mhurhangee/patent-ind-claim-en huggingface dataset:
A printed product made of a flat material , the printed product having a plurality of perforation lines , wherein a portion of the printed product forms an envelope portion which is folded into an envelope having an inner receiving space, wherein an insert portion is integrally connected to the envelope portion , the transition between the envelope portion and the insert portion being formed by a connecting portion , wherein a first perforation line is formed in the flat material between the connecting portion and the insert portion , wherein the insert portion is inserted into the envelope portion folded into an envelope by folding along the connecting portion , wherein a second perforation line is formed on the envelope portion , by which a detachable flap is formed in such a way that the detachable flap is connected to the connecting portion and can be detached from the insert portion together with the connecting portion along the first perforation line , characterised in that the envelope portion is folded into an envelope with a broken wrapping fold, wherein the connecting portion extends along the envelope portion between two adjacent breaks . wherein a portion of the printed product forms an envelope portion which is folded into an envelope having an inner receiving space, wherein an insert portion is integrally connected to the envelope portion , the transition between the envelope portion and the insert portion being formed by a connecting portion , wherein a first perforation line is formed in the flat material between the connecting portion and the insert portion , wherein the insert portion is inserted into the envelope portion folded into an envelope by folding along the connecting portion , wherein a second perforation line is formed on the envelope portion , by which a detachable flap is formed in such a way that the detachable flap is connected to the connecting portion and can be detached from the insert portion together with the connecting portion along the first perforation line , characterised in that the envelope portion is folded into an envelope with a broken wrapping fold, wherein the connecting portion extends along the envelope portion between two adjacent breaks .
A computer-implemented method for planning an ablation plan of a target tissue in a patient, the method comprising: receiving data characterizing patient-specific anatomy comprising at least the target tissue, wherein the data include data on dielectric properties associated with the target tissue; calculating by computer simulated results of one or more operations to lesion the target tissue, based on the received data; producing a planned target form of the lesion, wherein the planned target form is selected based on one or more criteria evaluated on the simulated results; providing an indication of the planned target form; producing an ablation plan for producing the planned target form; wherein the received data characterize geometry of a target anatomical structure, and the ablation plan describes the adjustment of parameters of ablation as a function of geometry along the planned target form of the lesion; characterized in that the parameters of ablation are adjusted as a function of structure thickness along the planned target form of the lesion. receiving data characterizing patient-specific anatomy comprising at least the target tissue, wherein the data include data on dielectric properties associated with the target tissue; calculating by computer simulated results of one or more operations to lesion the target tissue, based on the received data; producing a planned target form of the lesion, wherein the planned target form is selected based on one or more criteria evaluated on the simulated results; providing an indication of the planned target form; producing an ablation plan for producing the planned target form; wherein the received data characterize geometry of a target anatomical structure, and the ablation plan describes the adjustment of parameters of ablation as a function of geometry along the planned target form of the lesion; characterized in that the parameters of ablation are adjusted as a function of structure thickness along the planned target form of the lesion.
A biosignal monitoring system for reducing a motion artifact from at least one biopotential electrical signal input , the biosignal monitoring system comprising a signal processing module , a motion artifact extraction module and a subtraction module , wherein the motion artifact extraction module and the signal processing module receive the biopotential electrical signal input and the subtraction module receives both an extracted signal from an output of the motion artifact extraction module and a biopotential electrical signal from an output of the signal processing module ; and the subtraction module is configured for subtracting the extracted signal from the biopotential electrical signal; characterized in that : the motion artifact extraction module is implemented as analog domain electronic circuit and comprises a filter network, configured for attenuating differential mode signals of the biopotential electrical signal input from a first frequency (F1), and passing a representation of the motion artifact signal from the biopotential electrical signal input up to a second frequency (F2) at the output of the motion artifact extraction module .
