mhurhangee/patent-ind-claim-en huggingface dataset:
A method for sealing a pouch casing of a pouch-type secondary battery, which comprises the steps of: a receiving step (S10) in which an electrode assembly is received in an inner space formed between an upper pouch and a lower pouch ; and a sealing step (S20) in which a first pressure is applied to an outer circumferential sealing portion, where the upper pouch and the lower pouch are sealed, in the longitudinal direction, and then the pressure is relieved, wherein the sealing step (S20) is carried out by applying external force to the upper pouch in the upward direction (D) and to the lower pouch in the downward direction (D'), or by applying a second pressure working in perpendicular to the first pressure to the sealing portion from the inner part of the pouch casing in a direction (E) toward the outside, wherein the extent of the external force applied to the upper pouch in the upward direction is 2-5 times of the weight of the upper pouch , and the extent of the external force applied to the lower pouch in the downward direction is 2-5 times of the weight of the lower pouch , wherein the external force application time in the sealing step is 1.5-2 times of the first pressure application time, wherein the second pressure in the sealing step is 0.1-0.15 MPa, and wherein the second pressure application time in the sealing step is 1.5-2 times of the first pressure application time. a receiving step (S10) in which an electrode assembly is received in an inner space formed between an upper pouch and a lower pouch ; and a sealing step (S20) in which a first pressure is applied to an outer circumferential sealing portion, where the upper pouch and the lower pouch are sealed, in the longitudinal direction, and then the pressure is relieved, wherein the sealing step (S20) is carried out by applying external force to the upper pouch in the upward direction (D) and to the lower pouch in the downward direction (D'), or by applying a second pressure working in perpendicular to the first pressure to the sealing portion from the inner part of the pouch casing in a direction (E) toward the outside, wherein the extent of the external force applied to the upper pouch in the upward direction is 2-5 times of the weight of the upper pouch , and the extent of the external force applied to the lower pouch in the downward direction is 2-5 times of the weight of the lower pouch , wherein the external force application time in the sealing step is 1.5-2 times of the first pressure application time, wherein the second pressure in the sealing step is 0.1-0.15 MPa, and wherein the second pressure application time in the sealing step is 1.5-2 times of the first pressure application time.
A computer-implemented method for processing seismic data corresponding to a subsurface, the method comprising: receiving input seismic data (d i ) provided by a receiver comprising N spatial coordinates, wherein the input seismic data is in a first spatial domain; expanding the N spatial coordinates of the input seismic data (d i ) to N' modified spatial coordinates, where N' is greater than N, to provide spatially expanded seismic data (d e ) that is in a second spatial domain, characterized in that expanding said N spatial coordinates is conducted by executing a mapping function for each coordinate associated with the spatially expanded seismic data, thereby replacing non-linear responses in the input seismic data (d ¡ ) with pseudo-linear responses in the spatially expanded seismic data (d e ); transforming the spatially expanded seismic data (d e ) to a model domain to provide model domain data (d m ); and generating a final image (d f ) of the subsurface using the model domain data (d m ). wherein the input seismic data is in a first spatial domain; expanding the N spatial coordinates of the input seismic data (d i ) to N' modified spatial coordinates, where N' is greater than N, to provide spatially expanded seismic data (d e ) that is in a second spatial domain, characterized in that expanding said N spatial coordinates is conducted by executing a mapping function for each coordinate associated with the spatially expanded seismic data, thereby replacing non-linear responses in the input seismic data (d ¡ ) with pseudo-linear responses in the spatially expanded seismic data (d e ); transforming the spatially expanded seismic data (d e ) to a model domain to provide model domain data (d m ); and generating a final image (d f ) of the subsurface using the model domain data (d m ). transforming the spatially expanded seismic data (d e ) to a model domain to provide model domain data (d m ); and generating a final image (d f ) of the subsurface using the model domain data (d m ).
A gold sputtering target consisting of 99.99% or more gold and balancing inevitable impurities, comprising: a surface to be sputtered, wherein an average value of Vickers hardness is 40 or more and 60 or less, an average crystal grain size is 15 μm or more and 200 μm or less, and a { 1 10} plane of gold is preferentially oriented at the surface, wherein the average value of Vickers hardness is measured in accordance with the specifics given in the description and wherein the average crystal grain size is calculated on the basis of average values of the crystal grain sizes at the sputtering surface, the first cross-section, and the second cross-section in accordance with the specifics given in the description. an average value of Vickers hardness is 40 or more and 60 or less, an average crystal grain size is 15 μm or more and 200 μm or less, and a { 1 10} plane of gold is preferentially oriented at the surface, wherein the average value of Vickers hardness is measured in accordance with the specifics given in the description and wherein the average crystal grain size is calculated on the basis of average values of the crystal grain sizes at the sputtering surface, the first cross-section, and the second cross-section in accordance with the specifics given in the description.
