mhurhangee/ep-ind-claims huggingface dataset:
Household dishwasher having a self-cleaning filter system, which has a rotatably mounted filter element for filtering washing liquor, a drive facility which is designed to rotate the filter element about an axis of rotation, and a cleaning nozzle, which is designed to clean different subregions (26, 27) of the filter element with the aid of a water jet depending on the rotational position (α) of the filter element, wherein the household dishwasher has a sump, in which the filter element is provided in a rotatably mounted manner, wherein the axis of rotation of the filter element is arranged horizontally and wherein in a washing operation of the household appliance, a first subregion of the filter element is passed through by washing liquor and a second subregion of the filter element is arranged above a surface of the washing liquor, and wherein the cleaning nozzle is designed to clean the second subregion and wherein the household dishwasher has a draw-down zone upstream of the filter element, wherein the draw-down zone is formed by a housing section of the sump, the base of which lies below a lower edge of the filter element, and wherein the draw-down zone is designed to receive particles cleaned off from the second subregion of the filter element with the aid of the water jet, wherein a height level of the draw-down zone lies below the lower edge of the filter element, and wherein a lye pump is provided, which has its suction connection adjoining the draw-down zone.
Method for implementing welcoming illumination with the headlamps (5, 5') of a motor vehicle, which each have a pivotable lighting module (8, 8'), the form of which imitate human eyes at least in the illuminated state, comprising the following steps: a) defining an authorization zone having a specifiable circumcircle around the motor vehicle; b) registering whether at least one authorized user is located within the authorization zone; c) starting a first illumination sequence of the welcoming illumination, in which the lighting modules (8, 8') pivot, with respect to a vehicle coordinate system, out of a downwards rest position into a horizontally aligned driving position; d) determining the position of the authorized user within the authorization zone with respect to the vehicle coordinate system; wherein the method is characterized in that it includes the following step: e) starting a second illumination sequence of the welcoming illumination, in which the lighting modules (8, 8') initially pivot in the direction of the registered authorized user and then pivot back into the driving position that is aligned horizontally and to the front. a) defining an authorization zone having a specifiable circumcircle around the motor vehicle; b) registering whether at least one authorized user is located within the authorization zone; c) starting a first illumination sequence of the welcoming illumination, in which the lighting modules (8, 8') pivot, with respect to a vehicle coordinate system, out of a downwards rest position into a horizontally aligned driving position; d) determining the position of the authorized user within the authorization zone with respect to the vehicle coordinate system; wherein the method is characterized in that it includes the following step: e) starting a second illumination sequence of the welcoming illumination, in which the lighting modules (8, 8') initially pivot in the direction of the registered authorized user and then pivot back into the driving position that is aligned horizontally and to the front.
A method for guiding an aircraft during a final approach towards a runway, the method comprising: receiving a geographic position of the aircraft; receiving a geographic position of a runway threshold of the runway; receiving a runway azimuth of the runway; computing a distance from the aircraft to the runway threshold utilizing the geographic position of the aircraft and the geographic position of the runway threshold; computing a bearing to the runway threshold utilizing the geographic position of the aircraft and the geographic position of the runway threshold; projecting the distance from the aircraft to the runway threshold into an along runway component and a cross runway component utilizing the runway azimuth of the runway and the bearing to the runway threshold, wherein the along runway component is the product of the distance from the aircraft to the runway threshold and the cosine of the difference between the bearing to the runway threshold and the runway azimuth; determining a distance from the runway threshold to a localizer transmitter; computing a distance from the aircraft to the localizer transmitter by adding the distance from the runway threshold to the localizer transmitter to the along runway component of the projected distance from the aircraft to the runway threshold; converting an angular localizer deviation into a rectilinear localizer deviation utilizing, in part, the distance from the aircraft to the localizer transmitter; and providing the rectilinear localizer deviation to a guidance system for guiding the aircraft during the final approach towards the runway. receiving a geographic position of the aircraft; receiving a geographic position of a runway threshold of the runway; receiving a runway azimuth of the runway; computing a distance from the aircraft to the runway threshold utilizing the geographic position of the aircraft and the geographic position of the runway threshold; computing a bearing to the runway threshold utilizing the geographic position of the aircraft and the geographic position of the runway threshold; projecting the distance from the aircraft to the runway threshold into an along runway component and a cross runway component utilizing the runway azimuth of the runway and the bearing to the runway threshold, wherein the along runway component is the product of the distance from the aircraft to the runway threshold and the cosine of the difference between the bearing to the runway threshold and the runway azimuth; determining a distance from the runway threshold to a localizer transmitter; computing a distance from the aircraft to the localizer transmitter by adding the distance from the runway threshold to the localizer transmitter to the along runway component of the projected distance from the aircraft to the runway threshold; converting an angular localizer deviation into a rectilinear localizer deviation utilizing, in part, the distance from the aircraft to the localizer transmitter; and providing the rectilinear localizer deviation to a guidance system for guiding the aircraft during the final approach towards the runway.
