mhurhangee/ep-ind-claims huggingface dataset:
A method for confidentially querying a database hosted by a server, the database contains a table of records, each record being obtained by means of a totally or partially homomorphic encryption of plaintext values, in which: (a) the user transmits a request, comprising a predicate to the server, said predicate being a logical expression applied to one or several fields of the table of records; (b) the server calculates the encrypted Boolean value of the predicate for each record in the table; characterized in that: (c) the server constructs a container ( B m) comprising a predetermined number of locations and blindly stores to said locations of records verifying the predicate and not previously transmitted to the user, from the encrypted Boolean values ( r i, i = 1,...,N) obtained in step (b); (d) the server transmits the container thus constructed to the user; (e) the user receives the container, decrypts the contents of each location, and determines whether the container is full or not; if the container is full, the user transmits a continuation request ( RC m) to the server for a new iteration of steps (c), (d) and (e); if the container is not full, the user obtains the response to said request from the records stored in the containers received and decrypted in step(s) (e). (a) the user transmits a request, comprising a predicate to the server, said predicate being a logical expression applied to one or several fields of the table of records; (b) the server calculates the encrypted Boolean value of the predicate for each record in the table; (c) the server constructs a container ( B m) comprising a predetermined number of locations and blindly stores to said locations of records verifying the predicate and not previously transmitted to the user, from the encrypted Boolean values ( r i, i = 1,...,N) obtained in step (b); (d) the server transmits the container thus constructed to the user; (e) the user receives the container, decrypts the contents of each location, and determines whether the container is full or not; if the container is full, the user transmits a continuation request ( RC m) to the server for a new iteration of steps (c), (d) and (e); if the container is not full, the user obtains the response to said request from the records stored in the containers received and decrypted in step(s) (e).
An air conditioning device for a vehicle comprising: a case that has an internal space in which delivery air flows; a platy sliding door that is disposed slidably in the internal space; a rack that has a plurality of teeth parts protruding toward an upstream side from the sliding door and arranged in a sliding direction; a rotary driving unit that has a shaft part rotatably supported on the case at a position upstream of the sliding door and a pinion designed to rotate integrally with the shaft part and mesh with the rack; and a guide groove that has an upstream-side guide rail formed in a planar shape in the case so as to extend in the sliding direction at a position upstream of the sliding door and a downstream-side guide rail formed in the case so as to be opposed to the upstream-side guide rail at a position downstream of the sliding door, and that is designed to slidably support the sliding door, characterized in that a curvature radius of the sliding door in a single unit state is different from a curvature radius of the guide groove, and the rack is formed so that a pitch line of the plurality of teeth parts with the sliding door supported by the guide groove forms a circle substantially concentric with the guide groove. a case that has an internal space in which delivery air flows; a platy sliding door that is disposed slidably in the internal space; a rack that has a plurality of teeth parts protruding toward an upstream side from the sliding door and arranged in a sliding direction; a rotary driving unit that has a shaft part rotatably supported on the case at a position upstream of the sliding door and a pinion designed to rotate integrally with the shaft part and mesh with the rack; and a guide groove that has an upstream-side guide rail formed in a planar shape in the case so as to extend in the sliding direction at a position upstream of the sliding door and a downstream-side guide rail formed in the case so as to be opposed to the upstream-side guide rail at a position downstream of the sliding door, and that is designed to slidably support the sliding door, characterized in that a curvature radius of the sliding door in a single unit state is different from a curvature radius of the guide groove, and the rack is formed so that a pitch line of the plurality of teeth parts with the sliding door supported by the guide groove forms a circle substantially concentric with the guide groove.
A rear structure of a saddle-ride type vehicle having a rear fender halved into a first fender and a second fender connected to each other, the first fender being formed with a hanging portion so as to cover the rearward and upside of a rear wheel and the second fender covering the upside of the rear wheel, wherein a fresh air inlet is provided lateral to and in front of the rear wheel, the first fender and the second fender are disposed to overlap each other in an anteroposterior direction, the second fender is disposed on the vehicle-widthwise inside of the first fender, and the second fender has anteroposteriorly and downward extending sidewalls at both vehicle-widthwise lateral end portions, wherein a luggage box is disposed in front of the second fender and has a bottom wall lower surface located to face the rear wheel, and a given gap is provided between a front end of the second fender and a bottom wall rear end of the luggage box, and a base wall and a left and a right sidewalls (66u, 66u) of the second fender define a water-guide passage below the base wall, and the water-guide passage is formed in a U-shape in cross-section extending in the anteroposterior direction so as to lead forward rainwater or the like splashed by the rear wheel.
