mhurhangee/patent-ind-claim-en huggingface dataset:
A compound selected from the group shown in the following table: No. Structure 3 4 5 6 7 8 9 10 11 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 123 124 125 126 127 128 129 130 131 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 or a pharmaceutically acceptable salt thereof.
An aircraft wing comprising a fixed wing centre body , as well as at least one mobile leading edge flap for being moved relative to said fixed centre body between an extended position and a retracted position, the fixed wing centre body comprising a front spar delimiting a wing box at the front of which said mobile flap is located, the latter being associated with at least one guiding device for guiding it with respect to the fixed wing centre body , the guiding device being totally arranged at the front of the front spar of the wing box, this device including the following elements: - a first pivoting member having a first end connected to the front spar of the wing box through a first hinged connection ; - a second pivoting member connected to a second end of the first pivoting member through a second hinged connection arranged between a first and a second end of the second pivoting member, the first end of this second pivoting member being connected to a module for connecting the mobile flap through a third hinged connection ; and - a guiding rail integral with the front spar of the wing box, the guiding rail receiving a follower member arranged at the second end of the second pivoting member , characterized in that the guiding rail defines a trajectory lying on the surface of a dummy sphere , and in that the hinging axes of the three hinged connections converge to a same point corresponding to the centre of the dummy sphere . the guiding device being totally arranged at the front of the front spar of the wing box, this device including the following elements: - a first pivoting member having a first end connected to the front spar of the wing box through a first hinged connection ; - a second pivoting member connected to a second end of the first pivoting member through a second hinged connection arranged between a first and a second end of the second pivoting member, the first end of this second pivoting member being connected to a module for connecting the mobile flap through a third hinged connection ; and - a guiding rail integral with the front spar of the wing box, the guiding rail receiving a follower member arranged at the second end of the second pivoting member , characterized in that the guiding rail defines a trajectory lying on the surface of a dummy sphere , - a first pivoting member having a first end connected to the front spar of the wing box through a first hinged connection ; - a second pivoting member connected to a second end of the first pivoting member through a second hinged connection arranged between a first and a second end of the second pivoting member, the first end of this second pivoting member being connected to a module for connecting the mobile flap through a third hinged connection ; and - a guiding rail integral with the front spar of the wing box, the guiding rail receiving a follower member arranged at the second end of the second pivoting member , characterized in that the guiding rail defines a trajectory lying on the surface of a dummy sphere , and in that the hinging axes of the three hinged connections converge to a same point corresponding to the centre of the dummy sphere .
A package coated on at least a portion thereof with a coating, the coating being derived from a coating composition, the coating composition comprising: (a) a film-forming resin comprising a functional group having an active hydrogen atom; and (b) a crosslinking material operable to crosslink the functional group having an active hydrogen atom on the film-forming resin, the crosslinking material comprising the reaction product of a reaction mixture comprising: (i) a cyclic unsaturated acid anhydride and/or diacid derivative thereof; (ii) an ethylenically unsaturated monomer; and (iii) an alcohol, amine and/or thiol, wherein at least a portion of the cyclic unsaturated acid anhydride and/or diacid derivative thereof is reacted with the alcohol, amine and/or thiol; wherein the film-forming resin comprises an emulsion polymerised acrylic latex material; and wherein (i) the coating composition comprises 5 to 30 wt% of the crosslinking material based on the total solid weight of the coating composition; and/or (ii) wherein the coating composition is a sprayable coating composition. (a) a film-forming resin comprising a functional group having an active hydrogen atom; and (b) a crosslinking material operable to crosslink the functional group having an active hydrogen atom on the film-forming resin, the crosslinking material comprising the reaction product of a reaction mixture comprising: (i) a cyclic unsaturated acid anhydride and/or diacid derivative thereof; (ii) an ethylenically unsaturated monomer; and (iii) an alcohol, amine and/or thiol, (i) a cyclic unsaturated acid anhydride and/or diacid derivative thereof; (ii) an ethylenically unsaturated monomer; and (iii) an alcohol, amine and/or thiol, wherein at least a portion of the cyclic unsaturated acid anhydride and/or diacid derivative thereof is reacted with the alcohol, amine and/or thiol; wherein the film-forming resin comprises an emulsion polymerised acrylic latex material; and wherein (i) the coating composition comprises 5 to 30 wt% of the crosslinking material based on the total solid weight of the coating composition; and/or (ii) wherein the coating composition is a sprayable coating composition. (i) the coating composition comprises 5 to 30 wt% of the crosslinking material based on the total solid weight of the coating composition; and/or (ii) wherein the coating composition is a sprayable coating composition.
