mhurhangee/patent-ind-claim-en huggingface dataset:
A skirting board , comprising a core with an upper side , an opposed lower side and a front side and back side situated opposite to each other and extending between the lower side and the upper side , and a plate-shaped material , which is attached to the core and covers at least the front side , wherein the plate-shaped material , seen from the upper side of the core , extends to beyond the lower side of the core , whereby the plate-shaped material is a synthetic material sheet made of a vinyl-containing material and having a thickness larger than 1.8 mm, wherein said synthetic material sheet at least comprises a basic layer, a decoration layer and a transparent top layer, wherein said plate-shaped material is bent at the location of the tip of a V-groove, such that said plate-shaped material also covers said upper side and wherein said V-groove is provided in the core in the direction of the plate-shaped material , however remaining remote from the top layer and the decoration layer, such that at least the side of the plate-shaped material facing away from the core covers the front side and the upper side of the core uninterruptedly.
A method for producing shaped bodies from a building material by means of an additive manufacturing method, in which during a construction process, a layerwise construction of a shaped body takes place by successively solidifying layers of the building material through the action of electromagnetic radiation in a layer area having a contour specified for the respective layer, wherein in the construction process together with the shaped body , a sleeve-like frame surrounding the shaped body at a distance is constructed layer by layer from the building material, and wherein in addition in the construction process, a plurality of pin-like connections is constructed integral with the frame and the shaped body , which are distributed around the shaped body and which connect the shaped body with the frame , characterized in that the shaped body is a tooth replacement part, such as a tooth crown, and the pin-like connections which connect the tooth replacement part to the frame are constructed on the oral or vestibular surfaces of the tooth replacement part . wherein in the construction process together with the shaped body , a sleeve-like frame surrounding the shaped body at a distance is constructed layer by layer from the building material, and wherein in addition in the construction process, a plurality of pin-like connections is constructed integral with the frame and the shaped body , which are distributed around the shaped body and which connect the shaped body with the frame , characterized in that the shaped body is a tooth replacement part, such as a tooth crown, and the pin-like connections which connect the tooth replacement part to the frame are constructed on the oral or vestibular surfaces of the tooth replacement part .
A non-invasive method for measuring motion characteristics of a myocardial tissue, wherein the method comprises: transmitting a plurality of generated synchronous orthogonal, phase controllable and adjustable alternating currents with different frequencies into an organism so as to generate a plurality of synchronous periodic AC voltage signals with different frequencies; receiving the periodic AC voltage signals modulated by changes in the organism's heart tissue to obtain organism's frequency responses; calculating resistances and capacitances of the heart tissue according to the frequency responses; and estimating the motion characteristics of the myocardial tissue according to the resistances and the capacitances, wherein the estimating the motion characteristics of the myocardial tissue according to the resistances and the capacitances comprises: calculating an average longitudinal length of myocardial cells and its change according to the capacitances, and/or calculating heart pumping blood flow according to the resistances; and obtaining an overall longitudinal elastic state of the heart according to the average longitudinal length of the myocardial cells and its change and/or the heart pumping blood flow. transmitting a plurality of generated synchronous orthogonal, phase controllable and adjustable alternating currents with different frequencies into an organism so as to generate a plurality of synchronous periodic AC voltage signals with different frequencies; receiving the periodic AC voltage signals modulated by changes in the organism's heart tissue to obtain organism's frequency responses; calculating resistances and capacitances of the heart tissue according to the frequency responses; calculating an average longitudinal length of myocardial cells and its change according to the capacitances, and/or calculating heart pumping blood flow according to the resistances; and obtaining an overall longitudinal elastic state of the heart according to the average longitudinal length of the myocardial cells and its change and/or the heart pumping blood flow.
