mhurhangee/patent-ind-claim-en huggingface dataset:
A computer-implemented method for predicting pore pressure in a subsurface geological environment, comprising: receiving velocity data for a target volume, the target volume comprising an array of measurement locations, each measurement location having an associated velocity value; performing geomechanical modeling for the target volume, wherein said geomechanical modeling comprises obtaining a total stress tensor across the target volume; determining, at a subset of measurement locations, a mean effective stress from a pore pressure value and the total stress tensor, wherein the velocity value and the pore pressure value are known at each of the subset of measurement locations; establishing a mathematical regression relationship between the velocity values and a surrogate stress at the subset of measurement locations, wherein the surrogate stress is an equivalent effective stress defined as the mean effective stress for a given porosity where the shear stress is zero; determining , at each measurement location, the surrogate stress based on the established mathematical regression relationship between the velocity values and the surrogate stress at the subset of measurement locations; determining , at each measurement location, a mean effective stress from the surrogate stress at each measurement location and the total stress tensor; determining a prediction of a pore pressure value for each measurement location within the target volume as the difference between a mean total stress from the total stress tensor and the mean effective stress at each measurement location; and outputting the result to an output device. receiving velocity data for a target volume, the target volume comprising an array of measurement locations, each measurement location having an associated velocity value; performing geomechanical modeling for the target volume, wherein said geomechanical modeling comprises obtaining a total stress tensor across the target volume; determining, at a subset of measurement locations, a mean effective stress from a pore pressure value and the total stress tensor, wherein the velocity value and the pore pressure value are known at each of the subset of measurement locations; establishing a mathematical regression relationship between the velocity values and a surrogate stress at the subset of measurement locations, wherein the surrogate stress is an equivalent effective stress defined as the mean effective stress for a given porosity where the shear stress is zero; determining , at each measurement location, the surrogate stress based on the established mathematical regression relationship between the velocity values and the surrogate stress at the subset of measurement locations; determining , at each measurement location, a mean effective stress from the surrogate stress at each measurement location and the total stress tensor; determining a prediction of a pore pressure value for each measurement location within the target volume as the difference between a mean total stress from the total stress tensor and the mean effective stress at each measurement location; and outputting the result to an output device.
A network slice configuration method, comprising: sending , by a distributed unit of a base station, network slice configuration information to a centralized unit of the base station, so that the centralized unit of the base station stores network slice information corresponding to the network slice configuration information, wherein the network slice configuration information comprises information of a network slice supported by a tracing area, TA. sending , by a distributed unit of a base station, network slice configuration information to a centralized unit of the base station, so that the centralized unit of the base station stores network slice information corresponding to the network slice configuration information, wherein the network slice configuration information comprises information of a network slice supported by a tracing area, TA.
Magnetic-inductive antenna for a hearing instrument, with two antenna surfaces which are formed from magnetic, flexible foil, and with a base wound with an antenna winding , wherein the antenna surfaces are formed from separate magnetic foil blanks , which are separated from one another, and the base comprises respectively one opening on its end sides , into which respectively one of the foil blanks is inserted, characterized in that the base is formed from a hollow base body , into which the two foil blanks are inserted in such a way that they overlap in the interior of the base body or abut against one another.
A method for proving a turbine meter for use in a natural gas conduit, the method comprising: providing a prover system (10; 40), the prover system including a reference meter ; connecting the turbine meter to the prover system (10: 40) for fluid communication therewith; introducing a test medium into the prover system (10; 40); circulating the test medium through the reference meter and the turbine meter ; measuring the flow rate of the test medium through the prover system (10; 40) using each of the reference meter and the turbine meter ; and comparing the flow rate measured by the reference meter to the flow rate measured by the turbine meter to establish thereby the accuracy of the turbine meter , wherein the method is characterised in that the test medium is a gas other than air or natural gas having a Reynolds number greater than the Reynolds number of air or natural gas at a given pressure. providing a prover system (10; 40), the prover system including a reference meter ; connecting the turbine meter to the prover system (10: 40) for fluid communication therewith; introducing a test medium into the prover system (10; 40); circulating the test medium through the reference meter and the turbine meter ; measuring the flow rate of the test medium through the prover system (10; 40) using each of the reference meter and the turbine meter ; and comparing the flow rate measured by the reference meter to the flow rate measured by the turbine meter to establish thereby the accuracy of the turbine meter , wherein the method is characterised in that the test medium is a gas other than air or natural gas having a Reynolds number greater than the Reynolds number of air or natural gas at a given pressure.
