mhurhangee/ep-ind-claims huggingface dataset:
A falling film evaporator used in a refrigeration apparatus, the falling film evaporator comprising: a heat transfer tube bundle to the interior of which a heat medium is channeled, the heat transfer tube bundle having a plurality of longitudinally extending heat transfer tubes; a tank inside of which said heat transfer tube bundle is disposed, the tank being provided with a refrigerant inflow port; a liquid refrigerant sprinkling part for dropping liquid refrigerant, which is contained in gas/liquid two-phase refrigerant supplied into said tank through said refrigerant inflow port, onto said heat transfer tube bundle; a vapor outlet tube extending from an upper part of said tank; a cover having a portion positioned in a location inside said tank and higher than said liquid refrigerant sprinkling part; an impeding member which is provided between said liquid refrigerant sprinkling part and said cover to a different position than said vapor outlet tube along the longitudinal direction of said heat transfer tubes, and which impedes the flow of refrigerant that flows between said liquid refrigerant sprinkling part and said cover and flows in the longitudinal direction of said heat transfer tubes, characterized in that said impeding member extends downward from a lower surface of said cover. a heat transfer tube bundle to the interior of which a heat medium is channeled, the heat transfer tube bundle having a plurality of longitudinally extending heat transfer tubes; a tank inside of which said heat transfer tube bundle is disposed, the tank being provided with a refrigerant inflow port; a liquid refrigerant sprinkling part for dropping liquid refrigerant, which is contained in gas/liquid two-phase refrigerant supplied into said tank through said refrigerant inflow port, onto said heat transfer tube bundle; a vapor outlet tube extending from an upper part of said tank; a cover having a portion positioned in a location inside said tank and higher than said liquid refrigerant sprinkling part; an impeding member which is provided between said liquid refrigerant sprinkling part and said cover to a different position than said vapor outlet tube along the longitudinal direction of said heat transfer tubes, and which impedes the flow of refrigerant that flows between said liquid refrigerant sprinkling part and said cover and flows in the longitudinal direction of said heat transfer tubes, characterized in that said impeding member extends downward from a lower surface of said cover.
An integrated device for faeces sampling and occult blood detection, comprising a lid, a main body container sealed tube, a stop block, a piston, a test strip slot seat, a sealing sheet, a base, and a faeces sampling stick, the lid being provided with an inner ring and a C-shaped outer ring, the diameter of the inner ring being adapted to the inner diameter of a round tube chamber, the diameter of the C-shaped outer ring being adapted to the outer diameter of the round tube chamber, a clearance between the inner ring and the C-shaped outer ring being adapted to the tube wall of the round tube chamber, the faeces sampling stick being fixed at the center of the inner ring, the free end of the faeces sampling stick being provided with a threaded structure, the faeces sampling stick being tightly adapted to a round hole inside a separation layer, a small hole being provided in the tube wall of the inner ring at the opening of the C-shaped outer ring to be adapted to a bulge of the stop block, the main body container sealed tube being formed by combining the round tube chamber which is for storing liquid and a rectangular tube chamber, the separation layer which has a funnel shape with the round hole in the center being provided in the round tube chamber, the shape of the stop block being adapted to the section of the top of the rectangular tube chamber, the bulge being provided on an inside wall of the stop block and adapted to the small hole of the lid, the stop block being located at the top of the rectangular tube chamber, a test strip slot being provided at one side of the test strip slot seat, a piston slot with a hole in the center being provided at the other side of the test strip slot seat, two piston supports being provided on the upper edge of the piston slot, the outer shape of the test strip slot seat being adapted to the main body container sealed tube, the base being inserted into the bottom of the test strip slot seat, a solution receiving slot being provided on one side of the base, the other side of the base being provided with a groove in a part located below the test strip slot, a slope being provided between the receiving slot and the groove, and the sealing sheet being clung to the back of the piston slot, and the piston being placed in the piston supports.
