mhurhangee/patent-ind-claim-en huggingface dataset:
A milli- or micro-fluidic conduit device comprising - a capillary pump , comprising a solid sorbent enclosed in an enclosure, and having an inlet and an outlet, - a fluid conduit operationally connected to the inlet of the capillary pump , - a gas-permeable liquid-sealed unit with a vent hole wherein said unit is gas-permeable to the outside through the vent hole , the unit being engaged with the fluid conduit at a predetermined location, and - an actuator unit upstream of the fluid conduit, characterized in that the fluid conduit comprises at least three interconnected zones, the at least three interconnected zones comprising: i) a first conduit zone prefilled with a first volume of trigger liquid, upstream of the unit with the vent hole and downstream of the actuator unit , ii) a third conduit zone with a further volume, upstream of the capillary pump but downstream of the unit with the vent hole , and iii) a second conduit zone pre-filled with a working liquid before actuation of the actuator unit, the actuator unit being for moving the working liquid so as to contact the solid sorbent, the second conduit zone being positioned downstream the unit with the vent hole , between the first conduit zone and the third conduit zone and functionally connected to both, and directly connected to the first conduit zone , wherein the first volume is proportionally larger than or equal to the further volume of the third conduit zone . - a capillary pump , comprising a solid sorbent enclosed in an enclosure, and having an inlet and an outlet, - a fluid conduit operationally connected to the inlet of the capillary pump , - a gas-permeable liquid-sealed unit with a vent hole wherein said unit is gas-permeable to the outside through the vent hole , the unit being engaged with the fluid conduit at a predetermined location, and - an actuator unit upstream of the fluid conduit, i) a first conduit zone prefilled with a first volume of trigger liquid, upstream of the unit with the vent hole and downstream of the actuator unit , ii) a third conduit zone with a further volume, upstream of the capillary pump but downstream of the unit with the vent hole , and iii) a second conduit zone pre-filled with a working liquid before actuation of the actuator unit, the actuator unit being for moving the working liquid so as to contact the solid sorbent, the second conduit zone being positioned downstream the unit with the vent hole , between the first conduit zone and the third conduit zone and functionally connected to both, and directly connected to the first conduit zone ,
A vehicle with an emergency egress system, comprising: a rope compartment , wherein the rope compartment is located on or near a vertical plane along a longitudinal axis of the vehicle, within reach of one or more occupant seats of a plurality of occupant seats ; a rope , wherein at least a portion of the rope is stored within the rope compartment and is securely tethered to the vehicle; and a rope compartment cover to secure the rope in the rope compartment ; characterised in that the rope comprises a fluorescent material and the rope compartment comprises a light source that is installed within the rope compartment that charges the fluorescent material within the rope . a rope compartment , wherein the rope compartment is located on or near a vertical plane along a longitudinal axis of the vehicle, within reach of one or more occupant seats of a plurality of occupant seats ; a rope , wherein at least a portion of the rope is stored within the rope compartment and is securely tethered to the vehicle; and a rope compartment cover to secure the rope in the rope compartment ; characterised in that the rope comprises a fluorescent material and the rope compartment comprises a light source that is installed within the rope compartment that charges the fluorescent material within the rope .
