mhurhangee/patent-ind-claim-en huggingface dataset:
A method for installing an offshore platform, comprising: 1) pre-installing a first installation element on a topside module , and pre-installing a second installation element on an offshore installation frame (S 1), wherein the offshore installation frame is provided with an area allowing for entry of a vessel ; 2) reducing buoyancy of a floating structure through an adjustment mechanism to lower the vessel carrying the floating structure until a deck of the vessel is flush with a land; and transferring the topside module to the deck of the vessel (S2), wherein the floating structure and the vessel are detachably connected; and; 3) when the vessel sails offshore, increasing the buoyancy of the floating structure through the adjustment mechanism ; and transferring the topside module near the offshore installation frame through the vessel and the floating structure (S3), 4) detaching the floating structure from the vessel (S4); 5) driving the vessel carrying the topside module to enter the area allowing for entry of a vessel ; and aligning the first installation element with the second installation element (S5); and 6) sinking the vessel to mate the first installation element with the second installation element to complete installation (S6). 1) pre-installing a first installation element on a topside module , and pre-installing a second installation element on an offshore installation frame (S 1), wherein the offshore installation frame is provided with an area allowing for entry of a vessel ; 2) reducing buoyancy of a floating structure through an adjustment mechanism to lower the vessel carrying the floating structure until a deck of the vessel is flush with a land; and transferring the topside module to the deck of the vessel (S2), wherein the floating structure and the vessel are detachably connected; and; 3) when the vessel sails offshore, increasing the buoyancy of the floating structure through the adjustment mechanism ; and transferring the topside module near the offshore installation frame through the vessel and the floating structure (S3), 4) detaching the floating structure from the vessel (S4); 5) driving the vessel carrying the topside module to enter the area allowing for entry of a vessel ; and aligning the first installation element with the second installation element (S5); and 6) sinking the vessel to mate the first installation element with the second installation element to complete installation (S6).
Device for air-conditioning rooms, having - a channel comprising at least a first channel portion extending in a longitudinal direction (L) and a second channel portion arranged parallel and next to the first channel portion , - wherein the first channel portion has at least a source air feed and a first opening portion which is designed to discharge source air , wherein the first opening portion is oriented towards an opening side of the channel , - the second channel portion has a temperature-control element and a second opening portion which is designed to receive secondary air and to discharge temperature-controlled secondary air , wherein the second opening portion is oriented towards the opening side of the channel , - one or more slot outlets , oriented in the longitudinal direction (L), for discharging source air are provided at the first opening portion , - the second opening portion has an inlet portion for admitting the secondary air and an outlet portion for discharging the temperature-controlled secondary air , - wherein the inlet portion and the outlet portion are arranged parallel to and alongside one another in the longitudinal direction (L), and - the inlet portion is arranged between the outlet portion and the first opening portion . - a channel comprising at least a first channel portion extending in a longitudinal direction (L) and a second channel portion arranged parallel and next to the first channel portion , - wherein the first channel portion has at least a source air feed and a first opening portion which is designed to discharge source air , wherein the first opening portion is oriented towards an opening side of the channel , - the second channel portion has a temperature-control element and a second opening portion which is designed to receive secondary air and to discharge temperature-controlled secondary air , wherein the second opening portion is oriented towards the opening side of the channel , - one or more slot outlets , oriented in the longitudinal direction (L), for discharging source air are provided at the first opening portion , - the second opening portion has an inlet portion for admitting the secondary air and an outlet portion for discharging the temperature-controlled secondary air , - wherein the inlet portion and the outlet portion are arranged parallel to and alongside one another in the longitudinal direction (L), and - the inlet portion is arranged between the outlet portion and the first opening portion .
A nerve integrity monitoring system for use during operation of an electrosurgical unit, comprising: a plurality of sensing probes each constituting a separate channel and adapted to generate a corresponding plurality of input signals; an input module electrically coupled to the plurality of sensing probes and adapted to receive the plurality of input signals; an EMG detection module coupled to the input module and adapted to detect conditions in each input signal and classify the conditions as a function of a level of EMG activity received from the patient; an artifact detection module coupled to the input module and adapted to detect an artifact indicative of metal-to-metal contact in the input signals and to mute a channel for which an artifact is detected, independent of other channels; and an output module coupled to the EMG detection module and the artifact detection module, and adapted to provide a first output signal indicative of the detected conditions in the first input signal and provide a second output signal indicative of the artifact. a plurality of sensing probes each constituting a separate channel and adapted to generate a corresponding plurality of input signals; an input module electrically coupled to the plurality of sensing probes and adapted to receive the plurality of input signals; an EMG detection module coupled to the input module and adapted to detect conditions in each input signal and classify the conditions as a function of a level of EMG activity received from the patient; an artifact detection module coupled to the input module and adapted to detect an artifact indicative of metal-to-metal contact in the input signals and to mute a channel for which an artifact is detected, independent of other channels; and an output module coupled to the EMG detection module and the artifact detection module, and adapted to provide a first output signal indicative of the detected conditions in the first input signal and provide a second output signal indicative of the artifact.
