mhurhangee/patent-ind-claim-en huggingface dataset:
A method for supplying power from an inductive power supply to a plurality of remote devices , the inductive power supply comprising: - an inverter , the inverter having a duty cycle and an operating frequency; - a resonant circuit coupled to the inverter, the resonant circuit having a resonant frequency, and a primary winding for transferring power to the remote devices ; and - a power source coupled to the inverter, the power source having a rail voltage; said method comprising: receiving, in the inductive power supply , power usage information from each remote device present with respect to the inductive power supply; maintaining a remote device list of the power information for each of the remote devices in the inductive power supply , and updating the remote device list when a new remote device is present, a remote device is no longer present, and/or a remote device changes its power usage; determining whether the inductive power supply can be configured to adequately power all of the remote devices present with respect to the inductive power supply based on the power usage information; adjusting power consumption characteristics of one or more of the remote devices present with respect to the power supply in response to a determination that power cannot be adequately supplied to all of the remote devices ; and reconfiguring the inductive power supply to supply power to the remote devices based on the received power usage information by setting the operating frequency, the duty cycle, the resonant frequency, and the rail voltage. - a resonant circuit coupled to the inverter, the resonant circuit having a resonant frequency, and a primary winding for transferring power to the remote devices ; and - a power source coupled to the inverter, the power source having a rail voltage; receiving, in the inductive power supply , power usage information from each remote device present with respect to the inductive power supply; maintaining a remote device list of the power information for each of the remote devices in the inductive power supply , and updating the remote device list when a new remote device is present, a remote device is no longer present, and/or a remote device changes its power usage; determining whether the inductive power supply can be configured to adequately power all of the remote devices present with respect to the inductive power supply based on the power usage information; adjusting power consumption characteristics of one or more of the remote devices present with respect to the power supply in response to a determination that power cannot be adequately supplied to all of the remote devices ; and reconfiguring the inductive power supply to supply power to the remote devices based on the received power usage information by setting the operating frequency, the duty cycle, the resonant frequency, and the rail voltage.
A solar plant having at least one pivotable module table which supports at least one photovoltaic solar module , preferably multiple photovoltaic solar modules , and is coupled in such a manner to at least one gear element pivotable about an axis (A) that pivoting the gear element causes the module table (2a to 2c) to be pivoted so that the solar modules track the motion of the sun, the gear element being driven and thus pivoted by an electrically driven drive shaft , at least one actuation element being integrated in the drive shaft , the gear element being both driven and blocked by the actuation element , the actuation element engaging into the toothing of the gear element for driving or blocking the gear element , characterized in that the actuation element comprises at least two actuation pins which are disposed essentially parallel to each other and engage into the toothing of the gear element in order to drive (pivot) or block the gear element , preferably both actuation pins each resting in a tooth space, in particular in adjacent tooth spaces , of the toothing of the gear element and remaining there for blocking the gear element .
A manufacturing method for heat radiation fins in a liquid-type cooling apparatus , wherein the liquid-type cooling apparatus in which there are provided a jacket through which a coolant flows and a heat sink that makes contact with the coolant flowing in the jacket and in which heat generated by a heat-generating device is transferred to the coolant through the intermediary of the heat sink so that the heat is radiated, wherein the heat sink includes a heat sink base member having a first surface portion that faces the inside of the jacket and a plurality of heat radiation fins that are provided on the first surface portion of the heat sink base member and make contact with the coolant flowing in the jacket , and wherein the plurality of heat radiation fins are inclined toward the downstream side of the coolant flowing in the jacket , wherein on the first surface portion of the heat sink base member , a plate-shaped heat radiation fin region protruding by a predetermined dimension from the first surface portion is formed, and wherein a plurality of circular blades that are arranged in such a way as to be spaced a predetermined distance away from one another and whose diameters are different from one another are rotated and then the plurality of circular blades concurrently cut the heat radiation fin region at an inclination angle with respect to the first surface portion so that the plurality of heat radiation fins are formed. wherein the liquid-type cooling apparatus in which there are provided a jacket through which a coolant flows and a heat sink that makes contact with the coolant flowing in the jacket and in which heat generated by a heat-generating device is transferred to the coolant through the intermediary of the heat sink so that the heat is radiated, wherein the heat sink includes a heat sink base member having a first surface portion that faces the inside of the jacket and a plurality of heat radiation fins that are provided on the first surface portion of the heat sink base member and make contact with the coolant flowing in the jacket , and wherein the plurality of heat radiation fins are inclined toward the downstream side of the coolant flowing in the jacket , wherein on the first surface portion of the heat sink base member , a plate-shaped heat radiation fin region protruding by a predetermined dimension from the first surface portion is formed, and wherein a plurality of circular blades that are arranged in such a way as to be spaced a predetermined distance away from one another and whose diameters are different from one another are rotated and then the plurality of circular blades concurrently cut the heat radiation fin region at an inclination angle with respect to the first surface portion so that the plurality of heat radiation fins are formed.
