mhurhangee/patent-ind-claim-en huggingface dataset:
A method for navigating a commute implemented on a mobile device , comprising: setting two pre-defined locations based on user input; activating a navigation function on the mobile device ; determining a current location of the mobile device ; comparing the current location of the mobile device and each of the two pre-defined locations to determine, if the current location is within a distance threshold to any of the two pre-defined locations; selecting a destination from the two pre-defined locations, characterised in that the selecting the destination comprises: in response to determining that the current location of the mobile device is within a distance threshold to one of the two pre-defined locations , automatically selecting the other of the two pre-defined locations as the destination, and in response to determining that the current location of the mobile device is within a distance threshold to neither of the two pre-defined locations , selecting the destination from the two pre-defined locations based on a time criteria; and producing a navigation output using the selected destination. setting two pre-defined locations based on user input; activating a navigation function on the mobile device ; determining a current location of the mobile device ; comparing the current location of the mobile device and each of the two pre-defined locations to determine, if the current location is within a distance threshold to any of the two pre-defined locations; selecting a destination from the two pre-defined locations, characterised in that the selecting the destination comprises: in response to determining that the current location of the mobile device is within a distance threshold to one of the two pre-defined locations , automatically selecting the other of the two pre-defined locations as the destination, and in response to determining that the current location of the mobile device is within a distance threshold to neither of the two pre-defined locations , selecting the destination from the two pre-defined locations based on a time criteria; and in response to determining that the current location of the mobile device is within a distance threshold to one of the two pre-defined locations , automatically selecting the other of the two pre-defined locations as the destination, and in response to determining that the current location of the mobile device is within a distance threshold to neither of the two pre-defined locations , selecting the destination from the two pre-defined locations based on a time criteria; and producing a navigation output using the selected destination.
Cleaning apparatus for dispensing a gaseous medium (M1), in particular compressed air (DL), and/or a media mixture (MG) consisting of the gaseous medium (M1) and a liquid medium (M2), in particular water, preferably as a media sequence (MS), comprising: - a mixing element having - a first feed connection in a main medium supply line (MZ1) for supplying the gaseous medium (M1) for passage through the mixing element , and - second feed connection in a branching medium supply line (MZ2) for supplying the liquid medium (M2) transversely for passage into the mixing element , and - a dispensing connection for dispensing the gaseous medium (M1) and/or the media mixture (MG), - a pressure chamber on the main medium supply line (MZ1), - a switching valve is arranged in the main medium supply line (MZ1), which is designed to prevent a passage of the gaseous medium (M1) through the mixing element in a first switching state (S1) and to allow said passage in a second switching state (S2), wherein - the switching valve is arranged in the main medium supply line (MZ1) downstream of and/or on the pressure chamber , and the switching valve is formed as a 3/2-way valve or as a double check valve, characterized in that the switching valve is formed as a bypass valve having a bypass connection for bypassing the mixing element , wherein the bypass connection is directly connected to the dispensing connection . - a mixing element having - a first feed connection in a main medium supply line (MZ1) for supplying the gaseous medium (M1) for passage through the mixing element , and - second feed connection in a branching medium supply line (MZ2) for supplying the liquid medium (M2) transversely for passage into the mixing element , and - a dispensing connection for dispensing the gaseous medium (M1) and/or the media mixture (MG), - a pressure chamber on the main medium supply line (MZ1), - a switching valve is arranged in the main medium supply line (MZ1), which is designed to prevent a passage of the gaseous medium (M1) through the mixing element in a first switching state (S1) and to allow said passage in a second switching state (S2), wherein - the switching valve is arranged in the main medium supply line (MZ1) downstream of and/or on the pressure chamber , and the switching valve is formed as a 3/2-way valve or as a double check valve,
A chuck comprising: a dust-proof mechanism for preventing the entry of foreign matter into the chuck , the dust-proof mechanism comprising: a fluid supply source ; an inner space (A) that is provided in the chuck and through which a supply fluid supplied from the fluid supply source can pass as a pressurized fluid; a discharge clearance that is provided in the chuck and through which the pressurized fluid can be discharged to outside of the chuck from the inner space (A); wherein the discharge clearance is a gap between a guide groove provided in a chuck main body of the chuck , which groove extends in a radial direction, and a master jaw inserted in the guide groove ; wherein the gap is open on a surface of a side where a claw is attached, in the gap between the guide groove and the master jaw ; the said dust-proof mechanism further comprising a second sealing member that covers the gap between the master jaw and the guide groove from outside in the radial direction. a dust-proof mechanism for preventing the entry of foreign matter into the chuck , the dust-proof mechanism comprising: a fluid supply source ; an inner space (A) that is provided in the chuck and through which a supply fluid supplied from the fluid supply source can pass as a pressurized fluid; a discharge clearance that is provided in the chuck and through which the pressurized fluid can be discharged to outside of the chuck from the inner space (A); wherein the discharge clearance is a gap between a guide groove provided in a chuck main body of the chuck , which groove extends in a radial direction, and a master jaw inserted in the guide groove ; wherein the gap is open on a surface of a side where a claw is attached, in the gap between the guide groove and the master jaw ; the said dust-proof mechanism further comprising a second sealing member that covers the gap between the master jaw and the guide groove from outside in the radial direction. a fluid supply source ; an inner space (A) that is provided in the chuck and through which a supply fluid supplied from the fluid supply source can pass as a pressurized fluid; a discharge clearance that is provided in the chuck and through which the pressurized fluid can be discharged to outside of the chuck from the inner space (A); wherein the discharge clearance is a gap between a guide groove provided in a chuck main body of the chuck , which groove extends in a radial direction, and a master jaw inserted in the guide groove ; wherein the gap is open on a surface of a side where a claw is attached, in the gap between the guide groove and the master jaw ; the said dust-proof mechanism further comprising a second sealing member that covers the gap between the master jaw and the guide groove from outside in the radial direction.
