mhurhangee/ep-ind-claims huggingface dataset:
A method for producing metal panels comprising: - supplying a metal melt with liquid metal by filling a casting frame with the metal melt; - bringing into contact a substrate with said metal melt, wherein said substrate comprises one or more first grooves which extend over the entire width of said metal panels to be produced, and wherein said substrate has a lower temperature than said liquid metal, so that some of said liquid metal crystallises on said substrate; - moving said substrate, wherein the substrate is a substrate band, underneath the casting frame relative to said metal melt so that a metal foil is formed on said substrate; - separating the metal foil from said substrate, wherein said metal foil is divided into metal panels at points where said first grooves are located, which grooves have such a width and depth that because of a surface tension of the liquid metal the liquid metal does not run in these grooves and interruptions occur in the metal foil, characterised in that the substrate comprises second grooves (52, 54; 92) with such dimensions that each second groove is filled by said liquid metal to form a thickening of the metal foil, so that thickening enforcements are formed on said metal panels in the second grooves (52, 54;92), whilst the remainder of the panels remains thinner, the thickening enforcements reinforcing the metal panel as a whole. - supplying a metal melt with liquid metal by filling a casting frame with the metal melt; - bringing into contact a substrate with said metal melt, wherein said substrate comprises one or more first grooves which extend over the entire width of said metal panels to be produced, and wherein said substrate has a lower temperature than said liquid metal, so that some of said liquid metal crystallises on said substrate; - moving said substrate, wherein the substrate is a substrate band, underneath the casting frame relative to said metal melt so that a metal foil is formed on said substrate; - separating the metal foil from said substrate, wherein said metal foil is divided into metal panels at points where said first grooves are located, which grooves have such a width and depth that because of a surface tension of the liquid metal the liquid metal does not run in these grooves and interruptions occur in the metal foil, characterised in that
A tire, comprising a tread, at least part of the tread comprising a tread rubber composition, comprising: a diene rubber; silica; and at least one of sulfur or a sulfur-containing compound, the tread rubber composition satisfying the following relationships to: EB / M 300 ≥ 75 M 100 ≥ 2.2 MPa and EB ≥ 500 % wherein EB is the elongation at break, M100 is 100% modulus and M300 is 300% modulus, and wherein EB, M100 and M300 are measured in accordance with JIS K6251:2010. a diene rubber; silica; and at least one of sulfur or a sulfur-containing compound, the tread rubber composition satisfying the following relationships to: EB / M 300 ≥ 75 M 100 ≥ 2.2 MPa and EB ≥ 500 % wherein EB is the elongation at break, M100 is 100% modulus and M300 is 300% modulus, and wherein EB, M100 and M300 are measured in accordance with JIS K6251:2010.
A method of controlling a robot, wherein the method comprises the steps of: monitoring the robot; and carrying out a selected one of a number of predetermined fault responses on the basis of the monitoring of the robot; wherein the fault response is selected on the basis of a monitoring of an operational capability and an output quantity of at least one motor (1.1) of the robot, characterised in that the number of predetermined fault responses comprises at least one motor-active fault response, in particular a deceleration of the motor with or without subsequent disconnection from a source of energy, a compliance control and / or a retraction movement, and at least one motor-passive fault response, in particular an immediate disconnection from a source of energy without deceleration of the motor, wherein the output quantity comprises a force, in particular a torque, and / or an integral quantity thereof, in particular a work and / or a power. monitoring the robot; and carrying out a selected one of a number of predetermined fault responses on the basis of the monitoring of the robot; wherein the fault response is selected on the basis of a monitoring of an operational capability and an output quantity of at least one motor (1.1) of the robot, characterised in that the number of predetermined fault responses comprises at least one motor-active fault response, in particular a deceleration of the motor with or without subsequent disconnection from a source of energy, a compliance control and / or a retraction movement, and at least one motor-passive fault response, in particular an immediate disconnection from a source of energy without deceleration of the motor, wherein the output quantity comprises a force, in particular a torque, and / or an integral quantity thereof, in particular a work and / or a power.
Steering column for a motor vehicle, having a rotatably mounted steering shaft and having an adjustment unit which bears a section of the steering shaft adjoining a steering wheel-side end of the steering shaft and which, in the open state of a locking apparatus, is pivotable relative to a bracket unit about a pivot axis for adjustment of the steering column in an adjustment direction for a height or tilt adjustment and the pivoting of which relative to the bracket unit about the pivot axis is locked in the closed state of the locking apparatus, wherein the pivot axis is formed by a spindle bolt which can be mounted so as to be fixed with respect to the vehicle and which extends through a first and a second elongated hole (22, 23) of the adjustment unit, and wherein, in the event of a vehicle crash, the adjustment unit is displaceable relative to the spindle bolt with displacement of the spindle bolt in the elongated holes (22, 23), wherein, in a region situated between the first and the second elongated hole (22, 23) in relation to the direction of the pivot axis, there is arranged an energy absorption part, characterized in that the spindle bolt, during the displacement thereof in the elongated holes (22, 23), interacts with the energy absorption part with plastic deformation of the energy absorption part owing to exertion of pressure on the energy absorption part and displacement of material of the energy absorption part, wherein the energy absorption part is arranged in a depression in the adjustment unit.
