mhurhangee/patent-ind-claim-en huggingface dataset:
A method for forming an oxide coated substrate comprising: heating a pre-coating mixture in contact with a substrate to synthesize an oxide coating on the substrate; wherein the pre-coating mixture comprises a reducing additive and an oxidizing additive; wherein heating is conducted at a temperature of 100°C to 1500°C; and wherein the reducing additive and oxidizing additive are solubilized in water and the solubilized reducing additive comprises a metal containing precursor, the metal containing precursor comprising Titanium(IV) bis(ammonium lactato)dihydroxide. heating a pre-coating mixture in contact with a substrate to synthesize an oxide coating on the substrate; wherein the pre-coating mixture comprises a reducing additive and an oxidizing additive; wherein heating is conducted at a temperature of 100°C to 1500°C; and wherein the reducing additive and oxidizing additive are solubilized in water and the solubilized reducing additive comprises a metal containing precursor, the metal containing precursor comprising Titanium(IV) bis(ammonium lactato)dihydroxide.
A method for optimising image capturing carried out by an airborne radar imaging device, with the mission of said device being to produce an SAR-type radar image of a given target , said method being implemented in a flight mission system and having a step of computing the trajectory of the carrier of said imaging device based on the considered position of said carrier, called initial position, and having at least: - a phase of computing a trajectory segment for image capturing, as a function of the position of said target and of the type of image to be produced, said image capturing segment being dedicated to the imaging device capturing an image of said target; - a phase of adding a trajectory segment for stabilising the carrier, located upstream in the extension of said image capturing segment, for stabilising the flight of the carrier before entering the image capturing segment; then - a phase of adding a trajectory segment for homing the carrier onto said stabilising segment, homing the carrier from its initial position to the stabilising segment; said segment for image capturing being computed in order to comply with at least the following features: - it is tangent to a circle centred on said target ; - its centre is located on the line connecting said carrier, in its initial position, to said target; - it is fully integrated in a ring , in which image capturing by said imaging device is possible. - a phase of computing a trajectory segment for image capturing, as a function of the position of said target and of the type of image to be produced, said image capturing segment being dedicated to the imaging device capturing an image of said target; - a phase of adding a trajectory segment for stabilising the carrier, located upstream in the extension of said image capturing segment, for stabilising the flight of the carrier before entering the image capturing segment; then - a phase of adding a trajectory segment for homing the carrier onto said stabilising segment, homing the carrier from its initial position to the stabilising segment; - it is tangent to a circle centred on said target ; - its centre is located on the line connecting said carrier, in its initial position, to said target; - it is fully integrated in a ring , in which image capturing by said imaging device is possible.
A cooling system (100; 200; 300; 400; 500) configured to directly cool an electronic device immersed in a coolant (C), the cooling system comprising: a cooling tank containing the coolant; characterized by further comprising a leakage receiving portion (21; 41) disposed between the cooling tank and a floor surface so as to receive the coolant (L) leaked from the cooling tank ; an additional leakage receiving portion (23; 33) disposed to receive the coolant overflown from the leakage receiving portion which stores the leaked coolant by a volume in excess of a predetermined volume; and a passage (25; 35) that connects the leakage receiving portions (21; 23) for passing the overflown coolant (L) by the volume in excess of the predetermined volume, wherein the cooling tank (50; 60) includes a lower structure (53; 63) fixed to the floor surface , an upper structure (51; 61) having the electronic device immersed in the coolant (C), and a seismic isolation device disposed between the lower structure (53; 63) and the upper structure (51; 61) a cooling tank containing the coolant; characterized by further comprising a leakage receiving portion (21; 41) disposed between the cooling tank and a floor surface so as to receive the coolant (L) leaked from the cooling tank ; an additional leakage receiving portion (23; 33) disposed to receive the coolant overflown from the leakage receiving portion which stores the leaked coolant by a volume in excess of a predetermined volume; and a passage (25; 35) that connects the leakage receiving portions (21; 23) for passing the overflown coolant (L) by the volume in excess of the predetermined volume, wherein the cooling tank (50; 60) includes a lower structure (53; 63) fixed to the floor surface , an upper structure (51; 61) having the electronic device immersed in the coolant (C), and a seismic isolation device disposed between the lower structure (53; 63) and the upper structure (51; 61)
Indicator system comprising a composition which comprises at least one NCO-reactive compound and at least one polyisocyanate, and comprising at least one proton source and at least one indicator dye, the at least one indicator dye having at least one xanthene skeleton, for indicating the curing of the composition by change in color of the at least one indicator dye, characterized in that the at least one indicator dye has a first color after contacting with the uncured composition and in the cured composition is colorless.