A rotor blade for a wind turbine having a longitudinal direction from a root region to a blade tip, a transverse direction from a leading edge to a trailing edge, a thickness orthogonally with respect to the longitudinal direction and orthogonally with respect to the transverse direction, and a pressure side and a suction side opposite the pressure side, comprising - a front pressure-side spar cap and a rear pressure-side spar cap and - a front suction-side spar cap and a rear suction-side spar cap, - a load introduction device (310, 320), which is arranged between at least one of the pressure-side spar caps (110, 120) and at least one of the suction-side spar caps (130, 140), wherein - the load introduction device has a load coupling device (330, 340), which is arranged and designed so as to receive a lifting device passed through a lifting opening (410, 420), - the lifting opening is arranged on the pressure side and/or the suction side, and - the lifting opening is arranged between the front pressure-side spar cap and the rear pressure-side spar cap in the transverse direction and/or between the front suction-side spar cap and the rear suction-side spar cap in the transverse direction, wherein the rotor blade comprises a front spar web and a rear spar web, wherein the load introduction device (310, 320) is arranged on the front spar web and the rear spar web.. - a front pressure-side spar cap and a rear pressure-side spar cap and - a front suction-side spar cap and a rear suction-side spar cap, - a load introduction device (310, 320), which is arranged between at least one of the pressure-side spar caps (110, 120) and at least one of the suction-side spar caps (130, 140), wherein - the load introduction device has a load coupling device (330, 340), which is arranged and designed so as to receive a lifting device passed through a lifting opening (410, 420), - the lifting opening is arranged on the pressure side and/or the suction side, and - the lifting opening is arranged between the front pressure-side spar cap and the rear pressure-side spar cap in the transverse direction and/or between the front suction-side spar cap and the rear suction-side spar cap in the transverse direction,
- Centralized architecture for the illumination of an aircraft, comprising: - at least one laser generator configured to emit a laser beam having a power of light, - a control module configured to distribute the full power of the laser beam into several partial power beams (9a, 9b, 9c) to provide different sources of light to the aircraft, - a cover dimensioned to house the at least one laser generator and the control module, the cover comprising several outputs for the passage of the partial power beams (9a, 9b, 9c), - a set of optical fibers, each optical fiber having an input disposed to receive the light of one partial power beam (9a, 9b, 9c), and an output disposed to illuminate a target area, - a phosphor optical element disposed to receive the light of the at least one partial power beam (9a, 9b, 9c) upon exiting the optical fiber output to provide a diffuse light to the target area, - a mirror disposed to receive the light upon reflecting the phosphor optical element to orient and shape the beam according to a desired illumination function, - the control module being also configured to switch on and switch off the power assigned to each one of the partial power beams (9a, 9b, 9c) to thus provide different illuminating functions to the aircraft, characterized in that it further comprises a light sensor placed at the output of the optical fiber and adapted to bounce the light upon exiting the optical fiber to be received by the control module, and wherein the control module is further configured to detect a cut in an optical fiber from an absence of a light bounce to monitor the status of the optical fiber. - at least one laser generator configured to emit a laser beam having a power of light, - a control module configured to distribute the full power of the laser beam into several partial power beams (9a, 9b, 9c) to provide different sources of light to the aircraft, - a cover dimensioned to house the at least one laser generator and the control module, the cover comprising several outputs for the passage of the partial power beams (9a, 9b, 9c), - a set of optical fibers, each optical fiber having an input disposed to receive the light of one partial power beam (9a, 9b, 9c), and an output disposed to illuminate a target area, - a phosphor optical element disposed to receive the light of the at least one partial power beam (9a, 9b, 9c) upon exiting the optical fiber output to provide a diffuse light to the target area, - a mirror disposed to receive the light upon reflecting the phosphor optical element to orient and shape the beam according to a desired illumination function, - the control module being also configured to switch on and switch off the power assigned to each one of the partial power beams (9a, 9b, 9c) to thus provide different illuminating functions to the aircraft,
A method comprising: determining whether to operate in a first mode or second mode of operation based on a reference frequency signal; in response to determining to operate in the first mode of operation, generating a first control signal and enabling a digital frequency locked-loop to control an output frequency of a digitally-controlled oscillator based on the first control signal; and in response to determining to operate in the second mode of operation, generating a second control signal and, and enabling a digital phase locked-loop to control the output frequency of the digitally-controlled oscillator based on the second control signal. determining whether to operate in a first mode or second mode of operation based on a reference frequency signal; in response to determining to operate in the first mode of operation, generating a first control signal and enabling a digital frequency locked-loop to control an output frequency of a digitally-controlled oscillator based on the first control signal; and in response to determining to operate in the second mode of operation, generating a second control signal and, and enabling a digital phase locked-loop to control the output frequency of the digitally-controlled oscillator based on the second control signal.
