mhurhangee/ep-ind-claims huggingface dataset:
An apparatus (4, 5, 6, 7, 9, 70) for mining vehicle (4, 5, 6, 7) positioning, the apparatus comprising at least one processor and at least one memory storing computer program code configured to, when executed by the at least one processor, cause the apparatus (4, 5, 6, 7, 9, 70) at least to: - detect a first position of a mining vehicle (4, 5, 6, 7) with reference to a first worksite model, - receive information on a plurality of transformation matrices associated with the first worksite model, - select a transformation matrix associated with the first worksite model based on the first position of the mining vehicle (4, 5, 6, 7), - perform, based on the selected transformation matrix, a coordinate transformation from input coordinates indicative of a second position of the mining vehicle (4, 5, 6, 7) in the first worksite model to transformed coordinates of a second worksite model, and - provide the transformed coordinates to represent the second position of the mining vehicle (4, 5, 6, 7) for performing mining automation control by a control device of a mining automation system or a control unit of a mining vehicle (4, 5, 6, 7) based on the second worksite model. - detect a first position of a mining vehicle (4, 5, 6, 7) with reference to a first worksite model, - receive information on a plurality of transformation matrices associated with the first worksite model, - select a transformation matrix associated with the first worksite model based on the first position of the mining vehicle (4, 5, 6, 7), - perform, based on the selected transformation matrix, a coordinate transformation from input coordinates indicative of a second position of the mining vehicle (4, 5, 6, 7) in the first worksite model to transformed coordinates of a second worksite model, and - provide the transformed coordinates to represent the second position of the mining vehicle (4, 5, 6, 7) for performing mining automation control by a control device of a mining automation system or a control unit of a mining vehicle (4, 5, 6, 7) based on the second worksite model.
Multispeed transmission having at least four planetary gear sets (P1, P2, P3, P4) arranged one behind the other along a main rotation shaft, each having a sun gear (P11, P21, P31, P41), a planetary gear carrier (P12, P22, P32, P42) and a ring gear (P13, P23, P33, P43), characterised by a bearing which axially supports the sun gear of the second planetary gear set and the ring gear of the third planetary gear set against each other.
A vehicle for carrying a camera crane, with a deck on the vehicle and a ramp extendible from the deck at the back end of the vehicle to the ground, characterised by: a front elevator including front left and front right lifting actuators movable vertically between up and down positions, at a forward position on the deck; a back elevator including back left and back right lifting actuators movable vertically between up and down positions, at a back position on the deck; with the front and back elevators (86, 88) at the level of the deck when in the up position, and with the front and back elevators (86, 88) at least 25 cm below the level of the deck when in the down position; the deck comprising a continuous flat surface when the front and back elevators (86, 88) are in the up position. a front elevator including front left and front right lifting actuators movable vertically between up and down positions, at a forward position on the deck; a back elevator including back left and back right lifting actuators movable vertically between up and down positions, at a back position on the deck; with the front and back elevators (86, 88) at the level of the deck when in the up position, and with the front and back elevators (86, 88) at least 25 cm below the level of the deck when in the down position; the deck comprising a continuous flat surface when the front and back elevators (86, 88) are in the up position.
A device for preparation of a sample of biological fluid for its bacteriological analysis and comprising a container provided with a chamber in which a piston is movable between an open position and closing position, and said device being characterized in that the chamber comprises a separation zone and a means for introduction (15, 16) of a fluid into said chamber, said means of introduction being arranged in the upper part of the chamber, and in that the piston comprises a closure means cooperating with the separation zone in order to define an upper volume and a lower volume on both sides of said zone, the upper volume and the lower volume communicating with each other when the piston is in the open position and tightly isolated from each other when the piston is in the closing position, and said device being characterized in that the separation zone comprises a bottleneck, the lower volume extending under said bottleneck, the closure means being constructed to close said bottleneck when the piston is in the closing position in order to isolate the lower volume from the upper volume.
