mhurhangee/ep-ind-claims huggingface dataset:
System for industrial application including - a machine capable of changing its position and having machine communication means for wireless communication and - a controller designed for controlling the machine and having controller communication means for wireless communication with the machine communication means, - wherein the controller is provided to give an instruction to the machine to change its position, thus the new position or movement is known or inherently contained in the instruction so that the movement or new position of the machine can be predicted with the content of the instruction and - as a consequence the controller communication means and the machine communication means are dynamically aligned to each other due to the available instructions of the controller, - wherein a first table stored in the controller contains alignment values of the controller, - wherein a second table stored in the machine contains alignment values of the machine and - wherein the alignment values are alignment values for each position of the machine. - a machine capable of changing its position and having machine communication means for wireless communication and - a controller designed for controlling the machine and having controller communication means for wireless communication with the machine communication means, - wherein the controller is provided to give an instruction to the machine to change its position, thus the new position or movement is known or inherently contained in the instruction so that the movement or new position of the machine can be predicted with the content of the instruction and - as a consequence the controller communication means and the machine communication means are dynamically aligned to each other due to the available instructions of the controller, - wherein a first table stored in the controller contains alignment values of the controller, - wherein a second table stored in the machine contains alignment values of the machine and - wherein the alignment values are alignment values for each position of the machine.
Aircraft capable of changing over from air travel to space travel, comprising a single-deck provided with at least one manned cabin and comprising: • aerobic propulsion means and steerable anaerobic propulsion means; • a system for controlling the environment of the manned cabin, powered by the aerobic propulsion means, and • a store of breathable survival gas, which store is only capable of temporarily supplying said manned cabin with breathable gas in the event of said system for controlling the environment of the cabin malfunctioning at high altitude, the aircraft comprising an additional store of breathable gas, which is activated only during a stage of flight when the aerobic propulsion is interrupted, characterized in that said additional store of breathable gas is capable of supplying said system for controlling the environment of said manned cabin by replacing the aerobic propulsion means. • aerobic propulsion means and steerable anaerobic propulsion means; • a system for controlling the environment of the manned cabin, powered by the aerobic propulsion means, and • a store of breathable survival gas, which store is only capable of temporarily supplying said manned cabin with breathable gas in the event of said system for controlling the environment of the cabin malfunctioning at high altitude,
A communication system, comprising: - an analog front end comprising: at least one amplifier for amplifying a received analog signal; and an analog to digital converter that is configured to convert the analog signal to digital samples; - an automatic gain controller comprising: first comparator circuitry that is configured to compare each of the digital samples with an upper threshold and a lower threshold; counter circuitry that is configured to count a high-count number of the digital samples having magnitudes that are greater than the upper threshold during each count window and that is configured to count a low count number of the digital samples having magnitudes that are less than the lower threshold during the count window; and a gain controller that is configured to adjust a gain of the at least one amplifier of the analog front end by an amount based on the high-count number and the low count number; characterized in that the communication system further comprises second comparator circuitry that is configured to compare the high-count number of digital samples with a plurality of high-count thresholds for reducing gain by a corresponding plurality of different gain adjust amounts. - an analog front end comprising: at least one amplifier for amplifying a received analog signal; and an analog to digital converter that is configured to convert the analog signal to digital samples; at least one amplifier for amplifying a received analog signal; and an analog to digital converter that is configured to convert the analog signal to digital samples; - an automatic gain controller comprising: first comparator circuitry that is configured to compare each of the digital samples with an upper threshold and a lower threshold; counter circuitry that is configured to count a high-count number of the digital samples having magnitudes that are greater than the upper threshold during each count window and that is configured to count a low count number of the digital samples having magnitudes that are less than the lower threshold during the count window; and a gain controller that is configured to adjust a gain of the at least one amplifier of the analog front end by an amount based on the high-count number and the low count number; first comparator circuitry that is configured to compare each of the digital samples with an upper threshold and a lower threshold; counter circuitry that is configured to count a high-count number of the digital samples having magnitudes that are greater than the upper threshold during each count window and that is configured to count a low count number of the digital samples having magnitudes that are less than the lower threshold during the count window; and a gain controller that is configured to adjust a gain of the at least one amplifier of the analog front end by an amount based on the high-count number and the low count number;
A composition comprising at least one thermoplastic polyurethane TPU-1 based on an aliphatic diisocyanate, at least one metal hydroxide and at least one phosphorus-containing flame retardant, wherein the composition further comprises at least one thermoplastic polyurethane TPU-2 based on an aromatic diisocyanate.