A cast-in-place anchor comprising: a body defining a cavity and having a base for positioning the body on a wooden form board, the body being configured to be secured to the wooden form board by at least one fixing member ; an opening in the base of the body in communication with the cavity ; a plurality of additional openings in the body in communication with the cavity ; a threaded member provided in the cavity ; a support member also provided in the cavity for supporting the threaded member and for restricting the ingress of wet concrete through the additional openings into contact with the threaded member in use, whereby during concrete pouring physical contact occurs between the concrete and support member ; wherein the anchor is configured such that after concrete pouring, concrete setting and form board removal in use a threaded rod can be inserted into the opening in the base of the body , past the support member and into threaded engagement with the threaded member , whereby interaction between the set concrete and support member enables suspending a load from the anchor . a body defining a cavity and having a base for positioning the body on a wooden form board, the body being configured to be secured to the wooden form board by at least one fixing member ; an opening in the base of the body in communication with the cavity ; a plurality of additional openings in the body in communication with the cavity ; a threaded member provided in the cavity ; a support member also provided in the cavity for supporting the threaded member and for restricting the ingress of wet concrete through the additional openings into contact with the threaded member in use, whereby during concrete pouring physical contact occurs between the concrete and support member ; wherein the anchor is configured such that after concrete pouring, concrete setting and form board removal in use a threaded rod can be inserted into the opening in the base of the body , past the support member and into threaded engagement with the threaded member , whereby interaction between the set concrete and support member enables suspending a load from the anchor .
A molded or extruded article comprising at least one insulation layer and at least one semiconductive layer, the semiconductive layer consisting of in weight percent: A. 1 to less than 40 wt% of conductive filler comprising conductive carbon black for a volume resistivity of less than 1000 ohm-cm, measured according to ASTM D-991; B. 10 to 80 wt% of a non-olefin elastomer, wherein the elastomer is a silicone and/or urethane rubber; and C. 10 to 80 wt% of an olefin elastomer selected from the group consisting of polyolefin homopolymers, ethylene/a-olefin interpolymers and propylene/α-olefin interpolymers; and D. optionally, 0.5 to 2.5 wt% of peroxide; E. optionally at least one additive selected from the group consisting of antioxidants, curing agents, cross linking co-agents, cure boosters and scorch retardants, processing aids, coupling agents, ultraviolet stabilizers, antistatic agents, nucleating agents, slip agents, plasticizers, lubricants, viscosity control agents, tackifiers, anti-blocking agents, surfactants, extender oils, acid scavengers, flame retardants and metal deactivators. A. 1 to less than 40 wt% of conductive filler comprising conductive carbon black for a volume resistivity of less than 1000 ohm-cm, measured according to ASTM D-991; B. 10 to 80 wt% of a non-olefin elastomer, wherein the elastomer is a silicone and/or urethane rubber; and C. 10 to 80 wt% of an olefin elastomer selected from the group consisting of polyolefin homopolymers, ethylene/a-olefin interpolymers and propylene/α-olefin interpolymers; and D. optionally, 0.5 to 2.5 wt% of peroxide; E. optionally at least one additive selected from the group consisting of antioxidants, curing agents, cross linking co-agents, cure boosters and scorch retardants, processing aids, coupling agents, ultraviolet stabilizers, antistatic agents, nucleating agents, slip agents, plasticizers, lubricants, viscosity control agents, tackifiers, anti-blocking agents, surfactants, extender oils, acid scavengers, flame retardants and metal deactivators.
A compound of formula (IIB) or an N -oxide thereof, or a pharmaceutically acceptable salt or solvate thereof, or a glucuronide derivative thereof: wherein E represents -CH 2 ; V represents C-R 22 or N; R 12 represents hydrogen, fluoro, chloro, trifluoromethyl, methyl, or ethoxycarbonylethyl; R 15 represents difluoromethoxy; R 16 represents hydrogen, halogen, cyano, C 1-6 alkyl, trifluoromethyl, difluoromethoxy, or amino; R 21 represents hydroxy(C 1-6 )alkyl or R 21 represents (C 3-7 )heterocycloalkyl, which group may be optionally substituted by one, two or three substituents independently selevted from C 1-6 alkylsulphonyl, oxo and carboxy; R 22 represents hydrogen, halogen or C 1-6 alkyl; and R 23 represents hydrogen, C 1-6 alkyl, trifluoromethyl or C 1-6 alkoxy. E represents -CH 2 ; V represents C-R 22 or N; R 12 represents hydrogen, fluoro, chloro, trifluoromethyl, methyl, or ethoxycarbonylethyl; R 15 represents difluoromethoxy; R 16 represents hydrogen, halogen, cyano, C 1-6 alkyl, trifluoromethyl, difluoromethoxy, or amino; R 21 represents hydroxy(C 1-6 )alkyl or R 21 represents (C 3-7 )heterocycloalkyl, which group may be optionally substituted by one, two or three substituents independently selevted from C 1-6 alkylsulphonyl, oxo and carboxy; R 22 represents hydrogen, halogen or C 1-6 alkyl; and R 23 represents hydrogen, C 1-6 alkyl, trifluoromethyl or C 1-6 alkoxy.
