mhurhangee/patent-ind-claim-en huggingface dataset:
An antiskid brake control system, comprising: a brake control unit, BCU ; a wheel/brake assembly comprising a wheel , a brake stack , and an actuator configured to apply a braking force onto the brake stack; and a wheel speed sensor in electronic communication with the BCU, the wheel speed sensor configured to detect a wheel speed corresponding to the wheel; wherein the BCU is configured to: receive an aircraft mass from an avionics unit; calculate an aircraft kinetic energy; generate an antiskid brake command signal based upon the aircraft kinetic energy; and send the antiskid brake command signal to a brake control component for controlling the braking force; and characterised in that the BCU is further configured to calculate an aircraft speed based upon the wheel speed, and the BCU calculates the aircraft kinetic energy using the aircraft speed and the aircraft mass, and wherein the BCU is further configured to adjust an antiskid parameter based upon the aircraft kinetic energy. a brake control unit, BCU ; a wheel/brake assembly comprising a wheel , a brake stack , and an actuator configured to apply a braking force onto the brake stack; and a wheel speed sensor in electronic communication with the BCU, the wheel speed sensor configured to detect a wheel speed corresponding to the wheel; wherein the BCU is configured to: receive an aircraft mass from an avionics unit; calculate an aircraft kinetic energy; generate an antiskid brake command signal based upon the aircraft kinetic energy; and send the antiskid brake command signal to a brake control component for controlling the braking force; and receive an aircraft mass from an avionics unit; calculate an aircraft kinetic energy; generate an antiskid brake command signal based upon the aircraft kinetic energy; and send the antiskid brake command signal to a brake control component for controlling the braking force; and characterised in that the BCU is further configured to calculate an aircraft speed based upon the wheel speed, and the BCU calculates the aircraft kinetic energy using the aircraft speed and the aircraft mass, and wherein the BCU is further configured to adjust an antiskid parameter based upon the aircraft kinetic energy.
An engine bleed control system for a gas turbine engine of an aircraft when installed and in use, the engine bleed control system comprising: an engine bleed tap coupled to a fan-air source or a compressor source of a lower pressure compressor section before a highest pressure compressor section of the gas turbine engine; a turbo-compressor in fluid communication with the engine bleed tap; and a valve for selectively driving the turbo-compressor; a controller configured to selectively drive the turbo-compressor by controlling the valve to boost a bleed air pressure from the engine bleed tap as pressure augmented bleed air and control delivery of the pressure augmented bleed air to an aircraft use , wherein the turbo-compressor is selectively driven by a high pressure compressor bleed air source and an exhaust flow of the turbo-compressor is provided to one or more of: a manifold to combine with the pressure augmented bleed air; a thrust recovery source of the gas turbine engine; and a thrust recovery source of the turbo-compressor; a pneumatic bleed being at a different engine stage than the engine bleed tap; and characterized in that the pneumatic bleed is for anti-icing at least a nacelle inlet of the gas turbine engine and in that the system further comprises a valve configured to be selectively activated by the controller to enable the anti-icing of at least the nacelle inlet of the gas turbine engine. an engine bleed tap coupled to a fan-air source or a compressor source of a lower pressure compressor section before a highest pressure compressor section of the gas turbine engine; a turbo-compressor in fluid communication with the engine bleed tap; and a valve for selectively driving the turbo-compressor; a controller configured to selectively drive the turbo-compressor by controlling the valve to boost a bleed air pressure from the engine bleed tap as pressure augmented bleed air and control delivery of the pressure augmented bleed air to an aircraft use , wherein the turbo-compressor is selectively driven by a high pressure compressor bleed air source and an exhaust flow of the turbo-compressor is provided to one or more of: a manifold to combine with the pressure augmented bleed air; a thrust recovery source of the gas turbine engine; and a thrust recovery source of the turbo-compressor; a pneumatic bleed being at a different engine stage than the engine bleed tap; and characterized in that the pneumatic bleed is for anti-icing at least a nacelle inlet of the gas turbine engine and in that the system further comprises a valve configured to be selectively activated by the controller to enable the anti-icing of at least the nacelle inlet of the gas turbine engine.
