mhurhangee/patent-ind-claim-en huggingface dataset:
Induction-based cooking appliance comprising multiple heating power transferring elements and multiple heating power energy units for powering said heating power transferring elements , each heating power energy unit comprising one or more power switching devices, in particular power transistors, for providing electrical power to the heating power transferring elements , characterised in that - a first heating power transferring element is powered by a heating power energy unit comprising a first type (T1) of power switching device, in particular power transistor, adapted to be operated in a first frequency range (FR1) and a second heating power transferring element is powered by a heating power energy unit comprising a second type (T2) of power switching device, in particular power transistor, adapted to be operated in a second frequency range (FR2) essentially identical, in particular identical, to the first frequency range (FR1). - a first heating power transferring element is powered by a heating power energy unit comprising a first type (T1) of power switching device, in particular power transistor, adapted to be operated in a first frequency range (FR1) and a second heating power transferring element is powered by a heating power energy unit comprising a second type (T2) of power switching device, in particular power transistor, adapted to be operated in a second frequency range (FR2) essentially identical, in particular identical, to the first frequency range (FR1).
A method comprising steps of: switching on, by a primary controller (IC1), a first switch (S1), on a primary side of a transformer (T1), at a beginning of a primary time interval of a time period (Tperiod) at zero voltage and switching off, by said primary controller (IC1), the first switch at an end of the primary time interval; switching on, by a secondary controller (IC2), a second switch (S2), on a secondary side of the transformer, at a beginning of a secondary time interval of the time period (Tperiod) and switching off, by said secondary controller (IC2), the second switch (S2) at an end of the secondary time interval of the time period (Tperiod); and switching on, by said secondary controller (IC2), the second switch (S2) a second time, at a beginning of a bi-directional flyback action of the time period (Tperiod), at an end of a ringing period of the time period (Tperiod) and switching off, by said secondary controller (IC2), the second switch at an end of said bi-directional flyback action, wherein the ringing period starts after the secondary time interval; and wherein the duration of the bi-directional flyback action is increased such as to provide a fixed switching frequency for the first switch; and wherein during the bi-directional flyback action energy is built up in the transformer (T1), and wherein the time period (Tperiod) has a fall time (Tfall) which ends the time period and begins the next time period, and wherein the fall time is the time for the drain voltage of the first switch to reach zero voltage after the bi-directional flyback action. switching on, by a primary controller (IC1), a first switch (S1), on a primary side of a transformer (T1), at a beginning of a primary time interval of a time period (Tperiod) at zero voltage and switching off, by said primary controller (IC1), the first switch at an end of the primary time interval; switching on, by a secondary controller (IC2), a second switch (S2), on a secondary side of the transformer, at a beginning of a secondary time interval of the time period (Tperiod) and switching off, by said secondary controller (IC2), the second switch (S2) at an end of the secondary time interval of the time period (Tperiod); and switching on, by said secondary controller (IC2), the second switch (S2) a second time, at a beginning of a bi-directional flyback action of the time period (Tperiod), at an end of a ringing period of the time period (Tperiod) and switching off, by said secondary controller (IC2), the second switch at an end of said bi-directional flyback action, wherein the ringing period starts after the secondary time interval; and wherein the duration of the bi-directional flyback action is increased such as to provide a fixed switching frequency for the first switch; and wherein during the bi-directional flyback action energy is built up in the transformer (T1), and wherein the time period (Tperiod) has a fall time (Tfall) which ends the time period and begins the next time period, and wherein the fall time is the time for the drain voltage of the first switch to reach zero voltage after the bi-directional flyback action.
A refrigerator , comprising: a first storage chamber ; a second storage chamber spatially-separated from the first storage chamber ; a first refrigeration cycle system which includes a first compressor to compress a first refrigerant and circulates the first refrigerant from the first compressor to cool the first storage chamber ; and a second refrigeration cycle system which includes a second compressor to compress a second refrigerant and circulates the second refrigerant from the second compressor to cool the second storage chamber , characterized in that, the second refrigerant of the second refrigeration cycle system has a smaller refrigeration capacity per unit volume than that of the first refrigerant of the first refrigeration cycle system . a first storage chamber ; a second storage chamber spatially-separated from the first storage chamber ; a first refrigeration cycle system which includes a first compressor to compress a first refrigerant and circulates the first refrigerant from the first compressor to cool the first storage chamber ; and a second refrigeration cycle system which includes a second compressor to compress a second refrigerant and circulates the second refrigerant from the second compressor to cool the second storage chamber , characterized in that, the second refrigerant of the second refrigeration cycle system has a smaller refrigeration capacity per unit volume than that of the first refrigerant of the first refrigeration cycle system .
