mhurhangee/ep-ind-claims huggingface dataset:
A speed retarding device for a rotary nozzle comprising: a hollow cylindrical housing; a rotatable tubular shaft rotatably carried by the housing, the shaft having a drag sleeve portion in the housing and having a shaft end extending through at least one end of the housing, wherein the shaft end is adapted to receive a rotary nozzle thereon; a pair of support bearings (112, 114) supporting the drag sleeve portion of the shaft in the housing; an annular inner seal between each of the support bearings (112, 114) and the drag sleeve portion, wherein the inner seals, the housing and the drag sleeve portion define a cavity within the housing; and a viscous fluid confined within the cavity. a hollow cylindrical housing; a rotatable tubular shaft rotatably carried by the housing, the shaft having a drag sleeve portion in the housing and having a shaft end extending through at least one end of the housing, wherein the shaft end is adapted to receive a rotary nozzle thereon; a pair of support bearings (112, 114) supporting the drag sleeve portion of the shaft in the housing; an annular inner seal between each of the support bearings (112, 114) and the drag sleeve portion, wherein the inner seals, the housing and the drag sleeve portion define a cavity within the housing; and a viscous fluid confined within the cavity.
A method for operating a flowmeter diagnostic tool as follows: calculating a standard deviation σ of the flowmeter sensor assembly flow rate; determining the number of samples used to calculate σ; determine the sampling duration; calculating a meter-specific factor, wherein the meter-specific factor comprises a sampling rate for total prove time measurements. calculating an estimated total prove time necessary to pass a predetermined repeatability requirement using the meter-specific factor and the σ; interfacing the diagnostic tool with a flowmeter sensor assembly; inputting a base prover volume into the diagnostic tool; inputting a desired number of passes per run into the diagnostic tool; receiving flowmeter data; calculating an estimated minimum number of runs needed to achieve the calculated estimated total prove time. calculating a standard deviation σ of the flowmeter sensor assembly flow rate; determining the number of samples used to calculate σ; determine the sampling duration; calculating a meter-specific factor, wherein the meter-specific factor comprises a sampling rate for total prove time measurements. calculating an estimated total prove time necessary to pass a predetermined repeatability requirement using the meter-specific factor and the σ; interfacing the diagnostic tool with a flowmeter sensor assembly; inputting a base prover volume into the diagnostic tool; inputting a desired number of passes per run into the diagnostic tool; receiving flowmeter data; calculating an estimated minimum number of runs needed to achieve the calculated estimated total prove time.
A supersonic aircraft including a fuselage and a sharp, modified biconvex laminar flow enabling wing with less than 30 degrees leading edge sweep and thickness to chord ratio (t/c) of 2% or less as a span-wise average over the majority of the wing, excluding a zone near the inboard end, which may be thicker, up to about 4% thickness to chord ratio (t/c) in combination with area ruling, characterized in that said wing is configured to improve laminar flow and improve drag by including: a) a strake extending forwardly of the wing inboard extent; and b) wing leading edge convexity in plan view at the junction of the strake with the leading edge of the wing. a) a strake extending forwardly of the wing inboard extent; and b) wing leading edge convexity in plan view at the junction of the strake with the leading edge of the wing.
A film covered battery comprising: a battery element having a positive electrode and a negative electrode opposing each other; lead terminals connected to said positive electrode and said negative electrode, respectively; a flexible casing for sealing said element and said terminals together with an electrolytic solution, said terminals partially extending from said casing; characterized in that a buffer for accumulating gas generated within said casing through deformation of said casing, is formed in at least a portion of said casing outside said battery element with respect to in plane direction on main surface of said battery element, and said buffer is formed along the complete length of at least one side that extends along the sealed inner surfaces of said casing and said buffer is formed continuously with and outside a region in which said battery element is accommodated. a battery element having a positive electrode and a negative electrode opposing each other; lead terminals connected to said positive electrode and said negative electrode, respectively; a flexible casing for sealing said element and said terminals together with an electrolytic solution, said terminals partially extending from said casing; characterized in that a buffer for accumulating gas generated within said casing through deformation of said casing, is formed in at least a portion of said casing outside said battery element with respect to in plane direction on main surface of said battery element, and said buffer is formed along the complete length of at least one side that extends along the sealed inner surfaces of said casing and said buffer is formed continuously with and outside a region in which said battery element is accommodated.
Process for manufacturing a bakery product comprising the steps of forming a dough; forming a powder, the powder particles comprising between 50 wt.% and 70 wt.% starch-based material and between 30 wt.% and 50 wt.% salty tastant on a dry basis; and applying the powder to at least one surface of the dough wherein the powder is formed by coating the starch-based material with an aqueous solution of salty tastant and then drying the coated edible carrier and wherein the bakery product is a pizza or a savoury turnover, and wherein the weight of the powder particles comprising a starch-based material and a salty tastant are between 1.2 and 6.0 % of the weight of the un-powdered bakery product on a dry basis, and wherein the bakery product has a sodium level of below 600 mg per 100 g.