A method of preparing a superabsorbent polymer, the method comprising the steps of: preparing a base resin in which an acrylic acid-based monomer having acidic groups which are at least partially neutralized and an internal crosslinking agent are crosslinked; and heating the base resin in the presence of an epoxy-based surface crosslinking agent to carry out surface modification of the base resin, wherein the epoxy-based surface crosslinking agent is added in an amount of 0.005 parts by weight or more to 0.2 parts by weight or less with respect to 100 parts by weight of the base resin, wherein the internal crosslinking agent includes at the same time a first epoxy crosslinking agent having an epoxy equivalent weight of 100 g/eq or more to less than 130 g/eq, and a second epoxy crosslinking agent having an epoxy equivalent weight of 130 g/eq or more, wherein the first epoxy crosslinking agent and the second epoxy crosslinking agent are included in an amount of 0.01 part by weight to 0.5 parts by weight, respectively, with respect to 100 parts by weight of the acrylic acid-based monomer, and wherein a weight ratio of first epoxy crosslinking agent : second epoxy crosslinking agent is 1: 1 to 30:1. preparing a base resin in which an acrylic acid-based monomer having acidic groups which are at least partially neutralized and an internal crosslinking agent are crosslinked; and heating the base resin in the presence of an epoxy-based surface crosslinking agent to carry out surface modification of the base resin, wherein the epoxy-based surface crosslinking agent is added in an amount of 0.005 parts by weight or more to 0.2 parts by weight or less with respect to 100 parts by weight of the base resin, wherein the internal crosslinking agent includes at the same time a first epoxy crosslinking agent having an epoxy equivalent weight of 100 g/eq or more to less than 130 g/eq, and a second epoxy crosslinking agent having an epoxy equivalent weight of 130 g/eq or more, wherein the first epoxy crosslinking agent and the second epoxy crosslinking agent are included in an amount of 0.01 part by weight to 0.5 parts by weight, respectively, with respect to 100 parts by weight of the acrylic acid-based monomer, and wherein a weight ratio of first epoxy crosslinking agent : second epoxy crosslinking agent is 1: 1 to 30:1.
A knit textile formed from a yarn that has been space-treated with a functional finish prior to the yarn being formed into the knit textile , wherein the functional finish is a finish that alters, changes, or modifies the performance of the yarn and/or contributes to a specific attribute of the yarn without substantially altering the visual appearance of the yarn , the knit textile comprising: a first zone formed from the yarn , wherein yarn segments of the yarn in the first zone have a high level of penetration of the functional finish; a second zone integrally extending from the first zone , wherein yarn segments of the yarn in the second zone have a medium level of penetration of the functional finish; and a third zone integrally extending from the second zone , wherein yarn segments of the yarn in the third zone have a low level of penetration of the functional finish; characterized in that the knit textile is comprised in a shirt; and the first zone is positioned over an upper part of the shirt adjacent a neck opening of the shirt and/or the third zone is positioned near a bottom of the shirt adjacent to a waist opening of the shirt. a first zone formed from the yarn , wherein yarn segments of the yarn in the first zone have a high level of penetration of the functional finish; a second zone integrally extending from the first zone , wherein yarn segments of the yarn in the second zone have a medium level of penetration of the functional finish; and a third zone integrally extending from the second zone , wherein yarn segments of the yarn in the third zone have a low level of penetration of the functional finish; characterized in that the knit textile is comprised in a shirt; and the first zone is positioned over an upper part of the shirt adjacent a neck opening of the shirt and/or the third zone is positioned near a bottom of the shirt adjacent to a waist opening of the shirt.
