mhurhangee/patent-ind-claim-en huggingface dataset:
A fusing device comprising: a fusing belt that is rotatable; a pressing member disposed to face the fusing belt and form a fusing nip (N) with the fusing belt; a heat source disposed inside the fusing belt and at a side of the fusing nip; a guide member including a heat source seat , on which the heat source is mountable, and configured to guide a rotation of the fusing belt; and a pressing support member at one side of the heat source seat and configured to press the heat source toward an other side of the heat source seat that is opposite the one side of the heat source seat, characterised in that the heat source seat includes a plurality of protrusions formed protruding from an inner surface thereof on which the heat source is mounted. a fusing belt that is rotatable; a pressing member disposed to face the fusing belt and form a fusing nip (N) with the fusing belt; a heat source disposed inside the fusing belt and at a side of the fusing nip; a guide member including a heat source seat , on which the heat source is mountable, and configured to guide a rotation of the fusing belt; and a pressing support member at one side of the heat source seat and configured to press the heat source toward an other side of the heat source seat that is opposite the one side of the heat source seat, characterised in that the heat source seat includes a plurality of protrusions formed protruding from an inner surface thereof on which the heat source is mounted.
A process for combined ethylbenzene reforming and xylene isomerisation comprising contacting a hydrocarbon feedstock containing ethylbenzene and xylene with a catalyst comprising a catalyst carrier and one or more metal(s) supported on the catalyst carrier, wherein the catalyst carrier is an extrudate comprising (i) a ZSM-48 and/or EU-2 type zeolite and (ii) an alumina binder, the extrudate having a shape with a C/A value of at least 3, where C is the circumference of the extrudate and A is the cross-sectional area of the extrudate.
An imaging device comprising: a light source projection unit configured to project intensity-modulated spatial pattern light; a time-of-flight distance measurement camera configured to measure a distance to an object on the basis of a time of flight of a modulated component included in reflected light of the spatial pattern light from the object ; a spatial information distance measurement camera configured to measure a distance to the object on the basis of spatial information included in the reflected light; and a depth synthesizing unit configured to synthesize measurement results of the distances in the time-of-flight distance measurement camera and the spatial information distance measurement camera to determine a depth value of each pixel position of an image imaged by the time-of-flight distance measurement camera or the spatial information distance measurement camera , wherein an exposure time of the time-of-flight distance camera and an exposure time of the spatial information distance measurement camera are set, and wherein the light source projection unit is further configured to project, when the exposure time of the time-of-flight distance camera is elapsed, non-modulated fixed light until the exposure time of the spatial information distance measurement camera is elapsed. a light source projection unit configured to project intensity-modulated spatial pattern light; a time-of-flight distance measurement camera configured to measure a distance to an object on the basis of a time of flight of a modulated component included in reflected light of the spatial pattern light from the object ; a spatial information distance measurement camera configured to measure a distance to the object on the basis of spatial information included in the reflected light; and a depth synthesizing unit configured to synthesize measurement results of the distances in the time-of-flight distance measurement camera and the spatial information distance measurement camera to determine a depth value of each pixel position of an image imaged by the time-of-flight distance measurement camera or the spatial information distance measurement camera , wherein an exposure time of the time-of-flight distance camera and an exposure time of the spatial information distance measurement camera are set, and wherein the light source projection unit is further configured to project, when the exposure time of the time-of-flight distance camera is elapsed, non-modulated fixed light until the exposure time of the spatial information distance measurement camera is elapsed.
Apparatus for holding lighters , having a basic body and at least one holding device for the lighter , in which the holding device is realized as an elongate opening or as an elongate cutout in the basic body of the apparatus , with the result that the lighter is able to be held by virtue of the lighter being able to be plugged, at least in certain regions, laterally into the cutout or opening of the holding device , wherein the openings or cutouts are arranged next to one another in the manner of rows and/or above one another, and wherein an inner contour of the openings or cutouts is configured to be similar to the outer contour of the lighter , and wherein the similarity between the outer contour and the inner contour comprises both a vertical direction and a horizontal direction, characterized in that the openings or cutouts have a trapezium-like configuration.
