mhurhangee/patent-ind-claim-en huggingface dataset:
A method for generating a virtual viewpoint image, comprising: separating (F06305, F06306), by a first image processing apparatus (110a-110z), a foreground image and a background image in a first image captured by a first camera (112a-112z); separating (F06305, F06306), by a second image processing apparatus (110a-110z), a foreground image and a background image in a second image captured by a second camera (112a-112z); transmitting (F06310, F06311, F06312), from the second image processing apparatus, the foreground image separated by the second image processing apparatus to the first image processing apparatus which is connected to the second image processing apparatus; transmitting (F06311, F06312, F06315, F06316, F06317), from the first image processing apparatus to a third image processing apparatus , the foreground image separated by the first image processing apparatus and the foreground image which is separated by the second image processing apparatus and which is transmitted to the first image processing apparatus; specifying a viewpoint in the virtual viewpoint image; and generating, by the third image processing apparatus , a virtual viewpoint image corresponding to the specified viewpoint based on the foreground image separated by the first image processing apparatus and the foreground image separated by the second image processing apparatus. separating (F06305, F06306), by a first image processing apparatus (110a-110z), a foreground image and a background image in a first image captured by a first camera (112a-112z); separating (F06305, F06306), by a second image processing apparatus (110a-110z), a foreground image and a background image in a second image captured by a second camera (112a-112z); transmitting (F06310, F06311, F06312), from the second image processing apparatus, the foreground image separated by the second image processing apparatus to the first image processing apparatus which is connected to the second image processing apparatus; transmitting (F06311, F06312, F06315, F06316, F06317), from the first image processing apparatus to a third image processing apparatus , the foreground image separated by the first image processing apparatus and the foreground image which is separated by the second image processing apparatus and which is transmitted to the first image processing apparatus; specifying a viewpoint in the virtual viewpoint image; and generating, by the third image processing apparatus , a virtual viewpoint image corresponding to the specified viewpoint based on the foreground image separated by the first image processing apparatus and the foreground image separated by the second image processing apparatus.
A chemical substance concentrator configured to concentrate a chemical substance in a gaseous object, the chemical substance concentrator comprising: a channel in which the gaseous object flows; an adsorbent disposed in the channel , the adsorbent being conductive and configured to adsorb the chemical substance; and a pair of electrodes configured to cause a current to flow in the adsorbent , characterized in that the adsorbent comprises a plurality of groups of adsorbents (32A-32D, 33A-33D) disposed separately from one another, and the plurality of groups of adsorbents (32A-32D, 33A-33D) of the adsorbent comprises groups made of different materials or groups having different surface modifications thereon, the chemical substance concentrator further comprises a cooling unit configured to cool the gaseous object flowing in the channel . a channel in which the gaseous object flows; an adsorbent disposed in the channel , the adsorbent being conductive and configured to adsorb the chemical substance; and a pair of electrodes configured to cause a current to flow in the adsorbent , characterized in that the adsorbent comprises a plurality of groups of adsorbents (32A-32D, 33A-33D) disposed separately from one another, and the plurality of groups of adsorbents (32A-32D, 33A-33D) of the adsorbent comprises groups made of different materials or groups having different surface modifications thereon, the chemical substance concentrator further comprises a cooling unit configured to cool the gaseous object flowing in the channel .
Method for monitoring a triggering device (AE) of a fire extinguishing system, wherein the triggering device (AE) is connected to an extinguishing control centre (EST) by way of a supply line, wherein when a fire alarm (AL) is received by the extinguishing control centre (EST) the triggering device (AE) is triggered by means of an electromechanical relay (R), wherein a semiconductor switching element (FET) is connected in series with the relay (R) in order to avoid a false triggering of the triggering device (AE) on account of a mechanical influence on the electromechanical relay (R), wherein the triggering occurs only when both switching elements (R, FET) are activated to close, and wherein the semiconductor switching element (FET) is repeatedly, in particular cyclically, activated by the extinguishing control centre (EST) in the event that no fire alarm (AL) is received, in order to impress a testing current (iP) for monitoring the connected triggering device (AE) by way of the supply line.
