mhurhangee/patent-ind-claim-en huggingface dataset:
A system for circulating a volatile composition throughout at least one room, the system comprising: a central communication unit capable of receiving incoming signals and sending outgoing instructions, the central communication unit comprising a memory configured to store settings; a volatile composition dispenser capable of delivering the volatile composition into the air, wherein the volatile composition dispenser is communicably connectable with the central communication unit through a wireless communication link; and an air handling device communicably connectable with the central communication unit and configured to move air throughout the at least one room upon receipt of an outgoing instruction from the central communication unit, characterized in that the central communication unit is adapted to send a first outgoing instruction to the volatile composition dispenser to turn off the volatile composition dispenser after a first set point is reached, wherein the central communication unit is adapted to send a second outgoing instruction to the air handling device to turn on the air handling device after a second set point is reached, wherein the second set point is spaced from the first set point, wherein the central communication unit is adapted to send a further outgoing instruction to the air handling device to turn off the air handling device after a third set point is reached, and wherein the first and third set points are durations of time. a central communication unit capable of receiving incoming signals and sending outgoing instructions, the central communication unit comprising a memory configured to store settings; a volatile composition dispenser capable of delivering the volatile composition into the air, wherein the volatile composition dispenser is communicably connectable with the central communication unit through a wireless communication link; and an air handling device communicably connectable with the central communication unit and configured to move air throughout the at least one room upon receipt of an outgoing instruction from the central communication unit, characterized in that the central communication unit is adapted to send a first outgoing instruction to the volatile composition dispenser to turn off the volatile composition dispenser after a first set point is reached, wherein the central communication unit is adapted to send a second outgoing instruction to the air handling device to turn on the air handling device after a second set point is reached, wherein the second set point is spaced from the first set point, wherein the central communication unit is adapted to send a further outgoing instruction to the air handling device to turn off the air handling device after a third set point is reached, and wherein the first and third set points are durations of time.
A method implemented in a terminal device , comprising: receiving from a base station an indication of uplink semi-persistent scheduling deactivation; obtaining an uplink resource semi-persistently scheduled by the base station for the terminal device and to be deactivated based on said indication, and sending to the base station confirmation of the deactivation, wherein the sending to the base station the confirmation of the deactivation comprises: sending to the base station the confirmation of the deactivation using the obtained semi-persistently scheduled uplink resource, wherein the confirmation of the deactivation is sent as a Media Access Control, MAC, Control Element, CE, wherein the MAC CE is associated with a predefined Media Access Control Protocol Data Unit, MAC PDU, sub-header for identifying the confirmation of the deactivation, and deactivating the semi-persistently scheduled uplink resource. receiving from a base station an indication of uplink semi-persistent scheduling deactivation; obtaining an uplink resource semi-persistently scheduled by the base station for the terminal device and to be deactivated based on said indication, and sending to the base station confirmation of the deactivation, wherein the sending to the base station the confirmation of the deactivation comprises: sending to the base station the confirmation of the deactivation using the obtained semi-persistently scheduled uplink resource, wherein the confirmation of the deactivation is sent as a Media Access Control, MAC, Control Element, CE, wherein the MAC CE is associated with a predefined Media Access Control Protocol Data Unit, MAC PDU, sub-header for identifying the confirmation of the deactivation, and deactivating the semi-persistently scheduled uplink resource. sending to the base station the confirmation of the deactivation using the obtained semi-persistently scheduled uplink resource, wherein the confirmation of the deactivation is sent as a Media Access Control, MAC, Control Element, CE, wherein the MAC CE is associated with a predefined Media Access Control Protocol Data Unit, MAC PDU, sub-header for identifying the confirmation of the deactivation, and deactivating the semi-persistently scheduled uplink resource.