A securing part structure of a turbine nozzle provided with a plurality of turbine nozzle segments, each having a plurality of stator vanes, arranged annularly around an axis of a jet engine and secured between a turbine case and a shroud of the jet engine, wherein in the turbine nozzle segment, an arc-shaped outer band coupling each of distal ends of stator vanes on a side opposite to the axis to each other is provided; on the outer band in the turbine nozzle segment, a hook engaged with a nozzle support groove formed on the turbine case and a protruding portion protruding toward a rear of the jet engine are formed; and the turbine nozzle segment is secured between the turbine case and the shroud by engaging the hook of the outer band with the nozzle support groove of the turbine case from behind the jet engine and fitting an anti-rotation slot formed on the shroud with the protruding portion formed on a back side of a recessed portion from behind the jet engine, characterized in that the recessed portion is formed on the outer band in the turbine nozzle segment and is fitted with an anti-rotation tab secured to the turbine case; the protruding portion is formed in conformity to a recess of the recessed portion, on the back side of this recessed portion; and the recessed portion of the outer band is fitted with the anti-rotation tab from behind the jet engine when the turbine nozzle segment is secured between the turbine case and the shroud.
A saddle type vehicle comprising: a vehicle body frame; an engine mounted on the vehicle body frame and including at least a crankcase; a seat located higher than the crankcase of the engine; a handlebar unit (5, 205) located forward of the seat and higher than the crankcase of the engine; and a display device (16, 216, 316) located forward of the seat and higher than the crankcase of the engine, the display device (16, 216, 316) includes a screen configured to display a rotation speed of the engine and having a front end portion and a rear end portion positioned lower than the front end portion, wherein the display device (16, 216, 316) is configured to display at least one warning icon (36, 37, 38, 39) indicating a warning, characterized in that the screen of the display device is a dot-matrix display, and the display device (16, 216, 316) is configured to display the warning icon (36, 37, 38, 39) on the screen between the front end portion of the screen and an engine rotation speed indicator (22, 122) indicating the rotation speed of the engine. a vehicle body frame; an engine mounted on the vehicle body frame and including at least a crankcase; a seat located higher than the crankcase of the engine; a handlebar unit (5, 205) located forward of the seat and higher than the crankcase of the engine; and a display device (16, 216, 316) located forward of the seat and higher than the crankcase of the engine, the display device (16, 216, 316) includes a screen configured to display a rotation speed of the engine and having a front end portion and a rear end portion positioned lower than the front end portion, wherein
Multi-pass boiler for cooling or for cooling and simultaneously cleaning a flue gas of a waste incineration plant, wherein the boiler has a first pass, a lower opening in which flue gas is introduced and a second pass, a superheater, a heat exchanger, a base having a lower opening and a rising channel, through which the flue gas leaves the second pass, a downwardly moving fill which comprises spherical members in the second pass of the boiler and which is removed through the lower opening of the base and passed through an upper opening into the second pass, wherein, as a result of the movement of the fill over the surface of the heating faces, the corrosive components of the fly ash are removed, wherein the superheater and the heat exchanger are arranged in the second pass, wherein, as a result of the downwardly moving fill, there are embedded in the spherical members superheaters and heat exchangers which transfer heat and ensure that the superheater only indirectly comes into contact with the flue gas.
A resettable drive assembly for a drug delivery device comprising a first drive member and a second drive member configured to form a drive unit for driving a piston rod in a dispense operation of the drug delivery device, a locking means configured to prevent a relative rotational movement of the first drive member and the second drive member such that they are locked to each other for building the drive unit during dispense operation and configured to allow a relative rotational movement between the first drive member and the second drive member for enabling a resetting of the piston rod towards an initial position relative to the first drive member characterized in that the locking means are configured to unlock the first and second drive member by exerting a load onto the first drive member in a proximal direction of the drive assembly.
