mhurhangee/patent-ind-claim-en huggingface dataset:
A pump including - a stator , - a rotor slidably and rotatably mounted at least partially in the stator, the rotor comprising a first axial extension having a first diameter (D1) and a second axial extension having a second diameter (D2) greater than the first diameter, - a first valve (V1) formed by a first valve seal mounted on the stator around the first axial extension, in conjunction with a first channel in the rotor that is configured to allow liquid communication across the first valve seal when the first valve is in an open position, - a second valve (V2) formed by a second valve seal mounted on the stator around the second axial extension, in conjunction with a second channel in the rotor that is configured to allow liquid communication across the second valve seal when the second valve is in an open position, - a pump chamber formed between the rotor and stator and between the first valve seal and second valve seal, and - a pump chamber seal circumscribing the rotor second axial extension and separating the pump chamber from an external environment, characterized in that the stator further comprises a dead-zone seal section surrounding a dead-zone volume formed between the rotor second axial extension and the stator wherein the dead-zone seal section comprises axially extending portions connected to upper and lower radial portions to form a closed sealing circuit. - a stator , - a rotor slidably and rotatably mounted at least partially in the stator, the rotor comprising a first axial extension having a first diameter (D1) and a second axial extension having a second diameter (D2) greater than the first diameter, - a first valve (V1) formed by a first valve seal mounted on the stator around the first axial extension, in conjunction with a first channel in the rotor that is configured to allow liquid communication across the first valve seal when the first valve is in an open position, - a second valve (V2) formed by a second valve seal mounted on the stator around the second axial extension, in conjunction with a second channel in the rotor that is configured to allow liquid communication across the second valve seal when the second valve is in an open position, - a pump chamber formed between the rotor and stator and between the first valve seal and second valve seal, and - a pump chamber seal circumscribing the rotor second axial extension and separating the pump chamber from an external environment, characterized in that the stator further comprises a dead-zone seal section surrounding a dead-zone volume formed between the rotor second axial extension and the stator wherein the dead-zone seal section comprises axially extending portions connected to upper and lower radial portions to form a closed sealing circuit.
A service steering and control function, SSF, including: means for receiving a service steering and control, SSC, rule, the SSC rule to include an SSC rule identifier, a service dataflow, SDF, identifier, and one or more service enabler, SE, identifiers; means for identifying a service dataflow, SDF, based on the SDF identifier within an operator network ; means for routing the SDF through one or more service enablers in a (S)Gi-LAN based on the one or more SE identifiers, wherein routing the SDF through one or more service enablers includes causing the SDF to be transmitted through a chain of a plurality of service enablers in an order defined by the SSC rule; characterised by further including means for collecting dynamic load status information from individual service enablers of the one or more service enablers; and means for transmitting the dynamic load status information to a policy and charging rules function, PCRF . means for receiving a service steering and control, SSC, rule, the SSC rule to include an SSC rule identifier, a service dataflow, SDF, identifier, and one or more service enabler, SE, identifiers; means for identifying a service dataflow, SDF, based on the SDF identifier within an operator network ; means for routing the SDF through one or more service enablers in a (S)Gi-LAN based on the one or more SE identifiers, wherein routing the SDF through one or more service enablers includes causing the SDF to be transmitted through a chain of a plurality of service enablers in an order defined by the SSC rule; characterised by further including means for collecting dynamic load status information from individual service enablers of the one or more service enablers; and means for transmitting the dynamic load status information to a policy and charging rules function, PCRF .
