mhurhangee/ep-ind-claims huggingface dataset:
Method for carrying out autonomous braking in the case of a single-track motor vehicle, in which - the need for a vehicle deceleration is detected by means of an environment sensor system, - depending on that, rider-independent vehicle deceleration is initiated, - once the vehicle deceleration has been initiated, a rider readiness variable characterizing the readiness of the rider to control the vehicle deceleration manoeuvre is ascertained and - depending on the rider readiness variable, the temporal progression of the vehicle deceleration is continued (106, 107), characterized in that the rider readiness variable can assume three values, wherein - one of the three values signals a state of the rider in which the rider is ready for the vehicle deceleration manoeuvre, - another of the three values signals a neutral state of the rider, and - the remaining one of the three values signals a state of the rider in which the rider is not ready for the vehicle deceleration manoeuvre, and in that - in the case of a ready state of the rider, the autonomous braking is carried out with a planned setpoint braking force progression, - in the case of a neutral state of the rider, the autonomous braking is carried out with a braking force progression which has a lower deceleration and/or a less intense jolt in comparison with the planned setpoint braking force progression, - in the case of an unready state of the rider, the autonomous braking is either discontinued or is carried out with a braking force progression which has a lower deceleration and/or a less intense jolt in comparison with the braking force progression in the case of a neutral state of the rider. - the need for a vehicle deceleration is detected by means of an environment sensor system, - depending on that, rider-independent vehicle deceleration is initiated, - once the vehicle deceleration has been initiated, a rider readiness variable characterizing the readiness of the rider to control the vehicle deceleration manoeuvre is ascertained and - depending on the rider readiness variable, the temporal progression of the vehicle deceleration is continued (106, 107), - one of the three values signals a state of the rider in which the rider is ready for the vehicle deceleration manoeuvre, - another of the three values signals a neutral state of the rider, and - the remaining one of the three values signals a state of the rider in which the rider is not ready for the vehicle deceleration manoeuvre, and in that - in the case of a ready state of the rider, the autonomous braking is carried out with a planned setpoint braking force progression, - in the case of a neutral state of the rider, the autonomous braking is carried out with a braking force progression which has a lower deceleration and/or a less intense jolt in comparison with the planned setpoint braking force progression, - in the case of an unready state of the rider, the autonomous braking is either discontinued or is carried out with a braking force progression which has a lower deceleration and/or a less intense jolt in comparison with the braking force progression in the case of a neutral state of the rider.
Use of a bi-modal blend of a first polyalphaolefin base stock with a viscosity over 100 cSt KV 100 °C and a viscosity index over 100 and of a second PAO base stock with a viscosity at least 25 cSt KV 100 °C less than the viscosity of the first PAO base stock for improving the frictional properties of a constant velocity joint grease comprising a polyurea thickener in an amount of from 5 to less than 25 wt%, the first PAO being present in an amount of from 40 to less than 90 wt% of the grease and the second PAO being present in an amount of from 10 to less than 40 wt% of the grease.
A lubricant composition having a worked penetration of not less than 355 at 25°C comprising a lubricant base oil and a thickener; wherein the thickener comprises at least two types of thickeners including at least lithium stearate, characterized in that a content of lithium stearate is 0.5 mass% to 3 mass% based on the total of the lubricant composition.
Cooling device for a multi-layered laminate, - with a housing which at least partially surrounds a transport section along which the at least one laminate composite is moved, - with an inlet opening and outlet opening provided on the housing, and - with cooling devices (28, 29) arranged on both sides of the transport path in the housing, the cooling devices (28, 29) being located opposite one another in pairs, characterized in that the cooling devices (28, 29) are matched to one another so that they generate a common air flow, which crosses the transport path and forms a cooling path for the at least one laminate composite and leads a heat removal from the housing of the cooling device to the outside. - with a housing which at least partially surrounds a transport section along which the at least one laminate composite is moved, - with an inlet opening and outlet opening provided on the housing, and - with cooling devices (28, 29) arranged on both sides of the transport path in the housing, the cooling devices (28, 29) being located opposite one another in pairs, characterized in that the cooling devices (28, 29) are matched to one another so that they generate a common air flow, which crosses the transport path and forms a cooling path for the at least one laminate composite and leads a heat removal from the housing of the cooling device to the outside.
