mhurhangee/patent-ind-claim-en huggingface dataset:
An apparatus for tracking a blade of a work machine , the apparatus comprising: a blade that is pivotable; first and second optical targets operatively coupled to the blade, each of the optical targets comprising a pattern of shapes; a first camera for collecting first imaging data of the first optical target within a first field of view, the first camera mounted on the work machine; a second camera for collecting second imaging data of the second optical target within a second field of view, the second camera mounted on the work machine; a selector to select the first or second imaging data; and a processor to determine an orientation of the blade based on the selected first or second imaging data; characterised in that the selector is configured to select the first or second imaging data based on the confidence index of each camera, whereby the selector is configured to select the imaging data of the camera with the highest corresponding confidence index, and wherein the confidence index comprises a number indicative of locational data meeting a criteria or threshold for the respective one of the optical targets . a blade that is pivotable; first and second optical targets operatively coupled to the blade, each of the optical targets comprising a pattern of shapes; a first camera for collecting first imaging data of the first optical target within a first field of view, the first camera mounted on the work machine; a second camera for collecting second imaging data of the second optical target within a second field of view, the second camera mounted on the work machine; a selector to select the first or second imaging data; and a processor to determine an orientation of the blade based on the selected first or second imaging data; characterised in that the selector is configured to select the first or second imaging data based on the confidence index of each camera, whereby the selector is configured to select the imaging data of the camera with the highest corresponding confidence index, and wherein the confidence index comprises a number indicative of locational data meeting a criteria or threshold for the respective one of the optical targets .
A rotor assembly , comprising: a rotor disc having a central axis (O); a plurality of rotor blades fixed to the rotor disc and extending radially outward in a radial direction of the rotor disc ; and at least one rolling element configured to roll on a curved surface (CS) facing inward in the radial direction of the rotor disc , wherein the at least one rolling element includes: a first rolling element configured to roll on a first curved surface (CS1) as the curved surface (CS); and a second rolling element configured to roll on a second curved surface (CS2) as the curved surface (CS), characterized in that a first curvature radius (R1) of the first curved surface (CS1) is different from a second curvature radius (R2) of the second curved surface (CS2). a rotor disc having a central axis (O); a plurality of rotor blades fixed to the rotor disc and extending radially outward in a radial direction of the rotor disc ; and at least one rolling element configured to roll on a curved surface (CS) facing inward in the radial direction of the rotor disc , wherein the at least one rolling element includes: a first rolling element configured to roll on a first curved surface (CS1) as the curved surface (CS); and a second rolling element configured to roll on a second curved surface (CS2) as the curved surface (CS), characterized in that a first curvature radius (R1) of the first curved surface (CS1) is different from a second curvature radius (R2) of the second curved surface (CS2). a first rolling element configured to roll on a first curved surface (CS1) as the curved surface (CS); and a second rolling element configured to roll on a second curved surface (CS2) as the curved surface (CS), characterized in that a first curvature radius (R1) of the first curved surface (CS1) is different from a second curvature radius (R2) of the second curved surface (CS2).