Apparatus for straightening metal products comprising: - at least one rotation shaft on which at least one straightening roll is installed in a selectively removable manner; - a first structure provided with at least a first support member configured to hold and support a first end of the rotation shaft ; - a second structure provided with at least a second support member configured to selectively support and hold a second end , opposite the first end , of the rotation shaft ; - a movement member configured to move the second structure toward/away from the first structure and to allow the installation or removal of the straightening roll from the rotation shaft , characterized in that said second structure is provided with gripping means , able to be selectively activated to take and hold the straightening roll on the second structure at least during the movement of the second structure . - at least one rotation shaft on which at least one straightening roll is installed in a selectively removable manner; - a first structure provided with at least a first support member configured to hold and support a first end of the rotation shaft ; - a second structure provided with at least a second support member configured to selectively support and hold a second end , opposite the first end , of the rotation shaft ; - a movement member configured to move the second structure toward/away from the first structure and to allow the installation or removal of the straightening roll from the rotation shaft ,
A method comprising: performing a clear channel assessment, CCA, by an initiating wireless device (101; 201) to gain a transmitting opportunity, TXOP, wherein the initiating device, STA1, detects channel busy due to other interfering radio signals in a wireless network; obtaining a spatially orthogonal, SO, condition with the other interfering radio signals (311; 312); and transmitting radio signals to a target device, AP1, using a beamformed antenna pattern upon satisfying the SO condition, wherein the SO condition is detected when the initiating wireless device (101; 201) does not receive the other interfering radio signals (311; 312) using the beamformed antenna pattern during an observation period, characterized in that the SO condition is obtained via the beamformed antenna pattern that is derived from channel knowledge of the other interfering radio signals (311; 312). performing a clear channel assessment, CCA, by an initiating wireless device (101; 201) to gain a transmitting opportunity, TXOP, wherein the initiating device, STA1, detects channel busy due to other interfering radio signals in a wireless network; obtaining a spatially orthogonal, SO, condition with the other interfering radio signals (311; 312); and transmitting radio signals to a target device, AP1, using a beamformed antenna pattern upon satisfying the SO condition, wherein the SO condition is detected when the initiating wireless device (101; 201) does not receive the other interfering radio signals (311; 312) using the beamformed antenna pattern during an observation period, characterized in that the SO condition is obtained via the beamformed antenna pattern that is derived from channel knowledge of the other interfering radio signals (311; 312).
A parachute assembly for fastening to a person, wherein the parachute assembly comprises an automatic deployment mechanism, a main parachute and a spare parachute, - having a pressure sensor for sensing a pressure (p) in the surroundings of the parachute assembly and/or a mechanism for determining the altitude, - having a control device for determining a deployment signal for the main parachute or spare parachute, wherein the deployment signal is generated when a current altitude (h avg ) calculated in the control device is less than a predefined minimum altitude (h min ) and when a current falling velocity (Δp/Δt) calculated in the control device is greater than a predefined falling velocity limit (A), - having an initiation device for releasing the main parachute or spare parachute as a function of the deployment signal of the control device , characterized in that the control device is provided with means such that the predefined falling velocity limit (A) is modified when a state of the parachute assembly changes as a result of an opening of the main parachute, wherein the predefined falling velocity limit (A) is increased to a further falling velocity limit (B). - having a pressure sensor for sensing a pressure (p) in the surroundings of the parachute assembly and/or a mechanism for determining the altitude, - having a control device for determining a deployment signal for the main parachute or spare parachute, wherein the deployment signal is generated when a current altitude (h avg ) calculated in the control device is less than a predefined minimum altitude (h min ) and when a current falling velocity (Δp/Δt) calculated in the control device is greater than a predefined falling velocity limit (A), - having an initiation device for releasing the main parachute or spare parachute as a function of the deployment signal of the control device ,
A method of managing memory on a computing device, comprising: initializing a hypervisor , a security monitor , and a high-level operating system, HLOS, ; disabling the hypervisor after initialization; monitoring for a signal from the security monitor to start a sandbox session; enabling the hypervisor when the signal is received to start the sandbox session; implementing access control while the hypervisor is enabled; and allocating memory by the HLOS during the sandbox session such that one or more intermediate physical addresses in the HLOS's intermediate physical address space are mapped to one or more corresponding physical addresses in a physical address space . initializing a hypervisor , a security monitor , and a high-level operating system, HLOS, ; disabling the hypervisor after initialization; monitoring for a signal from the security monitor to start a sandbox session; enabling the hypervisor when the signal is received to start the sandbox session; implementing access control while the hypervisor is enabled; and allocating memory by the HLOS during the sandbox session such that one or more intermediate physical addresses in the HLOS's intermediate physical address space are mapped to one or more corresponding physical addresses in a physical address space .
A method for capacity expansion of an energy storage system, applied to a controller in the energy storage system, the energy storage system further comprising one or more first energy storage devices, a charge/discharge power converter, and one or more second energy storage devices to be added into the energy storage system, wherein the one or more second energy storage devices have a same value of a characteristic parameter, the method is characterized in comprising: acquiring (S110, S210, S310) the value of the characteristic parameter of the one or more second energy storage devices as a target characteristic value; controlling (S120) the charge/discharge power converter to charge or discharge the one or more first energy storage devices until a proximity of a value of the characteristic parameter of at least one of the one or more first energy storage devices to the target characteristic value is less than a preset proximity; and generating and outputting (S130, S230, S330) a signal indicating that the one or more second energy storage devices are allowed to be connected into the energy storage system. acquiring (S110, S210, S310) the value of the characteristic parameter of the one or more second energy storage devices as a target characteristic value; controlling (S120) the charge/discharge power converter to charge or discharge the one or more first energy storage devices until a proximity of a value of the characteristic parameter of at least one of the one or more first energy storage devices to the target characteristic value is less than a preset proximity; and generating and outputting (S130, S230, S330) a signal indicating that the one or more second energy storage devices are allowed to be connected into the energy storage system.