A method of forming a valve seat of a poppet valve comprising a stem and a valve head formed at one end thereof, said method comprising: forming a rounded cladded part on the valve head by welding; and forming a valve seat surface having a predetermined aperture angle on the cladded part, characterized in that the outer circumference of the valve head is cut into a predetermined dimension, the surface of the cladded part is cut to form a first smooth surface thereon, and said first smooth surface is forged by applying a uniform contact pressure at a temperature range possible for cold or warm forging while being less than the recrystallization temperature, thereby being plastically deformed. forming a rounded cladded part on the valve head by welding; and forming a valve seat surface having a predetermined aperture angle on the cladded part, characterized in that the outer circumference of the valve head is cut into a predetermined dimension, the surface of the cladded part is cut to form a first smooth surface thereon, and said first smooth surface is forged by applying a uniform contact pressure at a temperature range possible for cold or warm forging while being less than the recrystallization temperature, thereby being plastically deformed.
A method for producing a fluororesin film, which comprises extruding a fluororesin material containing a melt-processable fluororesin through an extrusion die, wherein the temperature of the extrusion die is from 305 to 355°C, and the average flow velocity v 0.95 of the fluororesin material as obtained by the following formula is at least 1×10 -4 m/sec.: v 0.95 = Q 0.95 / A 0.95 wherein when the distance x from the flow inlet of the extrusion die to the end portion of the manifold of the extrusion die, is set to be 1, Q 0.95 is the flow rate in m 3 /sec. of the fluororesin material flowing in the manifold at a position of x=0.95 from the flow inlet, wherein Q 0.95 can be obtained from the following formula: Q 0.95 = 1 / 2 × Q 0 × 1 − 0.95 wherein Q 0 is the flow rate in m 3 /sec. of the fluororesin material to be supplied to the flow inlet of the extrusion die, and A 0.95 is the cross-sectional area in m 2 of the manifold at a position of x=0.95 from the flow inlet, and the fluororesin is a fluororesin having adhesive functional groups selected from the group consisting of carbonyl group-containing groups, hydroxy groups, epoxy groups and isocyanate groups. the temperature of the extrusion die is from 305 to 355°C, and the average flow velocity v 0.95 of the fluororesin material as obtained by the following formula is at least 1×10 -4 m/sec.: v 0.95 = Q 0.95 / A 0.95 wherein when the distance x from the flow inlet of the extrusion die to the end portion of the manifold of the extrusion die, is set to be 1, Q 0.95 is the flow rate in m 3 /sec. of the fluororesin material flowing in the manifold at a position of x=0.95 from the flow inlet, wherein Q 0.95 can be obtained from the following formula: Q 0.95 = 1 / 2 × Q 0 × 1 − 0.95 wherein Q 0 is the flow rate in m 3 /sec. of the fluororesin material to be supplied to the flow inlet of the extrusion die, and A 0.95 is the cross-sectional area in m 2 of the manifold at a position of x=0.95 from the flow inlet, and the fluororesin is a fluororesin having adhesive functional groups selected from the group consisting of carbonyl group-containing groups, hydroxy groups, epoxy groups and isocyanate groups.
A method for manufacturing a metal matrix ceramic composite, the method comprising the following steps: (i) heating ceramic granules, having a diameter between 1mm and 15mm, a multilayer structure and a volume that is within a range of 10% - 80% of the metal matrix ceramic composite, and maintaining a heating temperature of the ceramic granules between 400°C and 1400°C according to type of matrix metals and ceramics used; (ii) putting the ceramic granules into a cavity of a squeeze-casting mold; (iii) determining whether to lay metallic or non-metallic wire meshes and a number of layers of wire meshes to be laid between the ceramic granules, and then performing compaction; (iv) pouring molten metal matrix into a cavity of the mold; (v) pressurizing and maintaining a pressure, based on material of the metal matrix, type of ceramic granules, and a desired product structure and specification; (vi) adjusting the pressure between 50MPa and 200MPa, and maintaining the pressure for a time between 30s and 5min; (vii) after maintaining the pressure, removing the metal matrix ceramic composite out from the mold. (i) heating ceramic granules, having a diameter between 1mm and 15mm, a multilayer structure and a volume that is within a range of 10% - 80% of the metal matrix ceramic composite, and maintaining a heating temperature of the ceramic granules between 400°C and 1400°C according to type of matrix metals and ceramics used; (ii) putting the ceramic granules into a cavity of a squeeze-casting mold; (iii) determining whether to lay metallic or non-metallic wire meshes and a number of layers of wire meshes to be laid between the ceramic granules, and then performing compaction; (iv) pouring molten metal matrix into a cavity of the mold; (v) pressurizing and maintaining a pressure, based on material of the metal matrix, type of ceramic granules, and a desired product structure and specification; (vi) adjusting the pressure between 50MPa and 200MPa, and maintaining the pressure for a time between 30s and 5min; (vii) after maintaining the pressure, removing the metal matrix ceramic composite out from the mold.