An assembly comprising: a hydraulic machine comprising a first assembly and a second assembly that are movable in rotation relative to each other along a main axis (X-X), the first assembly comprising a shaft and the second assembly comprising a casing, said hydraulic machine having three portions extending successively from a proximal end to a distal end along the main axis (X-X), - a proximal portion , comprising a distributor and fluid supply and discharge ducts, - a middle portion , comprising a cylinder block and a cam , - a distal portion , comprising bearings , said hydraulic machine having an internal volume and comprising a circuit for sweeping the internal volume, characterized in that said sweep circuit has a fluid inlet orifice in the proximal portion , a fluid outlet orifice in the proximal portion , said sweep circuit being configured so as to form a primary sweep stream (F1) circulating from the inlet orifice successively in the proximal portion , in the middle portion and in the distal portion of the hydraulic machine , then in the middle portion and in the proximal portion up to the outlet orifice . a hydraulic machine comprising a first assembly and a second assembly that are movable in rotation relative to each other along a main axis (X-X), the first assembly comprising a shaft and the second assembly comprising a casing, said hydraulic machine having three portions extending successively from a proximal end to a distal end along the main axis (X-X), - a proximal portion , comprising a distributor and fluid supply and discharge ducts, - a middle portion , comprising a cylinder block and a cam , - a distal portion , comprising bearings , - a proximal portion , comprising a distributor and fluid supply and discharge ducts, - a middle portion , comprising a cylinder block and a cam , - a distal portion , comprising bearings , said hydraulic machine having an internal volume and comprising a circuit for sweeping the internal volume, characterized in that said sweep circuit has a fluid inlet orifice in the proximal portion , a fluid outlet orifice in the proximal portion , said sweep circuit being configured so as to form a primary sweep stream (F1) circulating from the inlet orifice successively in the proximal portion , in the middle portion and in the distal portion of the hydraulic machine , then in the middle portion and in the proximal portion up to the outlet orifice .
A semiconductor structure , comprising: a first layer of a nitride semiconductor material; a relaxed nitride interlayer on the first layer of nitride semiconductor material, the relaxed nitride interlayer having a first lattice constant, wherein the relaxed nitride interlayer comprises: a first portion comprising Al 1-x Ga x N and conductively doped with an n-type dopant, wherein 0.1 ≤ x ≤ 0.9; and a plurality of discrete portions of GaN and/or InGaN with a bandgap lower than that of the first portion, a density between 0.1/μm 2 and 100/μm 2 , and a size between 0.01 and 0.1 μm in diameter in order to increase the vertical conductivity of the interlayer without detrimentally affecting their strain-reducing effects; a second layer of the nitride semiconductor material on the nitride interlayer; wherein the first layer of the nitride semiconductor material, the nitride interlayer, and the second layer of the nitride semiconductor material together have a thickness of at least 0.5 μm; and wherein the nitride semiconductor material has a second lattice constant, such that the first layer of the nitride semiconductor material is more tensile strained on one side of the relaxed nitride interlayer than the second layer of the nitride semiconductor material is on the other side of the relaxed nitride interlayer. a first layer of a nitride semiconductor material; a relaxed nitride interlayer on the first layer of nitride semiconductor material, the relaxed nitride interlayer having a first lattice constant, wherein the relaxed nitride interlayer comprises: a first portion comprising Al 1-x Ga x N and conductively doped with an n-type dopant, wherein 0.1 ≤ x ≤ 0.9; and a plurality of discrete portions of GaN and/or InGaN with a bandgap lower than that of the first portion, a density between 0.1/μm 2 and 100/μm 2 , and a size between 0.01 and 0.1 μm in diameter in order to increase the vertical conductivity of the interlayer without detrimentally affecting their strain-reducing effects; a first portion comprising Al 1-x Ga x N and conductively doped with an n-type dopant, wherein 0.1 ≤ x ≤ 0.9; and a plurality of discrete portions of GaN and/or InGaN with a bandgap lower than that of the first portion, a density between 0.1/μm 2 and 100/μm 2 , and a size between 0.01 and 0.1 μm in diameter in order to increase the vertical conductivity of the interlayer without detrimentally affecting their strain-reducing effects; a second layer of the nitride semiconductor material on the nitride interlayer; wherein the first layer of the nitride semiconductor material, the nitride interlayer, and the second layer of the nitride semiconductor material together have a thickness of at least 0.5 μm; and wherein the nitride semiconductor material has a second lattice constant, such that the first layer of the nitride semiconductor material is more tensile strained on one side of the relaxed nitride interlayer than the second layer of the nitride semiconductor material is on the other side of the relaxed nitride interlayer.