A method carried out by a computer comprising: monitoring , at a server, a number of non-Transmission Control Protocol, non-TCP, endpoints that are stored in a memory of the server; determining whether the number of non-TCP endpoints stored in the memory is outside of a range defined by a lower threshold and an upper threshold; adjusting an endpoint lifetime value and a cleanup interval value in response to the number of non-TCP endpoints being outside the range defined by the lower threshold and the upper threshold; and removing one or more of non-TCP endpoints from the memory of the server in response to at least one of the adjusted endpoint lifetime value and the adjusted cleanup interval value. monitoring , at a server, a number of non-Transmission Control Protocol, non-TCP, endpoints that are stored in a memory of the server; determining whether the number of non-TCP endpoints stored in the memory is outside of a range defined by a lower threshold and an upper threshold; adjusting an endpoint lifetime value and a cleanup interval value in response to the number of non-TCP endpoints being outside the range defined by the lower threshold and the upper threshold; and removing one or more of non-TCP endpoints from the memory of the server in response to at least one of the adjusted endpoint lifetime value and the adjusted cleanup interval value.
A multicopter including a flight vehicle body and a plurality of rotary wings arranged around the flight vehicle body when viewed from above and below during flight, the multicopter further comprising an airspeed measurement system, characterized by the airspeed measurement system comprising: a first flow sensor mounted on the flight vehicle body and configured to measure an airspeed along at least two axes in a horizontal direction during flight of the multicopter , wherein the first flow sensor is a thermal flow sensor including at least one heat source and at least two sets of temperature sensors that are arranged along the at least two axes, and the temperature sensors in each set are arranged on both sides of the heat source in one axis direction of the heat source , and a 1-axis flow sensor mounted outside the plurality of rotary wings with respect to the flight vehicle body and configured to measure an airspeed along an axis in a vertical direction during flight of the multicopter , wherein the 1-axis flow sensor is a 1-axis thermal flow sensor including a heat source and temperature sensors that are arranged on both sides of the heat source in the vertical direction during flight of the multicopter . a first flow sensor mounted on the flight vehicle body and configured to measure an airspeed along at least two axes in a horizontal direction during flight of the multicopter , wherein the first flow sensor is a thermal flow sensor including at least one heat source and at least two sets of temperature sensors that are arranged along the at least two axes, and the temperature sensors in each set are arranged on both sides of the heat source in one axis direction of the heat source , and a 1-axis flow sensor mounted outside the plurality of rotary wings with respect to the flight vehicle body and configured to measure an airspeed along an axis in a vertical direction during flight of the multicopter , wherein the 1-axis flow sensor is a 1-axis thermal flow sensor including a heat source and temperature sensors that are arranged on both sides of the heat source in the vertical direction during flight of the multicopter .
A transport refrigeration unit comprising: a combustion engine system including a turbo-charger constructed and arranged to receive air in a cold state and expel the air in a compressed hot state; an evaporator ; and a charge air cooler ; characterised by : a defrost heat exchanger constructed and arranged to receive at least a portion of the air in the compressed hot state and expel the air in a compressed cooled state for defrosting the evaporator; and an evaporator fan constructed and arranged to flow air through the defrost heat exchanger and the evaporator . a combustion engine system including a turbo-charger constructed and arranged to receive air in a cold state and expel the air in a compressed hot state; an evaporator ; and a charge air cooler ; characterised by : a defrost heat exchanger constructed and arranged to receive at least a portion of the air in the compressed hot state and expel the air in a compressed cooled state for defrosting the evaporator; and an evaporator fan constructed and arranged to flow air through the defrost heat exchanger and the evaporator . a defrost heat exchanger constructed and arranged to receive at least a portion of the air in the compressed hot state and expel the air in a compressed cooled state for defrosting the evaporator; and an evaporator fan constructed and arranged to flow air through the defrost heat exchanger and the evaporator .