A differential gain-stage circuit, comprising - a positive and a negative input terminal , - a first capacitor with a first and a second electrode , - a second capacitor with a first and a second electrode , wherein in a first phase (A), the first electrode of the first capacitor and the second electrode of the second capacitor are both connected to the positive input terminal and the second electrode of the first capacitor and the first electrode of the second capacitor are both connected to the negative input terminal and thus in the first phase (A), a parallel circuit of the first and the second capacitor is connected to the positive and the negative input terminal , - a first amplifier with an input , wherein the first electrode of the first capacitor is directly and permanently connected to the input of the first amplifier , - a second amplifier with an input , wherein the first electrode of the second capacitor is directly and permanently connected to the input of the second amplifier , - a positive output terminal coupled to an output of the first amplifier , - a negative output terminal coupled to an output of the second amplifier , - a first voltage node connected to the second electrode of the first capacitor , and - a second voltage node connected to the second electrode of the second capacitor , characterized in that the differential gain-stage circuit further comprises a digital-to-analog converter with outputs coupled to the first and the second voltage node , wherein the digital-to-analog converter is adapted to generate a first and a second adder voltage (VAP, VAN) in a second phase (B), and wherein in the second phase (B), the first adder voltage (VAP) is provided to the first voltage node and the second adder voltage (VAN) is provided to the second voltage node . - a positive and a negative input terminal , - a first capacitor with a first and a second electrode , - a second capacitor with a first and a second electrode , wherein in a first phase (A), the first electrode of the first capacitor and the second electrode of the second capacitor are both connected to the positive input terminal and the second electrode of the first capacitor and the first electrode of the second capacitor are both connected to the negative input terminal and thus in the first phase (A), a parallel circuit of the first and the second capacitor is connected to the positive and the negative input terminal , - a first amplifier with an input , wherein the first electrode of the first capacitor is directly and permanently connected to the input of the first amplifier , - a second amplifier with an input , wherein the first electrode of the second capacitor is directly and permanently connected to the input of the second amplifier , - a positive output terminal coupled to an output of the first amplifier , - a negative output terminal coupled to an output of the second amplifier , - a first voltage node connected to the second electrode of the first capacitor , and - a second voltage node connected to the second electrode of the second capacitor ,
A crew seat to be installed in an aircraft, comprising: - a seat structure which can be fixed to a fixed part of the aircraft, - a seat bottom , - a seat bottom slide provided with two arms positioned on either side of the seat bottom , and - the seat bottom being mounted so as to slide relative to the seat bottom slide between a retracted position and a deployed position, - one of the elements among the seat bottom and the seat bottom slide comprising rollers able to slide along corresponding rails provided in the other of the elements among the seat bottom and the seat bottom slide , - the rails having a curved shape so that the seat bottom can form in the deployed position an angle (A1) greater than 10 degrees, preferably of the order of 14 degrees, relative to a horizontal plane parallel to the aircraft floor, characterized in that said seat further comprises a backrest having a first end rotatably mounted relative to the seat bottom and a second end rotatably mounted relative to a headrest of said seat , said headrest being slidably mounted relative to the seat structure so as to follow a movement of said backrest . - a seat structure which can be fixed to a fixed part of the aircraft, - a seat bottom , - a seat bottom slide provided with two arms positioned on either side of the seat bottom , and - the seat bottom being mounted so as to slide relative to the seat bottom slide between a retracted position and a deployed position, - one of the elements among the seat bottom and the seat bottom slide comprising rollers able to slide along corresponding rails provided in the other of the elements among the seat bottom and the seat bottom slide , - the rails having a curved shape so that the seat bottom can form in the deployed position an angle (A1) greater than 10 degrees, preferably of the order of 14 degrees, relative to a horizontal plane parallel to the aircraft floor,