Method for joining comprising the steps of: - providing a fastening element with: ∘ a shaft-shaped anchor section which extends between a first end section and a second end section along an anchor axis (Xa); ∘ a flange section formed on and extending radially to the first end section of the anchor section, and the flange section at least partially forms an application section, and; ∘ a joining material, wherein the joining material is pre-applied to the application section, wherein the joining material is lying on the application section in an at least partially solid state,; - providing a workpiece, wherein the workpiece includes a carrier surface; - arranging the fastening element on the carrier surface of the workpiece, - joining the fastening element to the workpiece via cross-linking reaction of the joining material, wherein the joining material is mixed and the mixing occurs by rotating the fastening element relative to the workpiece, characterized in that before the joining step, the joining material includes a first adhesive material and a second adhesive material (50, 52) the fastening material comprises a first adhesive material and the second adhesive material, wherein before the joining step the first adhesive material fully covers the second adhesive material, in that a heating device heats the joining material before and/or after and/or during the rotation, and in that temperature sensor measures the temperature of the joining material and/or the flange section and/or the carrier surface and/or the workpiece. - providing a fastening element with: ∘ a shaft-shaped anchor section which extends between a first end section and a second end section along an anchor axis (Xa); ∘ a flange section formed on and extending radially to the first end section of the anchor section, and the flange section at least partially forms an application section, and; ∘ a joining material, wherein the joining material is pre-applied to the application section, wherein the joining material is lying on the application section in an at least partially solid state,; ∘ a shaft-shaped anchor section which extends between a first end section and a second end section along an anchor axis (Xa); ∘ a flange section formed on and extending radially to the first end section of the anchor section, and the flange section at least partially forms an application section, and; ∘ a joining material, wherein the joining material is pre-applied to the application section, wherein the joining material is lying on the application section in an at least partially solid state,; - providing a workpiece, wherein the workpiece includes a carrier surface; - arranging the fastening element on the carrier surface of the workpiece, - joining the fastening element to the workpiece via cross-linking reaction of the joining material, wherein the joining material is mixed and the mixing occurs by rotating the fastening element relative to the workpiece,
Crystalline solid salts of N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1), wherein the salts are selected from the group consisting of: N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1) • pyruvate; N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1) • glutarate; and N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1) • isethionate monohydrate. N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1) • pyruvate; N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1) • glutarate; and N-{4-[(6,7-dimethoxyquinolin-4-yl)oxy]phenyl}-N'-(4-fluorophenyl) cyclopropane-1,1-dicarboxamide (Compound 1) • isethionate monohydrate.
A multimodal unmanned aerial system comprising: a fuselage forming a payload bay; a control wing forward of the fuselage having a chord and including a first plurality of propulsion assemblies (30, 32); a primary wing aft of the fuselage having a chord and including a second plurality of propulsion assemblies (34, 36), the primary wing having a greater wingspan than the control wing; and a plurality of linkages (40, 42, 44, 46) rotatably coupling the fuselage to the control wing and the primary wing; wherein, the fuselage, the control wing and the primary wing are configured to synchronously rotate between a vertical takeoff and landing flight mode and a forward flight mode; wherein, with respect to the forward flight mode, the fuselage has a longitudinal direction and includes an underside and a topside; wherein the longitudinal direction of the fuselage, the chord of the control wing and the chord of the primary wing are substantially vertical in the vertical takeoff and landing flight mode and substantially horizontal in the forward flight mode; and wherein the underside of the fuselage faces the control wing and the topside of the fuselage faces the primary wing in the vertical takeoff and landing flight mode. a fuselage forming a payload bay; a control wing forward of the fuselage having a chord and including a first plurality of propulsion assemblies (30, 32); a primary wing aft of the fuselage having a chord and including a second plurality of propulsion assemblies (34, 36), the primary wing having a greater wingspan than the control wing; and a plurality of linkages (40, 42, 44, 46) rotatably coupling the fuselage to the control wing and the primary wing; wherein, the fuselage, the control wing and the primary wing are configured to synchronously rotate between a vertical takeoff and landing flight mode and a forward flight mode; wherein, with respect to the forward flight mode, the fuselage has a longitudinal direction and includes an underside and a topside; wherein the longitudinal direction of the fuselage, the chord of the control wing and the chord of the primary wing are substantially vertical in the vertical takeoff and landing flight mode and substantially horizontal in the forward flight mode; and wherein the underside of the fuselage faces the control wing and the topside of the fuselage faces the primary wing in the vertical takeoff and landing flight mode.