Commercial motor vehicle having a chassis, an engine compartment defined between parallel elongate beams (3R, 3L) of the chassis, and a driver cabin (7, 9) at least partially positioned over the engine compartment, the driver cabin (7, 9) being supported on the chassis by spaced resilient suspension devices (19, 21), and includes an upper cabin part that is tiltable to allow access to the engine compartment by being hinged about a lower edge and a lower cabin part that remains associated with the chassis when the upper cabin part is tilted, characterized in that the lower part of the driver cabin (7, 9) is supported by the resilient suspension devices (19, 21).
A value or security product, having a single-layer or multi-layer base body, wherein at least one of the layers of the base body comprises an upper side and a lower side, which is provided with a recess which is formed from an edge connecting the upper side to the lower side, and which is at least partially inclined at an angle with respect to a normal to the upper side or the lower side, wherein the recess is at least partially filled with a filling, which has an upper surface and a lower surface, and wherein the upper surface is connected to the lower surface by means of a side wall, wherein the side wall of the filling is designed to be complementary to the edge of the recess at least in some areas, characterized in that the edge of the recess extends at a first section inclined by a first angle with respect to the normal of the upper side or the lower side, and in that the edge of the recess extends at a second section inclined by a second angle deviating from the first angle with respect to the normal of the upper side or the lower side.
A method for manufacturing workpieces, at least a part of the surface of said workpieces being etched including etched by ion impact, comprising: • providing a carousel base drivingly rotatable about a carousel axis (A 20); • providing along the periphery of and on said carousel base at least two planetary carriers (22; 22a), each drivingly rotatable about a planetary axis (A 22; A 22a) parallel to said carousel axis; • generating a cloud (CL; B I; B PL; PL) comprising ions and having, considered in a cross-sectional plane perpendicular to said carousel and said planetary axes, a center axis (A CL) in a center of an area of maximum ion density (ρ max); • directing said center axis so as to intersect with said carousel axis, considered in said cross-sectional plane; • applying at least one workpiece to be etched on each of said planetary carriers, each of said planetary carriers defining by rotating about its planetary axis for a diameter (Φ) with respect to such planetary axis; • establishing said cloud comprising ions having an ion density (ρ) dropping to 50% of maximum ion density of said cloud at a distance from said center axis which is at most equal to 50% of said diameter, considered in said cross-sectional plane, and at the locus of moving path of said planetary axes, for preventing material, which is momentarily etched from workpieces on one of said planetary carriers, to be redeposited on workpieces of another of said planetary carriers; • rotating said carousel base in said planetary carriers about said respective axes; • etching the workpieces as moved into and through said cloud. • providing a carousel base drivingly rotatable about a carousel axis (A 20); • providing along the periphery of and on said carousel base at least two planetary carriers (22; 22a), each drivingly rotatable about a planetary axis (A 22; A 22a) parallel to said carousel axis; • generating a cloud (CL; B I; B PL; PL) comprising ions and having, considered in a cross-sectional plane perpendicular to said carousel and said planetary axes, a center axis (A CL) in a center of an area of maximum ion density (ρ max); • directing said center axis so as to intersect with said carousel axis, considered in said cross-sectional plane; • applying at least one workpiece to be etched on each of said planetary carriers, each of said planetary carriers defining by rotating about its planetary axis for a diameter (Φ) with respect to such planetary axis; • establishing said cloud comprising ions having an ion density (ρ) dropping to 50% of maximum ion density of said cloud at a distance from said center axis which is at most equal to 50% of said diameter, considered in said cross-sectional plane, and at the locus of moving path of said planetary axes, for preventing material, which is momentarily etched from workpieces on one of said planetary carriers, to be redeposited on workpieces of another of said planetary carriers; • rotating said carousel base in said planetary carriers about said respective axes; • etching the workpieces as moved into and through said cloud.