A tetraalkylammonium tetra- or hexa-hydroxometallate of the formula (N(Alkyl) 4 ) y [M(OH) x ], wherein M is a platinum; alkyl is an alkyl group selected from the group consisting of ethyl, propyl, isopropyl, n-butyl, isobutyl, tert.-butyl, n-pentyl, sec-pentyl, 3-pentyl, 2-methylbutyl, isopentyl, 3-methylbut-2-yl, 2-methyl-but-2-yl, neopentyl, n-hexyl, 3-methylpentyl, isohexyl, neohexyl, 2,3,-dimethylbutyl, or combinations thereof; Y is 2; and X is 4 or 6.
A shroud for a turbine engine, comprising: a first shroud segment having a first mate face and a second shroud segment having a second mate face , the first mate face being positioned circumferentially adjacent to the second mate face , a seal for sealing a gap between the first and second mate faces , wherein the seal is received, at least in part, in a first slot formed on the first mate face and a second slot formed on the second mate face , wherein the first and second slots extend axially between a leading edge and a trailing edge of the respective shroud segment , the first slot being open at the leading edge and at the trailing edge , the second slot being open at the leading edge and closed at the trailing edge , characterised in that the seal comprises axially extending first and second sides which are receivable respectively within the first slot and the second slot , the seal having an axial length (Ls) substantially equal to an axial length (L R ) of the shroud segments and having a cutout on the second side at a trailing edge end of the seal , such that a closed trailing edge end of the second slot engages with a shoulder formed by the cutout on the second side of the seal , to limit axial movement of the seal toward the trailing edge . a first shroud segment having a first mate face and a second shroud segment having a second mate face , the first mate face being positioned circumferentially adjacent to the second mate face , a seal for sealing a gap between the first and second mate faces , wherein the seal is received, at least in part, in a first slot formed on the first mate face and a second slot formed on the second mate face , wherein the first and second slots extend axially between a leading edge and a trailing edge of the respective shroud segment , the first slot being open at the leading edge and at the trailing edge , the second slot being open at the leading edge and closed at the trailing edge , characterised in that the seal comprises axially extending first and second sides which are receivable respectively within the first slot and the second slot , the seal having an axial length (Ls) substantially equal to an axial length (L R ) of the shroud segments and having a cutout on the second side at a trailing edge end of the seal , such that a closed trailing edge end of the second slot engages with a shoulder formed by the cutout on the second side of the seal , to limit axial movement of the seal toward the trailing edge .
