mhurhangee/patent-ind-claim-en huggingface dataset:
Method for operating an inductive conductivity measuring device , wherein the conductivity measuring device has a transmitting coil and a receiving coil , the transmitting coil has an input and the transmitting coil and the receiving coil are inductively coupled to one another by an electrically conductive medium and wherein an electrical preset alternating signal (U V ) is generated and fed to the input of the transmitting coil , characterized in that a frequency of the preset alternating signal (Uv) is varied in a frequency interval, that , in the frequency interval, a frequency-dependent minimum input impedance at the input of the transmitting coil is determined using a response alternating signal (U M ), that a minimum frequency of the response alternating signal (U M ) is determined at the minimum input impedance at the input of the transmitting coil , and that a conductivity of the medium is determined using the minimum frequency of the response alternating signal (U M ). wherein the conductivity measuring device has a transmitting coil and a receiving coil , the transmitting coil has an input and the transmitting coil and the receiving coil are inductively coupled to one another by an electrically conductive medium and wherein an electrical preset alternating signal (U V ) is generated and fed to the input of the transmitting coil , characterized in that a frequency of the preset alternating signal (Uv) is varied in a frequency interval, that , in the frequency interval, a frequency-dependent minimum input impedance at the input of the transmitting coil is determined using a response alternating signal (U M ), that a minimum frequency of the response alternating signal (U M ) is determined at the minimum input impedance at the input of the transmitting coil , and that a conductivity of the medium is determined using the minimum frequency of the response alternating signal (U M ).
Electrical contacting interface with a low and stable electrical transfer resistance comprising at least two contacting components , which interact for electrical contacting, wherein, in the case of one of the two contacting components , in the region of a contacting surface there is formed a structuring that protrudes out of the plane of the contacting surface of the one contacting component , the structuring being deformed under the influence of a mechanical force and causing a corresponding deformation in the form of a depression in the opposite contacting component , the structure that is protruding out of the plane being formed such that, even after the deformation caused in the opposite contacting component, the flat regions of the two contacting surfaces do not touch, and so the electrical current is forced to flow exclusively via the contacting surface created during the deformation process, such that the current transfer surfaces are exactly localized, characterized in that the structuring takes the form of crater-shaped projections, introduced with a centre punch, around a through-hole for a screwing operation.
A manufacturing method for a radiation detector , comprising: a process of coating an adhesion layer onto a reinforcement substrate having a size according to the size of a radiation detector ; a process of forming a substrate by providing a flexible base member to a support body with a separation layer interposed between the base member and the support body , and providing a plurality of pixels in a pixel region of the base member , the plurality of pixels accumulates charges generated in response to light converted from radiation; a process of forming a conversion layer that converts the radiation into light at a surface to which the pixel region of the base member is provided; a process of affixing the reinforcement substrate at a surface of the conversion layer opposite to a surface that faces a surface of the substrate side using the adhesion layer on the reinforcement substrate , the reinforcement substrate containing a material having a yield point and having a higher rigidity than the base member ; and a process of separating the substrate provided with the conversion layer and the reinforcement substrate from the support body . a process of coating an adhesion layer onto a reinforcement substrate having a size according to the size of a radiation detector ; a process of forming a substrate by providing a flexible base member to a support body with a separation layer interposed between the base member and the support body , and providing a plurality of pixels in a pixel region of the base member , the plurality of pixels accumulates charges generated in response to light converted from radiation; a process of forming a conversion layer that converts the radiation into light at a surface to which the pixel region of the base member is provided; a process of affixing the reinforcement substrate at a surface of the conversion layer opposite to a surface that faces a surface of the substrate side using the adhesion layer on the reinforcement substrate , the reinforcement substrate containing a material having a yield point and having a higher rigidity than the base member ; and a process of separating the substrate provided with the conversion layer and the reinforcement substrate from the support body .
A sintered bearing comprising: a bearing sleeve formed of a sintered material, a shaft hole being formed therein; an annular ring-shaped seal member that is disposed such that one surface thereof comes into contact with the bearing sleeve ; and a washer member that comes into contact with another surface of the seal member on a side opposite to the one surface and is configured for the seal member to engage with the bearing sleeve , wherein the washer member is fixed to the bearing sleeve , and the annular ring-shaped seal member has an inner circumferential surface , an inner diameter of the inner circumferential surface being smaller than a diameter of the shaft hole , characterized in that the seal member is firmly sandwiched between the bearing sleeve and the washer member which are engaged with each other due to caulking portions . a bearing sleeve formed of a sintered material, a shaft hole being formed therein; an annular ring-shaped seal member that is disposed such that one surface thereof comes into contact with the bearing sleeve ; and a washer member that comes into contact with another surface of the seal member on a side opposite to the one surface and is configured for the seal member to engage with the bearing sleeve , wherein the washer member is fixed to the bearing sleeve , and the annular ring-shaped seal member has an inner circumferential surface , an inner diameter of the inner circumferential surface being smaller than a diameter of the shaft hole , characterized in that the seal member is firmly sandwiched between the bearing sleeve and the washer member which are engaged with each other due to caulking portions .