A flexible and/or an elastic component, comprising an at least partially flexible and/or elastic substrate having a front side and a rear side as well as at least one electrically conductive elastomer matrix layer arranged regionally on the front side or the rear side of the substrate , the front side or the rear side of the substrate including at least one sub-region having the electrically conductive elastomer matrix layer arranged thereon and at least one sub-region having no electrically conductive elastomer matrix layer arranged thereon, the at least one elastomer matrix layer comprising at least one electrically conductive particulate filler, and wherein at least one electrically conductive metal layer is disposed at least regionally on the at least one elastomer matrix layer .
A microchip comprising: a channel permitting a sheath liquid to flow therethrough; a microtube configured to introduce a sample liquid containing particulates into a laminar flow of said sheath liquid flowing through said channel , wherein liquid feeding is performed in the condition where a laminar flow of said sample liquid introduced through said microtube is surrounded by said laminar flow of said sheath liquid; wherein said channel has a narrow-down section in which its area in a section orthogonal to the liquid feed direction decreases gradually or stepwise along the liquid feed direction, said sheath liquid laminar flow and said sample liquid laminar flow are made to pass while the laminar flow widths of said laminar flows are narrowed down in said narrow-down section; characterized by at least a fluid introduction inlet provided, as seen in a plan view, on a lateral side of the channel at a joining section located downstream of the narrow-down section , said fluid introduction inlet being adapted to introduce a fluid into the channel and to split the laminar flow of said sheath liquid surrounding said sample fluid into droplets. a channel permitting a sheath liquid to flow therethrough; a microtube configured to introduce a sample liquid containing particulates into a laminar flow of said sheath liquid flowing through said channel , wherein liquid feeding is performed in the condition where a laminar flow of said sample liquid introduced through said microtube is surrounded by said laminar flow of said sheath liquid; wherein said channel has a narrow-down section in which its area in a section orthogonal to the liquid feed direction decreases gradually or stepwise along the liquid feed direction, said sheath liquid laminar flow and said sample liquid laminar flow are made to pass while the laminar flow widths of said laminar flows are narrowed down in said narrow-down section; characterized by at least a fluid introduction inlet provided, as seen in a plan view, on a lateral side of the channel at a joining section located downstream of the narrow-down section , said fluid introduction inlet being adapted to introduce a fluid into the channel and to split the laminar flow of said sheath liquid surrounding said sample fluid into droplets.
Method for determining a position of a unit by means of satellite navigation, wherein the method includes the following steps: - receiving a plurality of satellite signals, namely at least - a first satellite signal, - a second satellite signal, - a third satellite signal, and - a fourth satellite signal, - performing a plurality of Doppler measurements on the satellite signals, in the process producing - a first Doppler value on the basis of the first satellite signal, - a second Doppler value on the basis of the second satellite signal, - a third Doppler value on the basis of the third satellite signal, and - a fourth Doppler value on the basis of the fourth satellite signal, - calculating the position on the basis of the first Doppler value, the second Doppler value, the third Doppler value and the fourth Doppler value, wherein the position is a variable of the calculation, - wherein, further, during the reception step, a further satellite navigation signal is received and - wherein the method further includes the following steps: - performing a time-of-flight measurement on the basis of the further satellite navigation signal, producing a time-of-flight value in the process, and - calculating a clock error of the unit on the basis of the position and the time-of-flight value. - receiving a plurality of satellite signals, namely at least - a first satellite signal, - a second satellite signal, - a third satellite signal, and - a fourth satellite signal, - a first satellite signal, - a second satellite signal, - a third satellite signal, and - a fourth satellite signal, - performing a plurality of Doppler measurements on the satellite signals, in the process producing - a first Doppler value on the basis of the first satellite signal, - a second Doppler value on the basis of the second satellite signal, - a third Doppler value on the basis of the third satellite signal, and - a fourth Doppler value on the basis of the fourth satellite signal, - calculating the position on the basis of the first Doppler value, the second Doppler value, the third Doppler value and the fourth Doppler value, wherein the position is a variable of the calculation, - wherein, further, during the reception step, a further satellite navigation signal is received and - wherein the method further includes the following steps: - performing a time-of-flight measurement on the basis of the further satellite navigation signal, producing a time-of-flight value in the process, and - calculating a clock error of the unit on the basis of the position and the time-of-flight value.