A method for sharing an uplink port among network slices, comprising: creating logical uplink ports for network slices; establishing a one-to-one logical mapping between the logical uplink ports and access AC interfaces of a VXLAN in a shared slice; and enabling the VXLAN in the shared slice, and transmitting service messages for the network slices through a physical uplink port for the shared slice; characterized in that, establishing a one-to-one logical mapping between the logical uplink ports and access AC interfaces of a VXLAN in a shared slice comprises: creating logical ports on the shared slice; and corresponding the logical ports with the logical uplink ports on a one-to-one basis, the logical ports being the access AC ports of the VXLAN; wherein enabling the VXLAN in the shared slice comprises: creating a VXLAN tunnel on the shared slice, the VXLAN tunnel comprising source IPs, destination IPs, and VNIs; dividing different VTEPs according to the source IPs, the destination IPs, and the VNIs; and carrying communications of the VTEPs on the physical uplink port. creating logical uplink ports for network slices; establishing a one-to-one logical mapping between the logical uplink ports and access AC interfaces of a VXLAN in a shared slice; and enabling the VXLAN in the shared slice, and transmitting service messages for the network slices through a physical uplink port for the shared slice; characterized in that, establishing a one-to-one logical mapping between the logical uplink ports and access AC interfaces of a VXLAN in a shared slice comprises: creating logical ports on the shared slice; and corresponding the logical ports with the logical uplink ports on a one-to-one basis, the logical ports being the access AC ports of the VXLAN; wherein enabling the VXLAN in the shared slice comprises: creating a VXLAN tunnel on the shared slice, the VXLAN tunnel comprising source IPs, destination IPs, and VNIs; dividing different VTEPs according to the source IPs, the destination IPs, and the VNIs; and carrying communications of the VTEPs on the physical uplink port. creating logical ports on the shared slice; and corresponding the logical ports with the logical uplink ports on a one-to-one basis, the logical ports being the access AC ports of the VXLAN; wherein enabling the VXLAN in the shared slice comprises: creating a VXLAN tunnel on the shared slice, the VXLAN tunnel comprising source IPs, destination IPs, and VNIs; dividing different VTEPs according to the source IPs, the destination IPs, and the VNIs; and carrying communications of the VTEPs on the physical uplink port. creating a VXLAN tunnel on the shared slice, the VXLAN tunnel comprising source IPs, destination IPs, and VNIs; dividing different VTEPs according to the source IPs, the destination IPs, and the VNIs; and carrying communications of the VTEPs on the physical uplink port.
A fluid handling apparatus for ejecting fluid into a tank and draining fluid from the tank, the fluid handling apparatus comprises: a fluid duct for draining fluid from the tank or for supplying fluid to the tank, wherein the fluid duct is configured for being in fluid communication with a tank opening at a bottom of the tank; a fluid inlet pipe for supplying fluid to the tank, wherein the fluid inlet pipe is extending at least partly through the fluid duct and configured to extend through the tank opening into the tank; a rotary fluid ejection device being in fluid communication with the fluid inlet pipe; and a rotary drive shaft extending at least partly inside the fluid inlet pipe, wherein the rotary drive shaft is rotatably connected to the rotary fluid ejection device, characterized in that the fluid handling apparatus is suitable for introduction and/or circulation of solid hops material into a fluid content of the tank. a fluid duct for draining fluid from the tank or for supplying fluid to the tank, wherein the fluid duct is configured for being in fluid communication with a tank opening at a bottom of the tank; a fluid inlet pipe for supplying fluid to the tank, wherein the fluid inlet pipe is extending at least partly through the fluid duct and configured to extend through the tank opening into the tank; a rotary fluid ejection device being in fluid communication with the fluid inlet pipe; and a rotary drive shaft extending at least partly inside the fluid inlet pipe, wherein the rotary drive shaft is rotatably connected to the rotary fluid ejection device, characterized in that the fluid handling apparatus is suitable for introduction and/or circulation of solid hops material into a fluid content of the tank.