Device for loading medical containers on dosing machines, which comprises an adaptor for medical containers and a support for said adaptor, wherein the support comprises attachment means to a dosing machine, characterised in that said adaptor and said support are independent between them and comprise means for pivoting relative to one another and means for clipping to each other, the pivoting means comprising at least one pivot and at least one paired surface in a recess, the pivot comprising a rounded projection with a rounded surface which allows pivoting between the support and the adaptor when the rounded projection is placed in the recess so that the rounded projection and the paired surface come in contact with one another, said clipping means being arranged in such a way that the pivoting of the adaptor and of the support by means of the pivoting means produces the clipping together of the adaptor and the support.
A vehicle body lower structure (S1, S2) comprising: a side sill ; a center tunnel ; a floor panel disposed between the side sill and the center tunnel ; and first and second frame members connected to a front side member , wherein the first frame member extends obliquely such that the first frame member is located more outward in a vehicle width direction as extending toward a vehicle body rear side, and is connected to the side sill , and the second frame member extends obliquely such that the second frame member is located more inward in the vehicle width direction as extending toward the vehicle body rear side, and is connected to the center tunnel , characterized in that one of the first and second frame members is provided on an upper surface of the floor panel and the other one of the first and second frame members is provided on a lower surface of the floor panel . a side sill ; a center tunnel ; a floor panel disposed between the side sill and the center tunnel ; and first and second frame members connected to a front side member , wherein the first frame member extends obliquely such that the first frame member is located more outward in a vehicle width direction as extending toward a vehicle body rear side, and is connected to the side sill , and the second frame member extends obliquely such that the second frame member is located more inward in the vehicle width direction as extending toward the vehicle body rear side, and is connected to the center tunnel , characterized in that one of the first and second frame members is provided on an upper surface of the floor panel and the other one of the first and second frame members is provided on a lower surface of the floor panel .
An apparatus comprising: a coil assembly comprising at least one winding configured to receive a varying electrical current; a core comprising multiple segments , the at least one winding wound around portions of the segments and configured to generate a magnetic flux; and cooling channels configured to transport coolant through the coil assembly or core in order to cool the coil assembly or core , wherein: portions of the segments of the core are separated from one another to form multiple cooling channels in a first direction through the core parallel to a direction of the magnetic flux; the multiple cooling channels are configured to transport the coolant through the core ; at least some segments of the core comprise protrusions that contact adjacent segments of the core to maintain separation of the segments and form the multiple cooling channels ; the core further comprises additional cooling channels in a second direction through the core generally orthogonal to the direction of the magnetic flux; and the segments comprise gaps forming the additional cooling channels in the second direction through the core . a coil assembly comprising at least one winding configured to receive a varying electrical current; a core comprising multiple segments , the at least one winding wound around portions of the segments and configured to generate a magnetic flux; and cooling channels configured to transport coolant through the coil assembly or core in order to cool the coil assembly or core , wherein: portions of the segments of the core are separated from one another to form multiple cooling channels in a first direction through the core parallel to a direction of the magnetic flux; the multiple cooling channels are configured to transport the coolant through the core ; at least some segments of the core comprise protrusions that contact adjacent segments of the core to maintain separation of the segments and form the multiple cooling channels ; the core further comprises additional cooling channels in a second direction through the core generally orthogonal to the direction of the magnetic flux; and the segments comprise gaps forming the additional cooling channels in the second direction through the core . portions of the segments of the core are separated from one another to form multiple cooling channels in a first direction through the core parallel to a direction of the magnetic flux; the multiple cooling channels are configured to transport the coolant through the core ; at least some segments of the core comprise protrusions that contact adjacent segments of the core to maintain separation of the segments and form the multiple cooling channels ; the core further comprises additional cooling channels in a second direction through the core generally orthogonal to the direction of the magnetic flux; and the segments comprise gaps forming the additional cooling channels in the second direction through the core .
