mhurhangee/ep-ind-claims huggingface dataset:
Drive apparatus with a first drive unit embodied as an internal combustion engine, a second drive unit embodied as an electrical engine and a transmission via which the first drive unit and/or the second drive unit are coupled or can be coupled to an output shaft of the drive apparatus, wherein the first drive unit and the second drive unit are temporarily connected to a common cooling circuit running through both drive units (5, 6) for temperature control, wherein the transmission has a transmission heat exchanger for temperature control, which is or can be fluidically connected to the cooling circuit via a circulation line, characterised in that a circulation line on both sides of the second drive unit opens into a line of the cooling circuit and is fluidically interrupted in a first switching state of a switching valve and released in a second switching state, so that in the first switching state of the switching valve the cooling circuit running through the first drive unit and the second drive unit, but not through the transmission heat exchanger, is formed and when the second drive unit is operated the resulting heat is fed to the first drive unit, and in the second switching state of the switching valve the heat exchange circuit is formed, in which the second drive unit and the transmission heat exchanger, but not the first drive unit, are present and the heat generated during operation of the second drive unit is used to control the temperature of the transmission.
Drill body for chip removing machining, comprising a rotationally symmetrical envelope surface and front and rear ends (1, 2) between which a centre axis extends around which the drill body is rotatable in a predetermined direction of rotation; a head formed in the front end that includes two cutting edges, each one of which comprises a first part edge and a second part edge, the first part edge being included in a central tip part having a front end portion situated along the centre axis, the second part edge extending between a peripheral end point positioned along the envelope surface and a radially inner end point where the second part edge transforms into the first part edge, the two first part edges converging at a positive nose angle (α) in an axially forward direction, and the two second part edges diverging at a negative angle (β) in the axially forward direction; and two internal fluid ducts for feeding cooling fluid to each one of the cutting edges; each cutting edge being delimited between a chip surface adjacent to a chip flute countersunk in the envelope surface, and a primary clearance surface that transforms into a secondary clearance surface situated rotationally behind the primary clearance surface; and each primary clearance surface including two part surfaces (13a, 13b), which mutually form an obtuse angle (χ), and which meet each other in a first chute bottom that runs rotationally rearward from the inner end point of the second part edge, characterized in that the same includes a second chute bottom, which extends in the extension of the first chute bottom and separates two second part surfaces (15a, 15b) included in the secondary clearance surface, the individual fluid duct mouthing in said second chute bottom.
System made up of battery units each of which comprises one or more basic cells coupled in series, wherein: 1.1. each battery unit has the shape of a right parallelepiped with an upper surface forming a terminal area comprising two terminals (6, 7), 1.2. said upper surface has longitudinal edges with a length (a) and lateral narrow edges with a width (b), 1.3. the length (a) is equal or nearly equal to twice the width (b), 1.4. the distance (b/2) of each terminal (6, 7) to both longitudinal edges as well as to the adjacent narrow edge is equal or nearly equal to half the width (b), 1.5. the terminals (6, 7) of adjacent battery units (2, 2') are adapted to be interconnected by means of terminal connectors made up of electrical junctions each of which comprises two connection points (16, 17) at its ends, the distance of which is equal or nearly equal to said width (b), 1.6. the battery units are stackable such that a gap is provided between two superimposed battery units (2, 2'), 1.7. the upper surface of each battery unit is provided with spacer elements cooperating with corresponding counterparts located on the lower surface of a superimposed battery unit, 1.8. the spacer elements provide to create said gap between said upper surface and said lower surface, said gap forming a seat for said terminal connectors. 1.1. each battery unit has the shape of a right parallelepiped with an upper surface forming a terminal area comprising two terminals (6, 7), 1.2. said upper surface has longitudinal edges with a length (a) and lateral narrow edges with a width (b), 1.3. the length (a) is equal or nearly equal to twice the width (b), 1.4. the distance (b/2) of each terminal (6, 7) to both longitudinal edges as well as to the adjacent narrow edge is equal or nearly equal to half the width (b), 1.5. the terminals (6, 7) of adjacent battery units (2, 2') are adapted to be interconnected by means of terminal connectors made up of electrical junctions each of which comprises two connection points (16, 17) at its ends, the distance of which is equal or nearly equal to said width (b), 1.6. the battery units are stackable such that a gap is provided between two superimposed battery units (2, 2'), 1.7. the upper surface of each battery unit is provided with spacer elements cooperating with corresponding counterparts located on the lower surface of a superimposed battery unit, 1.8. the spacer elements provide to create said gap between said upper surface and said lower surface, said gap forming a seat for said terminal connectors.