A mold for fabricating a multi-component optical system blank, which is shaped or formed from a first optical material to comprise: a cup portion , wherein the cup portion comprises an inner wall and a first cavity defined by the inner wall ; and wherein the mold comprises a first optical component, wherein the mold comprises a portion of the blank, wherein the first optical material is integral to and comprises a constituent of the blank, characterized in that the mold further comprises; an attachment portion extending from the cup portion ; and wherein the inner wall is concave. a cup portion , wherein the cup portion comprises an inner wall and a first cavity defined by the inner wall ; and wherein the mold comprises a first optical component, wherein the mold comprises a portion of the blank, wherein the first optical material is integral to and comprises a constituent of the blank, characterized in that the mold further comprises; an attachment portion extending from the cup portion ; and wherein the inner wall is concave.
A turbine nozzle , comprising: an airfoil that extends in span from an inner band to an outer band , wherein the inner band and the outer band define inner and outer flow boundaries of the turbine nozzle ; wherein a first set of cooling channels and a second set of cooling channels are provided in at least one of the inner band and the outer band and beneath a gas side surface of the band , wherein a coolant distribution plenum is enclosed in the band and is provided in fluid communication with the first and second sets of cooling channels (214a, 214b; 314a, 314b), wherein an inlet passage is provided in the band and provides for direct fluid communication between a coolant supply and the first set of cooling channels , characterized in that the first set of cooling channels is fluidly connected directly downstream from the inlet passage , the coolant distribution plenum is fluidly connected directly downstream from the first set of cooling channels , and the second set of cooling channels is fluidly connected directly downstream from the coolant distribution plenum . an airfoil that extends in span from an inner band to an outer band , wherein the inner band and the outer band define inner and outer flow boundaries of the turbine nozzle ; wherein a first set of cooling channels and a second set of cooling channels are provided in at least one of the inner band and the outer band and beneath a gas side surface of the band , wherein a coolant distribution plenum is enclosed in the band and is provided in fluid communication with the first and second sets of cooling channels (214a, 214b; 314a, 314b), wherein an inlet passage is provided in the band and provides for direct fluid communication between a coolant supply and the first set of cooling channels , characterized in that the first set of cooling channels is fluidly connected directly downstream from the inlet passage , the coolant distribution plenum is fluidly connected directly downstream from the first set of cooling channels , and the second set of cooling channels is fluidly connected directly downstream from the coolant distribution plenum .
An information processing apparatus comprising: an acquisition unit that acquires a captured image obtained by capturing an image of a wearable device including a module whose appearance changes according to time and whose appearance represents a current time; and an estimation unit that detects the module appearing in the captured image on the basis of a generated template image representing an appearance of the module according to the current time and estimates at least one of a position or a posture of the wearable device . an acquisition unit that acquires a captured image obtained by capturing an image of a wearable device including a module whose appearance changes according to time and whose appearance represents a current time; and an estimation unit that detects the module appearing in the captured image on the basis of a generated template image representing an appearance of the module according to the current time and estimates at least one of a position or a posture of the wearable device .