An ultra high strength steel plate having high formability and hole expandability, the ultra high strength steel plate consisting of, by wt%, carbon (C): 0.04% to 0.17%, silicon (Si): 2% or less, manganese (Mn): 4% to 10%, phosphorous (P): 0.05% or less excluding 0%, sulfur (S): 0.02% or less excluding 0%, aluminum (Al): 0.5% or less excluding 0%, nitrogen (N): 0.02% or less excluding 0%, and a balance of iron (Fe) and inevitable impurities, the steel plate further optionally comprising at least one selected from: titanium (Ti): 0.1% or less excluding 0%, niobium (Nb): 0.1% or less excluding 0%, vanadium (V): 0.2% or less excluding 0%, and molybdenum (Mo): 0.5% or less excluding 0%; or at least one selected from zirconium (Zr): 0.001% to 0.1%, and tungsten (W): 0.001% to 0.5%; or at least one selected from nickel (Ni): 1% or less excluding 0%, copper (Cu): 0.5% or less excluding 0%, and chromium (Cr): 1% or less excluding 0%; or at least one selected from antimony (Sb): 0.04% or less excluding 0%, calcium (Ca): 0.01% or less excluding 0%, and boron (B): 0.01% or less excluding 0%; wherein carbon (C) and manganese (Mn) satisfy Formula 1 below, and the ultra high strength steel plate has a microstructure comprising retained austenite in a volume fraction of 20% or greater and annealed martensite in a volume fraction of 50% or greater, wherein the ultra high strength steel plate has a tensile strength of 980 MPa or greater, and a yield ratio of 0.6 or greater, a product of tensile strength and elongation within a range of 25,000 MPa% or greater, and a hole expansion ratio of 15% or greater, C + Mn / 25 ≤ 0.46 titanium (Ti): 0.1% or less excluding 0%, niobium (Nb): 0.1% or less excluding 0%, vanadium (V): 0.2% or less excluding 0%, and molybdenum (Mo): 0.5% or less excluding 0%; or at least one selected from zirconium (Zr): 0.001% to 0.1%, and tungsten (W): 0.001% to 0.5%; or at least one selected from nickel (Ni): 1% or less excluding 0%, copper (Cu): 0.5% or less excluding 0%, and chromium (Cr): 1% or less excluding 0%; or at least one selected from antimony (Sb): 0.04% or less excluding 0%, calcium (Ca): 0.01% or less excluding 0%, and boron (B): 0.01% or less excluding 0%; wherein carbon (C) and manganese (Mn) satisfy Formula 1 below, and the ultra high strength steel plate has a microstructure comprising retained austenite in a volume fraction of 20% or greater and annealed martensite in a volume fraction of 50% or greater,
A device comprising a multitude of server modules , wherein said server modules are removable, are substantially plate shaped and extend parallel to each other, wherein each one of said server modules is connected to cable passages of a first switch by first data cables and to cable passages of a second switch by second data cables , wherein said first and second switches are removable, are shaped substantially as a flat box and extend parallel to and adjacent each other, and said first switch extends perpendicular to and adjacent an edge of said server modules , wherein said cable passages of said first switch extend in a first array and the cable passages of said second switch extend in a second array, wherein said first and second arrays extend parallel to each other, and wherein said first array of cable passages extends near an edge of said first switch and near said edge of said server modules , and wherein said second array of cable passages is mounted on a bracket which is mounted on said second switch , said bracket extending at a distance from the second switch and from said first array. wherein said server modules are removable, are substantially plate shaped and extend parallel to each other, wherein each one of said server modules is connected to cable passages of a first switch by first data cables and to cable passages of a second switch by second data cables , wherein said first and second switches are removable, are shaped substantially as a flat box and extend parallel to and adjacent each other, and said first switch extends perpendicular to and adjacent an edge of said server modules , wherein said cable passages of said first switch extend in a first array and the cable passages of said second switch extend in a second array, wherein said first and second arrays extend parallel to each other, and wherein said first array of cable passages extends near an edge of said first switch and near said edge of said server modules , and wherein said second array of cable passages is mounted on a bracket which is mounted on said second switch , said bracket extending at a distance from the second switch and from said first array.
An agricultural vehicle, in particular a tractor , comprising a drive train including an internal combustion engine which is operable to drive ground-engaging means of the vehicle by way of a hydrostatic-mechanical power-split transmission with a continuously variable transmission ratio (i), wherein the drive train can be put into an operating mode "neutral" in which a power transfer between the internal combustion engine and the ground-engaging means is interrupted and can be put into an operating mode "active standstill" in which power coming into the power-split transmission from the internal combustion engine is used to hold an output shaft of the power-split transmission at a zero rotary speed, characterised by means which in dependence on at least one operating criterion (v, Z B , Z S ) of the vehicle switch the drive train from the operating mode "neutral" into the operating mode "active standstill", wherein the drive train is switched from the operating mode "neutral" into the "active standstill" when at least the following conditions are fulfilled at the same time: a) the internal combustion engine is running, and b) the drive train is in the operating mode "neutral", c) in accordance with the state (ZB) detected by sensor means of the actuating device the brake is activated and/or d) the speed (v) detected by sensor means of the vehicle and/or a travel distance covered by the vehicle is not equal to zero or is greater than a defined limit value and/or e) in accordance with a state (ZS) detected by sensor means the driver's seat of the vehicle is unoccupied. a) the internal combustion engine is running, and b) the drive train is in the operating mode "neutral", c) in accordance with the state (ZB) detected by sensor means of the actuating device the brake is activated and/or d) the speed (v) detected by sensor means of the vehicle and/or a travel distance covered by the vehicle is not equal to zero or is greater than a defined limit value and/or e) in accordance with a state (ZS) detected by sensor means the driver's seat of the vehicle is unoccupied.