Method for forming a package from a container having a body, a neck and a bottom, the container having a deformable zone that can be deformed, using a mechanical push-rod able to move between a retracted position and a deployed position, from a deployed configuration in which the said zone projects towards the outside of the container, to a pushed-in configuration in which the said zone projects towards the inside of the container, this method comprising the following operations: - with the deformable zone in its deployed position, filling the container with a product at a temperature higher than the glass transition temperature of the material of the container; - sealing the container thus filled, using a cap mounted on the neck; this method being characterized in that it comprises the operations consisting in: - measuring the temperature of the capped container; - comparing the temperature thus measured against a predetermined threshold value; - if the measured temperature is below or equal to the threshold value, moving the push-rod from its retracted position towards its deployed position so as to cause the deformable zone to pass from its deployed configuration to its pushed-in configuration; - if the temperature measured is higher than the threshold value, keeping the push-rod at least temporarily in its retracted position. - with the deformable zone in its deployed position, filling the container with a product at a temperature higher than the glass transition temperature of the material of the container; - sealing the container thus filled, using a cap mounted on the neck; - measuring the temperature of the capped container; - comparing the temperature thus measured against a predetermined threshold value; - if the measured temperature is below or equal to the threshold value, moving the push-rod from its retracted position towards its deployed position so as to cause the deformable zone to pass from its deployed configuration to its pushed-in configuration; - if the temperature measured is higher than the threshold value, keeping the push-rod at least temporarily in its retracted position.
A lubricant comprising a silicon-containing ionic liquid of formula below wherein R 1 is an alkyl group of 1 to 10 carbon atoms, R 2 is an alkyl group of 8 to 20 carbon atoms and R 3 is an alkyl group of 1 to 8 carbon atoms, with the proviso that the number of carbon atoms in R 2 is higher than the number of carbons in R 1; and wherein the lubricant further comprises at least one additive selected from the group consisting of surfactants, dispersants, antioxidants, anti-wear agents, rust inhibitors, corrosion inhibitors, friction modifiers, extreme pressure additives, antifoam agents, viscosity modifiers and pour point depressants.
Method for network-controlled limitation of the volume and time of services based on GPRS/UMTS 2G/3G, wherein a number of data packets received or transmitted in an open or active telecommunications connection is determined within a period of time set by the network operator and is charged to a telecommunications customer by means of a corresponding method of calculation, wherein a network-controlled limitation of the volume and/or time is carried out on data packets within GPRS/UMTS-based services, forming a cost control for a user of the telecommunications connection for the telecommunications services used, characterised in that a minimum or maximum volume of data and/or volume of time is entered directly by the user of the telecommunications connection by means of a terminal device and the control of the transmitted data packets according to the volume and/or time is executed by means of an intra-network PDP context, wherein the message activating the PDP context is augmented by an information element IE, wherein acoustic signalling, executed by a generated signal tone, a generated short message service SMS or a generated multimedia message service MMS message and/or optical signalling is provided on reaching or exceeding the minimum or maximum value predetermined by the user for a volume of data and/or time window, and/or in that the transmission of data packets is terminated immediately when the volume of data and/or time window entered by the user is reached or exceeded, wherein the parameters required to terminate the data transmission are transmitted to the respective SGSN and GGSN in the specific information element IE during the activation of the PDP context, wherein the GGSN carries out the processing of the parameters.
A machine, comprising: an engine; a speed sensor coupled to the engine for detecting the speed change of the engine; a primary load drivingly coupled to the engine; a pump drivingly coupled to the engine, the pump being operatively connected to a motor, at least one of the pump and the motor having a variable displacement; a secondary load comprising a generator drivingly coupled to the motor; and a controller, being in communication with the engine, the speed sensor and at least one of the pump and the motor, wherein the controller is configured to: sense a change in engine speed in response to a change in the primary load; modify the engine speed in response to the sensed change in engine speed; and change a displacement of at least one of the pump and the motor to maintain a constant secondary load. an engine; a speed sensor coupled to the engine for detecting the speed change of the engine; a primary load drivingly coupled to the engine; a pump drivingly coupled to the engine, the pump being operatively connected to a motor, at least one of the pump and the motor having a variable displacement; a secondary load comprising a generator drivingly coupled to the motor; and a controller, being in communication with the engine, the speed sensor and at least one of the pump and the motor, wherein the controller is configured to: sense a change in engine speed in response to a change in the primary load; modify the engine speed in response to the sensed change in engine speed; and change a displacement of at least one of the pump and the motor to maintain a constant secondary load. sense a change in engine speed in response to a change in the primary load; modify the engine speed in response to the sensed change in engine speed; and change a displacement of at least one of the pump and the motor to maintain a constant secondary load.
