mhurhangee/patent-ind-claim-en huggingface dataset:
An ice machine, comprising at least: - a refrigerating unit including an evaporator designed for making ice elements and for conveying them to a container , - a hydraulic circuit designed for supplying water to said evaporator and including at least one water storage basin and a loading pipe extending between said basin and said evaporator , - and an electrically powered management system for said machine, - at least one drainage conduit designed for draining liquid water from said hydraulic circuit and from said evaporator , - at least one drainage valve designed for opening and closing said drainage conduit on command, and characterised in that it further comprises - control means configured for repeating a timed opening of said drainage valve at least each time said machine's operation is interrupted. - a refrigerating unit including an evaporator designed for making ice elements and for conveying them to a container , - a hydraulic circuit designed for supplying water to said evaporator and including at least one water storage basin and a loading pipe extending between said basin and said evaporator , - and an electrically powered management system for said machine, - at least one drainage conduit designed for draining liquid water from said hydraulic circuit and from said evaporator , - at least one drainage valve designed for opening and closing said drainage conduit on command, and characterised in that it further comprises - control means configured for repeating a timed opening of said drainage valve at least each time said machine's operation is interrupted.
A method of determining a temperature of a rotor (RT) of an electric induction machine comprising the steps of: - determining a set of temperature-independent comparative stator flux saturation saliency angles (CSA) in a reference frame, - determining an actual stator flux saturation saliency angle (ASA) in the reference coordinate frame depending on a machine model (MM) comprising at least one rotor temperature-dependent parameter, - determining a temperature-independent comparative stator flux saturation saliency angle (CSA), - determining a deviation between the actual stator flux saturation saliency angle (ASA) and the temperature-independent comparative stator flux saturation saliency angle (CSA), - determining the rotor temperature (RT) as the temperature which minimizes said deviation. - determining a set of temperature-independent comparative stator flux saturation saliency angles (CSA) in a reference frame, - determining an actual stator flux saturation saliency angle (ASA) in the reference coordinate frame depending on a machine model (MM) comprising at least one rotor temperature-dependent parameter, - determining a temperature-independent comparative stator flux saturation saliency angle (CSA), - determining a deviation between the actual stator flux saturation saliency angle (ASA) and the temperature-independent comparative stator flux saturation saliency angle (CSA), - determining the rotor temperature (RT) as the temperature which minimizes said deviation.
Crystalline methyl { -1-[ -2-(9-{2-[ -1-{ -2-[(methoxycarbonyl)amino]-2-phenylacetyl}-4-(methoxymethyl)pyrrolidin-2-yl]-1 H-imidazol-5-yl}-1,11-dihydroisochromeno[4',3':6,7]naphtho[1,2-d]imidazol-2-yl)-5-methylpyrrolidin-1-yl]-3-methyl-1-oxobutan-2-yl}carbamate phosphate (Compound I Phosphate Form XII) characterized by an X-ray powder diffractogram comprising the following peaks: 3.8, 7.5, and 16.9 °2θ ± 0.2 °2θ, as determined on a diffractometer using Cu-Kα radiation at a wavelength of 1.5406 Å.
An imaging array including rows and columns of vertical detector color pixel sensors, each vertical detector color pixel sensor (86, 88, 90 ... 96) disposed in a row and column (C0, C1, C2 ... C5) of the array and having individual color detectors (86r, 86g, 86b; 88r, 88g, 88b; etc.) for a number of colors, and a readout wiring architecture, the readout wiring architecture comprising: a plurality of row-select lines for each row of the array, the number of row-select lines equal to the number of colors in the vertical detector color pixel sensors in the array; an individual column line (118, 120, 122 ... 128) for each column of the array; a transfer transistor (86tg, 86tb, 88tr, 88tg, 88tb, etc.) for each individual color detector in each vertical detector color pixel sensor in the array, each transfer transistor coupled between a color detector in a column of the array and a column line of the array, each transfer transistor having a gate coupled to one of the plurality of row-select lines in a row of the array in which the vertical detector color pixel sensor is disposed; wherein the transfer transistors for each color detector in a vertical detector color pixel sensor (88,90,92, etc.) in a column (C1, C2, C3, etc.) of the array are coupled to a different one of the column line (118, 120, 122 etc.) immediately preceding the column line in which the vertical detector color pixel sensor is disposed, the column line (120,122,124, etc.) in which the vertical detector color pixel sensor is disposed, and the column line (122, 124, 126, etc.) immediately following the column line in which the vertical detector color pixel sensor is disposed. a plurality of row-select lines for each row of the array, the number of row-select lines equal to the number of colors in the vertical detector color pixel sensors in the array; an individual column line (118, 120, 122 ... 128) for each column of the array; a transfer transistor (86tg, 86tb, 88tr, 88tg, 88tb, etc.) for each individual color detector in each vertical detector color pixel sensor in the array, each transfer transistor coupled between a color detector in a column of the array and a column line of the array, each transfer transistor having a gate coupled to one of the plurality of row-select lines in a row of the array in which the vertical detector color pixel sensor is disposed; wherein the transfer transistors for each color detector in a vertical detector color pixel sensor (88,90,92, etc.) in a column (C1, C2, C3, etc.) of the array are coupled to a different one of the column line (118, 120, 122 etc.) immediately preceding the column line in which the vertical detector color pixel sensor is disposed, the column line (120,122,124, etc.) in which the vertical detector color pixel sensor is disposed, and the column line (122, 124, 126, etc.) immediately following the column line in which the vertical detector color pixel sensor is disposed.