Core drill bit comprising: a tubular shaft , a mounting platform provided on a proximal end of the tubular shaft for mounting the core drill bit on a power tool , an annular cutting section provided with abrasive cutting segments arranged at a distal end of the tubular shaft , a transponder , characterized in that a slit in the tubular shaft the slit forming a slit antenna for the transponder . a tubular shaft , a mounting platform provided on a proximal end of the tubular shaft for mounting the core drill bit on a power tool , an annular cutting section provided with abrasive cutting segments arranged at a distal end of the tubular shaft , a transponder , characterized in that a slit in the tubular shaft the slit forming a slit antenna for the transponder .
A method of controlling a deflagration combustion process in a pistonless combustor , the combustion process consisting of repeating working cycles divided to equally long time units from 0 to 1000, and the method comprising steps of: opening a first input valve and introducing air into the pistonless combustor thereby scavenging combustion products of the previous cycle; opening a second input valve after opening the first input valve and introducing air into the combustor thereby initiating a flow pattern having a first flow component within the combustor, the second input valve being opened at earliest 450 time units before a reference point and closed at the reference point; opening a fifth input valve after opening the second input valve and introducing air into the pistonless combustor in a nonparallel angle in relation to the input through the second input valve thereby creating a second flow component to the flow pattern within the pistonless combustor for increasing speed of combustion propagation, the fifth input valve being opened at earliest 170 time units before a reference point and closed at latest 100 time units after the reference point; introducing fuel from any input valve opening after the opening of the first input valve , wherein the fuel is mixed into the air creating a fuel-air mixture flowing within the flow pattern ; and igniting the fuel-air mixture within the pistonless combustor thereby increasing pressure within the pistonless combustor, where the ignition is performed at earliest 70 units before the reference point and at latest 60 units after the reference point, wherein the reference point is a closing event of the second input valve . opening a first input valve and introducing air into the pistonless combustor thereby scavenging combustion products of the previous cycle; opening a second input valve after opening the first input valve and introducing air into the combustor thereby initiating a flow pattern having a first flow component within the combustor, the second input valve being opened at earliest 450 time units before a reference point and closed at the reference point; opening a fifth input valve after opening the second input valve and introducing air into the pistonless combustor in a nonparallel angle in relation to the input through the second input valve thereby creating a second flow component to the flow pattern within the pistonless combustor for increasing speed of combustion propagation, the fifth input valve being opened at earliest 170 time units before a reference point and closed at latest 100 time units after the reference point; introducing fuel from any input valve opening after the opening of the first input valve , wherein the fuel is mixed into the air creating a fuel-air mixture flowing within the flow pattern ; and igniting the fuel-air mixture within the pistonless combustor thereby increasing pressure within the pistonless combustor, where the ignition is performed at earliest 70 units before the reference point and at latest 60 units after the reference point, wherein the reference point is a closing event of the second input valve .
A method of determining state information in a vacuum device having a gas flow unit, namely a valve, for controlling and/or providing a gas flow, wherein the method comprises the steps: measuring a first temperature measurement value in the region of the gas flow by means of a temperature sensor in a first activity state of the gas flow unit; setting the gas flow unit into a second activity state that is associated with a lower or a higher gas flow than the first activity state; measuring a second temperature measurement value in the region of the gas flow; determining a measured deviation of the second temperature measurement value from the first temperature measurement value; comparing the measured deviation with an expected deviation; and determining the state information based on the comparison, wherein the state information comprises information on an operability of the gas flow unit and/or of the temperature sensor. measuring a first temperature measurement value in the region of the gas flow by means of a temperature sensor in a first activity state of the gas flow unit; setting the gas flow unit into a second activity state that is associated with a lower or a higher gas flow than the first activity state; measuring a second temperature measurement value in the region of the gas flow; determining a measured deviation of the second temperature measurement value from the first temperature measurement value; comparing the measured deviation with an expected deviation; and determining the state information based on the comparison, wherein the state information comprises information on an operability of the gas flow unit and/or of the temperature sensor.