A computing device comprising: a display ; a base application configured to execute on the computing device and to present a first user interface on the display ; a dependent application configured to execute on the computing device and to present a second user interface on the display ; interface adaptation logic configured to adapt the second user interface for presentation within the first user interface; storage configured to store at least the dependent application ; and a microprocessor configured to execute at least the interface adaptation logic ; an operating system , wherein the base application and the dependent application are configured to both execute on the operating system; wherein the first user interface includes a virtual keyboard; characterized by data transfer logic configured to transfer data from the second user interface to the first user interface; wherein the computing device is adapted to share the dependent application by passing a link to the base application and to communicate the link from the computing device to another computing device via a network , wherein the link is configured for a user of the another computing device to retrieve or access the shared dependent application, wherein the shared dependent application includes further instances of interface adaptation logic and/or the data transfer logic . a display ; a base application configured to execute on the computing device and to present a first user interface on the display ; a dependent application configured to execute on the computing device and to present a second user interface on the display ; interface adaptation logic configured to adapt the second user interface for presentation within the first user interface; storage configured to store at least the dependent application ; and a microprocessor configured to execute at least the interface adaptation logic ; an operating system , wherein the base application and the dependent application are configured to both execute on the operating system; wherein the first user interface includes a virtual keyboard; characterized by data transfer logic configured to transfer data from the second user interface to the first user interface; wherein the computing device is adapted to share the dependent application by passing a link to the base application and to communicate the link from the computing device to another computing device via a network , wherein the link is configured for a user of the another computing device to retrieve or access the shared dependent application, wherein the shared dependent application includes further instances of interface adaptation logic and/or the data transfer logic .
A component for a gas turbine engine, the component comprising: an airfoil extending in a radial direction from a first end to a second end , and extending axially from a leading edge to a trailing edge , the airfoil having a pressure side and a suction side , wherein the airfoil has a non-leading edge stagnation line formed during operation such that the non-leading edge stagnation line transitions from a location along a leading edge surface of the airfoil at the first end to a location on the airfoil on a pressure side surface of the airfoil at the second end; and a stagnation impingement cavity formed within the airfoil and extending along a surface of the airfoil that aligns with the non-leading edge stagnation line, such that a portion of the stagnation impingement cavity is located proximate the leading edge surface of the airfoil at the first end and a portion of the stagnation impingement cavity is located proximate a side of the airfoil at the second end; characterised by a leading edge feed cavity formed in the leading edge of the airfoil, the leading edge feed cavity extending between the first end and the second end of the airfoil; and at least one impingement aperture fluidly connecting the leading edge feed cavity to the stagnation impingement cavity , wherein the at least one impingement aperture is arranged to impinge upon an interior surface of the airfoil at the non-leading edge stagnation line . an airfoil extending in a radial direction from a first end to a second end , and extending axially from a leading edge to a trailing edge , the airfoil having a pressure side and a suction side , wherein the airfoil has a non-leading edge stagnation line formed during operation such that the non-leading edge stagnation line transitions from a location along a leading edge surface of the airfoil at the first end to a location on the airfoil on a pressure side surface of the airfoil at the second end; and a stagnation impingement cavity formed within the airfoil and extending along a surface of the airfoil that aligns with the non-leading edge stagnation line, such that a portion of the stagnation impingement cavity is located proximate the leading edge surface of the airfoil at the first end and a portion of the stagnation impingement cavity is located proximate a side of the airfoil at the second end; characterised by a leading edge feed cavity formed in the leading edge of the airfoil, the leading edge feed cavity extending between the first end and the second end of the airfoil; and at least one impingement aperture fluidly connecting the leading edge feed cavity to the stagnation impingement cavity , wherein the at least one impingement aperture is arranged to impinge upon an interior surface of the airfoil at the non-leading edge stagnation line .
