (COMP1) and configured to integrate each ramp of the variable period ramp signal over a duration equal to the variable period (t ramp ), thus generating an integrated ramp signal, and to provide the RC circuit with the integrated ramp signal. - a comparator (COMP1) configured to compare the image voltage (Vinc) with a ramp signal and to reset the periodic ramp signal as soon as it is equal to the image voltage (Vine), thus generating a variable period ramp signal (t ramp ) having, for each variable period (t ramp ), a maximum amplitude equal to the image voltage (Vinc) at the same instant; - an integrator (INTG) connected to the output of the comparator (COMP1) and configured to integrate each ramp of the variable period ramp signal over a duration equal to the variable period (t ramp ), thus generating an integrated ramp signal, and to provide the RC circuit with the integrated ramp signal.
Process for preparing polyether carbonate polyols, comprising the step of reaction of alkylene oxide with carbon dioxide in the presence of an H-functional starter compound and double metal cyanide catalyst, characterized in that the process comprises the following steps: (α) optionally, in a first reactor, pretreating the double metal cyanide catalyst (DMC catalyst) at a temperature of 50 to 200°C and/or reduced pressure (absolute) of 10 mbar to 800 mbar, (β) in a first reactor, contacting the double metal cyanide catalyst and suspension medium with alkylene oxide to obtain a first reaction mixture; and (γ) continuously adding the first reaction mixture, alkylene oxide, carbon dioxide and optionally H-functional starter compound to a second reactor, wherein, in step (β), the suspension medium used is at least one H-functional starter compound selected from the group consisting of polyether polyols, polycarbonate polyols, polyester carbonate polyols, polyether ester carbonate polyols and polyether carbonate polyols, wherein these H-functional starter compounds each have a hydroxyl number in the range from 3.0 mg KOH/g to 1000 mg KOH/g, and wherein reaction products formed in step (γ) are withdrawn continuously from the second reactor. (α) optionally, in a first reactor, pretreating the double metal cyanide catalyst (DMC catalyst) at a temperature of 50 to 200°C and/or reduced pressure (absolute) of 10 mbar to 800 mbar, (β) in a first reactor, contacting the double metal cyanide catalyst and suspension medium with alkylene oxide to obtain a first reaction mixture; and (γ) continuously adding the first reaction mixture, alkylene oxide, carbon dioxide and optionally H-functional starter compound to a second reactor,
A method for calculating a creep elongation of a rotor, the method comprising a. providing a correlation for a given cross section of the rotor among o a reference temperature (T Ref ) indicative of the temperature of the rotor, o a creep elongation ( U r ), o a rate of creep elongation ( ΔU r / Δt ) , b. measuring the reference temperature (T Ref ) at a sampling moment i; c. calculating on the basis of the correlation the creep elongation (U ri ) of the rotor at the sampling moment i on the basis of the measured reference temperature (T Ref ) at the sampling moment i and the creep elongation at the sampling moment i-1; wherein the creep elongation (U r ) of the rotor is calculated as: U r = ∑ i = 0 i = n ΔU r Δt T Ref i U r i − 1 × Δt i if an effect of reference temperature (T Ref ) and load on the rate of creep elongation ( ΔU r / Δt ) of the rotor is judged to be the same, or the creep elongation (U r ) of the rotor is calculated as: U r = ∑ i = 0 i = n ΔU r Δt T R e f i Load i U r i − 1 × Δt i if the effect of reference temperature (T Ref ) and load on the rate of creep elongation (ΔU r / Δt ) of the rotor is judged to be different ,wherein the load of the gas turbine engine (Load i ) is included in the correlation. a. providing a correlation for a given cross section of the rotor among o a reference temperature (T Ref ) indicative of the temperature of the rotor, o a creep elongation ( U r ), o a rate of creep elongation ( ΔU r / Δt ) , o a reference temperature (T Ref ) indicative of the temperature of the rotor, o a creep elongation ( U r ), o a rate of creep elongation ( ΔU r / Δt ) , b. measuring the reference temperature (T Ref ) at a sampling moment i; c. calculating on the basis of the correlation the creep elongation (U ri ) of the rotor at the sampling moment i on the basis of the measured reference temperature (T Ref ) at the sampling moment i and the creep elongation at the sampling moment i-1;