End-grain panel separated from a multilayer formed body, in block or panel form, of high structural strength having two opposite broad faces and a laterally encircling side face containing, in layers, broad face to broad face, coated balsa wood veneers (2, 2', 2", 2"') and adhesives lying between the balsa wood veneers (2, 2', 2", 2"'), the end-grain panel being separated transversely to the broad faces of the formed body , and the grain of the end-grain panel averaged over all bonded balsa wood veneers (2, 2', 2", 2"') being substantially perpendicular to the panel plane, characterized in that the grain of at least one of the balsa wood veneers (2, 2', 2", 2"') deviates by 45° to 90° from the grain of the other balsa wood veneer(s) (2, 2', 2", 2"'), and in that the grain of at least some of the balsa wood veneers (2, 2', 2", 2"') deviates by 22.5° to 67.5° relative to a surface normal to a side face of the formed body .
Cathode active material in particulate form with a mean particle diameter in the range from 2 to 16 μm D50, wherein the cathode active material has the composition Li 1+x TM 1-x O 2 wherein x is in the range of from 0.1 to 0.2 and TM is a combination of elements according to general formula (I), (Ni a Co b Mn c ) 1-d-e M 1 d M 2 e (I) where the variables are each defined as follows: a is in the range from 0.20 to 0.40, b is in the range of from zero to 0.15, c is in the range of from 0.50 to 0.75, d is in the range of from zero to 0.015, and e is in the range of from zero to 0.02, M 1 is selected from Al, Ti, Zr, Mo, Fe, Nb, and Mg, M 2 is selected from B and K, with a + b + c = 1.0 wherein said composite oxide has a specific surface BET in the range from 0.5 m 2 /g to 10 m 2 /g and a pressed density of at least 2.9 g/cm 3 , and wherein said cathode active material has an average primary particle diameter in the range of from 200 to 3,000 nm. a is in the range from 0.20 to 0.40, b is in the range of from zero to 0.15, c is in the range of from 0.50 to 0.75, d is in the range of from zero to 0.015, and e is in the range of from zero to 0.02, M 1 is selected from Al, Ti, Zr, Mo, Fe, Nb, and Mg, M 2 is selected from B and K, wherein said composite oxide has a specific surface BET in the range from 0.5 m 2 /g to 10 m 2 /g and a pressed density of at least 2.9 g/cm 3 , and wherein said cathode active material has an average primary particle diameter in the range of from 200 to 3,000 nm.
A display system for an aircraft, comprising: a processing unit configured to receive data representative of a landing platform on a movable carrier, the data including current energy parameters of the movable carrier, the processing unit further configured to generate display commands associated with the landing platform and the energy parameters of the movable carrier; a communications unit coupled to the processing unit and configured to receive the data representative of the landing platform on the movable carrier from an inertial unit of the movable carrier, wherein the energy parameters include a current speed of the movable carrier relative to the aircraft; and a display device coupled to the processing unit for receiving the display commands and operable to render first symbology representing the landing platform and second symbology representing the energy parameters of the movable carrier, and wherein the second symbology includes additional information regarding the nature of the motion of the landing platform , the additional information including rendered speed symbology indicating the current speed of the movable carrier relative to the aircraft wherein the energy parameters include a current motion direction of the movable carrier in the horizontal plane, and wherein the second symbology includes an arrow oriented in the current motion direction of the movable carrier. a processing unit configured to receive data representative of a landing platform on a movable carrier, the data including current energy parameters of the movable carrier, the processing unit further configured to generate display commands associated with the landing platform and the energy parameters of the movable carrier; a communications unit coupled to the processing unit and configured to receive the data representative of the landing platform on the movable carrier from an inertial unit of the movable carrier, wherein the energy parameters include a current speed of the movable carrier relative to the aircraft; and a display device coupled to the processing unit for receiving the display commands and operable to render first symbology representing the landing platform and second symbology representing the energy parameters of the movable carrier, and wherein the second symbology includes additional information regarding the nature of the motion of the landing platform , the additional information including rendered speed symbology indicating the current speed of the movable carrier relative to the aircraft wherein the energy parameters include a current motion direction of the movable carrier in the horizontal plane, and wherein the second symbology includes an arrow oriented in the current motion direction of the movable carrier.