Luminaire having a light source which comprises at least one LED for producing indirect lighting, the light source being provided on one side of the luminaire which, in the mounted state of the luminaire, points in the direction of the ceiling of the room, wherein a free-form lens is arranged above the light source and the free-form lens has optical surfaces which are arranged to widen the light distribution of the indirect illumination by a combination of light refraction and total reflection with respect to the light distribution which the LED itself has, characterized in that the free-form lens is arranged so that a part of the light, which enters the free-form lens from the at least one LED, is totally reflected several times on two opposite optical surfaces (6, 7) and is transported in the free-form lens in the manner of a light guide in a direction perpendicular to the optical axis of the LED and is coupled out by at least one lateral light exit surface (9; 10).
A trailer refrigerating apparatus including a refrigerant circuit and cooling an in-compartment space of a trailer, comprising: a generator; an engine for driving the generator; an inverter section for converting power output from the generator and outputting the power; an electric compressor to be driven by the power output from the inverter section; a condenser for heat exchange between air outside the compartment of the trailer and refrigerant; characterized by a casing unit having a first machine chamber in which the generator, the engine and the inverter section are accommodated and a second machine chamber in which the electric compressor and the condenser are accommodated; and a cooling section (26, 40a, 90, 95) for cooling the inverter section by air outside a compartment of the trailer injected into the first machine chamber, wherein air outside a compartment of the trailer is sucked into the second machine chamber, passes through the condenser and is then joined with the air used for cooling the inverter section sent to the second machine chamber. a generator; an engine for driving the generator; an inverter section for converting power output from the generator and outputting the power; an electric compressor to be driven by the power output from the inverter section; a condenser for heat exchange between air outside the compartment of the trailer and refrigerant; characterized by a casing unit having a first machine chamber in which the generator, the engine and the inverter section are accommodated and a second machine chamber in which the electric compressor and the condenser are accommodated; and a cooling section (26, 40a, 90, 95) for cooling the inverter section by air outside a compartment of the trailer injected into the first machine chamber, wherein air outside a compartment of the trailer is sucked into the second machine chamber, passes through the condenser and is then joined with the air used for cooling the inverter section sent to the second machine chamber.
Method for operating a burner, which burner consists essentially of a swirl generator which forms a swirl flow of the combustion air stream, this swirl generator being followed downstream by a mixing zone in which, within a first transitional portion, flow guide means act which run in the flow direction and which take over the transfer of the swirl flow formed in the swirl generator into the mixing pipe acting downstream of the flow guide means, means for injecting a liquid and/or gaseous fuel into the combustion air stream being present in the swirl generator, and the fuel/air mixture thus obtained being ignited and burnt in a combustion chamber following the mixing zone downstream, at the same time forming a backflow zone, wherein a fuel (B H2) containing hydrogen or consisting of hydrogen is introduced within the flow guide means and/or downstream of these flow guide means into the upstream flow of the fuel/air mixture, characterized in that the infeed of the gaseous fuel containing hydrogen or consisting of hydrogen is carried out in such a way that a flow disturbance of the fuel/air swirl flow is minimized, wherein the infeed of the fuel takes place with a tangential component oriented in the swirl direction of the fuel/air swirl flow and with a radial component oriented longitudinally with respect to a burner axis.
A skin illumination device for treating subcutaneous fat comprising: a panel with fifty-six individual LEDs arranged in a matrix and configured to produce light with a centroid wavelength of 940 nm; a rectangular sapphire window acting as a contact surface for contact with an epidermis of a subject; and an aluminum frame through which coolant conduits pass, configured to transport a cooling-liquid to cool LEDs and the sapphire window, wherein the matrix of LEDs, when activated, produce an illumination light with a power density of 1.6 W/cm 2 that passes through the sapphire window to heat tissue. a panel with fifty-six individual LEDs arranged in a matrix and configured to produce light with a centroid wavelength of 940 nm; a rectangular sapphire window acting as a contact surface for contact with an epidermis of a subject; and an aluminum frame through which coolant conduits pass, configured to transport a cooling-liquid to cool LEDs and the sapphire window, wherein the matrix of LEDs, when activated, produce an illumination light with a power density of 1.6 W/cm 2 that passes through the sapphire window to heat tissue.