An outsole formed of a polymer crosslinked product, wherein the polymer crosslinked product comprises a rubber and a thermoplastic resin; has a JIS A hardness, according JIS K 6253, of 90 or less and a tear strength, according JIS K 6252, of 392.266 N/cm or more; and has a relationship of the expression below between a storage modulus (E 23 ) at 23 °C and 10 Hz and a storage modulus (E 160 ) at 160 °C and 10 Hz: 4 ≤ E 23 / E 160 ≤ 35 and wherein a density, according JIS K 7112, of the polymer crosslinked product is 1.0 g/cm 3 or less. wherein the polymer crosslinked product comprises a rubber and a thermoplastic resin; has a JIS A hardness, according JIS K 6253, of 90 or less and a tear strength, according JIS K 6252, of 392.266 N/cm or more; and has a relationship of the expression below between a storage modulus (E 23 ) at 23 °C and 10 Hz and a storage modulus (E 160 ) at 160 °C and 10 Hz: 4 ≤ E 23 / E 160 ≤ 35 and wherein a density, according JIS K 7112, of the polymer crosslinked product is 1.0 g/cm 3 or less.
A process for oxidizing 5-hydroxymethyl-2-furancarboxylic acid (HMFCA) to 5-formyl-2-furoic acid (FFA), the process comprising the step of incubating a cell in the presence of HMFCA, preferably under conditions conducive to the oxidation of HMFCA by the cell, wherein the cell comprises an expression construct for expression of a nucleotide sequence encoding an HMFCA dehydrogenase having an amino acid sequence with at least 45% identity with any one of the amino acid sequence of SEQ ID NO: 1 to 11, and wherein, the expression construct is expressible in the cell and expression of the dehydrogenase confers to or increases in the cell the ability to oxidize HMFCA to FFA, as compared to a corresponding wild type cell lacking the expression construct.
A lubricating oil composition comprising: a) major amount of a base oil; and b) minor amount of a synergistic friction modifier composition comprising: i) a molybdenum containing compound; and ii) a tertiary amine-containing compound having the following structure: wherein each R 1 and R 5 is independently a linear or branched-chain monovalent hydrocarbyl group having one to about twenty carbon atoms, wherein each R 2 , R 3 , and R 4 is independently a hydrogen, a linear or branched-chain monovalent hydrocarbyl group having one to about twenty carbon atoms, each m is independently from 0 to 4, each p is independently from 0 to 4, for each cyclic moiety m + p is from 2 to 4, and each n is independently from 1 to 6. a) major amount of a base oil; and b) minor amount of a synergistic friction modifier composition comprising: i) a molybdenum containing compound; and ii) a tertiary amine-containing compound having the following structure: i) a molybdenum containing compound; and ii) a tertiary amine-containing compound having the following structure:
A vehicle occupant (P) protection device , comprising: a seat belt device having a variable force limiter mechanism that is capable of changing a force limiter load that an occupant (P) who is sitting on a vehicle seat receives from a seat belt at a time of a frontal collision of a vehicle; an airbag device that is configured to deploy an airbag in front of the occupant at the time of the frontal collision; a seating position detection unit that is configured to detect a seating position of the occupant; and the vehicle occupant (P) protection device being characterized in that it comprises a control unit that is configured to reduce the force limiter load if, compared to a case in which the occupant (P) is positioned within a standard seating region, the seating position of the occupant (P) detected by the seating position detection unit is further toward a vehicle rear than the standard seating region and is within an airbag protection region in which the occupant (P) is protected by the airbag , wherein: the vehicle is an autonomous driving vehicle that is capable of switching between automatic driving and manual driving; the occupant (P) is a driver of the autonomous driving vehicle ; and the control unit is configured to detect the standard seating region based on the seating position of the occupant (P) during manual driving. a seat belt device having a variable force limiter mechanism that is capable of changing a force limiter load that an occupant (P) who is sitting on a vehicle seat receives from a seat belt at a time of a frontal collision of a vehicle; an airbag device that is configured to deploy an airbag in front of the occupant at the time of the frontal collision; a seating position detection unit that is configured to detect a seating position of the occupant; and the vehicle occupant (P) protection device being characterized in that it comprises the vehicle is an autonomous driving vehicle that is capable of switching between automatic driving and manual driving; the occupant (P) is a driver of the autonomous driving vehicle ; and the control unit is configured to detect the standard seating region based on the seating position of the occupant (P) during manual driving.