A method for controlling the product features during the production of foodstuffs attributable to the product group of raw sausage, in particular for obtaining the spreading or cutting property, characterized in that for the production of raw sausage the usual starting materials, not in the frozen state, are salted, mixed and coarsely pre-chopped, and said mixture is subjected to fermentation and acidification, i.e. a reduction in the pH value, followed by high-pressure treatment for the coagulation of protein and inactivation of microorganisms, wherein the mechanically separated raw meat materials remain separated, wherein fine comminution occurs after the high-pressure treatment step, and fat is added during the comminution to final grain size and subsequently a second high-pressure treatment is carried out on the filled product, and wherein depending on the performance and intensity of the high-pressure treatment the fraction of salt in the product is reduced, in that the salt content is reduced by approximately 10% in comparison with recipes which are produced according to conventional production methods.
Screw anchor for setting in concrete in a railway sleeper or ballastless track and force-locking connection to a sleeper screw, comprising: - a threaded section having external thread turns arranged on the outside of the screw anchor as well as internal thread turns arranged on the inside of the screw anchor; and - an upper partial section with no external thread located near the anchor opening when fitted; wherein the screw anchor has two components made of different materials, a base body made of plastic, and a cylindrical ring made of a steel material which is mounted on the base body in form-locking and/or force-locking relationship, characterised in that the coefficient of linear thermal expansion of the steel material of the cylindrical ring is at least ten times lower than that of the plastic material of the base body which it surrounds, and the coefficient of linear thermal expansion of the steel material of the cylindrical ring does not exceed 3·10 -5 l/K. - a threaded section having external thread turns arranged on the outside of the screw anchor as well as internal thread turns arranged on the inside of the screw anchor; and - an upper partial section with no external thread located near the anchor opening when fitted; wherein the screw anchor has two components made of different materials, a base body made of plastic, and a cylindrical ring made of a steel material which is mounted on the base body in form-locking and/or force-locking relationship, characterised in that the coefficient of linear thermal expansion of the steel material of the cylindrical ring is at least ten times lower than that of the plastic material of the base body which it surrounds, and the coefficient of linear thermal expansion of the steel material of the cylindrical ring does not exceed 3·10 -5 l/K.
An automated external defibrillator comprising: a main unit configured to connect with a first pad at least partially colored in a first color and a second pad at least partially colored in a second color, the first color being different from the second color, the main unit comprising a first guidance surface configured to visually inform a user how to attach the first pad and the second pad to the patient including where to attach the electrode pads (21, 22), characterized in that the first guidance surface comprises a first indicator configured to being turned on and/or blinked in the first color at a position on the first guidance surface corresponding to an attachment position of the first pad and a second indicator configured to being turned on and/or blinked in the second color at a position on the first guidance surface corresponding to an attachment position of the second pad. a main unit configured to connect with a first pad at least partially colored in a first color and a second pad at least partially colored in a second color, the first color being different from the second color, the main unit comprising a first guidance surface configured to visually inform a user how to attach the first pad and the second pad to the patient including where to attach the electrode pads (21, 22), characterized in that the first guidance surface comprises a first indicator configured to being turned on and/or blinked in the first color at a position on the first guidance surface corresponding to an attachment position of the first pad and a second indicator configured to being turned on and/or blinked in the second color at a position on the first guidance surface corresponding to an attachment position of the second pad.