A hydraulic and pneumatic control circuit for a turbojet, the circuit comprising: - a main hydraulic line having an oil/fuel heat exchanger with a function of transferring heat from the oil flowing in an oil circuit of the turbojet to the fuel flowing in the main hydraulic line; - a first hydraulic line for feeding fuel to a combustion chamber of the turbojet; - a second hydraulic line for feeding fuel to one or more hydraulic actuators serving to control variable geometry equipment of the turbojet, each hydraulic actuator being fed with fuel via an electrohydraulic servovalve , the first and second hydraulic lines being connected to each other upstream from the combustion chamber and the hydraulic actuators in order to form the main hydraulic line ; and - a pneumatic line for feeding air to a pneumatic control member for bleed valves of a compressor of the turbojet and a blade tip clearance control valve of a turbine of the turbojet; characterized in that for heating the fuel flowing in the second hydraulic line without needing the oil/fuel heat exchanger of the main line, the circuit further comprises a fuel/air heat exchanger positioned on the second hydraulic line upstream from the hydraulic servovalve and on the pneumatic line upstream from the pneumatic control member in order to transfer heat from the air flowing in the pneumatic line to the fuel flowing in the second hydraulic line. - a main hydraulic line having an oil/fuel heat exchanger with a function of transferring heat from the oil flowing in an oil circuit of the turbojet to the fuel flowing in the main hydraulic line; - a first hydraulic line for feeding fuel to a combustion chamber of the turbojet; - a second hydraulic line for feeding fuel to one or more hydraulic actuators serving to control variable geometry equipment of the turbojet, each hydraulic actuator being fed with fuel via an electrohydraulic servovalve , the first and second hydraulic lines being connected to each other upstream from the combustion chamber and the hydraulic actuators in order to form the main hydraulic line ; and - a pneumatic line for feeding air to a pneumatic control member for bleed valves of a compressor of the turbojet and a blade tip clearance control valve of a turbine of the turbojet; characterized in that for heating the fuel flowing in the second hydraulic line without needing the oil/fuel heat exchanger of the main line, the circuit further comprises a fuel/air heat exchanger positioned on the second hydraulic line upstream from the hydraulic servovalve and on the pneumatic line upstream from the pneumatic control member in order to transfer heat from the air flowing in the pneumatic line to the fuel flowing in the second hydraulic line.
Pump for an aeronautical module , the pump comprising a body having at least one substantially flat outer surface , the pump including an electrical connector , a hydraulic connector and a mechanical connector for electrical, hydraulic and mechanical connection of the pump to the aeronautical module , wherein the connectors are all arranged on its flat surface , and wherein the hydraulic connector is comprised of at least one fluid inlet port for the entry of fluid into the body and at least one fluid outlet port for the exit of fluid from the body .