A glass fiber sizing agent that is an aqueous polyurethane resin comprising an o-sulfobenzimide compound, wherein the o-sulfobenzimide compound is selected from the group consisting of the following compounds No. 1 to No. 5:
A pharmaceutical product in the form of a film, disk, pellet or patch for application to the skin, tissue or a mucous membrane comprising: - between 40% and 65% by mass of at least one active substance; - between 25% and 53% by mass of poly(vinyl) pyrrolidone; and - between 5% and 30% by mass of carboxymethylcellulose or one of its salts; the % by mass being expressed in relation to the total dry mass of said product. - between 40% and 65% by mass of at least one active substance; - between 25% and 53% by mass of poly(vinyl) pyrrolidone; and - between 5% and 30% by mass of carboxymethylcellulose or one of its salts;
A propeller fan comprising: a hub configured to rotate about an axis; and a plurality of blades extending outward in a radial direction of rotation from an outer peripheral surface of the hub, a ring being provided to surround the plurality of blades that are connected to each blade tip which is an outer end of each blade in the radial direction of rotation, when a maximum camber location is a location on a camber line where a distance from a chord line to a camber line in an arc-shaped cross section of each blade about the axis is maximum, and an axial height is a height from a trailing edge, which is a rear edge of each blade in a rotation direction thereof, to the camber line in a direction along the axis, the propeller fan being characterised in that each blade having a first portion which is provided inside in the radial direction of rotation and whose axial height at the maximum camber location is substantially constant, and a second portion which is provided outside in the radial direction of rotation and whose axial height at the maximum camber location increases toward the blade tip. a ring being provided to surround the plurality of blades that are connected to each blade tip which is an outer end of each blade in the radial direction of rotation, when a maximum camber location is a location on a camber line where a distance from a chord line to a camber line in an arc-shaped cross section of each blade about the axis is maximum, and an axial height is a height from a trailing edge, which is a rear edge of each blade in a rotation direction thereof, to the camber line in a direction along the axis, the propeller fan being characterised in that each blade having a first portion which is provided inside in the radial direction of rotation and whose axial height at the maximum camber location is substantially constant, and a second portion which is provided outside in the radial direction of rotation and whose axial height at the maximum camber location increases toward the blade tip.
A method for producing an outer skin part for vehicles, with an integrated solar cell arrangement, having the following steps: - providing a fabric or a fabric composite, - arranging a solar cell arrangement on the fabric, - pressing the solar cell arrangement onto the fabric by means of a mould, - injecting liquid resin into the mould, such that the solar cell arrangement glues to the fabric to form a raw part, - curing the resin, - removing the raw part from the mould, - covering the raw part with a protective layer, so that a smooth, joint-less raw-part surface is yielded, - subsequently processing the edges of the raw part, as a result of which the component is obtained. - providing a fabric or a fabric composite, - arranging a solar cell arrangement on the fabric, - pressing the solar cell arrangement onto the fabric by means of a mould, - injecting liquid resin into the mould, such that the solar cell arrangement glues to the fabric to form a raw part, - curing the resin, - removing the raw part from the mould, - covering the raw part with a protective layer, so that a smooth, joint-less raw-part surface is yielded, - subsequently processing the edges of the raw part, as a result of which the component is obtained.