A method of food control with a kitchen appliance for at least partially automating the processing of a recipe comprising the following stages: - Receiving user-specific health data that can be assigned to a user profile , - Creating an evaluation of the health data for the user profile by a computing unit , - Determining a recipe recommendation based on the evaluation of the health data , - Output of the recipe recommendation at a user interface of the kitchen appliance , characterized in that a user reaction and a vital change to a previous recipe recommendation are taken into account when creating the evaluation , as a result of which boundary conditions in the form of the user reaction and the vital change are set for the evaluation , the health data comprising vital data (210.1) of a user and/or creating the evaluation comprising a comparison (102.1) of the health data with reference data . - Receiving user-specific health data that can be assigned to a user profile , - Creating an evaluation of the health data for the user profile by a computing unit , - Determining a recipe recommendation based on the evaluation of the health data , - Output of the recipe recommendation at a user interface of the kitchen appliance ,
A composite structure having a surface, which surface has at least a portion made of a surface resin composition, and comprising a fibrous material selected from non-woven structures, textiles, fibrous battings and combinations thereof, said fibrous material being impregnated with a matrix resin composition, wherein the surface resin composition is selected from polyamide compositions comprising a blend of two or more fully aliphatic polyamides having a melting point of at least 250°C and wherein the matrix resin composition is selected from polyamide compositions comprising one or more fully aliphatic polyamides having a melting point of at least 250°C.
A surgical arm comprising: a first interface configured to receive a device for performing or assisting a surgical procedure; multiple adjustment members configured to adjust the surgical arm relative to a respective adjustment axis ; at least two operating members configured to operate different ones of the adjustment members , wherein the operating members are marked with different visual codings; characterized in further comprising: at least two locking members associated with different ones of the operating members , wherein each of the locking members is configured to lock the surgical arm in position with respect to a specific movement relative to the respective adjustment axis of the associated operating member , wherein the locking members are respectively coded with the same visual coding as the operating member associated with the respective adjustment axis . a first interface configured to receive a device for performing or assisting a surgical procedure; multiple adjustment members configured to adjust the surgical arm relative to a respective adjustment axis ; at least two operating members configured to operate different ones of the adjustment members , wherein the operating members are marked with different visual codings; at least two locking members associated with different ones of the operating members , wherein each of the locking members is configured to lock the surgical arm in position with respect to a specific movement relative to the respective adjustment axis of the associated operating member , wherein the locking members are respectively coded with the same visual coding as the operating member associated with the respective adjustment axis .
An air treatment device comprising: - an activated carbon filter (FCA); - a photocatalyst (PHC) having an interface (I) with the activated carbon filter, said photocatalyst comprising: a porous support (SP) having a longitudinal axis (AL), a catalytic coating (RC) disposed on the surface of the porous support, a plurality of light-emitting diodes (DEL), said device being characterized in that the light-emitting diodes (DEL) are arranged, relative to one another, such that all of the catalytic coating can be illuminated by said light-emitting diodes; the light-emitting diodes being arranged in the form of a plurality of grids (G 1 , G 2 , ... G N ) each provided with several light-emitting diodes, each grid extending over all of a section of the porous support (SP), said section being defined in a plane perpendicular to said longitudinal axis (AL) of the porous support (SP), the various grids being spaced apart from each other along said longitudinal axis and integrated into the porous support (SP). - an activated carbon filter (FCA); - a photocatalyst (PHC) having an interface (I) with the activated carbon filter, said photocatalyst comprising: a porous support (SP) having a longitudinal axis (AL), a catalytic coating (RC) disposed on the surface of the porous support, a plurality of light-emitting diodes (DEL), said device being characterized in that the light-emitting diodes (DEL) are arranged, relative to one another, such that all of the catalytic coating can be illuminated by said light-emitting diodes; the light-emitting diodes being arranged in the form of a plurality of grids (G 1 , G 2 , ... G N ) each provided with several light-emitting diodes, each grid extending over all of a section of the porous support (SP), said section being defined in a plane perpendicular to said longitudinal axis (AL) of the porous support (SP), the various grids being spaced apart from each other along said longitudinal axis and integrated into the porous support (SP). a porous support (SP) having a longitudinal axis (AL), a catalytic coating (RC) disposed on the surface of the porous support, a plurality of light-emitting diodes (DEL), said device being characterized in that the light-emitting diodes (DEL) are arranged, relative to one another, such that all of the catalytic coating can be illuminated by said light-emitting diodes; the light-emitting diodes being arranged in the form of a plurality of grids (G 1 , G 2 , ... G N ) each provided with several light-emitting diodes, each grid extending over all of a section of the porous support (SP), said section being defined in a plane perpendicular to said longitudinal axis (AL) of the porous support (SP), the various grids being spaced apart from each other along said longitudinal axis and integrated into the porous support (SP).