A stemless cup , having a first end and a second end , the stemless cup comprising an interior recess extending from the first end toward the second end and an exterior backside extending from the second end toward the first end, characterized in that the stemless cup further includes an upper interior surface with a recess extending into the stemless cup, wherein the recess is configured to receive a snap ring and an articulating liner so that a portion of the snap ring is fit into the recess and a portion of the snap ring is inserted into a groove of the articulating liner to securely hold the articulating liner to the stemless cup, and wherein the exterior backside is configured or sized and shaped to be received within the head of the humerus and has at least one fin, rib, or projection , which extends away from a base portion of the stemless cup and which is configured or sized and shaped to provide rotational control under a torsional load. having a first end and a second end , the stemless cup comprising an interior recess extending from the first end toward the second end and an exterior backside extending from the second end toward the first end, characterized in that the stemless cup further includes an upper interior surface with a recess extending into the stemless cup, wherein the recess is configured to receive a snap ring and an articulating liner so that a portion of the snap ring is fit into the recess and a portion of the snap ring is inserted into a groove of the articulating liner to securely hold the articulating liner to the stemless cup, and wherein the exterior backside is configured or sized and shaped to be received within the head of the humerus and has at least one fin, rib, or projection , which extends away from a base portion of the stemless cup and which is configured or sized and shaped to provide rotational control under a torsional load.
A shear web mould assembly for making a shear web for a wind turbine blade, the mould assembly comprising: an elongate male mould tool having a longitudinally-extending upper mould surface and a longitudinally-extending first side wall ; a longitudinally-extending detachable shim (40a-f) having an attachment portion for attaching to the first side wall of the mould tool and a shaping portion for supporting a flange structure of the shear web, wherein the attachment portion of the shim (40a-f) is attached to the first side wall of the mould tool by means of one or more fixing devices , and the shaping portion of the shim (40a-f) has an upper surface that forms an extension of the upper mould surface of the mould tool , wherein the one or more fixing devices include a longitudinally extending brace configured to bear against the outer surface of the shim (40a-f) and configured to releasably clamp the shim (40a-f) to the first side wall , and wherein said one or more fixing devices further include a plurality of fasteners which extend respectively through a plurality of holes provided in the shim (40a-f), wherein said brace is provided with a plurality of holes through which the plurality of fasteners may extend before extending through the holes in said shims (40a-f). an elongate male mould tool having a longitudinally-extending upper mould surface and a longitudinally-extending first side wall ; a longitudinally-extending detachable shim (40a-f) having an attachment portion for attaching to the first side wall of the mould tool and a shaping portion for supporting a flange structure of the shear web, wherein the attachment portion of the shim (40a-f) is attached to the first side wall of the mould tool by means of one or more fixing devices , and the shaping portion of the shim (40a-f) has an upper surface that forms an extension of the upper mould surface of the mould tool , wherein the one or more fixing devices include a longitudinally extending brace configured to bear against the outer surface of the shim (40a-f) and configured to releasably clamp the shim (40a-f) to the first side wall , and wherein said one or more fixing devices further include a plurality of fasteners which extend respectively through a plurality of holes provided in the shim (40a-f), wherein said brace is provided with a plurality of holes through which the plurality of fasteners may extend before extending through the holes in said shims (40a-f).
A grip device for the support and movement of preforms which extends along a longitudinal axis and is of the type provided with an access port which forms, at a rim , an annular radial flaring which lies on a surface of arrangement that is substantially perpendicular to said longitudinal axis , characterized in that it comprises a supporting element which is operatively associated with an air supply conduit and is connected to at least one air exit nozzle which is adapted to generate at least one respective air flow which is designed to arrange itself parallel to at least one portion of the radial flaring of a preform to be held in order to enable said preform to be supported without contact.
An ELA polypeptide or a nucleic acid encoding thereof comprising an amino acid sequence having at least 90% identity with SEQ ID NO: 1 (QRPVNLTMRRKLRKHNCLQRRCMPLHSRVPFP) wherein the arginine residue (R) at position 9, 10, 20 or 21 is substituted by an Alanine residue (A) and/or by a Serine residue (S) for use in the treatment of a kidney cancer.
A pharmaceutical composition comprising multiple dosage forms each comprising a core and an enteric coating, wherein the core comprises at least one nutrient compound selected from the group consisting of carbohydrates, fatty acids, bile acids, peptides, amino acids, alcohol amides, and anthocyanins, wherein the size of the dosage forms, with respect to the largest dimension of the dosage forms, is below 3 mm providing for entry of the dosage forms into the intestine of a subject independent of gastric emptying mechanisms, wherein the enteric coating comprises a pH sensitive polymer which substantially degrades and/or dissolves at a pH value being selected such that the coating substantially dissolves and/or is substantially degraded in the terminal jejunum of a subject such that the core is released into the terminal jejunum of the subject, and wherein the composition further comprises a gelling composition containing one or more gelling agents, and wherein the multiple dosage forms and the gelling composition form a heterogenous mixture.