An aircraft thrust and control system for an aircraft comprising a roll axis (x), a yaw axis (y) and a pitch axis (x), the aircraft thrust and control system comprising a central power unit which is open-type or housed in an aerodynamic duct , the central power unit comprising an upper propeller (5.1) and a lower propeller (5.2) arranged one above the other and adapted to rotate in opposite directions, and open-type peripheral power units each comprising an upper propeller (6.1) or an upper propeller (6.1) and a lower propeller (6.2), the peripheral power units being located outside an aerodynamic operating range of the upper and lower propellers (5.1, 5.2) of the central power unit , whereby the central power unit is adapted only for generating a lifting force of the aircraft with respect to F the yaw axis (y), whereby the peripheral power units are adapted for control of a direction of movement of the aircraft with respect to the roll (x), yaw (y) and pitch (x) axes by varying rotational speeds of the upper and lower propellers (6.1, 6.2), whereby the central power unit is not involved at all in controlling the direction of movement of the aircraft, whereby the upper propeller (5.1) of the central power unit operates in a t<w same plane as each upper propeller (6.1) of the peripheral power units when the peripheral power units are equipped only with the upper propellers (6.1), and whereby the upper propeller (5.1) of the central power unit operates in the same plane as each upper propeller (6.1) of the peripheral power units and the lower propeller (5.2) of the central power unit operates in a same plane as each lower propeller (6.2) of the peripheral power units when the peripheral power units are equipped with upper propellers (6.1) and lower propellers (6.2). whereby the central power unit is adapted only for generating a lifting force of the aircraft with respect to F the yaw axis (y), whereby the peripheral power units are adapted for control of a direction of movement of the aircraft with respect to the roll (x), yaw (y) and pitch (x) axes by varying rotational speeds of the upper and lower propellers (6.1, 6.2), whereby the central power unit is not involved at all in controlling the direction of movement of the aircraft, whereby the upper propeller (5.1) of the central power unit operates in a t<w same plane as each upper propeller (6.1) of the peripheral power units when the peripheral power units are equipped only with the upper propellers (6.1), and whereby the upper propeller (5.1) of the central power unit operates in the same plane as each upper propeller (6.1) of the peripheral power units and the lower propeller (5.2) of the central power unit operates in a same plane as each lower propeller (6.2) of the peripheral power units when the peripheral power units are equipped with upper propellers (6.1) and lower propellers (6.2).
Method for monitoring a heating system, in which method a monitoring value of the heating system, which monitoring value represents a degree of use of the system or on which the degree of use of the system is dependent or which is dependent on the degree of use of the system, is repeatedly calculated each time a first time interval elapses, characterized in that the calculation takes place on the basis of a variable-time model depending on an average utilization of the heating system, wherein the model describes the dependency between the utilization of the heating system and the standardized primary energy expended, and wherein the model is formed or modified, before the calculation of the monitoring value in each case after a second interval has elapsed, depending on heating system parameters which were previously recorded by measurement in the second time interval, and the monitoring value is compared with a comparison value, in particular a stored limit value, wherein an indication of the modification is carried out in the event of a modification of the calculated monitoring value beyond the comparison value.
A compound for use in the treatment of a rearranged during transfection (RET) altered cancer in a subject in need thereof, comprising administering to the subject 300 mg or 400 mg of Compound 1 or a pharmaceutically acceptable salt thereof once daily, wherein Compound 1 is: wherein the RET alteration comprises a RET mutation or a RET fusion, and wherein the RET altered cancer is selected from non-small cell lung cancer (NSCLC) and thyroid cancer.