An aircraft engine fuel system, comprising: a pump, including an inlet and an outlet, from which pressurized output is produced; a pressure regulating valve comprising a valve case which forms a valve inlet and a valve outlet and which defines a valve interior, and a piston translatable within the valve interior and integrally coupled to a drive shaft, the valve being disposed downstream from the pump outlet to receive and to direct the pump output flow toward the engine and to provide a leak tight seal when the pump is not operating, and wherein the valve outlet is fluidly coupled to the pump inlet via an inlet pressure sensing circuit; a sensor configured to sense the mechanical response of the drive shaft of the piston, and to issue a signal reflective of the axial translation state of the piston at engine startup and maximum fuel flow conditions; and an engine controller, operably coupled to the pump and the sensor, which is receptive of the signal and which is configured to compare the valve positions at engine startup and maximum fuel flow conditions to determine decreased pump capacity due to wear or degradation of the engine performance; and to modify performance models of the pump and engine accordingly. a pump, including an inlet and an outlet, from which pressurized output is produced; a pressure regulating valve comprising a valve case which forms a valve inlet and a valve outlet and which defines a valve interior, and a piston translatable within the valve interior and integrally coupled to a drive shaft, the valve being disposed downstream from the pump outlet to receive and to direct the pump output flow toward the engine and to provide a leak tight seal when the pump is not operating, and wherein the valve outlet is fluidly coupled to the pump inlet via an inlet pressure sensing circuit; a sensor configured to sense the mechanical response of the drive shaft of the piston, and to issue a signal reflective of the axial translation state of the piston at engine startup and maximum fuel flow conditions; and an engine controller, operably coupled to the pump and the sensor, which is receptive of the signal and which is configured to compare the valve positions at engine startup and maximum fuel flow conditions to determine decreased pump capacity due to wear or degradation of the engine performance; and to modify performance models of the pump and engine accordingly.
A worm reducer (12a; 12b; 12c) for a steering comprising: a housing having a wheel housing portion, and a worm housing portion (22; 22a) arranged in a skew position with respect to the wheel housing portion and having a middle section in an axial direction of the worm housing portion (22; 22a) which is open to the wheel housing portion; a worm wheel having wheel teeth on an outer circumferential surface thereof, and supported inside the wheel housing portion so as to be able to rotate freely; a worm having worm teeth which engage with the wheel teeth on an outer circumferential surface thereof, and supported inside the worm housing portion (22; 22a) so as to be able to rotate freely; a support bearing having an inner ring which is externally fitted to a tip end portion of the worm and an outer ring which is arranged coaxially with the inner ring around the inner ring; an elastic biasing means (81; 81a; 81b) elastically biasing the outer ring toward a side of the worm wheel either directly or through a member other than the outer ring; and characterized in that the worm reducer (12a; 12b; 12c) further comprises an elastic holding means (82; 82a) elastically holding the outer ring from both sides in a second direction orthogonal to a first direction which is a biasing direction by the elastic biasing means (81; 81a; 81b) and to a center axis of the worm housing portion (22; 22a) either directly or through a member other than the outer ring. a housing having a wheel housing portion, and a worm housing portion (22; 22a) arranged in a skew position with respect to the wheel housing portion and having a middle section in an axial direction of the worm housing portion (22; 22a) which is open to the wheel housing portion; a worm wheel having wheel teeth on an outer circumferential surface thereof, and supported inside the wheel housing portion so as to be able to rotate freely; a worm having worm teeth which engage with the wheel teeth on an outer circumferential surface thereof, and supported inside the worm housing portion (22; 22a) so as to be able to rotate freely; a support bearing having an inner ring which is externally fitted to a tip end portion of the worm and an outer ring which is arranged coaxially with the inner ring around the inner ring; an elastic biasing means (81; 81a; 81b) elastically biasing the outer ring toward a side of the worm wheel either directly or through a member other than the outer ring; and