A radio receiver , comprising: a radio frequency "RF" subsystem ; an analog to digital converter to receive input from the RF subsystem and to digitize a spectrum; a digital subsystem configured to: process the digitized spectrum into data according to at least two overlapping channel plans; the digital subsystem comprising a decoder bank comprising at least two decoders configured to: receive the data from a plurality of overlapping filters associated with each of a plurality of channels of the at least two overlapping channel plans, wherein the plurality of overlapping filters are distributed over the spectrum based at least in part on a possible frequency error of an incoming signal; and simultaneously decode the data of the at least two overlapping channel plans according to at least two modulation schemes. a radio frequency "RF" subsystem ; an analog to digital converter to receive input from the RF subsystem and to digitize a spectrum; a digital subsystem configured to: process the digitized spectrum into data according to at least two overlapping channel plans; the digital subsystem comprising a decoder bank comprising at least two decoders configured to: receive the data from a plurality of overlapping filters associated with each of a plurality of channels of the at least two overlapping channel plans, wherein the plurality of overlapping filters are distributed over the spectrum based at least in part on a possible frequency error of an incoming signal; and simultaneously decode the data of the at least two overlapping channel plans according to at least two modulation schemes. process the digitized spectrum into data according to at least two overlapping channel plans; the digital subsystem comprising a decoder bank comprising at least two decoders configured to: receive the data from a plurality of overlapping filters associated with each of a plurality of channels of the at least two overlapping channel plans, wherein the plurality of overlapping filters are distributed over the spectrum based at least in part on a possible frequency error of an incoming signal; and simultaneously decode the data of the at least two overlapping channel plans according to at least two modulation schemes. receive the data from a plurality of overlapping filters associated with each of a plurality of channels of the at least two overlapping channel plans, wherein the plurality of overlapping filters are distributed over the spectrum based at least in part on a possible frequency error of an incoming signal; and simultaneously decode the data of the at least two overlapping channel plans according to at least two modulation schemes.
A process for preparing C 2 to C 3 olefins, comprising: introducing a feed stream into a reactor, wherein the feed stream comprises hydrogen gas and carbon monoxide gas, such that a volumetric ratio of hydrogen to carbon monoxide ranges from greater than 0.5:1 to less than 5:1; and contacting the feed stream with a bifunctional catalyst in the reactor, wherein the bifunctional catalyst comprises: Cr/Zn oxide methanol synthesis component having a Cr to Zn molar ratio from greater than 1.0:1 to less than 2.15:1, and a SAPO-34 silicoaluminophosphate microporous crystalline material, wherein the reactor operates at reaction conditions comprising: (a) a reactor temperature ranging from 350 °C to 450 °C; and (b) a pressure ranging from 1.0 MPa (10 bar) to 6.0 MPa (60 bar), and wherein the process has a cumulative productivity of C 2 to C 3 olefins greater than 15 kg C 2 to C 3 olefins/kg catalyst, and wherein the methanol synthesis component is calcined at a temperature from 375 °C to 425 °C. introducing a feed stream into a reactor, wherein the feed stream comprises hydrogen gas and carbon monoxide gas, such that a volumetric ratio of hydrogen to carbon monoxide ranges from greater than 0.5:1 to less than 5:1; and contacting the feed stream with a bifunctional catalyst in the reactor, wherein the bifunctional catalyst comprises: Cr/Zn oxide methanol synthesis component having a Cr to Zn molar ratio from greater than 1.0:1 to less than 2.15:1, and a SAPO-34 silicoaluminophosphate microporous crystalline material, wherein the reactor operates at reaction conditions comprising: (a) a reactor temperature ranging from 350 °C to 450 °C; and (b) a pressure ranging from 1.0 MPa (10 bar) to 6.0 MPa (60 bar), and (a) a reactor temperature ranging from 350 °C to 450 °C; and (b) a pressure ranging from 1.0 MPa (10 bar) to 6.0 MPa (60 bar), and wherein the process has a cumulative productivity of C 2 to C 3 olefins greater than 15 kg C 2 to C 3 olefins/kg catalyst, and wherein the methanol synthesis component is calcined at a temperature from 375 °C to 425 °C.
A method of imaging a marine 3D survey area, comprising: a) obtaining or developing a geology model of a marine survey area; b) determining a bin size and orientation; c) wherein that determination of bin size is based on a smallest feature to be mapped and a shape of said marine geology model; d) determining a compressed seismig imaging source and receiver station and sampling design, CSI design, using compressive sensing concepts and based on the geology model and the determined bin size or orientation; characterized by determining a stability of said CSI design and if unstable modifying said bin size or orientation and re-determining said stability iteratively to produce a stable CSI design; e) establishing a set of sampling rules or criteria for coverage of said marine survey area to assure that appropriate data is recorded so said stable CSI design can be properly reconstructed; f) acquiring 3D seismic data traces over said marine survey area using said stable CSI design until said rules or criteria are met, wherein wind and current are not compensated for but allowed to direct vessel travel; g) reconstructing a wavefield and regularizing the traces using the appropriate reconstruction techniques to produce seismic data; and h) processing the seismic data and imaging the survey area. a) obtaining or developing a geology model of a marine survey area; b) determining a bin size and orientation; c) wherein that determination of bin size is based on a smallest feature to be mapped and a shape of said marine geology model; d) determining a compressed seismig imaging source and receiver station and sampling design, CSI design, using compressive sensing concepts and based on the geology model and the determined bin size or orientation; characterized by determining a stability of said CSI design and if unstable modifying said bin size or orientation and re-determining said stability iteratively to produce a stable CSI design; e) establishing a set of sampling rules or criteria for coverage of said marine survey area to assure that appropriate data is recorded so said stable CSI design can be properly reconstructed; f) acquiring 3D seismic data traces over said marine survey area using said stable CSI design until said rules or criteria are met, wherein wind and current are not compensated for but allowed to direct vessel travel; g) reconstructing a wavefield and regularizing the traces using the appropriate reconstruction techniques to produce seismic data; and h) processing the seismic data and imaging the survey area.