A drill bit insert for rock drilling comprising a sintered cemented carbide body having a bulk and a surface, and including a hard phase of tungsten carbide, WC, and a binder phase, wherein the cemented carbide body comprises: • 5.0 - 7.0 wt % Co, • 0.10 - 0.35 wt % Cr, • optionally a cubic carbides (W x M 1-x )C phase (M = Ti, Ta, Nb, Zr or Hf) up to 0.2 wt%, and • balance WC including possible impurities; characterized in, that the sintered cemented carbide body has a Cr/Co weight ratio of 0.015 - 0.058 and a mean WC grain size of 0.60-0.95 μm, wherein mean WC grain size is measured according to ISO 4499-2:2008 using SEM micrographs, and that the sintered cemented carbide body has a bulk hardness of 1520- 1660 Hv30 and a bulk toughness of K1 c ≥ 10.0 MN ∗ m^(-3/2) both measured in the bulk at a measurement position ≥ 5 mm from the surface of the body, and a mechanically induced surface toughness of K1 c ≥ 12.0 MN ∗ m^(-3/2) measured at a measurement position 0.5 mm below the surface of the body in a transverse direction to a longitudinal axis of the insert, wherein hardness is measured according to IS03878:1983 Hard metals - Vickers hardness test and toughness is measured according to ISO 28079:2009 Palmqvist toughness test for hard metals. • 5.0 - 7.0 wt % Co, • 0.10 - 0.35 wt % Cr, • optionally a cubic carbides (W x M 1-x )C phase (M = Ti, Ta, Nb, Zr or Hf) up to 0.2 wt%, and • balance WC including possible impurities; that the sintered cemented carbide body has a Cr/Co weight ratio of 0.015 - 0.058 and a mean WC grain size of 0.60-0.95 μm, wherein mean WC grain size is measured according to ISO 4499-2:2008 using SEM micrographs, and that the sintered cemented carbide body has a bulk hardness of 1520- 1660 Hv30 and a bulk toughness of K1 c ≥ 10.0 MN ∗ m^(-3/2) both measured in the bulk at a measurement position ≥ 5 mm from the surface of the body, and a mechanically induced surface toughness of K1 c ≥ 12.0 MN ∗ m^(-3/2) measured at a measurement position 0.5 mm below the surface of the body in a transverse direction to a longitudinal axis of the insert, wherein hardness is measured according to IS03878:1983 Hard metals - Vickers hardness test and toughness is measured according to ISO 28079:2009 Palmqvist toughness test for hard metals.
A method comprising: disposing a moisture pump partially within an enclosure, such that the moisture pump is in fluid communication with the enclosure and an external environment; wherein the enclosure comprises: water vapor; and a supersaturated salt solution; transferring, with the moisture pump, a portion of the water vapor from the enclosure to the external environment over at least one time-period; measuring a change in mass of the supersaturated salt solution over the at least one time-period; and calculating a rate of the portion of water vapor transferred, with the moisture pump, from the enclosure to the external environment over the at least one time-period; wherein the rate of water vapor transferred, with the moisture pump, from the enclosure to the external environment is calculated based on the change in mass of the supersaturated salt solution; and wherein the method is performed at an equilibrium relative humidity in the enclosure. disposing a moisture pump partially within an enclosure, such that the moisture pump is in fluid communication with the enclosure and an external environment; wherein the enclosure comprises: water vapor; and a supersaturated salt solution; water vapor; and a supersaturated salt solution; transferring, with the moisture pump, a portion of the water vapor from the enclosure to the external environment over at least one time-period; measuring a change in mass of the supersaturated salt solution over the at least one time-period; and calculating a rate of the portion of water vapor transferred, with the moisture pump, from the enclosure to the external environment over the at least one time-period; wherein the rate of water vapor transferred, with the moisture pump, from the enclosure to the external environment is calculated based on the change in mass of the supersaturated salt solution; and wherein the method is performed at an equilibrium relative humidity in the enclosure. wherein the rate of water vapor transferred, with the moisture pump, from the enclosure to the external environment is calculated based on the change in mass of the supersaturated salt solution; and wherein the method is performed at an equilibrium relative humidity in the enclosure.
Dapansutrite, or a pharmaceutically acceptable solvate thereof, as a pharmaceutical compound for use in a method for treating asthma, wherein said compound is administered by oral administration.
A method of making a plurality of cubic boron nitride (cBN) grains, comprising: providing a plurality of hexagonal boron nitride (hBN) grains; providing a catalyst; subjecting the hBN grains and the catalyst to a high pressure and high temperature (HPHT) operation for a time period sufficient to form a reaction mass containing cBN grains; and cleaning the cBN grains from the reaction mass by heating the cBN grains in caustic chemicals at a temperature in a range 400°C to 800°C for 10 minutes to 200 minutes thereby forming island-like structures on a surface of the plurality of cBN grains by removing stressed regions produced during the HPHT operation; wherein at least about 15% of the plurality of cBN grains have at least one grain face comprising features present as concave indentations, peaks, valleys, bumps, ellipsoid shapes or as waves, blisters, feathers or fish scales. providing a plurality of hexagonal boron nitride (hBN) grains; providing a catalyst; subjecting the hBN grains and the catalyst to a high pressure and high temperature (HPHT) operation for a time period sufficient to form a reaction mass containing cBN grains; and cleaning the cBN grains from the reaction mass by heating the cBN grains in caustic chemicals at a temperature in a range 400°C to 800°C for 10 minutes to 200 minutes thereby forming island-like structures on a surface of the plurality of cBN grains by removing stressed regions produced during the HPHT operation; wherein at least about 15% of the plurality of cBN grains have at least one grain face comprising features present as concave indentations, peaks, valleys, bumps, ellipsoid shapes or as waves, blisters, feathers or fish scales.