A method for inserting an electronic module in a structure , comprising: sliding at least one glide mechanism on a rail of the structure as the electronic module is being pushed into the structure , the at least one glide mechanism integrated with the electronic module and resiliently biased in a direction away from the electronic module to partially extend out from the electronic module in a direction towards the rail ; actuating a coupler to secure the electronic module to the rail and sandwich a thermal interface material between the electronic module and the rail ; and causing the at least one glide mechanism to be retracted into the electronic module while the coupler is being actuated; wherein the thermal interface material first comes in contact with the rail while the coupler is being actuated, and the thermal interface material is coupled to the electronic module and the at least one glide mechanism extends through the thermal interface material during the sliding. sliding at least one glide mechanism on a rail of the structure as the electronic module is being pushed into the structure , the at least one glide mechanism integrated with the electronic module and resiliently biased in a direction away from the electronic module to partially extend out from the electronic module in a direction towards the rail ; actuating a coupler to secure the electronic module to the rail and sandwich a thermal interface material between the electronic module and the rail ; and causing the at least one glide mechanism to be retracted into the electronic module while the coupler is being actuated; wherein the thermal interface material first comes in contact with the rail while the coupler is being actuated, and the thermal interface material is coupled to the electronic module and the at least one glide mechanism extends through the thermal interface material during the sliding.
Attenuation device for a fluid flow pulsation along a duct of a hydraulic circuit connected with a hydraulic machine, comprising a pressurized fluid and at least an attenuation module passed through by a pass-through duct configured to be placed in fluid communication with said duct of said hydraulic circuit, wherein in said attenuation module a first duct is obtained having an opened first end in fluid communication with said pass-through duct , and a closed second end, said first duct extending between said opened first end and said closed second end along a curved line comprising a plurality of curved sections, wherein at least two curved sections of said first duct are separated from one another by a shared separation wall , characterized in that the thickness (s) of the shared separation wall is configured to make the shared separation wall compliant towards a pressure difference between a first section and a second section of said at least two curved sections separated by said shared separation wall , wherein the thickness (s) of said wall is selected as a function of the ratio between the change in volume of the fluid caused by the pressure difference on the fluid and the change in volume defined by the deformation of said wall carried out by said pressure difference on the fluid to keep the volume change due to the compressibility of the fluid and the volume change due to the deformation of said separation wall of substantially comparable size, said first duct being adapted to attenuate the pulsation of said fluid flow along said duct of said hydraulic circuit to reduce the vibrations generated by said pulsation of said fluid flow.
A method for identifying a position of a receiver, the method comprising: receiving a plurality of first radio frequency signals including navigation information at the receiver , wherein the plurality of first radio frequency signals is sent from a plurality of platforms configured to receive second radio frequency signals with the navigation information from a plurality of satellites in a global positioning system ; and identifying the position of the receiver using a number of distances and a number of angles measured from the plurality of first radio frequency signals and a number of positions for the plurality of platforms , wherein a platform in the plurality of platforms is selected from one of an aircraft, a jet airplane, a helicopter, an unmanned aerial vehicle, a passenger aircraft, a cargo aircraft, a satellite, a space vehicle, a submarine, a personnel carrier and a surface ship, wherein a position of the platform in the plurality of platforms is identified using the navigation information in a radio frequency signal of the plurality of first radio frequency signals received from the platform . receiving a plurality of first radio frequency signals including navigation information at the receiver , wherein the plurality of first radio frequency signals is sent from a plurality of platforms configured to receive second radio frequency signals with the navigation information from a plurality of satellites in a global positioning system ; and identifying the position of the receiver using a number of distances and a number of angles measured from the plurality of first radio frequency signals and a number of positions for the plurality of platforms , wherein a platform in the plurality of platforms is selected from one of an aircraft, a jet airplane, a helicopter, an unmanned aerial vehicle, a passenger aircraft, a cargo aircraft, a satellite, a space vehicle, a submarine, a personnel carrier and a surface ship, wherein a position of the platform in the plurality of platforms is identified using the navigation information in a radio frequency signal of the plurality of first radio frequency signals received from the platform .