A compound of formula: wherein: R1 is hydrogen; R2 is R2', wherein R2' is R3 is NH 2, wherein L 2 is CH 2 CH 2, CH=CH or C≡C; A is direct bond, O, OCH 2, OCO, CON, CON O, CON N, CON SO 2, N, N CO, N SO 2 -, N CON, N CSN, N CON N, N COO, N CON SO 2 or N SO 2 N; Y is hydrogen or an optionally substituted straight or branched (C 1 -C 3) alkyl; R5 is hydrogen or an optionally substituted group selected from straight or branched (C 1 -C 8) alkyl, (C 2 -C 8) alkenyl, (C 2 -C 8) alkynyl, (C 3 -C 8) cycloalkyl, heterocyclyl, aryl and heteroaryl; R6 is selected from hydrogen, halogen, trifluoromethyl, (C 1 -C 3) alkyl and (C 1 -C 3) alkoxy; R4 is an optionally substituted group selected from straight or branched (C 1 -C 6) alkyl, (C 2 -C 6) alkenyl, (C 2 -C 6) alkynyl, (C 3 -C 6) cycloalkyl and heterocyclyl; and pharmaceutically acceptable salts. R1 is hydrogen; R2 is R2', wherein R2' is R3 is NH 2, wherein L 2 is CH 2 CH 2, CH=CH or C≡C; A is direct bond, O, OCH 2, OCO, CON, CON O, CON N, CON SO 2, N, N CO, N SO 2 -, N CON, N CSN, N CON N, N COO, N CON SO 2 or N SO 2 N; Y is hydrogen or an optionally substituted straight or branched (C 1 -C 3) alkyl; R5 is hydrogen or an optionally substituted group selected from straight or branched (C 1 -C 8) alkyl, (C 2 -C 8) alkenyl, (C 2 -C 8) alkynyl, (C 3 -C 8) cycloalkyl, heterocyclyl, aryl and heteroaryl; R6 is selected from hydrogen, halogen, trifluoromethyl, (C 1 -C 3) alkyl and (C 1 -C 3) alkoxy; L 2 is CH 2 CH 2, CH=CH or C≡C; A is direct bond, O, OCH 2, OCO, CON, CON O, CON N, CON SO 2, N, N CO, N SO 2 -, N CON, N CSN, N CON N, N COO, N CON SO 2 or N SO 2 N; Y is hydrogen or an optionally substituted straight or branched (C 1 -C 3) alkyl; R5 is hydrogen or an optionally substituted group selected from straight or branched (C 1 -C 8) alkyl, (C 2 -C 8) alkenyl, (C 2 -C 8) alkynyl, (C 3 -C 8) cycloalkyl, heterocyclyl, aryl and heteroaryl; R6 is selected from hydrogen, halogen, trifluoromethyl, (C 1 -C 3) alkyl and (C 1 -C 3) alkoxy; R4 is an optionally substituted group selected from straight or branched (C 1 -C 6) alkyl, (C 2 -C 6) alkenyl, (C 2 -C 6) alkynyl, (C 3 -C 6) cycloalkyl and heterocyclyl; and pharmaceutically acceptable salts.
An internal-circulating heat dissipation system for a stage light, the system comprising a support arm; a light holder; and a circulating heat dissipation system, wherein the light holder is pivotally connected to the support arm through a pivot shaft, the pivot shaft is of a shaft pipe structure, an internal space of the light holder is in communication with an internal space of the support arm through the pivot shaft, the circulating heat dissipation system comprises a cooling medium, a heat dissipation component located inside the support arm, and a power component that promotes the cooling medium to flow in circulation between the light holder and the heat dissipation component through the shaft pipe structure, and the cooling medium is isolated from an external space of the stage light, wherein the light holder is pivotally connected to the support arm through two pivot shafts, both the pivot shafts are of a shaft pipe structure, characterized in that the cooling medium flows into one of the shaft pipe structures and flows out of the other shaft pipe structure. a support arm; a light holder; and a circulating heat dissipation system, wherein the light holder is pivotally connected to the support arm through a pivot shaft, the pivot shaft is of a shaft pipe structure, an internal space of the light holder is in communication with an internal space of the support arm through the pivot shaft, the circulating heat dissipation system comprises a cooling medium, a heat dissipation component located inside the support arm, and a power component that promotes the cooling medium to flow in circulation between the light holder and the heat dissipation component through the shaft pipe structure, and the cooling medium is isolated from an external space of the stage light, wherein the light holder is pivotally connected to the support arm through two pivot shafts, both the pivot shafts are of a shaft pipe structure, characterized in that the cooling medium flows into one of the shaft pipe structures and flows out of the other shaft pipe structure.