A process for isomerizing a feed mixture comprising xylenes, the process comprising contacting the feed mixture in an isomerization zone with a catalyst at isomerization conditions, wherein a pervaporation process is carried out within the isomerization zone located within a catalytic membrane reactor, wherein the isomerization zone is operated at a temperature in the range of 20°C to 200°C, and producing an isomerized product comprising a higher proportion of p -xylene than in the feed mixture, wherein the catalyst comprises Nafion-H.
Waste end stretching device for a weaving machine comprising a suction nozzle adapted to be arranged in the path of a waste end of an inserted weft thread projecting beyond an edge of a woven fabric , wherein the suction nozzle is adapted for applying a suction force along a longitudinal direction of the suction nozzle , wherein the suction nozzle is adapted for being attached to the weaving machine such that the longitudinal direction of the suction nozzle extends in parallel to the weft insertion direction , characterized in that the suction nozzle is provided with a lateral suction slit extending along the longitudinal direction of the suction nozzle for sucking waste ends into the suction nozzle and with an opening provided at a first end of the suction nozzle facing the edge of the woven fabric for conveying waste ends held in the suction nozzle in a direction perpendicular to the longitudinal direction of the suction nozzle , and wherein a deflecting element is provided between the opening and the edge of the woven fabric , which deflecting element at least partly projects beyond the opening for deflecting waste ends held in the suction nozzle in their path between the edge of the woven fabric and the opening .
Hairdressing tool comprising a first mouthpiece , wherein the first mouthpiece comprises a mouthpiece body with a suction inlet , a suction outlet , and a suction duct extending between the suction inlet and the suction outlet , wherein the suction outlet is connectable to a suction unit , wherein the suction inlet is arranged for sucking in a section of hair from the human head into the suction duct and wherein the suction duct is arranged for retaining said section of hair along a retaining path (P) inside the suction duct , wherein the mouthpiece body is continuous between the suction inlet and the suction outlet such that the suction duct is open only at the suction inlet and the suction outlet , wherein the suction inlet comprises an inlet opening with an inlet width (W) and an inlet height (H), characterized in that the ratio between the inlet width (W) and the inlet height (H) is at least 10:1, wherein the suction duct defines a laminar flow area extending from the suction inlet towards the suction outlet along the retaining path (P), wherein the suction duct at the laminar flow area has a cross section perpendicular to the retaining path (P) that is constant or substantially constant in the laminar flow area so as to generate a laminar or a substantially laminar flow of air along said retaining path (P).
A mouthwash whitening composition, comprising an orally acceptable vehicle, sodium carbonate, a source of hydrogen peroxide that provides hydrogen peroxide, and a cyclic anhydride that generates a peracid with the hydrogen peroxide provided by the source of hydrogen peroxide wherein the molar ratio of the cyclic anhydride to the hydrogen peroxide provided by the source of hydrogen peroxide is from 0.8:1 to 1.3:1; wherein the orally acceptable vehicle further comprises one or more ingredient selected from antibacterial agents, anticalculus agents, humectants, surfactants and cooling agents, and wherein the cyclic anhydride is not a polymer-based cyclic anhydride. wherein the molar ratio of the cyclic anhydride to the hydrogen peroxide provided by the source of hydrogen peroxide is from 0.8:1 to 1.3:1; wherein the orally acceptable vehicle further comprises one or more ingredient selected from antibacterial agents, anticalculus agents, humectants, surfactants and cooling agents, and
Evaluation circuit for a capacitive sensor for recording the distance, the speed or the position of an object, having a reference capacitance and two measuring capacitances , wherein the reference capacitance and the measuring capacitances have a respective square-wave voltage (Takt0-Takt2) applied thereto via a respective resistor (Rref, Rel1, Rel2) and a variable-duration pulse is obtained using a first switching stage and further switching stages , which variable-duration pulse constitutes a measure of the respective measuring capacitance , the reference capacitance is connected to the input of the first switching stage , wherein each measuring capacitance is connected to the input of a respective further switching stage , wherein the further switching stages have enable inputs that are controlled by the output of the first switching stage , wherein the outputs of the further switching stages are connected in each case to inputs of integration stages , wherein a charging capacitor is charged via the outputs of the integration stages , wherein the switching stages (41-43) have threshold voltages and, when the threshold voltage of the first switching stage is reached, a start signal for starting the charging process of the charging capacitor is generated and, when the threshold voltage of a further switching stage is reached, a stop signal for stopping the charging process of the charging capacitor is generated.