An affordance for an item to be grasped by a robot system, the robot system comprising an end effector and configured, in use, to move the item; the affordance comprising: a first layer arranged to be grasped by the end effector; and a second layer arranged to adhere to the item, characterised in that the first layer comprises a structure with at least two substantially parallel surfaces, and that the first layer further comprises an indicator arranged to indicate to the robot system to grasp the item by way of the affordance. a first layer arranged to be grasped by the end effector; and a second layer arranged to adhere to the item, characterised in that the first layer comprises a structure with at least two substantially parallel surfaces, and that the first layer further comprises an indicator arranged to indicate to the robot system to grasp the item by way of the affordance.
A turbomachine component having an edge extending in a first direction (D 1 ), wherein the edge comprises a leading edge of a nozzle or turbine blade, the component comprising: a crack within the component and extending from the edge to a first depth in a second direction (D 2 ) orthogonal to the first direction (D 1 ); the turbomachine component characterized in that it further comprises: a filler disposed in the component at a location distal to the crack , the filler comprising: at least a first portion extending in the second direction (D 2 ) from the edge into the component to an opposing end at a second depth greater than the first depth, the first portion being distal to the crack along the edge ; and a second portion extending within the component from the opposing end of the first portion in a third direction (D 3 ) parallel to the first direction (D 1 ). a crack within the component and extending from the edge to a first depth in a second direction (D 2 ) orthogonal to the first direction (D 1 ); the turbomachine component characterized in that it further comprises: a filler disposed in the component at a location distal to the crack , the filler comprising: at least a first portion extending in the second direction (D 2 ) from the edge into the component to an opposing end at a second depth greater than the first depth, the first portion being distal to the crack along the edge ; and a second portion extending within the component from the opposing end of the first portion in a third direction (D 3 ) parallel to the first direction (D 1 ). at least a first portion extending in the second direction (D 2 ) from the edge into the component to an opposing end at a second depth greater than the first depth, the first portion being distal to the crack along the edge ; and a second portion extending within the component from the opposing end of the first portion in a third direction (D 3 ) parallel to the first direction (D 1 ).
Solenoid coil for an MR apparatus or for a magnetic particle imaging tomograph, having a first conductor section and a second conductor section adjoining the first conductor section in series, wherein the first and the second conductor section each have a plurality of turns and wherein the solenoid coil is a gradient coil and/or a shim coil, characterized in that at least one turn of the first conductor section is arranged between two adjacent turns of the second conductor section and in that the first conductor section and the second conductor section form sections of a conductor.
Compound 22 having the formula or a pharmaceutically acceptable salt thereof for use in a method of treating a fungal infection in a subject, said method comprising (i) administering a loading-dose of compound 22 or a pharmaceutically acceptable salt thereof to said subject; and (ii) administering one or more maintenance doses of compound 22, or a pharmaceutically acceptable salt thereof to said subject, wherein each of said loading-dose and said maintenance doses are administered in an amount that together are sufficient to treat said fungal infection.
A device for regulating and optimizing combustion in a solid-fuel heating device, the device comprising a flue gases sensor (S1) configured to measure a temperature; a residual oxygen sensor (S2) for measuring residual oxygen in flue gases; a negative pressure sensor (S3); three air flaps ; and a control unit (CU) with a pre-programmed algorithm that is configured to, on the basis of received commands triggered by power being switched on with a switch (S), a remote control (R), or a smart device (SD), like a smartphone or a smart tablet, open or close each of the three air flaps , and to receive data from the flue gases sensor (S1), the residual oxygen sensor (S2), and the negative pressure sensor (S3); wherein the control unit (CU) is configured to, when negative pressure is detected by the negative pressure sensor (S3), enable control of the air flaps during various phases of combustion such as to achieve a predetermined air flow in which escape of flue gases into a surrounding environment of the solid-fuel heating device is prevented.