A metal closure for seaming onto the end of a container, the closure comprising: a centre panel defined by a circumferential score ; a tab fixed to the panel by a rivet formed in the panel , the tab having a heel portion radially inside of the rivet and a nose portion radially outside of the rivet and adjacent to a radially inner edge of the score , such that lifting of the heel portion forces the nose portion into contact with a region of the panel adjacent to the radially inner edge of the circumferential score , thereby causing the closure to fracture partially along the score ; and two spaced apart, elongate raised beads formed in the panel , extending with a circumferential component of direction, characterised in that each raised bead has an end terminating under the tab radially between the rivet and the score to allow the tab to pivot about the two raised beads . a centre panel defined by a circumferential score ; a tab fixed to the panel by a rivet formed in the panel , the tab having a heel portion radially inside of the rivet and a nose portion radially outside of the rivet and adjacent to a radially inner edge of the score , such that lifting of the heel portion forces the nose portion into contact with a region of the panel adjacent to the radially inner edge of the circumferential score , thereby causing the closure to fracture partially along the score ; and two spaced apart, elongate raised beads formed in the panel , extending with a circumferential component of direction, characterised in that each raised bead has an end terminating under the tab radially between the rivet and the score to allow the tab to pivot about the two raised beads .
An anti-HIV antibody, wherein said antibody is PG16 having a heavy chain comprising the amino acid sequence of SEQ ID NO: 31 and a light chain comprising the amino acid sequence of SEQ ID NO: 32.
A method , comprising: receiving , by a cloud computing platform , a new record for a record store, the new record comprising one or more fields; selecting , by the cloud computing platform , a match rule applicable to the new record for detecting duplicitous records, the match rule comprising a unique identifier, one or more match types, and one or more fields of applicability; calculating , by the cloud computing platform , a match index value, wherein the match index value is a composite of the one or more fields of applicability as received in the one or more fields in the new record; deriving , by the cloud computing platform , an encrypted match index value, wherein the unique identifier of the match rule is used as an initialization vector in an encryption scheme used for deriving the encrypted match index value and the match index value is used as plaintext in the encryption scheme; storing , by the cloud computing platform , the encrypted match index value in an encrypted match index column; comparing, by the cloud computing platform , the encrypted match index value to existing values in the encrypted match index column to determine if the encrypted match index value duplicates one or more of the existing values; and if no duplicate record is found, adding the new record to the record store. receiving , by a cloud computing platform , a new record for a record store, the new record comprising one or more fields; selecting , by the cloud computing platform , a match rule applicable to the new record for detecting duplicitous records, the match rule comprising a unique identifier, one or more match types, and one or more fields of applicability; calculating , by the cloud computing platform , a match index value, wherein the match index value is a composite of the one or more fields of applicability as received in the one or more fields in the new record; deriving , by the cloud computing platform , an encrypted match index value, wherein the unique identifier of the match rule is used as an initialization vector in an encryption scheme used for deriving the encrypted match index value and the match index value is used as plaintext in the encryption scheme; storing , by the cloud computing platform , the encrypted match index value in an encrypted match index column; comparing, by the cloud computing platform , the encrypted match index value to existing values in the encrypted match index column to determine if the encrypted match index value duplicates one or more of the existing values; and if no duplicate record is found, adding the new record to the record store.