A method of determining the M. tuberculosis infection status of a subject comprising determining the expression level of NXNL1 and one or more genes selected from the group consisting of: PSMA7, C6orf61 and EMP1 in a sample from a subject, wherein a decreased expression level of the gene NXNL1; and a decreased expression level of PSMA7 or C6orf61 or an increased expression level of the gene EMP1, differentiates between subjects not infected with M. tuberculosis and subjects with latent M. tuberculosis and indicates that a subject has a latent M. tuberculosis infection, wherein the sample is a sample of blood, optionally whole blood, blood plasma or blood serum; sputum; saliva; wound exudate; urine; faeces; peritoneal fluid; or a respiratory section.
A compound, wherein the compound has the structure of Formula II: wherein: A 1 is selected from H, F, Cl, Br, I, CN, OMe, NO 2, and CO 2 H; A 2 is selected from H, F, Cl, Br, I, CN, OMe, NO 2, and CO 2 H; E 1 is and E 2 is H; or E 1 and E 2 form a ring having the structure wherein: D is H, Me, CH 2 Cl, CH 2 F, CH 2 Br, CH 2 I, CH 2 CN, CH 2 CH 2 OH, CH 2 OCH 2 -phenyl, CH 2 OH, or CO 2 Me; and G is CH 2 N(Me)CH 2 CO 2 H. A 1 is selected from H, F, Cl, Br, I, CN, OMe, NO 2, and CO 2 H; A 2 is selected from H, F, Cl, Br, I, CN, OMe, NO 2, and CO 2 H; E 1 is and E 2 is H; or E 1 and E 2 form a ring having the structure wherein: D is H, Me, CH 2 Cl, CH 2 F, CH 2 Br, CH 2 I, CH 2 CN, CH 2 CH 2 OH, CH 2 OCH 2 -phenyl, CH 2 OH, or CO 2 Me; and G is CH 2 N(Me)CH 2 CO 2 H. D is H, Me, CH 2 Cl, CH 2 F, CH 2 Br, CH 2 I, CH 2 CN, CH 2 CH 2 OH, CH 2 OCH 2 -phenyl, CH 2 OH, or CO 2 Me; and G is CH 2 N(Me)CH 2 CO 2 H.
Sliding and folding roof for a cabriolet vehicle, - with a respective guide rail on each side of the vehicle, - with a cabriolet-top cloth which is connected to bows and is adjustable between an open position and a closed position with the aid of said bows, - wherein the bows comprise a plurality of sliding bows which are mounted by the ends thereof on the guide rails in a displaceable manner, - wherein the bows comprise a corner bow which is connected to the cabriolet-top cloth in a transition region in which, in the closed position, a rear portion of the cabriolet-top cloth merges into a roof portion of the cabriolet-top cloth, characterized in that the corner bow is configured as a pivoting bow which is mounted by the ends thereof on the guide rails so as to be pivotable about a pivot axis. - with a respective guide rail on each side of the vehicle, - with a cabriolet-top cloth which is connected to bows and is adjustable between an open position and a closed position with the aid of said bows, - wherein the bows comprise a plurality of sliding bows which are mounted by the ends thereof on the guide rails in a displaceable manner, - wherein the bows comprise a corner bow which is connected to the cabriolet-top cloth in a transition region in which, in the closed position, a rear portion of the cabriolet-top cloth merges into a roof portion of the cabriolet-top cloth,
A device, comprising: a first electrode (4; 25); a second electrode (2; 28) disposed over the first electrode (4; 25); an insulating layer disposed below the second electrode (2; 28); and a cantilever electrode connected to a cantilever (5; 26), wherein the cantilever (5, 26) is positioned between the second electrode (2; 28) and the first electrode (4; 25); wherein the cantilever (5; 26) is positioned within a cavity; wherein the insulating layer is disposed between the cantilever (5; 26) and the second electrode (2; 28), and wherein the cantilever (5; 26) is moveable between the first electrode (4; 25) and the insulating layer; characterised by a first inter-metal dielectric layer having metallization structures formed therein and disposed below the first electrode (4; 25); wherein the second electrode (2; 28) is connected to the metallization structures through connecting vias; and the second electrode (2; 28) borders the cavity on at least one side perpendicular to the insulating layer. a first electrode (4; 25); a second electrode (2; 28) disposed over the first electrode (4; 25); an insulating layer disposed below the second electrode (2; 28); and a cantilever electrode connected to a cantilever (5; 26), wherein the cantilever (5, 26) is positioned between the second electrode (2; 28) and the first electrode (4; 25); wherein the cantilever (5; 26) is positioned within a cavity; wherein the insulating layer is disposed between the cantilever (5; 26) and the second electrode (2; 28), and wherein the cantilever (5; 26) is moveable between the first electrode (4; 25) and the insulating layer; characterised by a first inter-metal dielectric layer having metallization structures formed therein and disposed below the first electrode (4; 25); wherein the second electrode (2; 28) is connected to the metallization structures through connecting vias; and the second electrode (2; 28) borders the cavity on at least one side perpendicular to the insulating layer.