A method comprising the following steps: performing a first operation in a field with a first implement having a first width and generating a field map generated from location data collected during the first operation in the field, the field map including locations of a plurality of crop rows ; generating guidance lines for operation of a vehicle during a second operation on the field with a second implement of the vehicle performing the second operation on the field, the guidance lines based on the field map including the locations of the rows , causing the vehicle to traverse the field along the guidance lines; and causing the second implement to perform the second operation as the vehicle traverses the field along the guidance lines, characterized in that the guidance lines are generated based on the location of the rows and an operational width of the second implement and generated to ensure that the vehicle moves along a path that allows the second implement to perform its designated operation most efficiently by generating as few guidance lines as possible to cover the entire field, that implement operation data are monitored to update the field map based on operations that have been performed with the second implement , and that portions of the second implement are caused to perform the second operation upon crop rows which have not been operated upon while operations on rows that are passed over twice are not repeated. performing a first operation in a field with a first implement having a first width and generating a field map generated from location data collected during the first operation in the field, the field map including locations of a plurality of crop rows ; generating guidance lines for operation of a vehicle during a second operation on the field with a second implement of the vehicle performing the second operation on the field, the guidance lines based on the field map including the locations of the rows , causing the vehicle to traverse the field along the guidance lines; and causing the second implement to perform the second operation as the vehicle traverses the field along the guidance lines, characterized in that the guidance lines are generated based on the location of the rows and an operational width of the second implement and generated to ensure that the vehicle moves along a path that allows the second implement to perform its designated operation most efficiently by generating as few guidance lines as possible to cover the entire field, that implement operation data are monitored to update the field map based on operations that have been performed with the second implement , and that portions of the second implement are caused to perform the second operation upon crop rows which have not been operated upon while operations on rows that are passed over twice are not repeated.
A system for sludge treatment, which system is arranged in a container adapted to be transported by a truck and comprises: a sludge inlet for receiving a sludge; a reactor comprising an electrical heating arrangement for heat treatment of the sludge, which reactor is arranged downstream the sludge inlet; a flashing arrangement for cooling sludge treated in the reactor and providing at least one steam fraction, which flashing arrangement is arranged downstream the reactor; a steam routing arrangement capable of routing the at least one steam fraction from the flashing arrangement to preheat sludge transported from the sludge inlet to the reactor; and a separation arrangement for separating the cooled sludge from the flashing arrangement into a first fraction and a second fraction, wherein the suspended solids content is higher in the first fraction than in the second fraction, wherein the reactor comprises at least one outlet connected to the flashing arrangement and at least one recirculation conduit on which the electrical heating arrangement is arranged and wherein the reactor is adapted to provide an outlet fraction for leaving the reactor through the at least one outlet connected to the flashing arrangement and a recirculation fraction for recirculation in the recirculation conduit and wherein the average particle size is larger in the outlet fraction than in the recirculation fraction and wherein the reactor is vertical and an outlet for the recirculation conduit is arranged above the at least one outlet connected to the flashing arrangement . a sludge inlet for receiving a sludge; a reactor comprising an electrical heating arrangement for heat treatment of the sludge, which reactor is arranged downstream the sludge inlet; a flashing arrangement for cooling sludge treated in the reactor and providing at least one steam fraction, which flashing arrangement is arranged downstream the reactor; a steam routing arrangement capable of routing the at least one steam fraction from the flashing arrangement to preheat sludge transported from the sludge inlet to the reactor; and a separation arrangement for separating the cooled sludge from the flashing arrangement into a first fraction and a second fraction, wherein the suspended solids content is higher in the first fraction than in the second fraction,
A backrest for use in a chair, the backrest comprising: a back board arranged in a position to abut a back of a seated person on the chair, wherein a first area including a laterally central area of the back board has a thickness (L1) greater than a thickness (L2) of a second area of the back board located closer to each of left and right ends of the back board than the first area, wherein the back board includes a high rigidity portion provided at least in a lower area from a vertical center position at each of the left and right ends of the back board, and wherein the high rigidity portion has a rigidity higher than that of a surrounding area surrounding at least an upper part of the high rigidity portion in the back board, wherein the back board comprises an area having a thickness gradually decreasing from a lateral center of the back board toward the left and right ends, wherein at least a part in a vertical direction of each of the left and right ends of the back board is a portion having a smallest thickness at a same height of the back board. a back board arranged in a position to abut a back of a seated person on the chair, wherein a first area including a laterally central area of the back board has a thickness (L1) greater than a thickness (L2) of a second area of the back board located closer to each of left and right ends of the back board than the first area, wherein the back board includes a high rigidity portion provided at least in a lower area from a vertical center position at each of the left and right ends of the back board, and wherein the high rigidity portion has a rigidity higher than that of a surrounding area surrounding at least an upper part of the high rigidity portion in the back board, wherein the back board comprises an area having a thickness gradually decreasing from a lateral center of the back board toward the left and right ends, wherein at least a part in a vertical direction of each of the left and right ends of the back board is a portion having a smallest thickness at a same height of the back board.