A three-dimensional printing system, comprising: a fabrication bed ; a polymer build material on the fabrication bed, wherein the build material has a melting point ranging from 55 °C to 450 °C; a coalescing agent on the build material in the fabrication bed, the coalescing agent including: a co-solvent having a boiling point of less than 300°C; a surfactant having a hydrophilic lipophilic balance (HLB) value that is less than 10; a carbon black pigment; a polymeric dispersant; and a balance of water; an inkjet applicator configured to dispense the coalescing agent; and a radiation source exposing the coalescing agent and the build material in the fabrication bed to electromagnetic radiation; wherein the co-solvent is present in an amount ranging from 15 wt% to 30 wt% of a total wt% of the coalescing agent; the surfactant is present in an amount ranging from 0.5 wt% to 1.4 wt% of the total wt% of the coalescing agent; and the carbon black pigment is present in an amount ranging from 3.0 wt% to 6.0 wt% of the total wt% of the coalescing agent. a fabrication bed ; a polymer build material on the fabrication bed, wherein the build material has a melting point ranging from 55 °C to 450 °C; a coalescing agent on the build material in the fabrication bed, the coalescing agent including: a co-solvent having a boiling point of less than 300°C; a surfactant having a hydrophilic lipophilic balance (HLB) value that is less than 10; a carbon black pigment; a polymeric dispersant; and a balance of water; a co-solvent having a boiling point of less than 300°C; a surfactant having a hydrophilic lipophilic balance (HLB) value that is less than 10; a carbon black pigment; a polymeric dispersant; and a balance of water; an inkjet applicator configured to dispense the coalescing agent; and a radiation source exposing the coalescing agent and the build material in the fabrication bed to electromagnetic radiation; wherein the co-solvent is present in an amount ranging from 15 wt% to 30 wt% of a total wt% of the coalescing agent; the surfactant is present in an amount ranging from 0.5 wt% to 1.4 wt% of the total wt% of the coalescing agent; and the carbon black pigment is present in an amount ranging from 3.0 wt% to 6.0 wt% of the total wt% of the coalescing agent.
A method of making a structural bonding adhesive comprising: mixing a first curable resin and a second curable resin to provide an uncured adhesive; and irradiating the uncured adhesive using a first actinic light source to polymerize the first curable resin selectively without polymerizing the second curable resin thereby providing a partially cured adhesive with reduced cold flow creep under ambient conditions, wherein the partially cured adhesive is a pressure-sensitive adhesive and is capable of being fully cured by irradiating the partially cured adhesive using a second actinic light source different from the first actinic light source to polymerize the second curable resin, and the partially cured adhesive displays a cold flow creep recovery of at least 40 percent as measured according to the General Creep and Creep-Recovery Test and Creep and Creep-Recovery Test 1 as disclosed in the description. mixing a first curable resin and a second curable resin to provide an uncured adhesive; and irradiating the uncured adhesive using a first actinic light source to polymerize the first curable resin selectively without polymerizing the second curable resin thereby providing a partially cured adhesive with reduced cold flow creep under ambient conditions, wherein the partially cured adhesive is a pressure-sensitive adhesive and is capable of being fully cured by irradiating the partially cured adhesive using a second actinic light source different from the first actinic light source to polymerize the second curable resin, and the partially cured adhesive displays a cold flow creep recovery of at least 40 percent as measured according to the General Creep and Creep-Recovery Test and Creep and Creep-Recovery Test 1 as disclosed in the description.
Extruded product made from alloy of composition (% by weight): Cu: 5.05 - 5.35 Mg: 0.20 - 0.40 Mn: 020 - 0.40 Zr: 0.08 - 0.15 Ti: 0.01 - 0.15 Zn: 0 - 0.15 Si < 0.10 Fe < 0.15 other elements < 0.05 each and < 0.15 in total, remainder Al, treated by solution heat treatment, quenching, controlled stretching and aging.
Screen device comprising a screen and a screen slat , which is fittable to a screen edge of the screen , wherein the screen , on this screen edge , is provided with a fitting element which is attached to or forms part of the screen , wherein the screen slat comprises a fitting slot , in which this fitting element is at least partly accommodable for fitting the screen slat to the said screen edge of the screen ,wherein the screen slat comprises an access opening to this fitting slot , through which the screen and/or the fitting element extends in the installed position, and wherein the screen slat is provided with a flange which at least partly delimits the access opening to the fitting slot , the screen device furthermore comprising one or several click-action means which are at least partly elastic in order to attach the fitting element in the fitting slot by means of a click-fit connection via the access opening , characterised in that the click-action means form part of the fitting element and/or of one or several separate click-fit elements and comprise at least one elastically displaceable click-fit leg which, in the mounted position, engages behind the flange in order to achieve the click-fit connection and which serves as a detaining element which, in the mounted position, prevents the click-action means from breaking loose from the fitting slot .