A method for correcting a result of a quantum computation, the method comprising: selecting , by one or more classical processors , a quantum error correcting code to perform the quantum computation, wherein the quantum error correcting code is defined by a respective set of stabilizer generators; determining , by the one or more classical processors, a set of symmetry operators, comprising: selecting a subset of the set of stabilizer generators, the subset comprising a plurality of stabilizer generators; determining, for each stabilizer generator in the selected subset, a sum between an identity operator and the stabilizer generator; and multiplying the determined sums together to form a summation of terms, wherein each term in the summation is equal to a respective symmetry operator; measuring , using quantum computing hardware , a projective correction of a physical observable over an output quantum state of the quantum computation using the determined set of symmetry operators, wherein the physical observable corresponds to the result of the quantum computation; and determining , by the one or more classical processors, a corrected result of the quantum computation using the measured projective correction of the physical observable. selecting , by one or more classical processors , a quantum error correcting code to perform the quantum computation, wherein the quantum error correcting code is defined by a respective set of stabilizer generators; determining , by the one or more classical processors, a set of symmetry operators, comprising: selecting a subset of the set of stabilizer generators, the subset comprising a plurality of stabilizer generators; determining, for each stabilizer generator in the selected subset, a sum between an identity operator and the stabilizer generator; and multiplying the determined sums together to form a summation of terms, wherein each term in the summation is equal to a respective symmetry operator; selecting a subset of the set of stabilizer generators, the subset comprising a plurality of stabilizer generators; determining, for each stabilizer generator in the selected subset, a sum between an identity operator and the stabilizer generator; and multiplying the determined sums together to form a summation of terms, wherein each term in the summation is equal to a respective symmetry operator; measuring , using quantum computing hardware , a projective correction of a physical observable over an output quantum state of the quantum computation using the determined set of symmetry operators, wherein the physical observable corresponds to the result of the quantum computation; and determining , by the one or more classical processors, a corrected result of the quantum computation using the measured projective correction of the physical observable.
A computer-implemented method for operating an autonomous driving vehicle, the method comprising: determining a first feedback parameter based on the difference between an actual speed and an expected speed of the autonomous driving vehicle in response to a speed control command issued based on a target speed; wherein the expected speed is determined using a vehicle-specific powertrain reference model associated with the design characteristics of the autonomous driving vehicle based on the target speed; determining a second feedback parameter by applying a speed control parameter adjustment model to a set of input parameters that are obtained in real-time, the set of input parameters representing a driving environment of the autonomous driving vehicle at a point in time; dynamically adjusting a control parameter of a speed controller that issued the speed control command based on the first feedback parameter and the second feedback parameter; and generating a subsequent speed control command based on the adjusted control parameter of the speed controller for a subsequent command cycle. determining a first feedback parameter based on the difference between an actual speed and an expected speed of the autonomous driving vehicle in response to a speed control command issued based on a target speed; wherein the expected speed is determined using a vehicle-specific powertrain reference model associated with the design characteristics of the autonomous driving vehicle based on the target speed; determining a second feedback parameter by applying a speed control parameter adjustment model to a set of input parameters that are obtained in real-time, the set of input parameters representing a driving environment of the autonomous driving vehicle at a point in time; dynamically adjusting a control parameter of a speed controller that issued the speed control command based on the first feedback parameter and the second feedback parameter; and generating a subsequent speed control command based on the adjusted control parameter of the speed controller for a subsequent command cycle.
A resin composition comprising: a bismaleimide compound (A) comprising a constituent unit represented by the following formula , and maleimide groups at both ends of the molecular chain; at least one resin or compound (B) selected from the group consisting of a cyanate compound, a benzoxazine compound, an epoxy resin, a carbodiimide compound, and a compound having more than one ethylenically unsaturated groups in a molecule; and a photo initiator (C): wherein R 1 represents a linear or branched alkylene group having 1 to 16 carbon atoms, or a linear or branched alkenylene group having 2 to 16 carbon atoms; R 2 represents a linear or branched alkylene group having 1 to 16 carbon atoms, or a linear or branched alkenylene group having 2 to 16 carbon atoms; each R 3 independently represents a hydrogen atom, a linear or branched alkyl group having 1 to 16 carbon atoms, or a linear or branched alkenyl group having 2 to 16 carbon atoms; and each n independently represents an integer of 1 to 10. a bismaleimide compound (A) comprising a constituent unit represented by the following formula , and maleimide groups at both ends of the molecular chain; at least one resin or compound (B) selected from the group consisting of a cyanate compound, a benzoxazine compound, an epoxy resin, a carbodiimide compound, and a compound having more than one ethylenically unsaturated groups in a molecule; and a photo initiator (C): wherein R 1 represents a linear or branched alkylene group having 1 to 16 carbon atoms, or a linear or branched alkenylene group having 2 to 16 carbon atoms; R 2 represents a linear or branched alkylene group having 1 to 16 carbon atoms, or a linear or branched alkenylene group having 2 to 16 carbon atoms; each R 3 independently represents a hydrogen atom, a linear or branched alkyl group having 1 to 16 carbon atoms, or a linear or branched alkenyl group having 2 to 16 carbon atoms; and each n independently represents an integer of 1 to 10.