A method for coating metallic surfaces with a composition comprising silane/silanol/siloxane/polysiloxane, wherein the composition comprises: a) at least one compound a) selected from silanes, silanols, siloxanes and polysiloxanes, the composition having a silane/silanol/siloxane/polysiloxane content in the range from 0.02 to 2 g/L, calculated on the basis of the corresponding silanols, b) at least one titanium-, hafnium-, zirconium-, aluminum- and/or boron-containing compound b), of which at least one is a complex fluoride, the composition having a content of compounds b) in the range from 0.1 to 5 g/L, calculated as the sum of the corresponding metals, c) manganese cations and/or at least one corresponding compound c), the composition having a content of manganese cations and/or corresponding compound c) in the range from 0.08 to 0.3 g/L, calculated as manganese, and also at least one substance d) selected from: d 1 ) aminoguanidine, d 2 ) anions of nitrate and/or compounds having at least one nitro group, d 3 ) compounds based on peroxide and d 4 ) phosphorus-containing compounds, anions of at least one phosphate and/or anions of at least one posphonate, and also, furthermore, e) comprises water, where the content of all kinds of substances d) is in the range from 0.01 to 25 g/L, where the composition has a content of nitrate in the range from 0.1 to 5 g/l. a) at least one compound a) selected from silanes, silanols, siloxanes and polysiloxanes, the composition having a silane/silanol/siloxane/polysiloxane content in the range from 0.02 to 2 g/L, calculated on the basis of the corresponding silanols, b) at least one titanium-, hafnium-, zirconium-, aluminum- and/or boron-containing compound b), of which at least one is a complex fluoride, the composition having a content of compounds b) in the range from 0.1 to 5 g/L, calculated as the sum of the corresponding metals, c) manganese cations and/or at least one corresponding compound c), the composition having a content of manganese cations and/or corresponding compound c) in the range from 0.08 to 0.3 g/L, calculated as manganese, d 1 ) aminoguanidine, d 2 ) anions of nitrate and/or compounds having at least one nitro group, d 3 ) compounds based on peroxide and d 4 ) phosphorus-containing compounds, anions of at least one phosphate and/or anions of at least one posphonate, and also, furthermore, e) comprises water,
A resin composition comprising a copolymer that contains a conjugated diene unit, a non-conjugated olefin unit and an aromatic vinyl unit and has a butylene unit content of 0 mol%, and an olefin resin.
A vehicular light-emitting device wherein a plurality of light-emitting units , each of which includes a light source and a lens for diffusing and emitting the light entered from the light source , are arranged side by side, one or more brightness peak values exist between the plurality of light-emitting units , the lens includes a lens body part , a notch part , and a light source introduction part , the notch part is provided in a position which is a center of the lens body part and which faces the light source , characterized in that : the light source introduction part protrudes to the light source side from a rear side of the notch part , and introduces an incident light from the light source , and a curvature of the notch part is larger than a curvature of a front edge portion of the lens body part the vehicular light-emitting device comprises a holding part which holds the plurality of light-emitting units , the holding part has a reflection part which reflects the light emitted from the lenses toward a light-emitting surface, the reflection part is formed with a plurality of convex parts at positions facing the light sources , and a planar part is provided between adjacent two of the plurality of convex parts . a plurality of light-emitting units , each of which includes a light source and a lens for diffusing and emitting the light entered from the light source , are arranged side by side, one or more brightness peak values exist between the plurality of light-emitting units , the lens includes a lens body part , a notch part , and a light source introduction part , the notch part is provided in a position which is a center of the lens body part and which faces the light source , the light source introduction part protrudes to the light source side from a rear side of the notch part , and introduces an incident light from the light source , and a curvature of the notch part is larger than a curvature of a front edge portion of the lens body part the vehicular light-emitting device comprises a holding part which holds the plurality of light-emitting units , the holding part has a reflection part which reflects the light emitted from the lenses toward a light-emitting surface, the reflection part is formed with a plurality of convex parts at positions facing the light sources , and a planar part is provided between adjacent two of the plurality of convex parts .