A method of forming a laminate, the method comprising: providing a metal substrate including a sintered layer, the sintered layer sintered from bronze particles; electrostatic spraying the metal substrate with a non-fluorinated thermoplastic powder selected from a poly-ether-ether-ketone (PEEK), an ultra-high-molecular-weight polyethylene (UHMWPE), a polyimide (PI), a polyamide (PA), a polyamideimide (PAI), or any combination thereof, and covering the bronze particles with the non-fluorinated thermoplastic powder to form a transition layer; spraying the transition layer with a fluorinated thermoplastic powder selected from polytetrafluoroethylene (PTFE), a perfluoroalkoxy polymer (PFA), fluorinated ehylene-propylene (FEP), polyvinylfluoride (PVF), polyvinylidene fluoride (PVDF), polychlorotrifluoroethylene (PCTFE), a polyethylenetetrafluoroethylene (ETFE), a polyethylenechlorotrifluoroethylene (ECTFE), or any combination thereof to form a compound layer; wherein the non-fluorinated thermoplastic powder has an average particle size of at least 1 micron, wherein the fluorinated thermoplastic powder comprises a filler comprising molybdenum disulfide and graphite. providing a metal substrate including a sintered layer, the sintered layer sintered from bronze particles; electrostatic spraying the metal substrate with a non-fluorinated thermoplastic powder selected from a poly-ether-ether-ketone (PEEK), an ultra-high-molecular-weight polyethylene (UHMWPE), a polyimide (PI), a polyamide (PA), a polyamideimide (PAI), or any combination thereof, and covering the bronze particles with the non-fluorinated thermoplastic powder to form a transition layer; spraying the transition layer with a fluorinated thermoplastic powder selected from polytetrafluoroethylene (PTFE), a perfluoroalkoxy polymer (PFA), fluorinated ehylene-propylene (FEP), polyvinylfluoride (PVF), polyvinylidene fluoride (PVDF), polychlorotrifluoroethylene (PCTFE), a polyethylenetetrafluoroethylene (ETFE), a polyethylenechlorotrifluoroethylene (ECTFE), or any combination thereof to form a compound layer; wherein the non-fluorinated thermoplastic powder has an average particle size of at least 1 micron, wherein the fluorinated thermoplastic powder comprises a filler comprising molybdenum disulfide and graphite.
A method comprising: presenting , on a display device of an autonomous vehicle, a user interface (2300, 3000a/b) comprising: a visual representation of an environment surrounding the autonomous vehicle, a first display element indicating a physical location of the autonomous vehicle with respect to the environment, and a plurality of second display elements, each second display element of the plurality of second display elements indicating a respective operational property of the autonomous vehicle, wherein, respectively, at least one second display element indicates an object detected by the autonomous vehicle, indicates a classification of the object detected by the autonomous vehicle, and indicates a confidence metric associated with the classification of the object detected by the autonomous vehicle; receiving , through the user interface, a user input specifying an operation to be performed by the autonomous vehicle; and responsive to receiving the user input, performing the specified operation using the autonomous vehicle. presenting , on a display device of an autonomous vehicle, a user interface (2300, 3000a/b) comprising: a visual representation of an environment surrounding the autonomous vehicle, a first display element indicating a physical location of the autonomous vehicle with respect to the environment, and a plurality of second display elements, each second display element of the plurality of second display elements indicating a respective operational property of the autonomous vehicle, wherein, respectively, at least one second display element indicates an object detected by the autonomous vehicle, indicates a classification of the object detected by the autonomous vehicle, and indicates a confidence metric associated with the classification of the object detected by the autonomous vehicle; a visual representation of an environment surrounding the autonomous vehicle, a first display element indicating a physical location of the autonomous vehicle with respect to the environment, and a plurality of second display elements, each second display element of the plurality of second display elements indicating a respective operational property of the autonomous vehicle, wherein, respectively, at least one second display element indicates an object detected by the autonomous vehicle, indicates a classification of the object detected by the autonomous vehicle, and indicates a confidence metric associated with the classification of the object detected by the autonomous vehicle; indicates an object detected by the autonomous vehicle, indicates a classification of the object detected by the autonomous vehicle, and indicates a confidence metric associated with the classification of the object detected by the autonomous vehicle; receiving , through the user interface, a user input specifying an operation to be performed by the autonomous vehicle; and responsive to receiving the user input, performing the specified operation using the autonomous vehicle.