Method for determining at least one amount of energy (E) of an individual vehicle, which one of several vehicles has taken from a power supply network outside of the vehicle by way of a contact wire, characterised in that the amount of energy (E) is determined by measurements on the power supply network side.
A heat storage system (HSS) by phase change material (PCM) comprising: - a tank for containing a PCM , - a circulation system dipped in the tank , for circulating a heat transfer fluid coming from an outer circulation network of the heat transfer fluid, - a device for controlling crystallisation of the PCM comprising a bubbling device configured to form gas bubbles , in the lower part of the tank , in the PCM , the heat storage system being characterised in that the device for controlling crystallisation additionally comprises a seeding device configured to form solid PCM seeds in the tank of PCM . - a tank for containing a PCM , - a circulation system dipped in the tank , for circulating a heat transfer fluid coming from an outer circulation network of the heat transfer fluid, - a device for controlling crystallisation of the PCM comprising a bubbling device configured to form gas bubbles , in the lower part of the tank , in the PCM , the heat storage system being characterised in that the device for controlling crystallisation additionally comprises a seeding device configured to form solid PCM seeds in the tank of PCM .
A body with a form embossing and a motor vehicle lamp arranged thereon, which is arranged in the form embossing , in which at least one ball stud with stud head and at least one fastening hole are arranged, wherein the motor vehicle lamp has a least one semi-cylindrical mounting , in which a resilient securing element is arranged, wherein - the stud head of the ball stud is arranged between a spherical depression formed on the inner surface of the mounting and a spherical embossing formed on the resilient securing element , - the resilient securing element consists of a base plate with clips and a resilient securing tab , on which a spherical embossing is formed, - grooves are formed on the mounting , in which the base plate of the resilient securing element is arranged, and - the grooves of the mounting have latching openings , in which the clips arranged on the base plate snap. - the stud head of the ball stud is arranged between a spherical depression formed on the inner surface of the mounting and a spherical embossing formed on the resilient securing element , - the resilient securing element consists of a base plate with clips and a resilient securing tab , on which a spherical embossing is formed, - grooves are formed on the mounting , in which the base plate of the resilient securing element is arranged, and - the grooves of the mounting have latching openings , in which the clips arranged on the base plate snap.
A client system comprising at least one hardware processor configured to execute a routine dispatcher , a bytecode translation virtual machine , and a behavioral assessment engine , wherein: the routine dispatcher is configured, in response to detecting an occurrence of a trigger event, to select an anti-malware bytecode routine for execution from a plurality of anti-malware bytecode routines, the anti-malware bytecode routine selected according to the trigger event, wherein the occurrence of the trigger event is caused by a monitored process executing within the client system; the bytecode translation virtual machine is configured, in response to the routine dispatcher selecting the anti-malware bytecode routine, to execute the anti-malware bytecode routine to determine whether the occurrence of the trigger event is indicative of malware, wherein executing the anti-malware bytecode routine comprises: translating a set of bytecode instructions of the anti-malware bytecode routine into a sequence of native processor instructions, and executing the sequence of native processor instructions; and the behavioral assessment engine is configured to determine whether the client system comprises malware according to a result of the bytecode translation virtual machine executing the anti-malware bytecode routine. the routine dispatcher is configured, in response to detecting an occurrence of a trigger event, to select an anti-malware bytecode routine for execution from a plurality of anti-malware bytecode routines, the anti-malware bytecode routine selected according to the trigger event, wherein the occurrence of the trigger event is caused by a monitored process executing within the client system; the bytecode translation virtual machine is configured, in response to the routine dispatcher selecting the anti-malware bytecode routine, to execute the anti-malware bytecode routine to determine whether the occurrence of the trigger event is indicative of malware, wherein executing the anti-malware bytecode routine comprises: translating a set of bytecode instructions of the anti-malware bytecode routine into a sequence of native processor instructions, and executing the sequence of native processor instructions; and translating a set of bytecode instructions of the anti-malware bytecode routine into a sequence of native processor instructions, and executing the sequence of native processor instructions; and the behavioral assessment engine is configured to determine whether the client system comprises malware according to a result of the bytecode translation virtual machine executing the anti-malware bytecode routine.