A power transmission device comprising: a motor including a rotor having a permanent magnet embedded therein and a stator , and configured to generate a rotational force; a reducer configured to transmit the rotational force of the motor; and a wet brake mechanism configured to put a brake on the rotation of the motor, wherein spaces accommodating the motor, the reducer, and the brake mechanism communicate with each other so that lubricant oil can flow through the spaces, and wherein each of the axial end faces of the rotor is provided with an end plate , and the end plate on a side away from the brake mechanism is formed with a through hole at a position corresponding to the permanent magnet such that a leakage magnetic flux at an axial end face of the rotor away from the brake mechanism is greater than that of the end face toward the brake mechanism. a motor including a rotor having a permanent magnet embedded therein and a stator , and configured to generate a rotational force; a reducer configured to transmit the rotational force of the motor; and a wet brake mechanism configured to put a brake on the rotation of the motor, wherein spaces accommodating the motor, the reducer, and the brake mechanism communicate with each other so that lubricant oil can flow through the spaces, and wherein each of the axial end faces of the rotor is provided with an end plate , and the end plate on a side away from the brake mechanism is formed with a through hole at a position corresponding to the permanent magnet such that a leakage magnetic flux at an axial end face of the rotor away from the brake mechanism is greater than that of the end face toward the brake mechanism.
An aircraft wing system comprising: an aircraft wing ; an edge device coupled to a leading edge or trailing edge of the aircraft wing ; a drive shaft rotatable about its axis; a crank arm , a first end of the crank arm being coupled to the drive shaft , and a second end of the crank arm opposite to the first end being coupled to the edge device ; a gear system coupled between the drive shaft and the first end of the crank arm ; a further crank arm , a first end of the further crank arm being coupled to the drive shaft , and a second end of the further crank arm opposite to the first end being coupled to the edge device , the further crank arm being spaced apart from the crank along a length of the drive shaft ; and a further gear system coupled between the drive shaft and the first end of the further crank arm ; characterized in that a length of the crank arm is different to that of the further crank arm . an aircraft wing ; an edge device coupled to a leading edge or trailing edge of the aircraft wing ; a drive shaft rotatable about its axis; a crank arm , a first end of the crank arm being coupled to the drive shaft , and a second end of the crank arm opposite to the first end being coupled to the edge device ; a gear system coupled between the drive shaft and the first end of the crank arm ; a further crank arm , a first end of the further crank arm being coupled to the drive shaft , and a second end of the further crank arm opposite to the first end being coupled to the edge device , the further crank arm being spaced apart from the crank along a length of the drive shaft ; and a further gear system coupled between the drive shaft and the first end of the further crank arm ; characterized in that a length of the crank arm is different to that of the further crank arm .
A gravity separator unit (1; 600) comprising a container for holding at least 1m 3 of water to be treated, the container having sidewalls and a floor (20; 620), wherein the floor comprises one or more corrugated pile sheets which define a plurality of alternating tops and parallel gutters facing the interior of the container, wherein the tops and lower portions of the gutters are vertically spaced apart by a distance (h) of between 3 and 30 cm from each other, wherein the gravity separator unit further comprises a scraping device that is at least partially arranged within the container at or near the floor, wherein the scraping device comprises at least two scraping elements , each scraping element comprising one or more scraping blades , wherein the scraping device is adapted for moving each of the scraping elements along the gutters towards an end of the gutters with each of the one or more scraping blades thereof extending at least partially in a corresponding gutter.
A method of managing heterogeneous parallel computing, comprising: determining , by a controller, a joint goal for a computational work construct; determining , by the controller at runtime for the computational work construct, a construct power state based at least in part on the joint goal, wherein the construct power state indicates a selected power state for each of a plurality of heterogeneous processing devices; assigning to each of the plurality of heterogeneous processing devices, by the controller, the selected power state for that respective one of the plurality of heterogeneous processing devices indicated in the construct power state for execution of work components; and preventing , by the controller, the assignment of new work components unrelated to the computational work construct to the plurality of heterogeneous processing devices until all of the work components of the computational work construct are finished executing. determining , by a controller, a joint goal for a computational work construct; determining , by the controller at runtime for the computational work construct, a construct power state based at least in part on the joint goal, wherein the construct power state indicates a selected power state for each of a plurality of heterogeneous processing devices; assigning to each of the plurality of heterogeneous processing devices, by the controller, the selected power state for that respective one of the plurality of heterogeneous processing devices indicated in the construct power state for execution of work components; and preventing , by the controller, the assignment of new work components unrelated to the computational work construct to the plurality of heterogeneous processing devices until all of the work components of the computational work construct are finished executing.