A bottom freezer refrigerator having an ice maker and dispenser comprising: a freezer compartment maintained at a temperature below 0° C.; a refrigerator compartment maintained at a temperature above 0° C. positioned above the freezer compartment; an insulated refrigerator compartment door; a refrigeration system for cooling the freezer compartment and the refrigerator compartment; an insulated sub-compartment (88, 114, 190) located in the refrigerator compartment; an automatic ice maker (82, 112) in the sub-compartment (88,114,190) for generating ice cubes; a water supply for the ice maker; an ice cube storage bin; an ice dispenser (72, 86,116) positioned on the refrigerator door to receive ice cubes from the ice cube storage bin and dispense ice cubes from the face of the refrigerator door; wherein the ice maker (82, 112) and ice cube storage bin are provided with air cooled below 0° C. for forming and storing ice pieces; and characterized in that the insulated sub-compartment is closed by the refrigerator door when the refrigerator door is closed. a freezer compartment maintained at a temperature below 0° C.; a refrigerator compartment maintained at a temperature above 0° C. positioned above the freezer compartment; an insulated refrigerator compartment door; a refrigeration system for cooling the freezer compartment and the refrigerator compartment; an insulated sub-compartment (88, 114, 190) located in the refrigerator compartment; an automatic ice maker (82, 112) in the sub-compartment (88,114,190) for generating ice cubes; a water supply for the ice maker; an ice cube storage bin; an ice dispenser (72, 86,116) positioned on the refrigerator door to receive ice cubes from the ice cube storage bin and dispense ice cubes from the face of the refrigerator door;
Strand-shaped seal profile having an anchor foot for latch-fitting into an undercut receptacle groove of a profile; a transition portion which adjoins the anchor foot; and a base portion which adjoins the transition portion; wherein a substantially closed cavity extends in the anchor foot and in the transition portion; wherein the cavity has a first cavity portion which has a substantially constant first clear breadth, forming substantially a rectangle in the cross section through the longitudinal extent of the seal profile, characterized in that the cavity has a second cavity portion which has a substantially constant second clear breadth which is smaller than the first clear breadth, forming substantially a rectangle in the cross section through the longitudinal extent of the seal profile, and wherein the second cavity portion is located in the region of the anchor foot.
A server connection method, comprising: providing ten servers, wherein each server comprises five nodes, wherein each node has 2 internal and 5 external connection ports, and the five nodes of each server are connected head-to-tail via the internal connection ports in series in a same connection manner (Step 101); and connecting, via the external connection ports, five nodes of any server in five of the ten servers to five nodes of each of the remaining five servers in a one-to-one correspondence manner, so as to form an optimal network of a Hoffman-Singleton graph (Step 102). providing ten servers, wherein each server comprises five nodes, wherein each node has 2 internal and 5 external connection ports, and the five nodes of each server are connected head-to-tail via the internal connection ports in series in a same connection manner (Step 101); and connecting, via the external connection ports, five nodes of any server in five of the ten servers to five nodes of each of the remaining five servers in a one-to-one correspondence manner, so as to form an optimal network of a Hoffman-Singleton graph (Step 102).
A method for installing a wind turbine blade on a wind turbine hub comprising: hoisting a blade towards the hub; bringing the blade and the hub into contact through an adaptable resilient body (5, 50, 60, 70, 80, 90, 200) such that the adaptable resilient body (5, 50, 60, 70, 80, 80, 90, 200) is compressed between the blade and the hub; reducing a dimension of the adaptable resilient body (5, 50, 60, 70, 80, 90, 200) such that the blade approaches the hub in a controlled fashion; and mounting the blade to the hub. hoisting a blade towards the hub; bringing the blade and the hub into contact through an adaptable resilient body (5, 50, 60, 70, 80, 90, 200) such that the adaptable resilient body (5, 50, 60, 70, 80, 80, 90, 200) is compressed between the blade and the hub; reducing a dimension of the adaptable resilient body (5, 50, 60, 70, 80, 90, 200) such that the blade approaches the hub in a controlled fashion; and mounting the blade to the hub.
A computer-implemented method, comprising: obtaining input data defining one or more 3D polygonal mesh models comprising separate meshes for two or more objects (201, 250); determining a number of perspectives for capturing depth map data of the one or more models, wherein the number of perspectives is based on, at least in part, a polygon count associated with the input data, wherein each perspective of the number of perspectives, which is selected based on the polygon count and used to capture the depth map data, is positioned at a respective position located in the virtual environment, wherein the number of perspectives is a plurality of perspectives; filtering and removing one or more components of the one or more 3D polygonal mesh models that are hidden from the perspectives by capturing depth map data from the plurality of perspectives of the one or more 3D polygonal mesh models in the virtual environment; generating point cloud data by merging the depth map data captured from the perspectives; and generating output mesh data by applying a surface reconstruction to the point cloud data and applying a mesh decimation algorithm to the output mesh data, wherein the output mesh data is a single mesh that is renderable to generate image data from the multiple of perspectives. obtaining input data defining one or more 3D polygonal mesh models comprising separate meshes for two or more objects (201, 250); determining a number of perspectives for capturing depth map data of the one or more models, wherein the number of perspectives is based on, at least in part, a polygon count associated with the input data, wherein each perspective of the number of perspectives, which is selected based on the polygon count and used to capture the depth map data, is positioned at a respective position located in the virtual environment, wherein the number of perspectives is a plurality of perspectives; filtering and removing one or more components of the one or more 3D polygonal mesh models that are hidden from the perspectives by capturing depth map data from the plurality of perspectives of the one or more 3D polygonal mesh models in the virtual environment; generating point cloud data by merging the depth map data captured from the perspectives; and generating output mesh data by applying a surface reconstruction to the point cloud data and applying a mesh decimation algorithm to the output mesh data, wherein the output mesh data is a single mesh that is renderable to generate image data from the multiple of perspectives.