An incubation chamber with a moisture reservoir, a climate conditioner which enables a desired temperature to be set, and an object holder for biological or chemical specimens, characterized in that the climate conditioner has two separate conditioning zones (14, 16) which are regulatable separately from one another, whereby the first conditioning zone is arranged in the vicinity of the cover of the chamber and temperature and humidity sensors are provided in the chamber, which control the temperature and the humidity in the chamber via a control device depending on the measured values.
Motor vehicle, preferably commercial vehicle, comprising: a first compressed air system comprising a first electrically driven air compressor, a first compressed air treatment unit, and a first valve device; a second compressed air system comprising a second electrically driven air compressor, a second compressed air treatment unit, and a second valve device at least one first compressed air consumer circuit (24, 26) connected to the first valve device; and at least one second compressed air consumer circuit (38, 40) connected to the second valve device. a first compressed air system comprising a first electrically driven air compressor, a first compressed air treatment unit, and a first valve device; a second compressed air system comprising a second electrically driven air compressor, a second compressed air treatment unit, and a second valve device at least one first compressed air consumer circuit (24, 26) connected to the first valve device; and at least one second compressed air consumer circuit (38, 40) connected to the second valve device.
Method for optimizing the functionality of a robot arm, comprising the steps of: Marking an input point or an input surface on the surface of the robot arm, upon pressing of which by an operator a detection of force and/or torque in at least one joint occurs, as well as deriving the position of the touch point on the surface of the robot arm, resulting in deriving a command that is to be triggered by pressing this input point and/or the input surface, characterized in that based on the known geometry of the robot arm, a two-dimensional image of at least part of the three-dimensional surface of the robot arm is created, on which at least one input point and/or at least one input surface (22a-c) is marked, at whose position on the surface of the first robot arm the input of a command is to occur. Marking an input point or an input surface on the surface of the robot arm, upon pressing of which by an operator a detection of force and/or torque in at least one joint occurs, as well as deriving the position of the touch point on the surface of the robot arm, resulting in deriving a command that is to be triggered by pressing this input point and/or the input surface, characterized in that based on the known geometry of the robot arm, a two-dimensional image of at least part of the three-dimensional surface of the robot arm is created, on which at least one input point and/or at least one input surface (22a-c) is marked, at whose position on the surface of the first robot arm the input of a command is to occur.
A method for controlling a hybrid vehicle, wherein: - the hybrid vehicle includes: - an engine connected to a generator and configured to be connected to a driving wheel, and - a motor configured to be connected to the driving wheel, the motor being driven by electric power supplied from a battery connected to the generator, - the method comprises in a direct drive mode in which the engine is connected to the driving wheel, when the battery is charged and a required charging electric power exceeds a threshold value, switching, by releasing a connection state between the engine and the driving wheel and connecting the motor to the driving wheel, to a series mode in which the engine drives the generator, and - the threshold value is chargeable electric power obtained by subtracting output required for traveling of the hybrid vehicle from maximum output of the engine that operates at a rotation speed corresponding to a vehicle speed of the hybrid vehicle. - the hybrid vehicle includes: - an engine connected to a generator and configured to be connected to a driving wheel, and - a motor configured to be connected to the driving wheel, the motor being driven by electric power supplied from a battery connected to the generator, - an engine connected to a generator and configured to be connected to a driving wheel, and - a motor configured to be connected to the driving wheel, the motor being driven by electric power supplied from a battery connected to the generator, - the method comprises in a direct drive mode in which the engine is connected to the driving wheel, when the battery is charged and a required charging electric power exceeds a threshold value, switching, by releasing a connection state between the engine and the driving wheel and connecting the motor to the driving wheel, to a series mode in which the engine drives the generator, and - the threshold value is chargeable electric power obtained by subtracting output required for traveling of the hybrid vehicle from maximum output of the engine that operates at a rotation speed corresponding to a vehicle speed of the hybrid vehicle.