A sensing system for gap management in a component in which this system is to be installed, the sensing system comprising at least one shim portion secured with respect to at least one nanogenerator portion, the at least one nanogenerator portion comprising: (a) a strain sensing portion; (b) an energy-harvesting portion configured to power the sensing system; and (c) a data managing portion configured to transmit measured data from the strain sensing portion to a remote location. (a) a strain sensing portion; (b) an energy-harvesting portion configured to power the sensing system; and (c) a data managing portion configured to transmit measured data from the strain sensing portion to a remote location.
A vacuum adiabatic body comprising: a first plate defining at least one portion of a first side of a wall adjacent to a first space having a first temperature; a second plate defining at least one portion of a second side of the wall adjacent to a second space having a second temperature different from the first temperature; a seal that seals the first plate and the second plate to provide a third space that has a third temperature between the first temperature and the second temperature and is in a vacuum state; a support that supports the first and second plates and is provided in the third space ; an exhaust port through which a gas in the third space is exhausted; a conductive resistance sheet having a first end connected to the first plate , the conductive resistance sheet configured to resist heat transfer between the second plate and the first plate ; characterized by a side frame connected to the conductive resistance sheet , the side frame defining at least one portion of a wall of the third space , wherein the side frame includes a first mounting surface connected to a second end of the conductive resistance sheet and a second mounting surface connected to the second plate , and the second mounting surface is supported by the support. a first plate defining at least one portion of a first side of a wall adjacent to a first space having a first temperature; a second plate defining at least one portion of a second side of the wall adjacent to a second space having a second temperature different from the first temperature; a seal that seals the first plate and the second plate to provide a third space that has a third temperature between the first temperature and the second temperature and is in a vacuum state; a support that supports the first and second plates and is provided in the third space ; an exhaust port through which a gas in the third space is exhausted; a conductive resistance sheet having a first end connected to the first plate , the conductive resistance sheet configured to resist heat transfer between the second plate and the first plate ; characterized by a side frame connected to the conductive resistance sheet , the side frame defining at least one portion of a wall of the third space , wherein the side frame includes a first mounting surface connected to a second end of the conductive resistance sheet and a second mounting surface connected to the second plate , and the second mounting surface is supported by the support.
A resin layered body comprising: a layer containing a polycarbonate-based resin (A); a layer containing a thermoplastic resin (B) on at least one surface of the layer containing a polycarbonate-based resin (A); and a hard coating layer on a surface of at least one of the layer(s) containing a thermoplastic resin (B), wherein the polycarbonate-based resin (A) has a glass-transition temperature of 115°C or higher and less than 130°C, a difference between the glass-transition temperature of the polycarbonate-based resin (A) and a glass-transition temperature of the thermoplastic resin (B) is in a range of from 0 to 15°C, the thermoplastic resin (B) comprises a methacrylic resin (C) and a styrene copolymer (D), a content of the methacrylic resin (C) is from 15 to 60 parts by mass and a content of the styrene copolymer (D) is from 85 to 40 parts by mass based on 100 parts by mass of a total content of the methacrylic resin (C) and the styrene copolymer (D), the styrene copolymer (D) is a copolymer consisting of styrene in an amount of from 68 to 84 mass% and maleic anhydride in an amount of from 16 to 32 mass%, and the hard coating layer is made of an acrylic hard coating. a layer containing a polycarbonate-based resin (A); a layer containing a thermoplastic resin (B) on at least one surface of the layer containing a polycarbonate-based resin (A); and a hard coating layer on a surface of at least one of the layer(s) containing a thermoplastic resin (B), wherein the polycarbonate-based resin (A) has a glass-transition temperature of 115°C or higher and less than 130°C, a difference between the glass-transition temperature of the polycarbonate-based resin (A) and a glass-transition temperature of the thermoplastic resin (B) is in a range of from 0 to 15°C, the thermoplastic resin (B) comprises a methacrylic resin (C) and a styrene copolymer (D), a content of the methacrylic resin (C) is from 15 to 60 parts by mass and a content of the styrene copolymer (D) is from 85 to 40 parts by mass based on 100 parts by mass of a total content of the methacrylic resin (C) and the styrene copolymer (D), the styrene copolymer (D) is a copolymer consisting of styrene in an amount of from 68 to 84 mass% and maleic anhydride in an amount of from 16 to 32 mass%, and the hard coating layer is made of an acrylic hard coating.