Metering unit for granular material, for example seed or fertilizer, for conveying the granular material in adjustable quantities, wherein the metering unit comprises a metering unit housing , a metering wheel arranged and drivable in the metering unit housing , and a displaceable shut-off valve , wherein the metering unit housing comprises a metering unit cover that can be moved into different positions, the metering unit cover comprises a first position protecting the metering wheel and a second position releasing the metering wheel , a locking means securing the metering unit cover in the first position is associated with the metering unit cover , and wherein the locking means comprises a locking element that can be pushed away, characterized in that the metering unit cover on the side facing the shut-off valve has a lug and the locking element is configured to provide a releasable, interlocking connection to the lug of the metering unit cover in the first position, in that the shut-off valve in the push-away direction of the locking element is arranged behind the locking means and comprises a receptacle for the locking element and in that the shut-off valve is configured by means of the receptacle to facilitate and/or to block the pushing away of the locking element .
A method performed by a wireless device for processing data using computing resources of a remote network computing device , comprising: determining a time required to complete each of a plurality of operations involved in completing a computing task; generating first metadata including the determined plurality of times and a latency budget for the computing task, the latency budget being the time for completion of the computing task; sending the first metadata, the data, and an elapsed time since the start of the computing task to the remote network computing device for processing as part of the computing task; receiving from the remote network computing device processed data of the computing task and second metadata including an indication of a remaining time in the latency budget; and adjusting dynamic clock and voltage scaling, DCVS, of one or more processors of the wireless device for post-processing the processed data, based on the second metadata, to complete the post-processing of the processed data within the latency budget, wherein the post-processing comprises one of the plurality of operations. determining a time required to complete each of a plurality of operations involved in completing a computing task; generating first metadata including the determined plurality of times and a latency budget for the computing task, the latency budget being the time for completion of the computing task; sending the first metadata, the data, and an elapsed time since the start of the computing task to the remote network computing device for processing as part of the computing task; receiving from the remote network computing device processed data of the computing task and second metadata including an indication of a remaining time in the latency budget; and adjusting dynamic clock and voltage scaling, DCVS, of one or more processors of the wireless device for post-processing the processed data, based on the second metadata, to complete the post-processing of the processed data within the latency budget, wherein the post-processing comprises one of the plurality of operations.
A method of making an electron beam irradiated osteoinductive implant, the method comprising: exposing an osteoinductive implant containing lyophilized demineralized bone matrix (DBM) fibers without carrier or binding agent to electron beam radiation at a dose of from 10 kilograys to 100 kilograys for a period of time from 1 minute to 60 minutes to reduce microorganisms in the osteoinductive implant and to obtain the electron beam irradiated osteoinductive implant, wherein the osteoinductive properties of the electron beam irradiated osteoinductive implant are decreased by 0 to up to 20%. exposing an osteoinductive implant containing lyophilized demineralized bone matrix (DBM) fibers without carrier or binding agent to electron beam radiation at a dose of from 10 kilograys to 100 kilograys for a period of time from 1 minute to 60 minutes to reduce microorganisms in the osteoinductive implant and to obtain the electron beam irradiated osteoinductive implant, wherein the osteoinductive properties of the electron beam irradiated osteoinductive implant are decreased by 0 to up to 20%.
Backing plate for a disk brake lining of a motor-vehicle partially lined disk brake , made from sheet-steel material as a carrier for friction material , which can be fixed permanently, centrally and directly or indirectly on a front side of the backing plate , and wherein the backing plate has protrusions oriented tangentially outward on diametrically opposite end faces , wherein one of the end faces has, radially on the inside, a retaining protrusion having a through-hole , characterized in that the opposite end face of the backing plate is provided radially on the outside with an open guide protrusion , which has a jaw opening having a receiving pocket .
A polymeric composition comprising: a substantially stable biocompatible polymer comprising a reaction product of: 2-oxo-2-(1 -oxo-1 -(1 -oxo-1 -(2,4,6- triiodophenoxy)propan-2-yloxy)propan-2-yloxy)ethoxy)ethyl acrylate or 1-((2-(methacryloyloxy)ethoxy)carbonyloxy) ethyl 3,5-diacetamido-2,4,6-triiodobenzoate; azobisisobutyronitrile; and hydroxyethyl methacrylate,; the composition further comprising a non-physiological solution; wherein the substantially stable biocompatible polymer is soluble in the non-physiological solution and insoluble in a physiological solution. 2-oxo-2-(1 -oxo-1 -(1 -oxo-1 -(2,4,6- triiodophenoxy)propan-2-yloxy)propan-2-yloxy)ethoxy)ethyl acrylate or 1-((2-(methacryloyloxy)ethoxy)carbonyloxy) ethyl 3,5-diacetamido-2,4,6-triiodobenzoate; azobisisobutyronitrile; and hydroxyethyl methacrylate,; the composition further comprising a non-physiological solution; wherein the substantially stable biocompatible polymer is soluble in the non-physiological solution and insoluble in a physiological solution.