Refrigeration device, in particular household refrigeration device, having a carcass , a heat-insulated inner container which is arranged in the carcass and forms a storage area for refrigerated items, and at least one door leaf which is attached to the carcass , can pivot about a vertical axis (A) and is mounted for opening and closing the storage area by means of a self-closing hinge assembly having a cam mechanism which has an engaging member and a cam member which interacts with the engaging member and which comprises a radial guideway along which the engaging member runs, characterised in that the engaging member has a counter-stop surface which is rigidly fastened to the engaging member and is embodied as flat, and the cam member has a fixed stop surface which limits the maximum opening angle of the door leaf and is embodied as flat, and which the counter-stop surface of the engaging member touches at the maximum opening angle of the door leaf , such that the fixed stop surface and the corresponding counter-stop surface meet in a plane lying perpendicular to their direction of approach when the maximum opening angle of the door leaf is reached.
A sound attenuating cell, comprising: a first sound attenuating cavity defined between a first sidewall and a second sidewall , the first sidewall opposite the second sidewall, the first sidewall including a first undulating surface and the second sidewall including a second undulating surface, with a deflector coupled to the first undulating surface, the deflector extending from the first undulating surface toward the second undulating surface, wherein the sound attenuating cell has a longitudinal axis (L10) and wherein the first undulating surface is axially misaligned with or offset from the second undulating surface to define a tortuous path between the first sidewall and the second sidewall, the first sound attenuating cavity having a first end and a second end, the first end opposite the second end, with an inlet and an outlet of the first sound attenuating cavity defined at the first end; and a second sound attenuating cavity nested within the inner perimeter of the first sound attenuating cavity. a first sound attenuating cavity defined between a first sidewall and a second sidewall , the first sidewall opposite the second sidewall, the first sidewall including a first undulating surface and the second sidewall including a second undulating surface, with a deflector coupled to the first undulating surface, the deflector extending from the first undulating surface toward the second undulating surface, wherein the sound attenuating cell has a longitudinal axis (L10) and wherein the first undulating surface is axially misaligned with or offset from the second undulating surface to define a tortuous path between the first sidewall and the second sidewall, the first sound attenuating cavity having a first end and a second end, the first end opposite the second end, with an inlet and an outlet of the first sound attenuating cavity defined at the first end; and a second sound attenuating cavity nested within the inner perimeter of the first sound attenuating cavity.
A system for an aircraft, the system comprising: an aircraft component that includes a heater routed through the aircraft component, the heater comprising: a resistive heating element ; and insulation surrounding the resistive heating element; wherein a first current flows into the resistive heating element to provide heating for the aircraft component and a second current flows out of the resistive heating element; a first sensor configured to produce a first sensor signal representing the first current; a second sensor configured to produce a second sensor signal representing the second current; a leakage sensor configured to produce a leakage sensor signal representing a leakage current; and a signal processor configured to sample and measure the first current, the second current, and a leakage current using a high frequency sampling rate to identify the presence of electric arcing; wherein the high frequency sampling rate is selected to be at least greater than two times the highest frequency of the electrical noise produced by the electric arcing. a resistive heating element ; and insulation surrounding the resistive heating element; wherein a first current flows into the resistive heating element to provide heating for the aircraft component and a second current flows out of the resistive heating element; a first sensor configured to produce a first sensor signal representing the first current; a second sensor configured to produce a second sensor signal representing the second current; a leakage sensor configured to produce a leakage sensor signal representing a leakage current; and a signal processor configured to sample and measure the first current, the second current, and a leakage current using a high frequency sampling rate to identify the presence of electric arcing; wherein the high frequency sampling rate is selected to be at least greater than two times the highest frequency of the electrical noise produced by the electric arcing.
A compound represented by Formula (I): or a stereoisomer or pharmaceutically acceptable salt thereof, wherein: X is -OR, =O, or -NR 1 R 2 ; R is H or C 1 -C 6 alkyl; R 1 and R 2 are each independently H, -C(O)-C 1 -C 6 alkyl, or R 1 and R 2 , together with the nitrogen atom to which they are attached, form a 5-, 8-, or 9-membered heteroaryl ring optionally comprising one or more additional heteroatoms selected from nitrogen, sulfur, and oxygen; u, v, and w together form (i), (ii), or (iii): y and z together form (v): and Het is heteroaryl comprising one or two 5- or 6-membered rings and 1-4 heteroatoms selected from nitrogen, sulfur, and oxygen, and optionally substituted, preferably with NH 2 , and wherein alkyl is optionally substituted. X is -OR, =O, or -NR 1 R 2 ; R is H or C 1 -C 6 alkyl; R 1 and R 2 are each independently H, -C(O)-C 1 -C 6 alkyl, or R 1 and R 2 , together with the nitrogen atom to which they are attached, form a 5-, 8-, or 9-membered heteroaryl ring optionally comprising one or more additional heteroatoms selected from nitrogen, sulfur, and oxygen; u, v, and w together form (i), (ii), or (iii): y and z together form (v): and Het is heteroaryl comprising one or two 5- or 6-membered rings and 1-4 heteroatoms selected from nitrogen, sulfur, and oxygen, and optionally substituted, preferably with NH 2 , and wherein alkyl is optionally substituted.