Mixer assembly unit, especially for an exhaust system of an internal combustion engine of a vehicle, comprising a mixer body with an inflow side and with an outflow side and with a plurality of flow deflection elements , and a carrier area provided radially outwards in relation to the mixer longitudinal axis (L) at the mixer body , wherein the mixer body is formed as one piece with the carrier area , characterized in that the carrier area has an exhaust gas guide element connection area for a fixed connection to a preferably tubular exhaust gas guide element and, radially outside the exit guide element connection area , a flange-like coupling section for coupling with a flange-like coupling section of another exhaust gas guide element .
A method for fabricating a gas turbine engine component (60; 60a; 60b) including a geometrically segmented coating section , the coating section including a wall , the method comprising: depositing a coating on the J wall , wherein the wall includes a first side and a second side opposite the first side , the second side includes an array of cells , and a cooling passage (78; 178) that extends through the wall and the coating to an encapsulation over the cooling passage , said encapsulation closes the cooling passage and thus prevents any coating material from entering into the cooling passage during the fabrication process, and the coating is deposited in the array of cells ; removing a portion of the coating along the array of cells ; and removing the encapsulation to open the cooling passage (78; 178). depositing a coating on the J wall , wherein the wall includes a first side and a second side opposite the first side , the second side includes an array of cells , and a cooling passage (78; 178) that extends through the wall and the coating to an encapsulation over the cooling passage , said encapsulation closes the cooling passage and thus prevents any coating material from entering into the cooling passage during the fabrication process, and the coating is deposited in the array of cells ; removing a portion of the coating along the array of cells ; and removing the encapsulation to open the cooling passage (78; 178).
A glass, the glass comprising from 54 mol% to 71 mol% SiO 2 ; from 16 mol% to 18 mol% Al 2 O 3 ; from 9 mol% to 18 mol% Na 2 O; at least one of MgO, CaO, ZnO, BaO, and SrO; from 0.5 mol% to 11 mol% B 2 O 3 ; and 0.5 mol% to about 11 mol% P 2 O 5 ;, wherein 0.5 mol% ≤ MgO(mol%) + CaO(mol%) ZnO(mol%) BaO(mol%) SrO(mol%) ≤ 4 mol%; 4 mol% ≤ B 2 O 3 (mol%) P 2 O 5 (mol%) ≤ 15 mol%; and Al 2 O 3 (mol%) ≥ B 2 O 3 (mol%) P 2 O 5 (mol%). from 54 mol% to 71 mol% SiO 2 ; from 16 mol% to 18 mol% Al 2 O 3 ; from 9 mol% to 18 mol% Na 2 O; at least one of MgO, CaO, ZnO, BaO, and SrO; from 0.5 mol% to 11 mol% B 2 O 3 ; and 0.5 mol% to about 11 mol% P 2 O 5 ;, wherein 0.5 mol% ≤ MgO(mol%) + CaO(mol%) ZnO(mol%) BaO(mol%) SrO(mol%) ≤ 4 mol%; 4 mol% ≤ B 2 O 3 (mol%) P 2 O 5 (mol%) ≤ 15 mol%; and Al 2 O 3 (mol%) ≥ B 2 O 3 (mol%) P 2 O 5 (mol%).
Method for straightening a workpiece with a longitudinal axis, wherein the workpiece , which is held in mounting heads at the end, is bent out from a starting position transversely to the longitudinal axis and bent back again, characterized in that the workpiece is bent out by means of the two mounting heads , which can be aligned coaxially with respect to one another and can be adjusted relative to one another in the direction of the coaxial straightening axis , in directions changing at least in predetermined angular ranges and bent back again.