A method of making a tobacco extract, the method comprising: (a) contacting tobacco with an extraction solvent at a first temperature and first pressure which are selected such that the extraction solvent is supercritical, such that tobacco flavor and/or aroma components are extracted from the tobacco into the solvent; (b) separating the residual tobacco solids from the supercritical extraction solvent containing tobacco components; (c) exposing the extraction solvent containing tobacco components to conditions in a vessel at which the extraction solvent is subcritical, thereby releasing the tobacco components from the extraction solvent, (d) contacting the residual tobacco solids with an extraction solvent at a second temperature and second pressure which are selected such that the extraction solvent is supercritical, such that nicotine are extracted from the tobacco into the extraction solvent; and wherein the second temperature and/or second pressure is higher than the respective first temperature or first pressure; (e) separating the residual tobacco solids from the supercritical extraction solvent containing tobacco components; (f) exposing the extraction solvent containing tobacco components to conditions in a vessel at which the extraction solvent is subcritical, thereby releasing the tobacco components from the extraction solvent, wherein during step (f), the vessel contains an entrapment solvent which dissolves the tobacco components released from the extraction solvent, and wherein the entrapment solvent comprises an aerosol generating agent. (a) contacting tobacco with an extraction solvent at a first temperature and first pressure which are selected such that the extraction solvent is supercritical, such that tobacco flavor and/or aroma components are extracted from the tobacco into the solvent; (b) separating the residual tobacco solids from the supercritical extraction solvent containing tobacco components; (c) exposing the extraction solvent containing tobacco components to conditions in a vessel at which the extraction solvent is subcritical, thereby releasing the tobacco components from the extraction solvent, (d) contacting the residual tobacco solids with an extraction solvent at a second temperature and second pressure which are selected such that the extraction solvent is supercritical, such that nicotine are extracted from the tobacco into the extraction solvent; and wherein the second temperature and/or second pressure is higher than the respective first temperature or first pressure; (e) separating the residual tobacco solids from the supercritical extraction solvent containing tobacco components; (f) exposing the extraction solvent containing tobacco components to conditions in a vessel at which the extraction solvent is subcritical, thereby releasing the tobacco components from the extraction solvent,
An injection-molded resin button comprising a button body having a through-hole at the center thereof and a gate trace, wherein the button body comprises a left half part and a right half part , the left and right half parts being segmented left and right by a virtual straight line (L) passing through the gate trace, on the button body , corresponding to a gate of a mold for molding the button and the center (O) of the button body , wherein the button body includes one or more concave portions or one or more convex portions on an outer surface of the button body , characterized in that the concave portions or the convex portions being provided asymmetrically in the left and right half parts . wherein the button body comprises a left half part and a right half part , the left and right half parts being segmented left and right by a virtual straight line (L) passing through the gate trace, on the button body , corresponding to a gate of a mold for molding the button and the center (O) of the button body , wherein the button body includes one or more concave portions or one or more convex portions on an outer surface of the button body , characterized in that the concave portions or the convex portions being provided asymmetrically in the left and right half parts .