A process for preparing a liquid alkylated diphenylamine composition comprising from 80 wt% to 100 wt% of one or more di-alkylated diphenylamines wherein more than 50 wt% of the di-alkylated diphenylamines are 4,4'-di-alkylated diphenylamines, 15 wt% or less of mono-alkylated diphenylamines, and less than 2 wt% unsubstituted diphenylamine, wherein each alkyl group is selected from C 4-24 alkyl and wherein at least one alkyl group of at least one di-alkylated diphenylamine contains from 8 to 24 carbon atoms, wherein a reaction mixture comprising: a di-alkylated diphenylamine, less than 25% by weight of mono-alkylated diphenylamine, less than 6% by weight of non-alkylated diphenylamine, Lewis acid catalyst, and a first olefin present in a quantity sufficient to suppress dealkylation, wherein each wt% is based on the total weight of all substituted and unsubstituted diphenylamine compounds in the reaction mixture, is reacted with a second olefin in sufficient quantity to reduce the amount of mono-alkylated diphenylamine to 15 wt% or less of the total weight of substituted and unsubstituted diphenylamine compounds in the reaction mixture. a di-alkylated diphenylamine, less than 25% by weight of mono-alkylated diphenylamine, less than 6% by weight of non-alkylated diphenylamine, Lewis acid catalyst, and a first olefin present in a quantity sufficient to suppress dealkylation,
A method for selecting a packet loss concealment procedure, the method comprising: detecting an audio type of a received audio frame, wherein detecting an audio type comprises determining a stability of a spectral envelope of signals of received audio frames; and in response to detection of a frame loss, determining a packet loss concealment procedure based at least partially on the audio type of the preceding correctly received audio frame. detecting an audio type of a received audio frame, wherein detecting an audio type comprises determining a stability of a spectral envelope of signals of received audio frames; and in response to detection of a frame loss, determining a packet loss concealment procedure based at least partially on the audio type of the preceding correctly received audio frame.
A method of making a simulated tissue structure comprising the steps of: providing a mandrel having a first end, a second end, a longitudinal axis and an outer diameter; providing at least one elastic ring having a central aperture; the at least one elastic ring having a relaxed diameter smaller than the outer diameter of the mandrel; stretching the at least one elastic ring onto the mandrel traverse to the longitudinal axis into a position in which the mandrel is located inside the central aperture and the at least one elastic ring is expanded around the outer diameter of the mandrel; applying a layer of uncured silicone onto the mandrel and the at least one elastic ring; curing the layer to adhere the layer to the at least one elastic ring while the elastic ring is expanded; removing the layer and the at least one elastic ring from the mandrel after the step of curing the layer; and allowing the at least one elastic ring to return toward its relaxed diameter. providing a mandrel having a first end, a second end, a longitudinal axis and an outer diameter; providing at least one elastic ring having a central aperture; the at least one elastic ring having a relaxed diameter smaller than the outer diameter of the mandrel; stretching the at least one elastic ring onto the mandrel traverse to the longitudinal axis into a position in which the mandrel is located inside the central aperture and the at least one elastic ring is expanded around the outer diameter of the mandrel; applying a layer of uncured silicone onto the mandrel and the at least one elastic ring; curing the layer to adhere the layer to the at least one elastic ring while the elastic ring is expanded; removing the layer and the at least one elastic ring from the mandrel after the step of curing the layer; and allowing the at least one elastic ring to return toward its relaxed diameter.
A roof box for a public transport vehicle , especially a railway vehicle, the box delimiting an inner volume and including: - a case including a set of side walls each extending along a respective extension plane, and - a cover at least partly closing the case , characterised in that the cover includes at least one peripheral skirt located outside the case and defining with at least one said side wall a gutter , the box further comprising a sealant disposed in the gutter . - a case including a set of side walls each extending along a respective extension plane, and - a cover at least partly closing the case , characterised in that the cover includes at least one peripheral skirt located outside the case and defining with at least one said side wall a gutter , the box further comprising a sealant disposed in the gutter .