A process for manufacturing turbomachine blades , wherein: a) a ceramic core piece that comprises two ceramic core elements (1', 1", 1′′′, 1"") and a clamping part that connects the ceramic core elements, is positioned in a wax forming device , subsequently; b) a molten wax material (W) is applied to the outside of the ceramic core piece in the wax forming device and the wax is allowed to solidify, subsequently; c) at least two turbomachine blades are cast using a crystallographically-oriented metal casting process to form a blade cast piece and the wax (W) and the ceramic core piece are removed, further characterized in d) cutting the blade cast piece to separate the at least two turbomachine blades from a portion of the blade cast piece defined by the clamping part . a) a ceramic core piece that comprises two ceramic core elements (1', 1", 1′′′, 1"") and a clamping part that connects the ceramic core elements, is positioned in a wax forming device , subsequently; b) a molten wax material (W) is applied to the outside of the ceramic core piece in the wax forming device and the wax is allowed to solidify, subsequently; c) at least two turbomachine blades are cast using a crystallographically-oriented metal casting process to form a blade cast piece and the wax (W) and the ceramic core piece are removed, further characterized in d) cutting the blade cast piece to separate the at least two turbomachine blades from a portion of the blade cast piece defined by the clamping part .
A process of making a catalyst composition, comprising: treating an organoaluminum compound with a modifier that decreases the initial reducing strength of the organoaluminum compound, wherein the modifier is selected from the group consisting of ethers, anhydrides, amines, amides, silicates, silyl ethers, siloxanes, esters, carbonates, ureas, carbamates, sulfoxides, sulfones, phosphoramides, silanes, and acetals; adding a transition metal complex to the mixture of the organoaluminum compound and the modifier; and obtaining a catalyst composition comprising the organoaluminum compound and the transition metal complex; wherein the molar ratio of the organoaluminum compound to the modifier is 1:10 to 1:2, preferably 1:5. treating an organoaluminum compound with a modifier that decreases the initial reducing strength of the organoaluminum compound, wherein the modifier is selected from the group consisting of ethers, anhydrides, amines, amides, silicates, silyl ethers, siloxanes, esters, carbonates, ureas, carbamates, sulfoxides, sulfones, phosphoramides, silanes, and acetals; adding a transition metal complex to the mixture of the organoaluminum compound and the modifier; and obtaining a catalyst composition comprising the organoaluminum compound and the transition metal complex; wherein the molar ratio of the organoaluminum compound to the modifier is 1:10 to 1:2, preferably 1:5.
A thermal stabilizer composition comprising: 100 parts by mass of a phosphorus-based antioxidant having a phosphite structure; and 0.001 to 10 parts by mass with respect to 100 parts by mass of the phosphorus-based antioxidant of a phenolic antioxidant having a substructure represented by the following Formula : wherein, R 1 , R 2 , R 3 and R 4 each independently represent a hydrogen atom or a hydrocarbon group having 1 to 10 carbon atoms; a represents an integer of 0 to 2; and, when a is 2, plural R 3 s are optionally the same or different. 100 parts by mass of a phosphorus-based antioxidant having a phosphite structure; and 0.001 to 10 parts by mass with respect to 100 parts by mass of the phosphorus-based antioxidant of a phenolic antioxidant having a substructure represented by the following Formula : wherein, R 1 , R 2 , R 3 and R 4 each independently represent a hydrogen atom or a hydrocarbon group having 1 to 10 carbon atoms; a represents an integer of 0 to 2; and, when a is 2, plural R 3 s are optionally the same or different.