A ramjet turbine, comprising a housing, a shaft rotatably mounted on the housing, at least one disk, which is attached to the shaft in a rotationally fixed manner and which divides the housing into a plurality of chambers comprising at least one precompression chamber and at least one exhaust chamber, and at least one pilot tube, which is connected to the at least one disk and in which a combustion of a fed fuel takes place and which leads from the at least one precompression chamber into the at least one exhaust chamber and which is arranged in such a way that a ram pressure builds up in the at least one pilot tube in response to the rotation of the at least one disk and that a thrust created by means of gas emitted from the at least one pilot tube into the at least one exhaust chamber effects a rotation of the at least one disk, characterized in that at least one exhaust turbocharger is provided, which conveys a gas under pressure into the at least one precompression chamber by utilizing an exhaust gas escaping from the at least one exhaust chamber.
A system, comprising: a first communication circuit configured to communicate data over a first data port using a first communication protocol; a second communication circuit configured to communicate data over a second data port using a second communication protocol that processes read and write requests in an order that the read and write requests are received; and a bridge circuit (120, 310) configured to communicate data between the first data port of the first communication circuit and the second data port of the second communication circuit, wherein the bridge circuit (120, 310) is configured to communicate all non-posted writes to the second communication circuit via a buffer circuit (122, 328) and communicate posted writes to the second communication circuit without buffering via a communication path that bypasses the buffer circuit. a first communication circuit configured to communicate data over a first data port using a first communication protocol; a second communication circuit configured to communicate data over a second data port using a second communication protocol that processes read and write requests in an order that the read and write requests are received; and a bridge circuit (120, 310) configured to communicate data between the first data port of the first communication circuit and the second data port of the second communication circuit, wherein the bridge circuit (120, 310) is configured to communicate all non-posted writes to the second communication circuit via a buffer circuit (122, 328) and communicate posted writes to the second communication circuit without buffering via a communication path that bypasses the buffer circuit.
Sensor network having sensors for measuring at least one measurement variable, each of these sensors having a measurement variable pick-up for converting the measurement variable into an electrical signal, a converter for converting the electrical signal into measurement data, a first communication interface for transmitting the measurement data and further data according to a first protocol, and a second communication interface for transmitting the measurement data and further data according to a second protocol, and a data interchange unit for interchanging data between the converter, the first communication interface and the second communication interface, characterized in that the sensors are connected to one another via their first communication interfaces, and are connected to a control room using a control room interface which is formed by the second communication interface of one of the sensors, and in that the sensors are designed to measure different measurement variables.
Pneumatic striking mechanism comprising: a free piston movable along a striking axis, an impact surface limiting the movement of the free piston along the striking axis in the impact direction, an exciter piston limiting the movement of the free piston along the striking axis in the opposite direction to the impact direction, a pneumatic chamber between the free piston and the exciter piston, and a drive for moving the exciter piston periodically along the striking axis with a stroke, the free piston being excited into a periodic movement between impact against the impact surface and a minimum distance from the exciter piston, characterised in that the stroke is selected as a function of the maximum length of the pneumatic chamber in such a manner that the periodic movement of the free piston on the path from impact against the impact surface to the minimum distance from the exciter piton temporarily has a speed of zero. a free piston movable along a striking axis, an impact surface limiting the movement of the free piston along the striking axis in the impact direction, an exciter piston limiting the movement of the free piston along the striking axis in the opposite direction to the impact direction, a pneumatic chamber between the free piston and the exciter piston, and a drive for moving the exciter piston periodically along the striking axis with a stroke, the free piston being excited into a periodic movement between impact against the impact surface and a minimum distance from the exciter piston, characterised in that the stroke is selected as a function of the maximum length of the pneumatic chamber in such a manner that the periodic movement of the free piston on the path from impact against the impact surface to the minimum distance from the exciter piton temporarily has a speed of zero.
A method for preparing a powder based on oxide(s) comprising uranium, at least one minor actinide and possibly plutonium comprising the following steps: a) a step of adding at least one monomer to an aqueous solution comprising nitrates ions and comprising uranium, at least one minor actinide and possibly plutonium, the monomer(s) comprising at least one ethylenic group and at least one polar group able to form hydrogen bonds; b) a step of obtaining a gel trapping said aqueous solution by polymerising the monomer(s) added in a); c) a step of obtaining a xerogel comprising uranium, at least one minor actinide and possibly plutonium nitrates by dehydrating the gel obtained in b); d) a step of obtaining said powder by thermally treating the xerogel obtained in c). a) a step of adding at least one monomer to an aqueous solution comprising nitrates ions and comprising uranium, at least one minor actinide and possibly plutonium, the monomer(s) comprising at least one ethylenic group and at least one polar group able to form hydrogen bonds; b) a step of obtaining a gel trapping said aqueous solution by polymerising the monomer(s) added in a); c) a step of obtaining a xerogel comprising uranium, at least one minor actinide and possibly plutonium nitrates by dehydrating the gel obtained in b); d) a step of obtaining said powder by thermally treating the xerogel obtained in c).