Reclosable package , comprising a cavity for storing products arranged within a container , surrounding the cavity , the container extending along a longitudinal direction and having a back side and a front side joined to each other at longitudinal sides parallel to the longitudinal direction and further having an upper side and a bottom side , both extending along intersecting directions to said longitudinal direction , wherein a zipper is arranged at one of either the upper side or the bottom side of the container , the other one of the upper side or the bottom side being permanently sealed, the zipper reversibly connecting two closure parts of the container , wherein respective end portions of the two closure parts of the container are sealed to each other as a sealed closure , the sealed closure being folded flat and attached to either the front side or the back side of the container before the first opening of the reclosable package , wherein, before said first opening of the reclosable package , a tear-off strip is arranged between the zipper and the sealed closure , the tear-off strip connecting unsealed first and second portions of each of the two closure parts of the container . comprising a cavity for storing products arranged within a container , surrounding the cavity , the container extending along a longitudinal direction and having a back side and a front side joined to each other at longitudinal sides parallel to the longitudinal direction and further having an upper side and a bottom side , both extending along intersecting directions to said longitudinal direction , wherein a zipper is arranged at one of either the upper side or the bottom side of the container , the other one of the upper side or the bottom side being permanently sealed, the zipper reversibly connecting two closure parts of the container , wherein respective end portions of the two closure parts of the container are sealed to each other as a sealed closure , the sealed closure being folded flat and attached to either the front side or the back side of the container before the first opening of the reclosable package , wherein, before said first opening of the reclosable package , a tear-off strip is arranged between the zipper and the sealed closure , the tear-off strip connecting unsealed first and second portions of each of the two closure parts of the container .
An aircraft comprising a fibre-optic communication system having: a light source operable to generate light, positioned in a temperature-conditioned area of the aircraft; a transceiver in optical communication with the light source so as to receive the light therefrom, the transceiver comprising a control input and a reflector , and the transceiver being positioned in a non-temperature-conditioned area of the aircraft; an optical fibre in optical communication with the transceiver; and a light detector in optical communication with the optical fibre; and wherein the transceiver is operable to generate an amplitude modulated light signal by selectively reflecting the light received from the light source into the optical fibre using the reflector according to information received at the control input, and wherein the light detector is operable to receive the amplitude modulated light signal from the optical fibre and to detect an amplitude of the amplitude modulated light signal to extract the information. a light source operable to generate light, positioned in a temperature-conditioned area of the aircraft; a transceiver in optical communication with the light source so as to receive the light therefrom, the transceiver comprising a control input and a reflector , and the transceiver being positioned in a non-temperature-conditioned area of the aircraft; an optical fibre in optical communication with the transceiver; and a light detector in optical communication with the optical fibre; and wherein the transceiver is operable to generate an amplitude modulated light signal by selectively reflecting the light received from the light source into the optical fibre using the reflector according to information received at the control input, and wherein the light detector is operable to receive the amplitude modulated light signal from the optical fibre and to detect an amplitude of the amplitude modulated light signal to extract the information.
A prosthetic mitral valve system comprising: an anchor assembly comprising an expandable anchor frame, the anchor assembly coupleable with a native mitral valve having an anterior leaflet and a posterior leaflet that cycle between an open valve orientation and a closed valve orientation in which free edges of the anterior and posterior leaflets oppose each other to define a coaptation line , wherein, while the anchor assembly is coupled with the native mitral valve, the anterior and posterior leaflets continue to cycle; and a valve assembly comprising an expandable valve frame and an occluder attached to the expandable valve frame, the valve assembly selectively coupleable with the anchor assembly ; characterized by a prosthetic element attached to the expandable anchor frame; wherein, while the anchor assembly is coupled with the native mitral valve , at least a portion of the prosthetic element is positioned along the coaptation line between the free edges of the anterior and posterior leaflets while the anterior and posterior leaflets are in the closed valve orientation; and the prosthetic element being configured to work in conjunction with the anterior and posterior leaflets to enhance the sealing function of the native mitral valve . an anchor assembly comprising an expandable anchor frame, the anchor assembly coupleable with a native mitral valve having an anterior leaflet and a posterior leaflet that cycle between an open valve orientation and a closed valve orientation in which free edges of the anterior and posterior leaflets oppose each other to define a coaptation line , wherein, while the anchor assembly is coupled with the native mitral valve, the anterior and posterior leaflets continue to cycle; and a valve assembly comprising an expandable valve frame and an occluder attached to the expandable valve frame, the valve assembly selectively coupleable with the anchor assembly ; characterized by a prosthetic element attached to the expandable anchor frame; wherein, while the anchor assembly is coupled with the native mitral valve , at least a portion of the prosthetic element is positioned along the coaptation line between the free edges of the anterior and posterior leaflets while the anterior and posterior leaflets are in the closed valve orientation; and the prosthetic element being configured to work in conjunction with the anterior and posterior leaflets to enhance the sealing function of the native mitral valve .