A method of manufacturing granules for a friction material, the method comprising: providing powder grains of a mixture including a friction modifying granular material and a resin binder, said friction modifying granular material being selected from abrasives, lubricants, organic dusts, and metals; introducing the powder grains into a vessel; introducing air into the vessel to bring the powder grains into a fluidized-bed state; and spraying a liquid including a water-soluble or water-dispersible binder to the powder grains in the fluidized-bed state to granulate the powder grains until granules for the friction material having a particle size of from 100 to 2000 μm, and a median diameter (D 50) of from 300 to 900 μm are obtained. providing powder grains of a mixture including a friction modifying granular material and a resin binder, said friction modifying granular material being selected from abrasives, lubricants, organic dusts, and metals; introducing the powder grains into a vessel; introducing air into the vessel to bring the powder grains into a fluidized-bed state; and spraying a liquid including a water-soluble or water-dispersible binder to the powder grains in the fluidized-bed state to granulate the powder grains until granules for the friction material having a particle size of from 100 to 2000 μm, and a median diameter (D 50) of from 300 to 900 μm are obtained.
A comb (1, 50, 60) comprising a comb main body (2, 52, 62) having one edge comb part (3, 53, 63) projecting from one end (2a, 52a, 62a) of the comb main body (2, 52, 62), another edge comb part (4, 54, 64) projecting from another end (2b, 52b, 62b) of the comb main body (2, 52, 62), and a plurality of comb teeth (6, 56, 66) projecting from the comb main body (2, 52, 62) between the one edge comb part (3, 53, 63) and the other edge comb part (4, 54, 64), wherein the one edge comb part (3, 53, 63) is divided into a range on a tip-end side having a tapered tip end, a range on the root side connected with the comb main body (2, 52, 62) and a range of a middle part which is between the tip-end side and the root side, and wherein an outer edge surface forming an edge of a perimeter of the one edge comb part (3, 53, 63) in a front view is concave at the middle part and convex at the tip-end side by forming a dented part at the middle part in the outer edge surface, characterized in that: a tip end through-hole (8, 58, 68) penetrating in the width directions of the one edge comb part (3, 53, 63) is formed within the range on the tip-end side, and a counter bore is formed around the tip end through-hole (8, 58, 68). a tip end through-hole (8, 58, 68) penetrating in the width directions of the one edge comb part (3, 53, 63) is formed within the range on the tip-end side, and a counter bore is formed around the tip end through-hole (8, 58, 68).
A process for preparing a compound of formula I: the process comprising: (a) reacting a compound of formula 1: with a C 1-6 alkyl 3-oxobutanoate in the presence of piperidine to form a compound of formula 2: wherein each R is independently selected from C 1-6 alkyl; (b) reacting the compound of formula 2 with an alkali metal hydroxide to form, after acidification of the reaction product with an acid, a compound of formula 3: (c) reacting the compound of formula 3 with an ammonia reagent to form a compound of formula 4: (d) reacting the compound of formula 4 with a reducing agent to form a compound of formula 5 or a salt thereof: (e) reacting the compound of formula 5 or a salt thereof with di-tert-butyl dicarbonate to form a compound of formula 6: (f) reacting the compound of formula 6 with an alkyl lithium reagent to form a compound of formula 7: (g) reacting the compound of formula 7 with carbon dioxide to form the compound of formula I. (a) reacting a compound of formula 1: with a C 1-6 alkyl 3-oxobutanoate in the presence of piperidine to form a compound of formula 2: wherein each R is independently selected from C 1-6 alkyl; (b) reacting the compound of formula 2 with an alkali metal hydroxide to form, after acidification of the reaction product with an acid, a compound of formula 3: (c) reacting the compound of formula 3 with an ammonia reagent to form a compound of formula 4: (d) reacting the compound of formula 4 with a reducing agent to form a compound of formula 5 or a salt thereof: (e) reacting the compound of formula 5 or a salt thereof with di-tert-butyl dicarbonate to form a compound of formula 6: (f) reacting the compound of formula 6 with an alkyl lithium reagent to form a compound of formula 7: (g) reacting the compound of formula 7 with carbon dioxide to form the compound of formula I.