A biocidal composition comprising: - at least one diallyl sulfide of formula where R is selected from - a polar diluent which comprises: dialkyl succinates, dialkyl glutarates, or dialkyl adipate, - surface active agents, - a C4-C9 alkanol which is 2-ethyl-1-hexanol, characterized in that the surface active agents comprise: - at least one non-ionic surfactant with an HLB value between 9.5 and 17, - at least one anionic surfactant selected from the group consisting of alkylsulfosuccinate salts, alkylbenzene sulfonate salts and ethoxylated aryl alkyl phosphate esters. - at least one diallyl sulfide of formula where R is selected from - a polar diluent which comprises: dialkyl succinates, dialkyl glutarates, or dialkyl adipate, - surface active agents, - a C4-C9 alkanol which is 2-ethyl-1-hexanol, characterized in that the surface active agents comprise: - at least one non-ionic surfactant with an HLB value between 9.5 and 17, - at least one anionic surfactant selected from the group consisting of alkylsulfosuccinate salts, alkylbenzene sulfonate salts and ethoxylated aryl alkyl phosphate esters.
A lighting device comprising: at least a first elongated carrier and a second elongated carrier , at least one of the first elongated carrier and the second elongated carrier being configured to support at least one light-emitting element , each of the first elongated carrier and the second elongated carrier being foldable; wherein at least the first elongated carrier and the second elongated carrier have been repeated folded over each other, thereby forming a plurality of folds in each of the first elongated carrier and the second elongated carrier, such that a plurality of sections of the first elongated carrier are interleaved with respect to a plurality of sections of the second elongated carrier so as to form an interleaved structure . at least a first elongated carrier and a second elongated carrier , at least one of the first elongated carrier and the second elongated carrier being configured to support at least one light-emitting element , each of the first elongated carrier and the second elongated carrier being foldable; wherein at least the first elongated carrier and the second elongated carrier have been repeated folded over each other, thereby forming a plurality of folds in each of the first elongated carrier and the second elongated carrier, such that a plurality of sections of the first elongated carrier are interleaved with respect to a plurality of sections of the second elongated carrier so as to form an interleaved structure .
A method comprising: reducing a number and/or size of air voids in a carbon allotrope heating clement to have an electrical resistivity between 0.005 Ω/sq and 3.0 Ω/sq; and applying the carbon allotrope heating element to a component of an aircraft. reducing a number and/or size of air voids in a carbon allotrope heating clement to have an electrical resistivity between 0.005 Ω/sq and 3.0 Ω/sq; and applying the carbon allotrope heating element to a component of an aircraft.
A method for transmitting notifications to at least one party based on image data analysis , the method comprising: receiving, from an unmanned aerial vehicle, current image data of a geographic location ; comparing the current image data with previous image data of the geographic location to identify a change in the geographic location ; analyzing the change to determine a category of the change in the geographic location ; determining at least one party to notify about the change based on the category ; and transmitting a notification to the at least one party via an unmanned aerial vehicle, UAV, , wherein transmitting the notification to the at least one party via the unmanned aerial vehicle comprises: querying a database to retrieve location information of at least one UAV and the at least one party; comparing the location information of the at least one UAV with the location information of the at least one party to determine a UAV within a threshold distance of the at least one party; and transmitting an instruction to the UAV within the threshold distance, the instruction to transmit the notification to the at least one party. receiving, from an unmanned aerial vehicle, current image data of a geographic location ; comparing the current image data with previous image data of the geographic location to identify a change in the geographic location ; analyzing the change to determine a category of the change in the geographic location ; determining at least one party to notify about the change based on the category ; and transmitting a notification to the at least one party via an unmanned aerial vehicle, UAV, , wherein transmitting the notification to the at least one party via the unmanned aerial vehicle comprises: querying a database to retrieve location information of at least one UAV and the at least one party; comparing the location information of the at least one UAV with the location information of the at least one party to determine a UAV within a threshold distance of the at least one party; and transmitting an instruction to the UAV within the threshold distance, the instruction to transmit the notification to the at least one party. querying a database to retrieve location information of at least one UAV and the at least one party; comparing the location information of the at least one UAV with the location information of the at least one party to determine a UAV within a threshold distance of the at least one party; and transmitting an instruction to the UAV within the threshold distance, the instruction to transmit the notification to the at least one party.