An electronic watch, including: a metal device case having a removable metal back cover and a metallic watch case ; and an antenna disposed inside said metal device case ; characterized by a ring-shaped spacer member being arranged between said watch case and said metal back cover in order to produce a clearance between said metal watch case and said back cover ; a waterproof ring between the watch case and the back cover ; and a magnetic sheet between said antenna and an inner surface of said watch case , said magnetic sheet having a magnetic permeability higher than the magnetic permeability of said metal device case ; wherein said antenna has a rod-shaped core and a coil wound around said core ; and said magnetic sheet is a plate-like or film-like sheet arranged in parallel to an axial direction of said core . a metal device case having a removable metal back cover and a metallic watch case ; and an antenna disposed inside said metal device case ; characterized by a ring-shaped spacer member being arranged between said watch case and said metal back cover in order to produce a clearance between said metal watch case and said back cover ; a waterproof ring between the watch case and the back cover ; and a magnetic sheet between said antenna and an inner surface of said watch case , said magnetic sheet having a magnetic permeability higher than the magnetic permeability of said metal device case ; wherein said antenna has a rod-shaped core and a coil wound around said core ; and said magnetic sheet is a plate-like or film-like sheet arranged in parallel to an axial direction of said core .
A composition comprising a compound represented by the following formula (I), a salt thereof, or a prodrug thereof, for use in treating intractable leukemia by administering simultaneously, separately or sequentially with dexamethasone: wherein, Ar 1 is a substituted or unsubstituted arylene group; Ar 2 is a substituted or unsubstituted aryl group or a substituted or unsubstituted aralkyl group, and L is an oxygen atom, -NHCO-, or -CONH-; provided that a said prodrug is a compound in which a C 2-7 -acyl group, a C 1-6 -alkoxy(C 2-7 -acyl) group, a C 1-6 -alkoxycarbonyl(C 2-7 -acyl) group, a C 1-6 -alkoxycarbonyl group, a C 1-6 -alkoxy(C 2-7 -alkoxycarbonyl) group, a (C 2-7 -acyloxy)methyl group, a 1-(C 2-7 -acyloxy)ethyl group, a (C 2-7 -alkoxycarbonyl) oxymethyl group or a 1-[(C 2-7 -alkoxycarbonyl)oxy]ethyl group is substituted for a hydroxyl or amino group of a compound of formula (I), or in which a C 1-6 -alkyl group, a C 1-6 -alkoxy-C 1-6 -alkyl group, a (C 2-7 -acyloxy)methyl group, a 1-(C 2-7 -acyloxy)ethyl group, a (C 2-7 -alkoxycarbonyl)oxymethyl group or a 1-[(C 2-7 -alkoxycarbonyl)oxy]ethyl group is substituted for a carboxyl group of a compound of formula (I). Ar 1 is a substituted or unsubstituted arylene group; Ar 2 is a substituted or unsubstituted aryl group or a substituted or unsubstituted aralkyl group, and L is an oxygen atom, -NHCO-, or -CONH-; provided that a said prodrug is a compound in which a C 2-7 -acyl group, a C 1-6 -alkoxy(C 2-7 -acyl) group, a C 1-6 -alkoxycarbonyl(C 2-7 -acyl) group, a C 1-6 -alkoxycarbonyl group, a C 1-6 -alkoxy(C 2-7 -alkoxycarbonyl) group, a (C 2-7 -acyloxy)methyl group, a 1-(C 2-7 -acyloxy)ethyl group, a (C 2-7 -alkoxycarbonyl) oxymethyl group or a 1-[(C 2-7 -alkoxycarbonyl)oxy]ethyl group is substituted for a hydroxyl or amino group of a compound of formula (I), or in which a C 1-6 -alkyl group, a C 1-6 -alkoxy-C 1-6 -alkyl group, a (C 2-7 -acyloxy)methyl group, a 1-(C 2-7 -acyloxy)ethyl group, a (C 2-7 -alkoxycarbonyl)oxymethyl group or a 1-[(C 2-7 -alkoxycarbonyl)oxy]ethyl group is substituted for a carboxyl group of a compound of formula (I).