A wind energy system , in particular an offshore wind energy system , comprising: - a plurality of wind turbines (104.1, 104.2, 104.3, 104.4) connected to at least one cable network , - wherein the cable network is configured to transmit the electrical power fed-in by the connected wind turbines (104.1, 104.2, 104.3, 104.4), - at least one control apparatus configured to control the power fed into the cable network by at least one of the wind turbine (104.1, 104.2, 104.3, 104.4) by providing at least one power set point, wherein - at least one temperature detecting device is provided, configured to detect the temperature of the cable network , - at least one condition detecting device is provided, configured to detect the condition of the wind energy system , and - the control apparatus comprises at least one control device configured to determine the power set point based on the detected temperature and the detected condition, characterized in that - the condition detecting device comprises at least one switching condition evaluating module configured to determine the electrical topology of the wind power system based on the switching states of a plurality of electrical switching devices of the wind power system , - the control device is configured at least to determine the power set point based on the determined electrical topology of the wind power system , - the condition detecting device is configured to provide a thermal model of the electrical topology of the wind energy system , and - the control device is configured at least to determine the power set point based on the provided thermal model. - a plurality of wind turbines (104.1, 104.2, 104.3, 104.4) connected to at least one cable network , - wherein the cable network is configured to transmit the electrical power fed-in by the connected wind turbines (104.1, 104.2, 104.3, 104.4), - at least one control apparatus configured to control the power fed into the cable network by at least one of the wind turbine (104.1, 104.2, 104.3, 104.4) by providing at least one power set point, - at least one temperature detecting device is provided, configured to detect the temperature of the cable network , - at least one condition detecting device is provided, configured to detect the condition of the wind energy system , and - the control apparatus comprises at least one control device configured to determine the power set point based on the detected temperature and the detected condition, - the condition detecting device comprises at least one switching condition evaluating module configured to determine the electrical topology of the wind power system based on the switching states of a plurality of electrical switching devices of the wind power system , - the control device is configured at least to determine the power set point based on the determined electrical topology of the wind power system , - the condition detecting device is configured to provide a thermal model of the electrical topology of the wind energy system , and - the control device is configured at least to determine the power set point based on the provided thermal model.
Double actuator , for example for a double clutch transmission, with a hollow-cylindrical radially outer piston and a hollow-cylindrical radially inner piston , in the case of which double actuator the inner piston is enclosed in sections coaxially by the outer piston , in the case of which double actuator the inner piston and the outer piston are guided in a cylinder housing such that it can be axially displaced parallel to the longitudinal centre axis of the latter, and in the case of which double actuator the cylinder housing has a radially inner cylinder section and a radially central cylinder section which encloses the former coaxially, characterized in that a sensor device is arranged on the central cylinder section of the cylinder housing , into which sensor device a first displacement sensor and a second displacement sensor are integrated axially next to one another, and in that the said displacement sensors are configured and arranged in such a way that an axial position of the outer piston and an axial position of the inner piston in relation to the central cylinder section can be measured in each case independently of one another and contactlessly.
A network monitoring entity for a communication network configured to support at least a portion of a network slice, the communication network being a single administration and comprising a plurality of sub-networks (203a-c), each sub-network (203a-c) being a technological domain in the single administration, and being configured to support at least a sub-portion (206a-c) of the portion of the network slice, the network monitoring entity comprising: a communication interface configured to communicate with a plurality of sub-network monitoring units (204a-c), wherein each sub-network monitoring unit (204a-c) comprises at least one monitoring probe (205a-c) and each monitoring probe (205a-c) is configured to monitor at least one performance measure of the sub-portion (206a-c) of the portion of the network slice supported by the sub-network (203a-c), wherein the monitoring probes (205a-c) of the plurality of sub-network monitoring units (204a-c) define a set of monitoring probes ; and a processor configured to select one or more monitoring probes (205a-c) from the set of monitoring probes for monitoring the portion of the network slice of the communication network ; wherein a further portion of the network slice is supported by a further communication network and wherein the communication interface of the network monitoring entity is configured to provide information about the set of monitoring probes to a communication interface of a corresponding further network monitoring entity of the further communication network . a communication interface configured to communicate with a plurality of sub-network monitoring units (204a-c), wherein each sub-network monitoring unit (204a-c) comprises at least one monitoring probe (205a-c) and each monitoring probe (205a-c) is configured to monitor at least one performance measure of the sub-portion (206a-c) of the portion of the network slice supported by the sub-network (203a-c), wherein the monitoring probes (205a-c) of the plurality of sub-network monitoring units (204a-c) define a set of monitoring probes ; and a processor configured to select one or more monitoring probes (205a-c) from the set of monitoring probes for monitoring the portion of the network slice of the communication network ; wherein a further portion of the network slice is supported by a further communication network and wherein the communication interface of the network monitoring entity is configured to provide information about the set of monitoring probes to a communication interface of a corresponding further network monitoring entity of the further communication network .