A vacuum insulating glazing unit provided with a first infrared reflecting coating and a second infrared reflecting coating, having a length L with 300 mm ≤L ≤ 4000 mm, and a width W, with 300 mm ≤ W ≤ 1500 mm, and comprising: a. a first glass pane having an inner pane face and an outer pane face , having a thickness Z 1 , bearing the first infrared reflecting coating on its outer pane face, the first glass pane having an energetical absorptance EA 1 and b. a second glass pane having an inner pane face and an outer pane face and having a thickness, Z 2 , the coated second glass pane having an energetical absorptance EA 2 ; c. a set of discrete spacers positioned between the first and second glass panes, maintaining a distance between the first and the second glass panes and forming an array having a pitch λ, the pitch, λ being comprised between 10 mm and 35 mm ; d. a hermetically bonding seal sealing the distance between the first and second glass panes over a perimeter thereof; e. an internal volume, V, defined by the first and second glass panes and the set of discrete spacers and closed by the hermetically bonding seal and wherein there is a vacuum of absolute pressure of less than 0.1 mbar, and f. wherein the inner pane faces of the first and second glass panes face the internal volume, V; g. the second infrared reflecting coating being borne on a glass pane face that faces the internal volume, and h. characterized in that the first glass pane is thicker than the second glass pane (Z 1 >Z 2 ), and in that ΔEA ≤ 0.0029 ΔZ 2 /mm 2 - 0.041 ΔZ/mm + 0.6375; wherein ΔEA = EA 1 - 2*EA 2 , and in that Z 1 ≥ 5 mm, Z 2 ≥ 3 mm, and ΔZ = (Z 1 - Z 2 ) ≥ 1 mm, and in that 10 mm ≤ λ ≤ 35 mm. a. a first glass pane having an inner pane face and an outer pane face , having a thickness Z 1 , bearing the first infrared reflecting coating on its outer pane face, the first glass pane having an energetical absorptance EA 1 and b. a second glass pane having an inner pane face and an outer pane face and having a thickness, Z 2 , the coated second glass pane having an energetical absorptance EA 2 ; c. a set of discrete spacers positioned between the first and second glass panes, maintaining a distance between the first and the second glass panes and forming an array having a pitch λ, the pitch, λ being comprised between 10 mm and 35 mm ; d. a hermetically bonding seal sealing the distance between the first and second glass panes over a perimeter thereof; e. an internal volume, V, defined by the first and second glass panes and the set of discrete spacers and closed by the hermetically bonding seal and wherein there is a vacuum of absolute pressure of less than 0.1 mbar, and f. wherein the inner pane faces of the first and second glass panes face the internal volume, V; g. the second infrared reflecting coating being borne on a glass pane face that faces the internal volume, and h. characterized in that the first glass pane is thicker than the second glass pane (Z 1 >Z 2 ), and in that ΔEA ≤ 0.0029 ΔZ 2 /mm 2 - 0.041 ΔZ/mm + 0.6375; wherein ΔEA = EA 1 - 2*EA 2 , and in that Z 1 ≥ 5 mm, Z 2 ≥ 3 mm, and ΔZ = (Z 1 - Z 2 ) ≥ 1 mm, and in that 10 mm ≤ λ ≤ 35 mm.
Butterfly valve for controllable fluid flow, characterized in that the design has at least five asymmetries in that the pivot point 6 of the valve disc 7 is offset from the center of the sealing surface 13 in the direction of the pipe axis 8 (asymmetry 1 ) and additionally the pivot point 6 of the valve disc 7 is offset from the center of the valve disc 7 , perpendicular to the pipe axis 8 in the direction of one of the pipe walls (asymmetry 2 ), and additionally the sealing surface 13 is described by the shape of the jacket of the body 10 , which has a first base 14 and a second base 15 , the centroids of this areas are connected to the straight line 16 , whereby this straight line 16 is not parallel, but at an angle 3 (asymmetry 3 ) to the pipe axis 8 and at least one of the base surfaces 14 and 15 is not circular and the shortest and longest extension of this not circular Base is of different lengths and those difference is represented by the dimension 4 (asymmetry 4 ) and where the straight lines of the family of straight lines connecting the base 14 with the base 15 do not intersect at a single point (asymmetry 5 ) and so the casing body 10 of the sealing surface is not a pyramid and is not a cone.