A luggage article comprising: a lower shell section having a plurality of walls including side walls (142, 144, 146, 148) and an inside bottom wall together defining a lower cavity; an upper shell section having a plurality of walls including side walls (152, 154, 156, 158) and an upper wall together defining an upper cavity, the upper and lower cavities together defining an interior cavity when closed; and a divider attached to the side walls to mount the divider in the interior cavity spaced from the bottom wall; the sidewalls including a plurality of discrete attachment locations at least some of which are positioned vertically above the bottom wall relative to an opening at a top of the lower cavity; the divider comprises a plurality of attachment fittings adapted to releasably and selectively engage a corresponding discrete attachment location to releasably and selectively connect the divider to at least one side wall at the discrete attachment locations; the discrete attachment locations being defined by receiver housings including one or more apertures, each operable to receive an attachment fitting with one or more radially extending tabs. a lower shell section having a plurality of walls including side walls (142, 144, 146, 148) and an inside bottom wall together defining a lower cavity; an upper shell section having a plurality of walls including side walls (152, 154, 156, 158) and an upper wall together defining an upper cavity, the upper and lower cavities together defining an interior cavity when closed; and a divider attached to the side walls to mount the divider in the interior cavity spaced from the bottom wall; the sidewalls including a plurality of discrete attachment locations at least some of which are positioned vertically above the bottom wall relative to an opening at a top of the lower cavity; the divider comprises a plurality of attachment fittings adapted to releasably and selectively engage a corresponding discrete attachment location to releasably and selectively connect the divider to at least one side wall at the discrete attachment locations; the discrete attachment locations being defined by receiver housings including one or more apertures, each operable to receive an attachment fitting with one or more radially extending tabs.
Charging base for wireless iron comprising an iron soleplate, said charging base including a lower surface intended to rest on a support surface, such as an ironing board, a base whereon the soleplate of the iron must rest during inactive ironing phases to enable an energy exchange between the charging base and the iron, and a stopper at an end of the base, the stopper comprising an electrical connector, characterised in that the base is bordered on at least two sides by an access ramp (21A, 21B) descending in the direction of the lower surface and enabling the transfer from the iron, from the support surface to the base by making it slide along the access ramp (21A, 21B).
Microscope having an optical system that defines an illumination beam path and comprises the following components: - a light source (22, 23, 24, 25, 26) providing a light distribution, - a microscope objective with a pupil plane and a focus, - a scan optical unit for generating a pupil plane (PE') conjugate to the pupil plane of the microscope objective, - at least two variably adjustable beam deflection units (30A, 30B) and - a concave mirror for imaging a respective point of the first and the second beam deflection unit (30A, 30B) onto one another, wherein the optical system images at least one point of the light distribution and a respective point of the focus onto one another, wherein a first intermediate image lies optically between the microscope objective and the scan optical unit, wherein the second beam deflection unit is arranged in the conjugate pupil plane (PE'), wherein the concave mirror and the first beam deflection unit and the second beam deflection unit are arranged such that the illumination beam path is reflected exactly once at the concave mirror and a first distortion, caused by the concave mirror, and a second distortion, caused by the first and the second beam deflection unit (30A, 30B), of the imaged representation at least partially compensate for one another, wherein the concave mirror and the first beam deflection unit and the second beam deflection unit are arranged for compensation of the first and second distortions such that a plane angle of reflection of an optical axis of the illumination beam path on the first beam deflection unit in a zero position of the first and the second beam deflection unit (30A, 30B), in which the latter steer the optical axis of the stationary illumination beam path coming from the light source coaxially to the optical axis of the microscope objective into the microscope objective, is twice as large as a plane angle of reflection of the optical axis at the concave mirror. - a light source (22, 23, 24, 25, 26) providing a light distribution, - a microscope objective with a pupil plane and a focus, - a scan optical unit for generating a pupil plane (PE') conjugate to the pupil plane of the microscope objective, - at least two variably adjustable beam deflection units (30A, 30B) and - a concave mirror for imaging a respective point of the first and the second beam deflection unit (30A, 30B) onto one another,