A cutter assembly for an undercutting machine for cutting a rock workface comprising: a shaft supporting structure ; a shaft at least partly arranged within the shaft supporting structure ; a cutter device arranged on the shaft or the shaft supporting structure ; and a first rolling element arranged between the shaft supporting structure and the shaft in floating or slidable manner in axial direction; a second rolling element arranged between the shaft supporting structure and the shaft , characterised by a virtual line orthogonal to an outer surface of a second roller of the second rolling element crosses the longitudinal axis (X) of the shaft at a centre plane of the first rolling element or within a range of +/-25% of an axial extension of the first rolling element from said centre plane , wherein the line passes through the second roller , and wherein the cutter device is detachably but rotationally rigid mounted on said shaft, and the shaft supporting structure is fixed. a shaft supporting structure ; a shaft at least partly arranged within the shaft supporting structure ; a cutter device arranged on the shaft or the shaft supporting structure ; and a first rolling element arranged between the shaft supporting structure and the shaft in floating or slidable manner in axial direction; a second rolling element arranged between the shaft supporting structure and the shaft , characterised by a virtual line orthogonal to an outer surface of a second roller of the second rolling element crosses the longitudinal axis (X) of the shaft at a centre plane of the first rolling element or within a range of +/-25% of an axial extension of the first rolling element from said centre plane , wherein the line passes through the second roller , and wherein the cutter device is detachably but rotationally rigid mounted on said shaft, and the shaft supporting structure is fixed.
A combine harvester with a chassis , a front axle and with a rear axle as well as steerable support wheels disposed behind the rear axle to relieve the load on the rear axle when travelling on roads, wherein the support wheels are disposed so as to be capable of dropping from a raised rest position into a travelling position, characterized in that the support wheels are individually pivoted by means of a respective swing arm on a common subframe and are self-steering, wherein the subframe is mounted on the chassis .
Shaping press comprising a lower tool , which is supported at a lower beam , and an upper tool, which is supported at an upper beam , in the form of a bending rail elongate in the direction of a longitudinal axis of the shaping press, wherein the bending rail is mounted to be pivotable about the longitudinal axis, characterised in that by means of a support element a settable variable support force opposing the pivotation is exerted on the bending rail so that a guide is provided which can be switched as required to be firm or soft so as to allow a behaviour of the bending rail which is optimised with respect to different reshaping processes.
Method for determining a channel load in vehicle-to-X communication, comprising the following steps: - receiving a number of vehicle-to-X messages , - determining a plurality of channel load parameters on the basis of the vehicle-to-X messages , and - determining the channel load on the basis of at least the channel load parameters; - wherein an increased channel load is determined in the step of determining the channel load if more than half of all channel load parameters taken into account in the step of determining the channel load indicate an increased channel load; - wherein a channel load parameter of the plurality of channel load parameters is determined using the following steps: - storing each received vehicle-to-X message in a buffer memory , wherein applications each cyclically read vehicle-to-X messages from the buffer memory , and - determining the channel load parameter on the basis of the number of vehicle-to-X messages stored in the buffer memory. - receiving a number of vehicle-to-X messages , - determining a plurality of channel load parameters on the basis of the vehicle-to-X messages , and - determining the channel load on the basis of at least the channel load parameters; - wherein an increased channel load is determined in the step of determining the channel load if more than half of all channel load parameters taken into account in the step of determining the channel load indicate an increased channel load; - wherein a channel load parameter of the plurality of channel load parameters is determined using the following steps: - storing each received vehicle-to-X message in a buffer memory , wherein applications each cyclically read vehicle-to-X messages from the buffer memory , and - determining the channel load parameter on the basis of the number of vehicle-to-X messages stored in the buffer memory.
Parking platform for a motor vehicle, in particular for a motorized parking apparatus for a motor vehicle, which parking platform (10; 80; 90) comprises profile parts (32; 92) which are arranged next to each other along a longitudinal direction and preferably are connected to each other and form a parking space for the motor vehicle, wherein profile parts (32; 92) are provided which each comprise a base region and a projecting region projecting therefrom, wherein the profile parts (32; 92) each comprise a profile section which has at least one base region and at least one projecting region , as well as a covering section which is arranged in the longitudinal direction next to the profile section and is connected thereto, wherein the covering section of a profile part (32; 92) covers at least one projection region of an adjacent profile part (32; 92), and wherein the covering section rests on at least one projection region of the profile section of the adjacent profile part (32; 92).