A method for implementing conditional packet forwarding control rules, performed by User Plane Function, UPF, the method comprising: receiving, from a Control Plane Function, CPF, a packet forwarding control rule (IDV500) comprising a Packet Detection Rule, PDR, wherein the PDR identifies a Multi-Access Rule, MAR associated with multiple Forward Action Rules, FARs, where at least one FAR is applicable for 3GPP access and at least one other FAR is applicable for Non-3GPP access; and applying the packet forwarding control rule (IDV502) according to the received PDR receiving, from a Control Plane Function, CPF, a packet forwarding control rule (IDV500) comprising a Packet Detection Rule, PDR, wherein the PDR identifies a Multi-Access Rule, MAR associated with multiple Forward Action Rules, FARs, where at least one FAR is applicable for 3GPP access and at least one other FAR is applicable for Non-3GPP access; and applying the packet forwarding control rule (IDV502) according to the received PDR
A refrigerator door, comprising: an outer door defining the front of the door, wherein extending portions are formed on both sides of the outer door to be bent and extend by a predetermined length, the outer door formed to have a display accommodating portion defined by depressing its front by a predetermined size; a door liner defining a rear external appearance of the refrigerator door, the door liner being coupled to the extending portions of the outer door , thus defining a predetermined space between the outer door and the door liner ; an insulating layer formed in a space between the outer door and the door liner ; a display portion inserted into the display accommodating portion ; a front decoration formed of a single sheet of transparent plate, positioned in front of the outer door to define the front of the refrigerator door; wherein the display portion is attached to a rear of the front decoration ; and wherein a rear surface of the front decoration is colored with a color, and wherein the front decoration has a transparent window formed in a position corresponding to the display portion for making it possible to observe the display portion . an outer door defining the front of the door, wherein extending portions are formed on both sides of the outer door to be bent and extend by a predetermined length, the outer door formed to have a display accommodating portion defined by depressing its front by a predetermined size; a door liner defining a rear external appearance of the refrigerator door, the door liner being coupled to the extending portions of the outer door , thus defining a predetermined space between the outer door and the door liner ; an insulating layer formed in a space between the outer door and the door liner ; a display portion inserted into the display accommodating portion ; a front decoration formed of a single sheet of transparent plate, positioned in front of the outer door to define the front of the refrigerator door; wherein the display portion is attached to a rear of the front decoration ; and wherein a rear surface of the front decoration is colored with a color, and wherein the front decoration has a transparent window formed in a position corresponding to the display portion for making it possible to observe the display portion .
A power connection/disconnection system for connecting/disconnecting an electric power module in a high-power modular uninterruptable power supply installation , the system comprising: - a frame , - a rigid support extending along a first direction (X), - a set of connectors mounted on said support and comprising a ground connector connected to the ground and power connectors intended to supply the module and a load, the connectors being successively aligned along the first direction (X) and each shaped to be electrically connected along a second direction (Y) orthogonal to said first direction (X) with ground and power bars of a power connection box of the installation , and - a device for translating the support configured to move, using an actuator , the support in said second direction (Y), characterized in that the ground connector extends higher along the second direction (Y) than the power connectors of the set of connectors of the electric power module , said ground connector being intended to be electrically connected to a ground bar of the power connection box . - a frame , - a rigid support extending along a first direction (X), - a set of connectors mounted on said support and comprising a ground connector connected to the ground and power connectors intended to supply the module and a load, the connectors being successively aligned along the first direction (X) and each shaped to be electrically connected along a second direction (Y) orthogonal to said first direction (X) with ground and power bars of a power connection box of the installation , and - a device for translating the support configured to move, using an actuator , the support in said second direction (Y),
A swellable composition for sealing and packing comprising: a matrix material ; and a condensed expandable graphite material disposed in the matrix material , wherein the condensed expandable graphite material has a bulk density of 1 to 8 g/cm 3 and comprises expandable graphite, characterized by further comprising: an activation material containing one or more of the following: a thermite; Al-Ni; Ti-Si; Ti-B; Zr-Si, Zr-B; Ti-Al; Ni-Mg; or Mg-Bi, wherein the thermite comprises a reducing agent and an oxidizing agent, wherein the reducing agent comprises one or more of the following: aluminum; magnesium; calcium; titanium; zinc; silicon; or boron; and the oxidizing agent comprises one or more of the following: boron oxide; silicon oxide; chromium oxide; manganese oxide; iron oxide; copper oxide; or lead oxide. a matrix material ; and a condensed expandable graphite material disposed in the matrix material , wherein the condensed expandable graphite material has a bulk density of 1 to 8 g/cm 3 and comprises expandable graphite, characterized by further comprising: an activation material containing one or more of the following: a thermite; Al-Ni; Ti-Si; Ti-B; Zr-Si, Zr-B; Ti-Al; Ni-Mg; or Mg-Bi, wherein the thermite comprises a reducing agent and an oxidizing agent, wherein the reducing agent comprises one or more of the following: aluminum; magnesium; calcium; titanium; zinc; silicon; or boron; and the oxidizing agent comprises one or more of the following: boron oxide; silicon oxide; chromium oxide; manganese oxide; iron oxide; copper oxide; or lead oxide.