A motor control method the method comprising: estimating an output voltage of an inverter of a motor drive using a Direct Current, DC, bus voltage and a duty ratio for the motor drive at a first switching frequency (207-1) and at least one second switching frequency (207-2); measuring an output current of the inverter at the first switching frequency and the at least one second switching frequency; calculating a first stator resistance (203-1) for the first switching frequency and at least one second stator resistance (203-2) for the at least one second switching frequency based on the estimated output voltage and the measured output current at the respective switching frequency; estimating a stator resistance at a DC condition based on the first stator resistance and the at least one second stator resistance; setting a dynamic compensation based on a stator resistance error between the first switching frequency and the at least one second switching frequency. estimating an output voltage of an inverter of a motor drive using a Direct Current, DC, bus voltage and a duty ratio for the motor drive at a first switching frequency (207-1) and at least one second switching frequency (207-2); measuring an output current of the inverter at the first switching frequency and the at least one second switching frequency; calculating a first stator resistance (203-1) for the first switching frequency and at least one second stator resistance (203-2) for the at least one second switching frequency based on the estimated output voltage and the measured output current at the respective switching frequency; estimating a stator resistance at a DC condition based on the first stator resistance and the at least one second stator resistance; setting a dynamic compensation based on a stator resistance error between the first switching frequency and the at least one second switching frequency.
An electrolyte for electropolishing metal surfaces, wherein the electrolyte comprises methanesulfonic acid, at least one phosphonic acid und at least one polyvalent alcohol and/or at least one polyalcohol.
A cooling circuit valve , suitable for being positioned on a degassing tank intended to receive a refrigerant, in particular a coolant for a heat engine, said valve comprising: - at least one first refrigerant supply duct , - a second air intake duct inside the valve, - a third refrigerant and/or air exhaust duct , in particular an exhaust for coolant or a gas formed by vaporization of that coolant, and - a connecting volume (V20) that is in communication with an inner volume (V30) of the degassing tank when the valve is positioned on the degassing tank, - a flap (C1) selectively opening a passage (P1) for an incoming stream (F3) of air going from the second duct toward the connecting volume, - a flap (C2) for selectively opening a passage (P3) for an outgoing stream (F8) of refrigerant and/or air, going from the connecting volume toward the third duct, and - a regulator which, under the effect of the pressure in the connecting volume (V20), selectively opens a passage (P2) of an incoming refrigerant stream (F1) going from the first duct toward the connecting volume (V20), wherein the regulator comprises a membrane that is elastically deformable under the effect of the pressure in the connecting volume (V20) and characterized in that the regulator comprises a seat and a housing between which the membrane is fixed by both of its edges . - at least one first refrigerant supply duct , - a second air intake duct inside the valve, - a third refrigerant and/or air exhaust duct , in particular an exhaust for coolant or a gas formed by vaporization of that coolant, and - a connecting volume (V20) that is in communication with an inner volume (V30) of the degassing tank when the valve is positioned on the degassing tank, - a flap (C1) selectively opening a passage (P1) for an incoming stream (F3) of air going from the second duct toward the connecting volume, - a flap (C2) for selectively opening a passage (P3) for an outgoing stream (F8) of refrigerant and/or air, going from the connecting volume toward the third duct, and - a regulator which, under the effect of the pressure in the connecting volume (V20), selectively opens a passage (P2) of an incoming refrigerant stream (F1) going from the first duct toward the connecting volume (V20),
A wind turbine drive system , comprising: a plurality of drive devices provided in a first structure and including a meshing portion meshing with a ring gear provided in a second structure , the first structure and the second structure being configured to rotate relative to each other, each of the plurality of drive devices including: a motor drive portion for outputting power; a speed reducing portion for receiving the power transmitted from the motor drive portion ; a motor braking portion for braking the motor drive portion ; a state quantity detection unit for detecting, for each of the plurality of drive devices , a load between the meshing portion of the each of the plurality of drive devices and the ring gear ; and a control unit for controlling the motor drive portion and/or the motor braking portion of each of the plurality of drive devices based on the load for the each of the plurality of drive devices detected by the state quantity detection unit , so as to reduce a degree of variation in the load among the plurality of drive devices , characterized in that in a state where the motor braking portion of each of the plurality of drive devices is applying a braking force to the corresponding motor drive portion , the control unit is configured to reduce the degree of variation in the load among the plurality of drive devices by controlling at least the motor braking portion of a drive device for which the load is largest among the plurality of drive devices to weaken the braking force thereof. a motor drive portion for outputting power; a speed reducing portion for receiving the power transmitted from the motor drive portion ; a motor braking portion for braking the motor drive portion ; a state quantity detection unit for detecting, for each of the plurality of drive devices , a load between the meshing portion of the each of the plurality of drive devices and the ring gear ; and a control unit for controlling the motor drive portion and/or the motor braking portion of each of the plurality of drive devices based on the load for the each of the plurality of drive devices detected by the state quantity detection unit , so as to reduce a degree of variation in the load among the plurality of drive devices , characterized in that in a state where the motor braking portion of each of the plurality of drive devices is applying a braking force to the corresponding motor drive portion , the control unit is configured to reduce the degree of variation in the load among the plurality of drive devices by controlling at least the motor braking portion of a drive device for which the load is largest among the plurality of drive devices to weaken the braking force thereof.