A non-therapeutic, cosmetic use of a preparation comprising sclareolide for treating hyperpigmentation induced by radiation of visible light in the range of from 400 nm to 700 nm, wherein said preparation is applied to human skin.
Information processing platform comprising: - a web server ; - an auxiliary web server ; - a back-end server , - a database , wherein the web server is configured to include an executable code in a web page requested by a web client, said executable code containing instructions which cause the web client to send a code request to the auxiliary web server, wherein the code request is a request for programming code that is specific to the web client; wherein the auxiliary web server is configured to: - receive the code request; and - forward the code request to the back-end server, and wherein the back-end server is configured to: - after receiving the code request from the auxiliary server, obtain platform code to be executed for the requesting web client from the database ; wherein the auxiliary web server or the back-end server is further configured to: - based on the platform code obtained from the database, build client-specific code which, when executed on the web client, causes the web client to collect data and send the data to the information processing platform ; - deliver the client-specific code to the web client; - receive data collected and sent to the information processing platform by the web client executing the client-specific code; - process the data according to the platform code. - a web server ; - an auxiliary web server ; - a back-end server , - a database , - receive the code request; and - forward the code request to the back-end server, and - after receiving the code request from the auxiliary server, obtain platform code to be executed for the requesting web client from the database ; - based on the platform code obtained from the database, build client-specific code which, when executed on the web client, causes the web client to collect data and send the data to the information processing platform ; - deliver the client-specific code to the web client; - receive data collected and sent to the information processing platform by the web client executing the client-specific code; - process the data according to the platform code.
A method for manufacturing a structure of composite material formed by a first structural component and a plurality of second structural components by joining said second structural components in uncured state to the first structural component in cured state by co-bonding, comprising the following steps: a) preparing for each second structural component an ensemble formed by a preform of the second structural component disposed between curing tools having previously placed on them a band of a suitable material to form a vacuum bag so that said preform is surrounded by the band except the surface to be joined to the first structural component in which is placed an adhesive layer for the co-bonding, being dimensioned such bands so that at least the zone of the structure located around the second structural components can be covered with them; b) placing the ensembles of the second structural components on the first structural component in the areas foreseen for their attachment and forming a vacuum bag joining the bands of each second structural component and complementary pieces of the same material as bands so that the vacuum bag covers entirely the first structural component ; c) applying an autoclave cycle to the assembly resulting from the previous step for performing the co-bonding of the second structural components to the first structural component . a) preparing for each second structural component an ensemble formed by a preform of the second structural component disposed between curing tools having previously placed on them a band of a suitable material to form a vacuum bag so that said preform is surrounded by the band except the surface to be joined to the first structural component in which is placed an adhesive layer for the co-bonding, being dimensioned such bands so that at least the zone of the structure located around the second structural components can be covered with them; b) placing the ensembles of the second structural components on the first structural component in the areas foreseen for their attachment and forming a vacuum bag joining the bands of each second structural component and complementary pieces of the same material as bands so that the vacuum bag covers entirely the first structural component ; c) applying an autoclave cycle to the assembly resulting from the previous step for performing the co-bonding of the second structural components to the first structural component .
A cover for magnetizing a tissue-penetrating medical device comprising: a sleeve member having a hollow body with an exterior surface, an interior surface, a proximal end, and a distal end to form a protective closure over a shaft of a tissue-penetrating medical device having a longitudinal axis, the proximal end of the hollow body providing a receiving space for receiving at least a shaft of the tissue-penetrating medical device; characterized in that one or more magnets disposed along the sleeve member effective to magnetize the shaft; and a magnetic shield ; the magnetic shield composed of one or more shielding materials spray-coated onto the exterior surface of the sleeve member, a first face of the one or more magnets being exposed to the receiving space and an opposite face of the one of one or more magnets being oriented towards the magnetic shield. a sleeve member having a hollow body with an exterior surface, an interior surface, a proximal end, and a distal end to form a protective closure over a shaft of a tissue-penetrating medical device having a longitudinal axis, the proximal end of the hollow body providing a receiving space for receiving at least a shaft of the tissue-penetrating medical device; characterized in that one or more magnets disposed along the sleeve member effective to magnetize the shaft; and a magnetic shield ; the magnetic shield composed of one or more shielding materials spray-coated onto the exterior surface of the sleeve member, a first face of the one or more magnets being exposed to the receiving space and an opposite face of the one of one or more magnets being oriented towards the magnetic shield.