A power supply device comprising: a battery stack in which battery cells are stacked, each of battery cells including a gas discharge valve that opens when an internal pressure of an outer covering can rises and an electrode disposed on an upper surface; a first cover that is provided on an upper surface of the battery stack and opens at a position corresponding to the gas discharge valve of each of the battery cells ; and a second cover that is provided above an upper surface of the first cover and defines a gas duct between the first cover and the second cover , wherein the gas duct includes a baffle plate between the first cover and a second cover , wherein the baffle plate is configured to bend the gas discharge path in the gas duct , to reduce the momentum and to lower the temperature to safely discharge the gas to the outside, and the power supply device further comprises a third cover that is provided on an upper surface of the second cover and abuts on an upper surface of the second cover , third cover being made of metal. a battery stack in which battery cells are stacked, each of battery cells including a gas discharge valve that opens when an internal pressure of an outer covering can rises and an electrode disposed on an upper surface; a first cover that is provided on an upper surface of the battery stack and opens at a position corresponding to the gas discharge valve of each of the battery cells ; and a second cover that is provided above an upper surface of the first cover and defines a gas duct between the first cover and the second cover , wherein the gas duct includes a baffle plate between the first cover and a second cover , wherein the baffle plate is configured to bend the gas discharge path in the gas duct , to reduce the momentum and to lower the temperature to safely discharge the gas to the outside, and the power supply device further comprises a third cover that is provided on an upper surface of the second cover and abuts on an upper surface of the second cover , third cover being made of metal.
Method for manufacturing a synthetic stone for a timepiece from a mineral body of monocrystalline type, the stone comprising a hole , said method comprising an ablation step in which the body is subjected to the ablation of material by scanning at least one face of the body with ultra-short pulse laser radiation for a duration of less than one hundred picoseconds, and the ray of which is guided by precession system of at least three axes configured to at least partially cancel the conical focusing angle of said laser, the laser ablation step comprising the recessing of an entrance cone of the hole .
A method for controlling a cylinder , comprising steps in which: - a cylinder is provided comprising a cylinder body and a piston translationally movable inside the cylinder body; - a servo valve is provided, configured to regulate the power supplied to said cylinder, in such a way as to control the position of the piston in the cylinder body; - a measuring device is provided comprising at least one first position sensor and one second position sensor ; - measurements (X 1 ,X 2 ) are taken of the position of the piston in the cylinder body simultaneously with the first position sensor and the second position sensor; - at least one first displacement speed (v 1 ) of the piston is determined on the basis of the piston position measurements obtained with the first position sensor; - at least one second displacement speed (v 2 ) of the piston is determined on the basis of the piston position measurements obtained with the second position sensor; - the presence of at least one malfunctioning position sensor is detected; then - when the presence of a malfunctioning position sensor is detected, each of the first and second determined displacement speeds of the piston are compared with a modelled (v mod ) or predetermined displacement speed of the piston, in such a way as to identify the most reliable position sensor, characterized in that a counter is initiated as soon as the presence of a malfunctioning position sensor is detected and the step of comparing the first and second determined displacement speeds (v 1 , v 2 ) of the piston with a modeled (v mod ) or predetermined displacement speed of the piston is stopped when the value of the counter is greater than a threshold of the counter. - a cylinder is provided comprising a cylinder body and a piston translationally movable inside the cylinder body; - a servo valve is provided, configured to regulate the power supplied to said cylinder, in such a way as to control the position of the piston in the cylinder body; - a measuring device is provided comprising at least one first position sensor and one second position sensor ; - measurements (X 1 ,X 2 ) are taken of the position of the piston in the cylinder body simultaneously with the first position sensor and the second position sensor; - at least one first displacement speed (v 1 ) of the piston is determined on the basis of the piston position measurements obtained with the first position sensor; - at least one second displacement speed (v 2 ) of the piston is determined on the basis of the piston position measurements obtained with the second position sensor; - the presence of at least one malfunctioning position sensor is detected; then - when the presence of a malfunctioning position sensor is detected, each of the first and second determined displacement speeds of the piston are compared with a modelled (v mod ) or predetermined displacement speed of the piston, in such a way as to identify the most reliable position sensor,