A method in a frequency division duplexing system, the method comprising: establishing a connection between a terminal and a current sector serving the terminal via a first frequency channel for a first link, wherein the first link is a downlink, and a second frequency channel for a second link, wherein the second link is an uplink, for utilizing frequency division duplexing; obtaining a selection of a third frequency channel from a set of frequency channels available in the current sector for the first link; switching the connection to the third frequency channel for the first link while maintaining the connection between the terminal and the current sector via the second frequency channel for the second link, wherein the first and second frequency channels have a first frequency distance that is different than a second frequency distance between the second and third frequency channels; and obtaining a selection of a fourth frequency channel for the second link and switching the connection to the fourth frequency channel for the second link, wherein the third and fourth frequency channels have a third frequency distance that is different than at least one of the first and second frequency distances, wherein the selection of the third frequency channel is made using sector information comprising Quality of Service, QoS, information for each frequency channel in the set of frequency channels, and wherein the selection of the fourth channel is made using sector information comprising QoS information for multiple uplink channels available for use. establishing a connection between a terminal and a current sector serving the terminal via a first frequency channel for a first link, wherein the first link is a downlink, and a second frequency channel for a second link, wherein the second link is an uplink, for utilizing frequency division duplexing; obtaining a selection of a third frequency channel from a set of frequency channels available in the current sector for the first link; switching the connection to the third frequency channel for the first link while maintaining the connection between the terminal and the current sector via the second frequency channel for the second link, wherein the first and second frequency channels have a first frequency distance that is different than a second frequency distance between the second and third frequency channels; and obtaining a selection of a fourth frequency channel for the second link and switching the connection to the fourth frequency channel for the second link, wherein the third and fourth frequency channels have a third frequency distance that is different than at least one of the first and second frequency distances, wherein the selection of the third frequency channel is made using sector information comprising Quality of Service, QoS, information for each frequency channel in the set of frequency channels, and wherein the selection of the fourth channel is made using sector information comprising QoS information for multiple uplink channels available for use.
A paper feeding device comprising: a paper feed cassette on which a paper bundle in which a plurality of sheets of paper are stacked is able to be placed; an alignment component which is able to align the paper bundle placed on the paper feed cassette ; a fan which is connected to the alignment component and able to generate airflow; a fan guiding duct component connected to the alignment component , positioned above the paper bundle placed on the paper feed cassette , and configured to generate a negative pressure between the fan guiding duct component and the uppermost sheet of paper in the paper bundle due to the airflow from the fan , characterized in that the paper feeding device further comprises: a connecting member which connects the fan and the fan guiding duct component , wherein: the alignment component includes an engaging recess which detachably engages the connecting member , the connecting member has a rectangular cylindrical shape, wherein the connecting member includes an air blowout port that opens so that airflow from the fan flows toward a space between the upper surface of the uppermost sheet of paper and the lower surface of the fan guiding duct component . a paper feed cassette on which a paper bundle in which a plurality of sheets of paper are stacked is able to be placed; an alignment component which is able to align the paper bundle placed on the paper feed cassette ; a fan which is connected to the alignment component and able to generate airflow; a fan guiding duct component connected to the alignment component , positioned above the paper bundle placed on the paper feed cassette , and configured to generate a negative pressure between the fan guiding duct component and the uppermost sheet of paper in the paper bundle due to the airflow from the fan , characterized in that the paper feeding device further comprises: a connecting member which connects the fan and the fan guiding duct component , wherein: the alignment component includes an engaging recess which detachably engages the connecting member , the connecting member has a rectangular cylindrical shape, wherein the connecting member includes an air blowout port that opens so that airflow from the fan flows toward a space between the upper surface of the uppermost sheet of paper and the lower surface of the fan guiding duct component . the alignment component includes an engaging recess which detachably engages the connecting member , the connecting member has a rectangular cylindrical shape, wherein the connecting member includes an air blowout port that opens so that airflow from the fan flows toward a space between the upper surface of the uppermost sheet of paper and the lower surface of the fan guiding duct component .