Radar system, comprising: a transmitter and receiver unit for transmitting and receiving radar signals; a device for determining azimuthal target parameters, which is designed to determine an azimuth angle for a detected target, characterized in that the device for determining azimuthal target parameters is further designed to ascertain a number of detected targets and to determine an azimuth angle for each detected target ; the radar system further comprising an elevation angle determination device which, on the basis of the azimuthal target parameters, is designed to form a control matrix A, to form a pseudo-inverse of the control matrix, and to calculate the amplitude relationships of the received signals with inclusion of the pseudo-inverse of the control matrix, and to determine a separate elevation angle for each detected target from the amplitude relationships of the received signals, the control matrix A being formed as follows: A = a θ 1 , a θ 2 , ... , a θ n where: n number of the detected targets θ 1 , ..., θ n azimuth angle of the respective targets, and a(θ 1 ), a(θ 2 ), ..., a(θ n ) control vectors of the parameters of the antenna diagrams on the basis of the respective azimuth angles θ 1 , ..., θ n , with control matrices inverted in advance being stored in a memory of the radar system. a transmitter and receiver unit for transmitting and receiving radar signals; a device for determining azimuthal target parameters, which is designed to determine an azimuth angle for a detected target, characterized in that the device for determining azimuthal target parameters is further designed to ascertain a number of detected targets and to determine an azimuth angle for each detected target ; the radar system further comprising an elevation angle determination device which, on the basis of the azimuthal target parameters, is designed to form a control matrix A, to form a pseudo-inverse of the control matrix, and to calculate the amplitude relationships of the received signals with inclusion of the pseudo-inverse of the control matrix, and to determine a separate elevation angle for each detected target from the amplitude relationships of the received signals, the control matrix A being formed as follows: A = a θ 1 , a θ 2 , ... , a θ n where: n number of the detected targets θ 1 , ..., θ n azimuth angle of the respective targets, and a(θ 1 ), a(θ 2 ), ..., a(θ n ) control vectors of the parameters of the antenna diagrams on the basis of the respective azimuth angles θ 1 , ..., θ n , n number of the detected targets θ 1 , ..., θ n azimuth angle of the respective targets, and a(θ 1 ), a(θ 2 ), ..., a(θ n ) control vectors of the parameters of the antenna diagrams on the basis of the respective azimuth angles θ 1 , ..., θ n , with control matrices inverted in advance being stored in a memory of the radar system.
Sensor having a housing in which a sensor element is disposed, and a gas-tight electrical feedthrough through the housing , said feedthrough being configured for directing electrical currents and/or voltages from electrical components that are disposed outside the housing into the housing and/or for diverting same out of the housing , characterized in that the electrical feedthrough has a ceramic molded body which has at least one through bore , the latter having a first end and a second end , wherein the through bore from the first end up to the second end is filled with a metallic paste , and the ceramic molded body in a sintering process is connected to the metallic paste , and in the region of the first end and/or of the second end of the through bore at least one metallic tube piece is attached to the sintered metallic paste .
LED light source having one or more LEDs disposed on a printed circuit board , wherein each of the LEDs comprises at least one LED die disposed on an LED PCB by means of a die attach , and the LED PCB comprises electrical rear side contacts on the side opposite the LED die , wherein the rear side contacts cover at least half the surface, preferably, aside from necessary exceptions, the entire surface of the LED PCB , wherein the LED die is cast in a material and the LED die is inserted into a reflector, wherein the LED PCB is a metal core printed circuit board and the LED die is mounted directly on the metal core, wherein the printed circuit board comprises contact surfaces with which the one or more LEDs (s) are in contact, and wherein the rear side contacts of the one or more LEDs are respectively soldered to the contact surfaces on at least half the surface of the LED PCB .