Method for filling a transport container with a fluid, where the fluid is conveyed through a purification device before the fluid is introduced into the transport container , where, in a fluid purification step, the fluid is conveyed through the purification device a number of times in a purification circuit and a contamination factor of an amount of fluid sample in the purification circuit is determined by means of a contamination measurement device , where the filling operation includes the single or multiple removal from the transport container of an amount of fluid that has already been introduced, and where a filling operation of the transport container with the fluid is only terminated after the contamination factor has fallen below a first threshold value, and which is specified so that the desired purity of the fluid introduced into the transport container is achieved and ensured sufficiently reliably.
A medical fibrous structure comprising: calcium carboxymethyl cellulose; and a chitosan compound, wherein at least one of the calcium carboxymethyl cellulose and the chitosan compound is in fibrous form. calcium carboxymethyl cellulose; and a chitosan compound, wherein at least one of the calcium carboxymethyl cellulose and the chitosan compound is in fibrous form.
A jaw crusher having a stationary crusher jaw and having a movable crusher jaw , between which a crushing chamber and a crushing gap are formed, wherein the movable crusher jaw can be driven by a crusher drive to generate a crushing motion, wherein an overload protection mechanism is assigned to one of the crusher jaws , preferably to the movable crusher jaw , wherein the overload protection mechanism comprises a control unit , which, in the event of an overload, causes the crusher jaws to move relative to one another in such a way that the crushing gap is enlarged, characterized in that an actuator unit is driven by means of the kinetic energy of a driven component of the jaw crusher, in particular of at least one flywheel of a crusher drive, of the movable crusher jaw and/or of the crusher drive driving the movable crusher jaw, in that at least one actuator is acted upon by the actuator unit using a transfer medium to effect the gap adjustment, in that the movable crusher jaw is coupled to a drive shaft of the crusher drive for rotation, in that the drive shaft has a deflector element , in particular an eccentric or a cam disk, and in that an actuation element of the actuator unit interacts with the deflector element to drive the actuator unit . wherein the movable crusher jaw can be driven by a crusher drive to generate a crushing motion, wherein an overload protection mechanism is assigned to one of the crusher jaws , preferably to the movable crusher jaw , wherein the overload protection mechanism comprises a control unit , which, in the event of an overload, causes the crusher jaws to move relative to one another in such a way that the crushing gap is enlarged, characterized in that an actuator unit is driven by means of the kinetic energy of a driven component of the jaw crusher, in particular of at least one flywheel of a crusher drive, of the movable crusher jaw and/or of the crusher drive driving the movable crusher jaw, in that at least one actuator is acted upon by the actuator unit using a transfer medium to effect the gap adjustment, in that the movable crusher jaw is coupled to a drive shaft of the crusher drive for rotation, in that the drive shaft has a deflector element , in particular an eccentric or a cam disk, and in that an actuation element of the actuator unit interacts with the deflector element to drive the actuator unit .
A thermal processing system , comprising: a plurality of laser energy sources (102A-D), each having an active q-switch; at least two combiners optically coupled to the laser energy sources, each combiner having a combining optic , the combining optic having a selecting surface ; an optical system to direct light from the plurality of laser energy sources to opposite sides of each selecting surface; a diagnostic module having an intensity profile detector that receives pulses from each combining optic; an energy detector that receives pulses from each combining optic; a pulse shaper with optical splitters configured to divide each pulse into a plurality of sub-pulses and mirror paths configured to send the sub-pulses along optical paths having different lengths, the pulse shaper optically coupled to the combiners ; and a homogenizer comprising at least two microlens arrays optically coupled to the pulse shaper. a plurality of laser energy sources (102A-D), each having an active q-switch; at least two combiners optically coupled to the laser energy sources, each combiner having a combining optic , the combining optic having a selecting surface ; an optical system to direct light from the plurality of laser energy sources to opposite sides of each selecting surface; a diagnostic module having an intensity profile detector that receives pulses from each combining optic; an energy detector that receives pulses from each combining optic; a pulse shaper with optical splitters configured to divide each pulse into a plurality of sub-pulses and mirror paths configured to send the sub-pulses along optical paths having different lengths, the pulse shaper optically coupled to the combiners ; and a homogenizer comprising at least two microlens arrays optically coupled to the pulse shaper.