Hydrodynamic coupling having a pump impeller as first blade wheel and having a turbine wheel as second blade wheel , wherein the pump impeller has pump-impeller blades connected to a main body of the pump impeller and wherein the turbine wheel has turbine-wheel blades connected to a main body of the turbine wheel, wherein the pump impeller and the turbine wheel are each mounted so as to be rotatable about a central axis and wherein the blades of the pump impeller have boundary edges which are arranged in a manner facing the boundary edges of the blades of the turbine wheel, such that at least one of the blades of one blade wheel has a boundary edge , wherein the boundary edge is subdivided into a first portion with a first edge contour and a second portion with a second edge contour , and wherein the first and the second edge contour are different and characterized in that the second portion with the second edge contour has a sharp-edged edge contour.
A method of detecting a malfunction of a management system of a battery comprising a plurality of stages (E i ) coupled in series, each stage comprising a plurality of cells (C i ) coupled in parallel by conductors (b i ), the management system comprising a plurality of voltage sensors (V i , A i ), said plurality of voltage sensors comprising a voltage sensor across each cell (C i ) and conductor (b i ), of the battery, the sensors (V i , A i ) define a set of meshes such that each sensor is comprised in several meshes of the set, and such that in each one of the meshes, in normal operation, the sum of the output values of the voltage sensors of the mesh is equal to 0 within the sensors measurement inaccuracies, the method comprising the steps of: a) reading the output values of said sensors; and b) determining, by means of a processing unit , whether the mesh equations of the set of meshes are satisfied by the read values, a mesh equation being considered as satisfied if the sum of the output values of the sensors of the mesh is equal to 0 within the sensors measurement inaccuracies. a) reading the output values of said sensors; and b) determining, by means of a processing unit , whether the mesh equations of the set of meshes are satisfied by the read values, a mesh equation being considered as satisfied if the sum of the output values of the sensors of the mesh is equal to 0 within the sensors measurement inaccuracies.
A method of fabricating a coating, the method comprising: providing a ceramic matrix composite that includes SiC fibers disposed in a SiC matrix; depositing a base slurry on the ceramic matrix composite, wherein the base slurry contains powders of a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, barium-magnesium-aluminosilicate, and a first carrier fluid; drying the deposited base slurry to produce a base green layer; depositing a transition slurry on the base green layer, wherein the transition slurry contains powders of a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, at least one of zirconium carbide, zirconium nitride, or zirconium oxide, barium-magnesium-aluminosilicate, and a second carrier fluid; drying the deposited transition slurry to produce a transition green layer; and forming a consolidated coating on the ceramic matrix composite by heating the base green layer and the at least one transition green layer, wherein the heating causes chemical reactions that convert the powders of the at least one of the silicon carbide, silicon nitride, or free silicon and the at least one of the zirconium carbide, zirconium nitride, or zirconium oxide to, respectively, metal-silicon-oxygen rich phase and metal-zirconium-oxygen rich phase. providing a ceramic matrix composite that includes SiC fibers disposed in a SiC matrix; depositing a base slurry on the ceramic matrix composite, wherein the base slurry contains powders of a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, barium-magnesium-aluminosilicate, and a first carrier fluid; a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, barium-magnesium-aluminosilicate, and a first carrier fluid; drying the deposited base slurry to produce a base green layer; depositing a transition slurry on the base green layer, wherein the transition slurry contains powders of a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, at least one of zirconium carbide, zirconium nitride, or zirconium oxide, barium-magnesium-aluminosilicate, and a second carrier fluid; a metal oxide, at least one of silicon carbide, silicon nitride, or free silicon, at least one of zirconium carbide, zirconium nitride, or zirconium oxide, barium-magnesium-aluminosilicate, and a second carrier fluid; drying the deposited transition slurry to produce a transition green layer; and forming a consolidated coating on the ceramic matrix composite by heating the base green layer and the at least one transition green layer, wherein the heating causes chemical reactions that convert the powders of the at least one of the silicon carbide, silicon nitride, or free silicon and the at least one of the zirconium carbide, zirconium nitride, or zirconium oxide to, respectively, metal-silicon-oxygen rich phase and metal-zirconium-oxygen rich phase.