A carbon fiber spoke, comprising a spoke body made of carbon fiber, a screw bushing that can be fit and connected with a rim and a nut cap bushing that can be fit and connected with the hub , wherein two end parts of the spoke body are fixedly provided with solid joints ; an outside surface of the solid joint is provided with a first tapered section with a small diameter close to the spoke body and a large diameter away from the spoke body ; the screw bushing and the nut cap bushing are provided with penetrable mounting holes , a hole wall surrounding the mounting hole is provided with a second tapered section ; the mounting hole of the screw bushing and the mounting hole of the nut cap bushing are respectively fixed to the two solid joints ; the second tapered section of the mounting hole and the first tapered section of the solid joint are fit and connected together characterized in that , the outside surface of the solid joint also comprises a first rotator section connected with the large diameter end of the first tapered section ; an outer diameter of the first rotator section is equal to or less than a maximum outer diameter of the first tapered section ; the hole wall of the corresponding mounting hole is also provided with a second rotator section connected with the second tapered section , and a minimum outer diameter of the first tapered section is larger than an outer diameter of the spoke body , and a first step surface is formed on the solid joint by said outer diameter difference between the outer diameter of the first tapered section and of the spoke body ; a minimum inner diameter of the second tapered section is larger than an inner diameter of the second rotator section , and a second step surface is defined on the mounting hole by the outer diameter difference; the first step surface and the second step surface are jointed together. the outside surface of the solid joint also comprises a first rotator section connected with the large diameter end of the first tapered section ; an outer diameter of the first rotator section is equal to or less than a maximum outer diameter of the first tapered section ; the hole wall of the corresponding mounting hole is also provided with a second rotator section connected with the second tapered section , and a minimum outer diameter of the first tapered section is larger than an outer diameter of the spoke body , and a first step surface is formed on the solid joint by said outer diameter difference between the outer diameter of the first tapered section and of the spoke body ; a minimum inner diameter of the second tapered section is larger than an inner diameter of the second rotator section , and a second step surface is defined on the mounting hole by the outer diameter difference; the first step surface and the second step surface are jointed together.
An image processing method of an image processing apparatus, comprising: projecting centers of pixels of a pixel grid onto a preset common axis; and mapping a boundary of a detector cell comprised in a detection unit on the preset common axis; CHARACTERIZED BY determining a detector value based on the projecting of the centers of the pixels onto the preset common axis and the mapping of the boundary of the detector cell on the preset common axis, wherein the detector value is determined based on an integrated pixel value between points at which the boundary of the detector cell is mapped on the common axis. projecting centers of pixels of a pixel grid onto a preset common axis; and mapping a boundary of a detector cell comprised in a detection unit on the preset common axis; CHARACTERIZED BY determining a detector value based on the projecting of the centers of the pixels onto the preset common axis and the mapping of the boundary of the detector cell on the preset common axis, wherein the detector value is determined based on an integrated pixel value between points at which the boundary of the detector cell is mapped on the common axis.
Method for laser welding two tubular workpieces situated axially in relation to one another, wherein, in the course of a relative movement of a laser beam in relation to the workpieces, the laser beam is aligned with its beam direction towards an outer circumferential surface (10") of the contact region, or the connection plane, of the two workpieces to be interconnected, wherein, when the workpieces have been placed against one another along their longitudinal axis as axis of rotation, the laser beam is aligned towards the outer circumferential surface (10") with its beam direction eccentrically offset from the axial centre of the workpieces , wherein, during the irradiation by the laser beam , the workpieces are rotated about their axis of rotation, wherein the offset from the axial centre is larger than the inner radius of the workpieces and wherein the offset of the laser beam is smaller than the outer radius of the workpieces , wherein the laser beam is configured such that material, located in each case in the region where the laser beam acts, on the outer surface of the workpieces melts owing to the absorption of laser radiation and a vapour capillary forms in the melt, that the length of the vapour capillary is considerably greater than the difference between the outer radius and the inner radius of the workpieces and that the vapour capillary follows the laser beam during the relative movement, with the result that a weld seam root is defined not by the end that fluctuates in the direction of longitudinal extent of the vapour capillary but by a stable central portion (14") of the vapour capillary , which stable central portion is next to an inner circumferential surface of the workpieces and is at a shorter radial distance from the inner circumferential surface than from the end of the vapour capillary .