A wheel assembly to be coupled to a hub of a vehicle, the wheel assembly comprising: an inner rim to be coupled to the hub of the vehicle; an outer rim surrounding the hub; a plurality of gas springs operatively coupled between said inner rim and said outer rim to provide a gas suspension for relative movement between said inner rim and said outer rim; an inner ring coupled to said inner rim characterised in that the wheel assembly further comprises a plurality of hydraulic dampers operatively coupled between said inner rim and said outer rim and wherein the inner ring defines a closeable gap with adjacent portions of said outer rim to define a mechanical stop to limit relative movement of said inner rim and said outer rim . an inner rim to be coupled to the hub of the vehicle; an outer rim surrounding the hub; a plurality of gas springs operatively coupled between said inner rim and said outer rim to provide a gas suspension for relative movement between said inner rim and said outer rim; an inner ring coupled to said inner rim characterised in that the wheel assembly further comprises a plurality of hydraulic dampers operatively coupled between said inner rim and said outer rim and wherein the inner ring defines a closeable gap with adjacent portions of said outer rim to define a mechanical stop to limit relative movement of said inner rim and said outer rim .
Method for shutting down at least one gas turbine , withat least one said gas turbine comprising a gas generator provided with rotary members and with a combustion chamber , with at least one said gas turbine comprising at least one power turbine , with at least one said gas turbine comprising a fuel circuit controlled by a computer , said computer being in communication with a selector , characterised in that the method comprises the following steps for shutting down at least one said gas turbine which is in operation and supplied with fuel by the fuel circuit : - generation of a command to shut down at least one gas turbine by means of the selector, - following said generation of the shutdown command, shutting off of the fuel circuit at the command of the computer , - following said generation of the shutdown command, when at least one said gas turbine is not idling prior to said shutoff or when said at least one gas turbine is idling at the time of said generation of the shutdown command for an operating time below a stored threshold, automatically setting said rotary members into rotation by means of an electric machine for a limited period. - generation of a command to shut down at least one gas turbine by means of the selector, - following said generation of the shutdown command, shutting off of the fuel circuit at the command of the computer , - following said generation of the shutdown command, when at least one said gas turbine is not idling prior to said shutoff or when said at least one gas turbine is idling at the time of said generation of the shutdown command for an operating time below a stored threshold, automatically setting said rotary members into rotation by means of an electric machine for a limited period.
An apparatus for forming a thin film comprising: a vacuum chamber in which film formation upon a surface of a container is to be performed in a vacuum state by using a heat generating element ; an vacuum evacuation device (VP1, VP2) that is arranged to vacuumize said vacuum chamber ; characterized by a relative shifting device that is arranged to, after vacuumization of said vacuum chamber has started, shift the container and the heat generating element relatively to each other within said vacuum chamber , wherein said vacuum chamber is divided into a first chamber arranged so that a container can be taken out or inserted thereinto, and a heat generating element protection chamber arranged so that the heat generating element is kept in a vacuum state, and a vacuum isolation device is provided linking said first chamber and said heat generating element protection chamber so as to be capable of intercepting communication between the heat generating element protection chamber and the first chamber , wherein said first chamber is a film deposition chamber, said relative shifting device being provided to shift the heat generating element between said heat generating element protection chamber and said first chamber . a vacuum chamber in which film formation upon a surface of a container is to be performed in a vacuum state by using a heat generating element ; an vacuum evacuation device (VP1, VP2) that is arranged to vacuumize said vacuum chamber ; characterized by a relative shifting device that is arranged to, after vacuumization of said vacuum chamber has started, shift the container and the heat generating element relatively to each other within said vacuum chamber , wherein said vacuum chamber is divided into a first chamber arranged so that a container can be taken out or inserted thereinto, and a heat generating element protection chamber arranged so that the heat generating element is kept in a vacuum state, and a vacuum isolation device is provided linking said first chamber and said heat generating element protection chamber so as to be capable of intercepting communication between the heat generating element protection chamber and the first chamber , wherein said first chamber is a film deposition chamber, said relative shifting device being provided to shift the heat generating element between said heat generating element protection chamber and said first chamber .