A zoom lens consisting of: (i) a first lens unit having negative refractive power, a second lens unit having positive refractive power, and a third lens unit having negative refractive power in order from an object side to an image side, or (ii) a first lens unit having negative refractive power, a second lens unit having positive refractive power, a third lens unit having negative refractive power, and a fourth lens unit in order from an object side to an image side, wherein a distance between the first lens unit and the second lens unit and a distance between the second lens unit and the third lens unit is arranged to change during at least one of zooming and focusing, wherein the first lens unit is arranged to move during zooming, wherein the first lens unit includes a first negative lens disposed closest to the object side and at least one positive lens, wherein lenses included in the second lens unit all have positive refractive power, wherein there are two or fewer lenses included in the third lens unit, wherein the third lens unit is arranged to move toward the image side during focusing from infinity to close range, and characterized in that the following inequalities are satisfied: 1.40 < Nd _ G 1 < 1.80, − 1.00 ≦ SF _ B 3 n < 0.50, and 18 < vd _ B3n < 36, where Nd_G1 is a refractive index of the first negative lens, SF_B3n is a shape factor of a negative lens having strongest negative refractive power among the third lens unit and vd_B3n is an Abbe number of the negative lens having strongest refractive power among negative lenses included in the third lens unit. (i) a first lens unit having negative refractive power, a second lens unit having positive refractive power, and a third lens unit having negative refractive power in order from an object side to an image side, or (ii) a first lens unit having negative refractive power, a second lens unit having positive refractive power, a third lens unit having negative refractive power, and a fourth lens unit in order from an object side to an image side, wherein a distance between the first lens unit and the second lens unit and a distance between the second lens unit and the third lens unit is arranged to change during at least one of zooming and focusing, wherein the first lens unit is arranged to move during zooming, wherein the first lens unit includes a first negative lens disposed closest to the object side and at least one positive lens, wherein lenses included in the second lens unit all have positive refractive power, wherein there are two or fewer lenses included in the third lens unit, wherein the third lens unit is arranged to move toward the image side during focusing from infinity to close range, and characterized in that the following inequalities are satisfied: 1.40 < Nd _ G 1 < 1.80, − 1.00 ≦ SF _ B 3 n < 0.50, and 18 < vd _ B3n < 36, where Nd_G1 is a refractive index of the first negative lens, SF_B3n is a shape factor of a negative lens having strongest negative refractive power among the third lens unit and vd_B3n is an Abbe number of the negative lens having strongest refractive power among negative lenses included in the third lens unit.
A cover of a draft shield of a precision balance, having a carrier frame, on which first retaining elements and/or guide rails for a front panel and/or at least one side panel are provided, and having a covering element which can be pivoted between a retaining position and a release position about a mounting provided along a periphery, wherein second retaining elements (72, 74) are provided on the periphery located opposite the mounting on the cover, which are designed such that they fix the covering element on the periphery of the carrier frame, wherein at least one section of the covering element can be displaced in the direction of the mounting, in order to release the second retaining elements (72, 74).
A seeder having a seed store, a discharge apparatus (4, 5, 6, 7, 8, 10, 11, 13) for discharging seed from the seed store, and a regulation apparatus for regulating the seed discharge effected by the discharge apparatus in dependence on at least one predefinable input parameter, wherein the regulation apparatus has an adaptive regulator for an adaptive determination of at least one control variable for the discharge apparatus, characterized in that the discharge apparatus has a metering apparatus connectable to the seed store, a distributor connected downstream of the metering apparatus, a plurality of discharge elements that are connectable to the distributor, and a separation and/or homogenization device arranged between the distributor and the discharge elements, with an image detection apparatus being provided for detecting the seed delivery that has a first camera that observes the infeed of the separation and/or homogenization apparatus and that has a second camera that observes the outlet of the separation and homogenization apparatus.
A compound for use in the prevention and/or reduction of ischemia-related damage in a subject, wherein said compound is a statin,wherein said compound is to be administered to said subject by intravenous administration after the onset of ischemia, but prior to reperfusion, wherein the compound is to be administered as early as possible after the onset of ischemia.
Vane pump for a compressible fluid, comprising a housing with a pump chamber in which a rotor with at least one slide element is arranged rotatably, the housing having a bottom plate, a stroke ring, a thrust washer with at least one fluid inlet opening and at least one fluid outlet opening (24, 26), a cover element and means for sound insulation (52, 60, 62), wherein at least one suction port, at least one fluid channel (52, 56, 58) and at least one pressure port (32, 66, 68) are provided such that fluid can be guided through the suction port, the pump chamber, the at least one fluid channel (52, 56, 58) to the pressure port (32, 66, 68), wherein the cover element comprises the at least one suction port, the at least one fluid channel (52, 56, 58), the at least one pressure port (32, 66, 68) and the means for sound insulation (52, 60, 62), characterized in that at least one check valve (40, 42, 64) extends into the fluid channel (52, 56, 58), which operatively connected with the at least one fluid outlet opening (24, 26) in the thrust washer and the means for sound insulation (52, 60, 62) in the fluid channel (52, 56, 58), wherein the thrust washer forms a valve seat for the check valve (40, 42, 44).