A battery temperature control device of a vehicle that controls a temperature of a battery by warming up the battery by a battery-driven heater on condition that when the battery temperature is less than a predetermined temperature (Tbat_start) and a charge state of the battery is equal to or greater than a setting battery charge state, which is the lowest charge state value permitting said battery warm-up characterized by: a battery state judging section (step S21) that judges whether or not a battery state is in a charge-capable condition, which is a battery state in which the vehicle is connected to a battery charging facility or the vehicle can travel by itself up to the battery charging facility, said battery state judging section being configured to be able to judge both situations; and a setting battery charge state decreasing section (step S22) that, when the battery state is in said charge-capable condition as judged by the battery state judging section (step S21), decreases the setting battery charge state, such as to allow battery warm-up. a battery state judging section (step S21) that judges whether or not a battery state is in a charge-capable condition, which is a battery state in which the vehicle is connected to a battery charging facility or the vehicle can travel by itself up to the battery charging facility, said battery state judging section being configured to be able to judge both situations; and a setting battery charge state decreasing section (step S22) that, when the battery state is in said charge-capable condition as judged by the battery state judging section (step S21), decreases the setting battery charge state, such as to allow battery warm-up.
A chip-scale inertial sensor for detecting a rate of rotation of the inertial sensor about an axis, the inertial sensor comprising: an optical vibratory gyroscope for detecting a first rate of rotation of the inertial sensor about the axis, the optical vibratory gyroscope configured to output a main signal corresponding to the first rate of rotation; an optical Sagnac gyroscope for concurrently detecting a second rate of rotation of the inertial sensor about the axis, the optical Sagnac gyroscope configured to output a supplementary signal corresponding to the second rate of rotation; and a microcontroller configured to: receive one or more inputs based on the main signal and supplementary signal; and determine, based on the one or more inputs, a corrected first rate of rotation of the inertial sensor about the axis. an optical vibratory gyroscope for detecting a first rate of rotation of the inertial sensor about the axis, the optical vibratory gyroscope configured to output a main signal corresponding to the first rate of rotation; an optical Sagnac gyroscope for concurrently detecting a second rate of rotation of the inertial sensor about the axis, the optical Sagnac gyroscope configured to output a supplementary signal corresponding to the second rate of rotation; and a microcontroller configured to: receive one or more inputs based on the main signal and supplementary signal; and determine, based on the one or more inputs, a corrected first rate of rotation of the inertial sensor about the axis. receive one or more inputs based on the main signal and supplementary signal; and determine, based on the one or more inputs, a corrected first rate of rotation of the inertial sensor about the axis.
A method of assisting a pilot of an ownship in managing the longitudinal interval from an aircraft from which the ownship is following, comprising: receiving a first location and a first airspeed of the aircraft; determining a second location and a second airspeed of the ownship; calculating a maximum airspeed and a minimum airspeed of the ownship; receiving a commanded airspeed from air traffic control; providing commands to a display for displaying an airspeed bar including a first marker indicating the minimum airspeed, a second marker indicating the maximum airspeed, a third marker indicating the indicated airspeed, and a fourth marker indicating the commanded airspeed; continually determining the distance between the aircraft and the ownship; and adjusting the position of the fourth marker in response to the distance between the aircraft and the ownship. receiving a first location and a first airspeed of the aircraft; determining a second location and a second airspeed of the ownship; calculating a maximum airspeed and a minimum airspeed of the ownship; receiving a commanded airspeed from air traffic control; providing commands to a display for displaying an airspeed bar including a first marker indicating the minimum airspeed, a second marker indicating the maximum airspeed, a third marker indicating the indicated airspeed, and a fourth marker indicating the commanded airspeed; continually determining the distance between the aircraft and the ownship; and adjusting the position of the fourth marker in response to the distance between the aircraft and the ownship.
A bearing arrangement for a wind turbine, comprising a first portion, a second portion, and a sound wave sensor which is configured to detect a thickness of the second portion, wherein one of the first portion and the second portion is movable relative to the other of the first portion and the second portion, and characterised in that the sound wave sensor is configured to detect the thickness of the second portion through the first portion.