A blade outer air seal (130; 132; 414; 412) for a gas turbine engine comprising: a platform partially defining an outer diameter of a core flowpath while the blade outer air seal (130; 132; 414; 412)) is in an installed configuration; an internal cooling cavity (140; 430) defined within the platform; at least one mateface of the platform including a cooling trench; and a first set of cooling holes connecting the internal cavity to the cooling trench, the at least one mateface of the platform including a mateface trench radially outward of the cooling trench; and characterised by a second set of cooling holes connecting the internal cooling cavity to the mateface trench. a platform partially defining an outer diameter of a core flowpath while the blade outer air seal (130; 132; 414; 412)) is in an installed configuration; an internal cooling cavity (140; 430) defined within the platform; at least one mateface of the platform including a cooling trench; and a first set of cooling holes connecting the internal cavity to the cooling trench, the at least one mateface of the platform including a mateface trench radially outward of the cooling trench; and characterised by a second set of cooling holes connecting the internal cooling cavity to the mateface trench.
An access method for a user equipment in an abnormal state, characterized in comprising: determining, by a local emergency center, whether a user equipment that initiates an attach procedure can continue the attach procedure; allocating, by the local emergency center, a temporary communication identity for the user equipment; and allowing, by the local emergency center, the user equipment to be attached to a network if the attach procedure cannot be continued. determining, by a local emergency center, whether a user equipment that initiates an attach procedure can continue the attach procedure; allocating, by the local emergency center, a temporary communication identity for the user equipment; and allowing, by the local emergency center, the user equipment to be attached to a network if the attach procedure cannot be continued.
A remote drive arrangement having a first and a second electric remote drive, the remote drives being mounted adjacent to each other on a top hat rail and each being configured for actuating a switching device of the electric installation mounted on the top hat rail separated laterally beside the remote drive having a shift lever, the remote drives each comprising a support element configured for a standard top-hat-rail mounting and having two actuators (10a, 10b) which can be controlled individually and alternatingly act on a displaceably mounted slider of the respective remote drive as opposing electromagnets (10a, 10b), the slider having a passage for receiving a first lever arm of a rocker lever of the respective remote drive, and a carrier rail being mounted parallel to the long side of the top hat rail on a second lever arm of the rocker lever, a shift lever of the switching device disposed next to the remote drive engaging into the carrier rail to the side of the second lever arm, the rocker lever being pivotable about a rocker-lever rotational axis which extends parallel to the long side of the top hat rail and passes through a rotational point of the shift lever, the remote drive arrangement comprising a locking mechanism which prevents a simultaneous start-up of both remote drives by locking one of the two sliders via the remaining slider during its movement from an OFF position to an ON position.
A turbine shroud for use in a gas turbine engine that extends around a central axis, the turbine shroud comprising a carrier (48, 148, 248), preferably an annular metallic carrier, adapted to be coupled to a gas turbine engine case and formed to include a cooling channel (56, 156, 256) that opens inwardly in a radial direction, a blade track (50, 150, 250), preferably an annular blade track, nested in the carrier (48, 148, 248) and arranged radially inward of the cooling channel (56, 156, 256), and a seal (52 - 852), preferably a metallic seal, including a first split ring (53 - 853) having a W-shaped cross section that opens outwardly in the radial direction, characterised in that the first split ring (53 - 853) is engaged with surfaces of the carrier (48, 148, 248) forming the cooling channel and with a radially-outer surface of the blade track (50, 150, 250) to block ingress of hot gasses into the cooling channel (56, 156, 256) at the interface of the blade track (50, 150, 250) and the carrier (48, 148, 248).
An apparatus for preparing an endoscope for an endoscopy procedure, comprising: a protecting shroud dimensioned to receive therein a distal end of the endoscope, the distal end comprising a view port configured to enable collecting an image of the surrounding of the view port there through, and a plasma generating field applicator electrically associated with an electric power source and having a slot configured to receive therein the distal end of the endoscope shrouded within said protecting shroud, the plasma generating field applicator being configured to apply electric power suitable for plasma generation within the protecting shroud, wherein the protecting shroud is detachable from the distal end of the endoscope and from the plasma generating field applicator. a protecting shroud dimensioned to receive therein a distal end of the endoscope, the distal end comprising a view port configured to enable collecting an image of the surrounding of the view port there through, and a plasma generating field applicator electrically associated with an electric power source and having a slot configured to receive therein the distal end of the endoscope shrouded within said protecting shroud, the plasma generating field applicator being configured to apply electric power suitable for plasma generation within the protecting shroud, wherein the protecting shroud is detachable from the distal end of the endoscope and from the plasma generating field applicator.