Device for testing at least one part of a drivetrain of a vehicle, having at least one rotatable drive drum which can be driven by means of a drive, wherein the drive drum has a frictional contact plate, wherein the frictional contact plate lies against a rotatably mounted tyred wheel, wherein the tyred wheel is connected to an output shaft, wherein the output shaft is connected to a rotationally fixedly mounted drive unit (4, 11), wherein the drive drum with the frictional contact plate is designed to exchange torque with the tyred wheel, characterized in that the frictional contact plate is arranged between the drive drum and the tyred wheel, and in that the axis of rotation of the drive drum is arranged on the same axis as the axis of rotation of the tyred wheel.
A screw configuration inference apparatus, comprising: an information acquisition unit configured to acquire input information including resin properties and acquires, as output information, a specified value of a physical quantity related to a kneaded resin or a kneading machine; a storage unit configured to store knowledge information including correlations between the input information, the physical quantity and a plurality of screw configurations; and a configuration inference unit configured to infer, on the basis of the input information and the knowledge information, a screw configuration that is able to meet the specified value; characterised in that the knowledge information reflects correlations among a process type, operation conditions, configuration data and analysis results learned by a learning procedure for learning the correlations based on learning information, wherein the learning information includes analysis results to be obtained by a numerical analysis carried out on the basis of analysis conditions, the analysis conditions including: a process type including resin properties, operation conditions including an extrusion amount and configuration data including such data that indicate screw configurations. an information acquisition unit configured to acquire input information including resin properties and acquires, as output information, a specified value of a physical quantity related to a kneaded resin or a kneading machine; a storage unit configured to store knowledge information including correlations between the input information, the physical quantity and a plurality of screw configurations; and a configuration inference unit configured to infer, on the basis of the input information and the knowledge information, a screw configuration that is able to meet the specified value; characterised in that the knowledge information reflects correlations among a process type, operation conditions, configuration data and analysis results learned by a learning procedure for learning the correlations based on learning information, wherein the learning information includes analysis results to be obtained by a numerical analysis carried out on the basis of analysis conditions, the analysis conditions including: a process type including resin properties, operation conditions including an extrusion amount and configuration data including such data that indicate screw configurations.
An implantable absorbable iron-based device, comprising an iron-based substrate, a zinc-containing protector in contact with the iron-based substrate, and a degradable polyester in contact with the iron-based substrate and/or the zinc-containing protector, wherein the ratio of the mass of the zinc-containing protector to the mass of the iron-based substrate ranges between 1:200 and 1:2; and in the degradable polyester, the mass fraction of a low molecular weight portion is less than or equal to 5 percent, and the molecular weight of the low molecular weight portion is less than 10,000; or in the degradable polyester, the mass fraction of the residual monomer is less than or equal to 2 percent. wherein the ratio of the mass of the zinc-containing protector to the mass of the iron-based substrate ranges between 1:200 and 1:2; and in the degradable polyester, the mass fraction of a low molecular weight portion is less than or equal to 5 percent, and the molecular weight of the low molecular weight portion is less than 10,000; or in the degradable polyester, the mass fraction of the residual monomer is less than or equal to 2 percent.
A gaspath component for a gas turbine engine comprising: a platform (112,120,132,134;300) including at least one internal cooling passage (320,330;410,420,430;710;720;810), each of the at least one internal cooling passage (320...810) having a plurality of trip strips (328,338;412,422,432;712,722;820) extending into the cooling passage (320...810) from at least one internal surface of the cooling passage (320...810), each of the trip strips (328...820) being defined by a z-shaped configuration, wherein the at least one internal cooling passage (320...810) includes a first internal cooling passage (320;410) and a second internal cooling passage (330;420,430), and wherein the first internal cooling passage (320;410) is adjacent a first platform edge; and wherein the second internal cooling passage (330;420,430) is adjacent to a second platform edge, and a locally upstream most portion, relative to a cooling flow direction through the second internal cooling passage, of each trip strip (338;422,432) within the second internal cooling passage (330;420,430) contacts a wall adjacent to the second platform edge. a platform (112,120,132,134;300) including at least one internal cooling passage (320,330;410,420,430;710;720;810), each of the at least one internal cooling passage (320...810) having a plurality of trip strips (328,338;412,422,432;712,722;820) extending into the cooling passage (320...810) from at least one internal surface of the cooling passage (320...810), each of the trip strips (328...820) being defined by a z-shaped configuration, wherein the at least one internal cooling passage (320...810) includes a first internal cooling passage (320;410) and a second internal cooling passage (330;420,430), and wherein the first internal cooling passage (320;410) is adjacent a first platform edge; and wherein the second internal cooling passage (330;420,430) is adjacent to a second platform edge, and a locally upstream most portion, relative to a cooling flow direction through the second internal cooling passage, of each trip strip (338;422,432) within the second internal cooling passage (330;420,430) contacts a wall adjacent to the second platform edge.