An apparatus for a wireless communication device (200; 200a), the apparatus comprising: a transceiver module for transmitting and receiving wireless transmissions; and a processing module configured to: control the transceiver module, communicate with a further wireless communication device via the transceiver module, wherein the communication with the further wireless communication device is based on a transmission of data frames between the wireless communication device and the further wireless communication device, wherein each data frame is based on a two-dimensional grid in a time-frequency plane having a time dimension resolution and a frequency dimension resolution, wherein the processing module is configured to select a communication mode from a plurality of communication modes for the communication between the wireless communication device and the further wireless communication device, wherein the communication mode defines a combination of a frequency dimension resolution and a time dimension resolution of the two-dimensional grid in the time-frequency plane. a transceiver module for transmitting and receiving wireless transmissions; and a processing module configured to: control the transceiver module, communicate with a further wireless communication device via the transceiver module, wherein the communication with the further wireless communication device is based on a transmission of data frames between the wireless communication device and the further wireless communication device, wherein each data frame is based on a two-dimensional grid in a time-frequency plane having a time dimension resolution and a frequency dimension resolution, wherein the processing module is configured to select a communication mode from a plurality of communication modes for the communication between the wireless communication device and the further wireless communication device, wherein the communication mode defines a combination of a frequency dimension resolution and a time dimension resolution of the two-dimensional grid in the time-frequency plane. control the transceiver module, communicate with a further wireless communication device via the transceiver module, wherein the communication with the further wireless communication device is based on a transmission of data frames between the wireless communication device and the further wireless communication device, wherein each data frame is based on a two-dimensional grid in a time-frequency plane having a time dimension resolution and a frequency dimension resolution, wherein the processing module is configured to select a communication mode from a plurality of communication modes for the communication between the wireless communication device and the further wireless communication device, wherein the communication mode defines a combination of a frequency dimension resolution and a time dimension resolution of the two-dimensional grid in the time-frequency plane.
A method for identifying at least one match among multiple potential organ donors for at least one recipient in need of a transplanted organ, where the method comprises: (a) assaying genomic DNA encoding membrane proteins other than human leukocyte antigens from the donors and from at least one recipient to determine the number of amino acid mismatches in said membrane proteins encoded by the donor genomes that at least one selected recipient immune system could recognize as non-self; (b) separately summing the number of amino acid mismatches for each donor compared to at least one selected recipient where the mismatches can be recognized as non-self by the selected recipient(s); (c) determining an allogenomics mismatch score Δ( r,d ) for each selected recipient r and each donor d, which is a sum of mismatches as shown in Equation 1: Δ r d = ∑ p ∈ P δ p G rp = genotype r p , G dp = genotype d p where δ p is defined in Equation 2; P is a set of all genomic positions of interest; p is a polymorphic site in a set P; G rp is the genotype of the recipient r at genomic site/position p; G dp is the genotype of the donor d at site p; δ p G rp G dp = ∑ a ∈ G dp { 0 if a ∈ G r , p 1 otherwise where a is an allele; and (d) identifying a match among the multiple potential organ donors for at least one recipient in need of a transplanted organ by identifying one or more donor with an allogenomics mismatch score that is below a threshold value, or by identifying the donor with the lowest allogenomics score for a selected recipient. (a) assaying genomic DNA encoding membrane proteins other than human leukocyte antigens from the donors and from at least one recipient to determine the number of amino acid mismatches in said membrane proteins encoded by the donor genomes that at least one selected recipient immune system could recognize as non-self; (b) separately summing the number of amino acid mismatches for each donor compared to at least one selected recipient where the mismatches can be recognized as non-self by the selected recipient(s); (c) determining an allogenomics mismatch score Δ( r,d ) for each selected recipient r and each donor d, which is a sum of mismatches as shown in Equation 1: Δ r d = ∑ p ∈ P δ p G rp = genotype r p , G dp = genotype d p where δ p is defined in Equation 2; P is a set of all genomic positions of interest; p is a polymorphic site in a set P; G rp is the genotype of the recipient r at genomic site/position p; G dp is the genotype of the donor d at site p; δ p G rp G dp = ∑ a ∈ G dp { 0 if a ∈ G r , p 1 otherwise where a is an allele; and δ p is defined in Equation 2; P is a set of all genomic positions of interest; p is a polymorphic site in a set P; G rp is the genotype of the recipient r at genomic site/position p; G dp is the genotype of the donor d at site p; (d) identifying a match among the multiple potential organ donors for at least one recipient in need of a transplanted organ by identifying one or more donor with an allogenomics mismatch score that is below a threshold value, or by identifying the donor with the lowest allogenomics score for a selected recipient.