A photoelectric sensor, comprising: a photo-detector component configured to receive optical information and convert the optical information to an analog signal, the optical information including a light beam having a modulated signal comprising a series of pulses emitted at a rate of one pulse per pulse period, wherein the timing between the series of pulses is either fixed, or varies according to a defined pattern; and a synchronization component configured to generate synchronization information for a receiver of the photoelectric sensor based on an analysis of the analog signal, characterized in that the synchronization component is further configured to: identify presence of pulses within the analog signal, determine respective durations between consecutive pulses of the series of pulses within the analog signal, and calculate, as at least a portion of the synchronization information, an estimated average pulse period based on an average of the respective durations. a photo-detector component configured to receive optical information and convert the optical information to an analog signal, the optical information including a light beam having a modulated signal comprising a series of pulses emitted at a rate of one pulse per pulse period, wherein the timing between the series of pulses is either fixed, or varies according to a defined pattern; and a synchronization component configured to generate synchronization information for a receiver of the photoelectric sensor based on an analysis of the analog signal, characterized in that the synchronization component is further configured to: identify presence of pulses within the analog signal, determine respective durations between consecutive pulses of the series of pulses within the analog signal, and calculate, as at least a portion of the synchronization information, an estimated average pulse period based on an average of the respective durations. generate synchronization information for a receiver of the photoelectric sensor based on an analysis of the analog signal, characterized in that the synchronization component is further configured to: identify presence of pulses within the analog signal, determine respective durations between consecutive pulses of the series of pulses within the analog signal, and calculate, as at least a portion of the synchronization information, an estimated average pulse period based on an average of the respective durations. identify presence of pulses within the analog signal, determine respective durations between consecutive pulses of the series of pulses within the analog signal, and calculate, as at least a portion of the synchronization information, an estimated average pulse period based on an average of the respective durations.
A cooking hob with illumination equipment, wherein: - the cooking hob includes at least one transparent or semi-transparent top panel arranged at a top side of said cooking hob , - the cooking hob includes at least one cooking zone and at least one control element for controlling said cooking zone, - the cooking hob includes at least one transparent or semi-transparent layer , - a plurality of symbols is printed on, applied on, impressed in and/or embossed in said layer , - the symbol corresponds with a cooking zone, a control element and/or an operation state of the cooking hob , - the cooking hob includes a light source element arranged below the top panel and the layer , - the light source element corresponds with one or more symbols , and - the symbols are completely invisible, when the related function is deactivated, characterized in that the cooking hob includes a plurality of light source elements arranged below the top panel and the layer , wherein the light source elements are activated on demand by the user and, if the corresponding cooking zone is activated, the corresponding control element is responsive or the corresponding operation state occurs, respectively, and wherein the cooking hob includes at least one on-off switch for activating and deactivating a part of said cooking hob , wherein only those light source elements within said part of the cooking hob are activated, and the layer is made of a thin paint coating, and wherein at least one of the symbols is elongated and extends along the bottom side of the top panel , and wherein said elongated symbol connects the control element to the corresponding cooking zone. - the cooking hob includes at least one transparent or semi-transparent top panel arranged at a top side of said cooking hob , - the cooking hob includes at least one cooking zone and at least one control element for controlling said cooking zone, - the cooking hob includes at least one transparent or semi-transparent layer , - a plurality of symbols is printed on, applied on, impressed in and/or embossed in said layer , - the symbol corresponds with a cooking zone, a control element and/or an operation state of the cooking hob , - the cooking hob includes a light source element arranged below the top panel and the layer , - the light source element corresponds with one or more symbols , and - the symbols are completely invisible, when the related function is deactivated,