A rocket engine comprising: a rocket engine combustion chamber, and a rocket engine nozzle including an aerospike including: a plurality of airfoil fins disposed at an exit end of the rocket engine combustion chamber and extending across an exit plane of the rocket engine combustion chamber, the plurality of airfoil fins being distributed around a central longitudinal axis; and a central airfoil hub from which each of the plurality of airfoil fins extend radially outward, wherein a maximum length of the central airfoil hub in a longitudinal direction is less than or equal to a maximum length of the plurality of airfoil fins in the longitudinal direction; wherein the plurality of airfoil fins and an inner perimeter of the rocket engine combustion chamber define a plurality of apertures between adjacent airfoil fins at the exit plane, the plurality of apertures being configured to choke an airflow exiting the rocket engine combustion chamber and cause the airflow to expand supersonically along the plurality of airfoil fins to create thrust. a rocket engine combustion chamber, and a rocket engine nozzle including an aerospike including: a plurality of airfoil fins disposed at an exit end of the rocket engine combustion chamber and extending across an exit plane of the rocket engine combustion chamber, the plurality of airfoil fins being distributed around a central longitudinal axis; and a central airfoil hub from which each of the plurality of airfoil fins extend radially outward, wherein a maximum length of the central airfoil hub in a longitudinal direction is less than or equal to a maximum length of the plurality of airfoil fins in the longitudinal direction; wherein the plurality of airfoil fins and an inner perimeter of the rocket engine combustion chamber define a plurality of apertures between adjacent airfoil fins at the exit plane, the plurality of apertures being configured to choke an airflow exiting the rocket engine combustion chamber and cause the airflow to expand supersonically along the plurality of airfoil fins to create thrust. a plurality of airfoil fins disposed at an exit end of the rocket engine combustion chamber and extending across an exit plane of the rocket engine combustion chamber, the plurality of airfoil fins being distributed around a central longitudinal axis; and a central airfoil hub from which each of the plurality of airfoil fins extend radially outward, wherein a maximum length of the central airfoil hub in a longitudinal direction is less than or equal to a maximum length of the plurality of airfoil fins in the longitudinal direction; wherein the plurality of airfoil fins and an inner perimeter of the rocket engine combustion chamber define a plurality of apertures between adjacent airfoil fins at the exit plane, the plurality of apertures being configured to choke an airflow exiting the rocket engine combustion chamber and cause the airflow to expand supersonically along the plurality of airfoil fins to create thrust.
Procedure designed for the verification of the current setting functionality of a device, which has an analog current output designed for a current value corresponding to a measured value or an actuating value of the device, and a current actuator assigned to the current output, said actuator setting the current value at the current output depending on a current target value provided in the device, wherein the current value representing a measured value or an actuating value is located within a range from a lower current limit value to an upper current limit value and wherein, during the normal operation of the device, the current target value is provided according to a measured value or an actuating value to be output via the analog current output, said procedure comprising the following steps, which are performed in the device: A) During normal mode, monitoring in the device to determine whether the current actuator sets a high current value at the current output corresponding to the current target value; B) Provision of a low current target value below the lower current limit value if the result of the step involving monitoring during normal operation is that a high current value corresponding to the current target value cannot be set by the current actuator; characterized in that the procedure comprises the following step: C) Final verification of the current setting functionality through the provision of a high current target value above the upper current limit value and through monitoring in the device, in the high current mode, whether a high current value corresponding to the high current target value can be set at the current output by the current actuator, wherein, if the device has a functional capacity to set the current, a current target value is provided in the device that corresponds to a measured value or actuating value to be output via the analog current output, and wherein, if the device does not have a functional capacity to set the current, a low current target value below the lower current limit value is then provided in the device. A) During normal mode, monitoring in the device to determine whether the current actuator sets a high current value at the current output corresponding to the current target value; B) Provision of a low current target value below the lower current limit value if the result of the step involving monitoring during normal operation is that a high current value corresponding to the current target value cannot be set by the current actuator; characterized in that the procedure comprises the following step: C) Final verification of the current setting functionality through the provision of a high current target value above the upper current limit value and through monitoring in the device, in the high current mode, whether a high current value corresponding to the high current target value can be set at the current output by the current actuator,
A method of operating LC sensors including: - accumulating excitation energy for an LC sensor, and - the LC sensor oscillating energized by energy accumulated, wherein the method includes: - detecting the energy accumulated reaching a charge threshold, and - terminating accumulating excitation energy for the sensor when the charge threshold is detected to be reached, the method characterized in that it includes coupling a reference capacitor (C ref) in series to the LC sensor, and - a) accumulating excitation energy for the sensor by coupling the series coupling of the sensor and the reference capacitor (C ref) to an energy source, or - b) starting accumulating excitation energy for the sensor by coupling the sensor to an energy source with the reference capacitor (C ref) short-circuited, and removing the short-circuit across the reference capacitor (C ref) while maintaining the LC sensor coupled to the energy source. - accumulating excitation energy for an LC sensor, and - the LC sensor oscillating energized by energy accumulated, - detecting the energy accumulated reaching a charge threshold, and - terminating accumulating excitation energy for the sensor when the charge threshold is detected to be reached, the method characterized in that it includes coupling a reference capacitor (C ref) in series to the LC sensor, and - a) accumulating excitation energy for the sensor by coupling the series coupling of the sensor and the reference capacitor (C ref) to an energy source, or - b) starting accumulating excitation energy for the sensor by coupling the sensor to an energy source with the reference capacitor (C ref) short-circuited, and removing the short-circuit across the reference capacitor (C ref) while maintaining the LC sensor coupled to the energy source.