Hairstyling device for curling hair comprising a winding device including: - a mandrel, - a reel configured to wind a lock of hair around the mandrel during its rotation in a predetermined direction. - a motor intended to rotate said reel - a hair immobilising device positioned at a distal end of the mandrel, characterised in that said hair immobilising device comprises a plurality of protruding pins at the distal end of the mandrel. - a mandrel, - a reel configured to wind a lock of hair around the mandrel during its rotation in a predetermined direction. - a motor intended to rotate said reel - a hair immobilising device positioned at a distal end of the mandrel, characterised in that said hair immobilising device comprises a plurality of protruding pins at the distal end of the mandrel.
A composition of matter comprising a compound of formula wherein n is 1 or 2; the weight ratio of the cis-diastereoisomers to the trans-diastereoisomers is comprised in the range between 90:10 and 99.5:0.5 and comprising at least 10% w/w of cis-(1S,2R) diastereoisomer, the percentage being relative to the total weight of the composition of matter.
A method of manufacturing a non-rotating turbine component, the method comprising: additive manufacturing an article having a proximal face sized and shaped to cover at least a portion of an upper surface of a platform of a base component and a contoured distal face opposite the proximal face, the base component and the article together forming the turbine component, the contoured distal face of the article having a contour surface serving as at least a portion of a hot gas path surface of the turbine component, the contour surface being arranged and disposed to provide a controlled flow pattern of a working fluid across the contour surface, characterised by the contour surface being customized based on a clock mounting location of the turbine component in a turbine and a hot gas flow and temperature distribution determined empirically or by modelling at the clock mounting location. additive manufacturing an article having a proximal face sized and shaped to cover at least a portion of an upper surface of a platform of a base component and a contoured distal face opposite the proximal face, the base component and the article together forming the turbine component, the contoured distal face of the article having a contour surface serving as at least a portion of a hot gas path surface of the turbine component, the contour surface being arranged and disposed to provide a controlled flow pattern of a working fluid across the contour surface, characterised by the contour surface being customized based on a clock mounting location of the turbine component in a turbine and a hot gas flow and temperature distribution determined empirically or by modelling at the clock mounting location.
Reflector assembly for illuminating different mutually spaced-apart regions (16; 20; 24), with a first light source and at least one second light source and a hollow reflector, which comprises the regions (16; 20; 24), wherein - a second reflector (64; 74) having at least two reflective surfaces (66; 76) inclined relative to one another is arranged, - the first light source and the second reflector are arranged one above the other, - the first light source is so arranged that illumination of the regions (16; 20; 24) is provided by light reflection via the second reflector (64; 74) and - the second reflector (64; 74) is arranged above the first light source, characterised in that - formed between the second reflector and an opposite wall of the hollow reflector are at least two channels which are each associated with at least one respective illuminatable region, comprising at least one second light source which is associated with at least one illuminatable region, wherein the second reflector serves as light partition for other illuminatable regions and - the at least one second light source is arranged eccentrically and faces the wall of the hollow reflector. - a second reflector (64; 74) having at least two reflective surfaces (66; 76) inclined relative to one another is arranged, - the first light source and the second reflector are arranged one above the other, - the first light source is so arranged that illumination of the regions (16; 20; 24) is provided by light reflection via the second reflector (64; 74) and - the second reflector (64; 74) is arranged above the first light source, - formed between the second reflector and an opposite wall of the hollow reflector are at least two channels which are each associated with at least one respective illuminatable region, comprising at least one second light source which is associated with at least one illuminatable region, wherein the second reflector serves as light partition for other illuminatable regions and - the at least one second light source is arranged eccentrically and faces the wall of the hollow reflector.