A clamp for clamping flexible tubing , comprising: a first element having a first surface with a first corner ; a second element having a second surface with a second corner ; and a flexible element coupled to the first and second elements , the flexible element configured such that: when the clamp is not actuated, the first and second surfaces are disposed at an angle to each other; when the first element is rotated about the flexible element toward the second element , with the flexible tubing between the first and second elements , the first and second corners are displaced toward each other and cooperate to sealingly compress a first length of the flexible tubing between the first and second corners ; and characterized in that when the first element is further rotated about the flexible element toward the second element , the first element rotates with respect to the second element such that (i) the first and second corners separate from each other, and (ii) the first and second surfaces cooperate to sealingly compress a second length of the flexible tubing between the first and second surfaces . a first element having a first surface with a first corner ; a second element having a second surface with a second corner ; and a flexible element coupled to the first and second elements , the flexible element configured such that: when the clamp is not actuated, the first and second surfaces are disposed at an angle to each other; when the first element is rotated about the flexible element toward the second element , with the flexible tubing between the first and second elements , the first and second corners are displaced toward each other and cooperate to sealingly compress a first length of the flexible tubing between the first and second corners ; and characterized in that when the first element is further rotated about the flexible element toward the second element , the first element rotates with respect to the second element such that (i) the first and second corners separate from each other, and (ii) the first and second surfaces cooperate to sealingly compress a second length of the flexible tubing between the first and second surfaces . when the clamp is not actuated, the first and second surfaces are disposed at an angle to each other; when the first element is rotated about the flexible element toward the second element , with the flexible tubing between the first and second elements , the first and second corners are displaced toward each other and cooperate to sealingly compress a first length of the flexible tubing between the first and second corners ; and characterized in that when the first element is further rotated about the flexible element toward the second element , the first element rotates with respect to the second element such that (i) the first and second corners separate from each other, and (ii) the first and second surfaces cooperate to sealingly compress a second length of the flexible tubing between the first and second surfaces .
A method of controlling a gas turbine engine having a propulsive fan and an engine core , the method including: measuring a first engine performance parameter indicative of the output of the fan ; measuring a second engine performance parameter indicative of the output of the engine core ; determining a fan thrust generated by the fan based on a first power setting parameter and the first engine performance parameter; determining a core thrust generated by the engine core based on a second power setting parameter and the second engine performance parameter; determining a total thrust based on the fan thrust and core thrust ; and controlling the engine based on the determined total thrust , wherein the total thrust comprises the fan thrust and the engine core thrust . measuring a first engine performance parameter indicative of the output of the fan ; measuring a second engine performance parameter indicative of the output of the engine core ; determining a fan thrust generated by the fan based on a first power setting parameter and the first engine performance parameter; determining a core thrust generated by the engine core based on a second power setting parameter and the second engine performance parameter; determining a total thrust based on the fan thrust and core thrust ; and controlling the engine based on the determined total thrust , wherein the total thrust comprises the fan thrust and the engine core thrust . wherein the total thrust comprises the fan thrust and the engine core thrust .
- Motor vehicle including - a base having a front and a rear part, - a cradle of engine, - a deflector underfloor fixed both under the front part of the said underfloor and under the said cradle , the said deflector underfloor consisting of a front and a rear portion, the front portion being arranged next to the said cradle ; the front and rear portion of the deflector underfloor extending according to horizontal plans vertical axis so that the front portion extends in a plane greater than the plane in which the rear portion extends, the vehicle being characterized in that it includes at least one means of reinforcement having a rear end fixed to the front part of the said underlay and a front end fixed to that cradle , the underfloor deflector being configured to partially cover the said means of reinforcement ) and having at least one opening at the front of it arranged to be crossed by the front end of a means of reinforcement . - a base having a front and a rear part, - a cradle of engine, - a deflector underfloor fixed both under the front part of the said underfloor and under the said cradle , the said deflector underfloor consisting of a front and a rear portion, the front portion being arranged next to the said cradle ; the front and rear portion of the deflector underfloor extending according to horizontal plans vertical axis so that the front portion extends in a plane greater than the plane in which the rear portion extends, the vehicle being characterized in that it includes at least one means of reinforcement having a rear end fixed to the front part of the said underlay and a front end fixed to that cradle , the underfloor deflector being configured to partially cover the said means of reinforcement ) and having at least one opening at the front of it arranged to be crossed by the front end of a means of reinforcement .