A brake for a roller blind, particularly for pleated roller blinds, the brake being configured to be arranged parallel to the longitudinal axis of a bar of said roller blind, the brake of having a labyrinth part with a labyrinth duct, wherein there are two rounded elements (8, 9), preferably wheels, one of said rounded elements (8, 9) at each end of the labyrinth duct, wherein the brake has a connector for connection with the labyrinth part, characterized in that the labyrinth part has a protrusion on the internal surface, the protrusion having the labyrinth duct furrowed, and the two rounded elements (8, 9) having a thickness equal to the thickness of the protrusion, wherein the individual sections of the labyrinth duct (7', 7") form angle α that ranges between 110° and 175°·
Combined electro-pneumatic braking system, which combines a pressure controller and a differential slip controller, containing: a detection and decision unit, which detects input values available from different signal sources available as part of a first input vector; and at least one control unit to determine at least one intermediate value for a brake pressure calculation, to which a second input vector containing at least one input value is supplied from the detection and decision unit, characterised in that a pre-processing means is provided, which performs an axle load sensor signal-free calculation of parameters relevant for a braking process and supplies this as a further part of the first input vector to the detection and decision unit; and the detection and decision unit: generates the at least one input value contained in the second input signal vector from the input values contained in the first input signal vector as a function of the detected operating situation or an availability of the input values, at the same time selects, from a plurality of calculation means available as a function of the detected operating situation or the availability of the input values, and in assignment to the at least one input value contained in the second input signal vector, at least one performable calculation means, and the control unit calculates for the brake pressure calculation the at least one intermediate value using the at least one selected, performable calculation means as a function of the content of the second input vector. a detection and decision unit, which detects input values available from different signal sources available as part of a first input vector; and at least one control unit to determine at least one intermediate value for a brake pressure calculation, to which a second input vector containing at least one input value is supplied from the detection and decision unit, generates the at least one input value contained in the second input signal vector from the input values contained in the first input signal vector as a function of the detected operating situation or an availability of the input values, at the same time selects, from a plurality of calculation means available as a function of the detected operating situation or the availability of the input values, and in assignment to the at least one input value contained in the second input signal vector, at least one performable calculation means, and the control unit calculates for the brake pressure calculation the at least one intermediate value using the at least one selected, performable calculation means as a function of the content of the second input vector.
A surveillance system controller comprising: a housing having a first cavity and a second cavity; a first control module (24, 26, 28) having a plurality of control keys, said first control module (24, 26, 28) being located in said first cavity and being rotatable around a first vertical axis with respect to the first cavity so that said first control module (24, 26, 28) can be rotated to a first angular position; and a second control module (24, 26, 28) having a plurality of control keys, said second control module (24, 26, 28) being located in said second cavity and being rotatable around a second vertical axis with respect to the second cavity so that said second control module (24, 26, 28) can be rotated to a second angular position independent of said first angular position to align said plurality of control keys of said first control module (24, 26, 28) and said plurality of control keys of said second control module (24, 26, 28) with a user to provide ergonomic comfort and advantage.
A process for preparing (meth)acrylic acid, wherein a crude (meth) acrylic acid is first prepared and this crude (meth)acrylic acid is then continuously purified, wherein the continuous purification of the crude (meth)acrylic acid comprises the following process steps: a) in a composition comprising (meth) acrylic acid and impurities, the impurities being a mixture of maleic acid, fumaric acid and maleic anhydride, precipitating the impurities out of the composition in crystalline form; b) separating the crystalline impurities precipitated out of the composition, wherein the precipitating of the maleic anhydride in step a) is effected by controlled hydrolysis of the maleic anhydride over a period of 1 to 250 hours. a) in a composition comprising (meth) acrylic acid and impurities, the impurities being a mixture of maleic acid, fumaric acid and maleic anhydride, precipitating the impurities out of the composition in crystalline form; b) separating the crystalline impurities precipitated out of the composition,