A SECDED (Single bit Error Correct and Double bit Error Detect)error detecting/correcting code generating circuit comprising: [log 2 (n+1)] first Exclusive-OR operation circuits , where [log 2 (n+1)] is a natural number given by rounding up log 2 (n+1); and m second Exclusive-OR operation circuits , wherein in response to an input of m bytes of an information portion, wherein each byte has n bits, [log2(n+1)] bits of a first redundant portion of the SECDED code are generated by the [log2(n+1)] first Exclusive-OR operation circuits each outputting one bit, and m bits of a second redundant portion of the SECDED code are generated by the m second Exclusive-OR operation circuits each outputting one bit and inputting k bits (k≧1) output from the [log2(n+1)] first Exclusive-OR operation circuits and one parity bit of a one-bit-error detection code, and, the SECDED code is generated to include the mn bits of the information portion, the [log 2 (n+1)] bits of the first redundant portion, and the m bits of the second redundant portion. [log 2 (n+1)] first Exclusive-OR operation circuits , where [log 2 (n+1)] is a natural number given by rounding up log 2 (n+1); and m second Exclusive-OR operation circuits , wherein in response to an input of m bytes of an information portion, wherein each byte has n bits, [log2(n+1)] bits of a first redundant portion of the SECDED code are generated by the [log2(n+1)] first Exclusive-OR operation circuits each outputting one bit, and m bits of a second redundant portion of the SECDED code are generated by the m second Exclusive-OR operation circuits each outputting one bit and inputting k bits (k≧1) output from the [log2(n+1)] first Exclusive-OR operation circuits and one parity bit of a one-bit-error detection code, and, the SECDED code is generated to include the mn bits of the information portion, the [log 2 (n+1)] bits of the first redundant portion, and the m bits of the second redundant portion.
A system comprising: an ambient backscatter transceiver comprising: an antenna configured to receive a backscattered ambient radio frequency (RF) signal; and a demodulator coupled to the antenna , wherein the demodulator is configured to demodulate the backscattered ambient RF signal to retrieve first data, characterized in that the backscattered ambient RF signal is an ambient RF signal backscattered at a first frequency, wherein the ambient RF signal is modulated at a second frequency to provide other data ; and a respective power harvest circuit configured to harvest energy from the ambient RF signal, wherein the harvested energy is used to power the ambient backscatter transceiver for demodulation of the backscattered ambient RF signal to retrieve first data. an antenna configured to receive a backscattered ambient radio frequency (RF) signal; and a demodulator coupled to the antenna , wherein the demodulator is configured to demodulate the backscattered ambient RF signal to retrieve first data, characterized in that the backscattered ambient RF signal is an ambient RF signal backscattered at a first frequency, wherein the ambient RF signal is modulated at a second frequency to provide other data ; and a respective power harvest circuit configured to harvest energy from the ambient RF signal, wherein the harvested energy is used to power the ambient backscatter transceiver for demodulation of the backscattered ambient RF signal to retrieve first data.