An aircraft sensor system comprising: a first sensor (90; 110; 430) configured to detect a parameter of an aircraft system;a first micro electro-mechanical-system (MEMS) (120, 122, 124, 126, 128; 410) disposed local to a first component within the aircraft system, the first MEMS (120, 122, 124, 126, 128; 410) being communicatively connected to a controller (92; 130; 420); and characterised by the controller (92; 130; 420) being configured to trigger in response to a corresponding parameter exceeding a threshold; and by the controller (92; 130; 420) being connected to an output of the first sensor (90; 110; 430) and including a non-transitory memory storing instructions configured to cause the controller (92; 130; 420) to increase a sampling rate of the first sensor (90; 110; 430) to a sampling rate corresponding to the first component for at least a predetermined length of time, for example having a length in the range of 100-400 ms, in response to the first MEMS (120, 122, 124, 126, 128; 410) being triggered. a first sensor (90; 110; 430) configured to detect a parameter of an aircraft system;a first micro electro-mechanical-system (MEMS) (120, 122, 124, 126, 128; 410) disposed local to a first component within the aircraft system, the first MEMS (120, 122, 124, 126, 128; 410) being communicatively connected to a controller (92; 130; 420); and characterised by the controller (92; 130; 420) being configured to trigger in response to a corresponding parameter exceeding a threshold; and by the controller (92; 130; 420) being connected to an output of the first sensor (90; 110; 430) and including a non-transitory memory storing instructions configured to cause the controller (92; 130; 420) to increase a sampling rate of the first sensor (90; 110; 430) to a sampling rate corresponding to the first component for at least a predetermined length of time, for example having a length in the range of 100-400 ms, in response to the first MEMS (120, 122, 124, 126, 128; 410) being triggered.
A lubricious coating comprising: a first coated layer comprising a vinyl pyrrolidone polymer and photoreactive groups, wherein the photoreactive groups are pendent from the vinyl pyrrolidone polymer or on a first cross-linking agent comprising at least two photoreactive groups, or both; and a second coated layer that is a top coating comprising an acrylic acid polymer, wherein the second coated layer is in direct contact with the first coated layer, wherein the first coated layer is between the second coated layer and a substrate surface. a first coated layer comprising a vinyl pyrrolidone polymer and photoreactive groups, wherein the photoreactive groups are pendent from the vinyl pyrrolidone polymer or on a first cross-linking agent comprising at least two photoreactive groups, or both; and a second coated layer that is a top coating comprising an acrylic acid polymer, wherein the second coated layer is in direct contact with the first coated layer, wherein the first coated layer is between the second coated layer and a substrate surface.
A multiview display system (100, 200) comprising: a multibeam backlight configured to provide emitted light as a plurality of directional light beams having different principal angular directions corresponding to respective different view directions of the multiview display, the multiview display configured to provide different views of a multiview image to the different view directions, an array of light valves (220,110) having a repeating plurality of color sub-pixels and arranged as multiview pixels configured to modulate the directional light beams as color pixels of the views of the multiview image; and a user tracker configured to track a position of a user relative to the multiview display, wherein locations of the multiview pixels relative to locations of color sub-pixels of the light valve array are configured to be shifted as a function of the tracked user position to provide dynamic color sub-pixel remapping. a multibeam backlight configured to provide emitted light as a plurality of directional light beams having different principal angular directions corresponding to respective different view directions of the multiview display, the multiview display configured to provide different views of a multiview image to the different view directions, an array of light valves (220,110) having a repeating plurality of color sub-pixels and arranged as multiview pixels configured to modulate the directional light beams as color pixels of the views of the multiview image; and a user tracker configured to track a position of a user relative to the multiview display, wherein locations of the multiview pixels relative to locations of color sub-pixels of the light valve array are configured to be shifted as a function of the tracked user position to provide dynamic color sub-pixel remapping.