A radio system adapted for relaying radio signals and providing a power measurement of transmit radio signals, the radio system comprising: - a calibration unit adapted to split a payload signal, thus producing at least two of the calibrated payload signals (18-1, 18-2,..., 18-N); - at least two transmit paths (70-1, 70-2,..., 70-N) for relaying the at least two calibrated payload signals (18-1, 18-2) as transmit signals (75-1, 75-2,..., 75-N), respectively, - at least two links (15-1, 15-2,..., 15-N) adapted to forward the at least two calibrated payload signals (75-1, 75-2,..., 75-N) to the at least two transmit paths (70-1, 70-2,..., 70-N), respectively, - at least two couplers (50-1, 50-2,..., 50-N) adapted to extract coupled transmit signals (90-1, 90-2,..., 90-N) from the transmit signals (75-1, 75-2,..., 75-N), - a power sensor for monitoring a transmit power of a portion of a first one of the coupled transmit signals (90-1, 90-2,..., 90-N), - a switch adapted to select one of the coupled transmit signals (90-1, 90-2,..., 90-N) as a feedback signal, wherein a power output of at least one transmit path (70-1, 70-2,..., 70-N) is measured by the calibration unit based on the feedback signal in response to the transmit power of the portion of the first one of the coupled transmit signals (90-1, 90-2,..., 90-N) not pertaining to the selected one of the coupled transmit signals. - a calibration unit adapted to split a payload signal, thus producing at least two of the calibrated payload signals (18-1, 18-2,..., 18-N); - at least two transmit paths (70-1, 70-2,..., 70-N) for relaying the at least two calibrated payload signals (18-1, 18-2) as transmit signals (75-1, 75-2,..., 75-N), respectively, - at least two links (15-1, 15-2,..., 15-N) adapted to forward the at least two calibrated payload signals (75-1, 75-2,..., 75-N) to the at least two transmit paths (70-1, 70-2,..., 70-N), respectively, - at least two couplers (50-1, 50-2,..., 50-N) adapted to extract coupled transmit signals (90-1, 90-2,..., 90-N) from the transmit signals (75-1, 75-2,..., 75-N), - a power sensor for monitoring a transmit power of a portion of a first one of the coupled transmit signals (90-1, 90-2,..., 90-N), - a switch adapted to select one of the coupled transmit signals (90-1, 90-2,..., 90-N) as a feedback signal, wherein a power output of at least one transmit path (70-1, 70-2,..., 70-N) is measured by the calibration unit based on the feedback signal in response to the transmit power of the portion of the first one of the coupled transmit signals (90-1, 90-2,..., 90-N) not pertaining to the selected one of the coupled transmit signals.
A breathing protector for use in a stoma of a laryngectomized or tracheotomised person, said breathing protector having at least one inlet and at least one outlet, such that an air flow in use will pass from the surroundings of said person through said inlet to said outlet, into trachea of said person, said breathing protector comprising a heat-moisture exchanger and a bacteriological filter, such that said air flow will pass through said heat-moisture exchanger and said bacteriological filter when said air flow in use passes through said inlet to said outlet, characterized by a closing member (6, 51, 63, 65) that may be activated to close the communication between said at least one inlet and said at least one outlet, wherein said bacteriological filter is arranged multi planar, such that an antibacteriological effect is obtained in more than one plane.
A wall structure for an aircraft, the wall structure comprising an exterior fuselage skin and an acoustic panel, the acoustic panel comprising: a first skin; a second skin; a core structure connected to and forming a plurality of cavities (54,56) between the first skin and the second skin, the cavities (54,56) including a first cavity and a second cavity, the first cavity fluidly coupled with one or more first perforations in the first skin, and the second cavity fluidly coupled with one or more second perforations in the second skin; and a plurality of vibration isolating mounts that attach the acoustic panel to the exterior fuselage skin, wherein the acoustic panel is arranged with the exterior fuselage skin and separated from the exterior fuselage skin by an air gap, wherein the air gap provides a resonance chamber between the exterior fuselage skin and the acoustic panels, wherein the core structure comprises a septum that partially defines and is between the first cavity and the second cavity, wherein the septum fluidly isolates the first cavity from the second cavity, and wherein the septum is a non-porous solid septum. a first skin; a second skin; a core structure connected to and forming a plurality of cavities (54,56) between the first skin and the second skin, the cavities (54,56) including a first cavity and a second cavity, the first cavity fluidly coupled with one or more first perforations in the first skin, and the second cavity fluidly coupled with one or more second perforations in the second skin; and a plurality of vibration isolating mounts that attach the acoustic panel to the exterior fuselage skin, wherein the acoustic panel is arranged with the exterior fuselage skin and separated from the exterior fuselage skin by an air gap, wherein the air gap provides a resonance chamber between the exterior fuselage skin and the acoustic panels, wherein the core structure comprises a septum that partially defines and is between the first cavity and the second cavity, wherein the septum fluidly isolates the first cavity from the second cavity, and wherein the septum is a non-porous solid septum.