A through riser landing string valve, comprising: a housing defining a flow path ; a valve member mounted in the housing ; a fluid rotary actuator coupled to the housing and operatively connected to the valve member by a drive arrangement , the fluid rotary actuator comprising a vane piston rotatable around a rotation axis (A) within an internal chamber, wherein a piston chamber is defined by the walls of the internal chamber and the vane piston , such that the volume of the piston chamber varies with movement of the vane piston ; and the drive arrangement extending through a wall of the housing and providing a rotational operative connection between the fluid rotary actuator and the valve member ; the fluid rotary actuator operable to operate the valve member to control fluid flow along the fluid pathway . a housing defining a flow path ; a valve member mounted in the housing ; a fluid rotary actuator coupled to the housing and operatively connected to the valve member by a drive arrangement , the fluid rotary actuator comprising a vane piston rotatable around a rotation axis (A) within an internal chamber, wherein a piston chamber is defined by the walls of the internal chamber and the vane piston , such that the volume of the piston chamber varies with movement of the vane piston ; and the drive arrangement extending through a wall of the housing and providing a rotational operative connection between the fluid rotary actuator and the valve member ; the fluid rotary actuator operable to operate the valve member to control fluid flow along the fluid pathway .
A system, comprising: an aircraft having a landing gear comprising a wheel ; a friction brake having a brake material coupled to the wheel ; a regenerative brake comprising a reversible taxi motor coupled to the wheel ; a sensor configured to measure a wheel parameter of the landing gear and a friction brake temperature of the friction brake; and a tangible, non-transitory memory configured to communicate with a controller , the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller , cause the controller to perform operations comprising: receiving, by the controller , a command signal, the wheel parameter, and the friction brake temperature; calculating, by the controller , a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal; and generating, by the controller , an allocated deceleration for the friction brake and the regenerative brake corresponding to the calculated brake material temperature and the command signal. an aircraft having a landing gear comprising a wheel ; a friction brake having a brake material coupled to the wheel ; a regenerative brake comprising a reversible taxi motor coupled to the wheel ; a sensor configured to measure a wheel parameter of the landing gear and a friction brake temperature of the friction brake; and a tangible, non-transitory memory configured to communicate with a controller , the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the controller , cause the controller to perform operations comprising: receiving, by the controller , a command signal, the wheel parameter, and the friction brake temperature; calculating, by the controller , a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal; and generating, by the controller , an allocated deceleration for the friction brake and the regenerative brake corresponding to the calculated brake material temperature and the command signal. receiving, by the controller , a command signal, the wheel parameter, and the friction brake temperature; calculating, by the controller , a brake material temperature based on the wheel parameter, the friction brake temperature, and the command signal; and generating, by the controller , an allocated deceleration for the friction brake and the regenerative brake corresponding to the calculated brake material temperature and the command signal.
An optical device for a near-eye display , the optical device comprising: a substrate transparent to visible light and infrared light and configured to be placed in front of an eye of a user of the near-eye display; a holographic grating conformally coupled to a surface of the substrate wherein a refractive index modulation of the holographic grating is apodized in a surface-normal direction of the substrate to reduce optical artifacts in the visible light, wherein apodized is the variation in the amplitude of the refractive index modulation at different regions; the substrate is configured to guide display light within the substrate through total internal reflection; and the holographic grating includes a grating coupler configured to couple at least a portion of the display light out of the substrate. a substrate transparent to visible light and infrared light and configured to be placed in front of an eye of a user of the near-eye display; a holographic grating conformally coupled to a surface of the substrate wherein a refractive index modulation of the holographic grating is apodized in a surface-normal direction of the substrate to reduce optical artifacts in the visible light, wherein apodized is the variation in the amplitude of the refractive index modulation at different regions; the substrate is configured to guide display light within the substrate through total internal reflection; and the holographic grating includes a grating coupler configured to couple at least a portion of the display light out of the substrate.