A method for determining a sufficient removal force (F A ), comprising the following steps: - providing an implant securely clamped to a catheter part, wherein the catheter part and implant extend along an axial direction (z), such that a removal force (F A ) on the catheter part in the axial direction (z) has to be exceeded in order to move the catheter part relative to the implant in the axial direction (z), - clamping the implant securely clamped on the catheter part between a first and a second holding jaw with a predefined contact pressure (F B ) perpendicularly to the axial direction (z), - exerting a predefined, desired removal force (F A ) on the catheter part in the axial direction (z), at which the catheter part should not move relative to the implant in the axial direction (z), wherein, if the catheter part moves relative to the implant in the axial direction (z), the removal force (F A ) of the implant is considered to be too low, and wherein if the position of the implant relative to the catheter part (F A ) is constant, the removal force (F A ) of the implant is considered to be sufficient. - providing an implant securely clamped to a catheter part, wherein the catheter part and implant extend along an axial direction (z), such that a removal force (F A ) on the catheter part in the axial direction (z) has to be exceeded in order to move the catheter part relative to the implant in the axial direction (z), - clamping the implant securely clamped on the catheter part between a first and a second holding jaw with a predefined contact pressure (F B ) perpendicularly to the axial direction (z), - exerting a predefined, desired removal force (F A ) on the catheter part in the axial direction (z), at which the catheter part should not move relative to the implant in the axial direction (z), wherein, if the catheter part moves relative to the implant in the axial direction (z), the removal force (F A ) of the implant is considered to be too low, and wherein if the position of the implant relative to the catheter part (F A ) is constant, the removal force (F A ) of the implant is considered to be sufficient.
A refrigerant pipe constituting a refrigerant circuit of a refrigeration apparatus, the refrigerant pipe comprising: a pipe body made of stainless steel; and a connecting tube made of copper or a copper alloy and provided to connect a different refrigerant pipe ; wherein the connecting tube is connected to an outer circumferential surface of an end in a pipe axis direction of the pipe body , and the connecting tube has an entirety in the pipe axis direction overlapped with the pipe body in a pipe diameter direction; characterized in that the connecting tube is brazed to the end of the pipe body with use of a first brazing filler material (B1), and the first brazing filler material (B1) is higher in melting point than a second brazing filler material (B2) used to braze the different refrigerant pipe to the connecting tube . a pipe body made of stainless steel; and a connecting tube made of copper or a copper alloy and provided to connect a different refrigerant pipe ; wherein the connecting tube is connected to an outer circumferential surface of an end in a pipe axis direction of the pipe body , and the connecting tube has an entirety in the pipe axis direction overlapped with the pipe body in a pipe diameter direction; characterized in that the connecting tube is brazed to the end of the pipe body with use of a first brazing filler material (B1), and the first brazing filler material (B1) is higher in melting point than a second brazing filler material (B2) used to braze the different refrigerant pipe to the connecting tube .
Electronic assembly (E) comprising at least two pieces of electronic equipment (10, C1, C2, C3, C4) connected together by an avionics network and/or by a direct link, characterized in that at least one of the at least two pieces of electronic equipment comprises an electronic device for the centralized computation and diffusion of the state(s) of an aircraft, and at least one of the at least two pieces of electronic equipment comprises at least one consumer avionics device (C1, C2, C3, C4) of at least one value of at least one state of the said aircraft, the electronic device for the centralized computation and diffusion being configured for at least : - calculate the value of one or more distinct aircraft state(s), characterized in that the electronic device for the centralized computation and diffusion is further configured for: - generate a list of aircraft state(s) whose value is suitable to be accessible via the electronic device for the centralized computation and diffusion, the list comprising, for each aircraft state(s), at least one representative item of information of the said aircraft state, - diffuse the list to each consumer avionics device (C1, C2, C3, C4) of at least one value of at least one state of the said aircraft, - receive, from at least one consumer avionics device (C1, C2, C3, C4), at least one request for transmission of one or more values of at least one first aircraft state selected from the list, the request comprising the said at least one representative information related to the said at least one first selected aircraft state, - transmit, to the said at least one consumer avionics device (C1, C2, C3, C4), only the value or values of the said at least one selected aircraft state. - calculate the value of one or more distinct aircraft state(s), - generate a list of aircraft state(s) whose value is suitable to be accessible via the electronic device for the centralized computation and diffusion, the list comprising, for each aircraft state(s), at least one representative item of information of the said aircraft state, - diffuse the list to each consumer avionics device (C1, C2, C3, C4) of at least one value of at least one state of the said aircraft, - receive, from at least one consumer avionics device (C1, C2, C3, C4), at least one request for transmission of one or more values of at least one first aircraft state selected from the list, the request comprising the said at least one representative information related to the said at least one first selected aircraft state, - transmit, to the said at least one consumer avionics device (C1, C2, C3, C4), only the value or values of the said at least one selected aircraft state.