An enteric contrast medium formulation which is formulated for oral delivery to a subject contemporaneous with a medical imaging procedure performed on the abdomen of said subject, said formulation comprising: an enteric contrast medium comprising a stable suspension of hollow borosilicate microsphere particles encapsulating gas or partial vacuum, and an aqueous vehicle component, where said aqueous vehicle component is a pharmaceutically acceptable aqueous vehicle comprising xanthan gum as suspension agent maintaining the microsphere particles in suspension, said encapsulated gas or partial vacuum particle is stable at room or body temperature, wherein said particle comprises a shell defining an interior void, said shell formed of a material contributing at least about 30 Hounsfield Units to the CT number of said contrast medium formulation or of a body cavity in which said contrast medium is distributed during said medical imaging procedure. an enteric contrast medium comprising a stable suspension of hollow borosilicate microsphere particles encapsulating gas or partial vacuum, and an aqueous vehicle component, where said aqueous vehicle component is a pharmaceutically acceptable aqueous vehicle comprising xanthan gum as suspension agent maintaining the microsphere particles in suspension, said encapsulated gas or partial vacuum particle is stable at room or body temperature, wherein said particle comprises a shell defining an interior void, said shell formed of a material contributing at least about 30 Hounsfield Units to the CT number of said contrast medium formulation or of a body cavity in which said contrast medium is distributed during said medical imaging procedure.
An electric Al-Zr alloy-plating bath which comprises an aluminum halide; one or at least two kinds of compounds selected from the group consisting of N-alkylpyridinium halides, N-alkylimidazolium halides, N,N'-alkylimidazolium halides, N-alkylpyrazolium halides and N,N'-alkylpyrazolium halides; and a zirconium halide, wherein the bath comprises the aluminum halide and the compound in a molar ratio ranging from 1:1 to 3:1 and wherein the bath further comprises one or at least two kinds of additives selected from the group consisting of an aromatic organic solvent; one or at least two kinds of organic polymers selected from the group consisting of styrenic polymers and aliphatic diene-derived polymers; and one or at least two kinds of brightening agents selected from the group consisting of aliphatic aldehydes, aromatic aldehydes, aromatic ketones, nitrogen atom-containing unsaturated heterocyclic compounds, hydrazide compounds, sulfur atom-containing heterocyclic compounds, aromatic hydrocarbons each carrying a sulfur atom-containing substituent, aromatic carboxylic acids and derivatives thereof, aliphatic carboxylic acids each having a double bond and derivatives thereof, acetylene alcohol compounds and trifluoro-chloro-ethylenic resins; and wherein the amount of zirconium halide is 1 to 50 g/L, the amount of aromatic organic solvent when added is 1 to 50% by volume, the amount of organic polymer when added is 1 to 10 g/L, and the amount of brightening agent when added is 0.001 to 0.1 mole/L.
A fuel and/or lubricant system for an engine, comprising: an engine component (101;201) configured to be in fluid communication with the fuel and/or lubricant; characterised by: an alternating current source electrically connected to the engine component (101;201) to create an electric field of alternating polarity to subject particles within the fuel and/or lubricant to dielectrophoresis as the fuel and/or lubricant passes through the electric field to prevent deposits from forming on the engine component (101;201), wherein the engine component (101;201) is a filter screen (101;201) configured to filter the fuel and/or lubricant to subject particles within the fuel and/or lubricant to dielectrophoresis as the fuel and/or lubricant passes through the filter screen (101;201). an engine component (101;201) configured to be in fluid communication with the fuel and/or lubricant; characterised by: an alternating current source electrically connected to the engine component (101;201) to create an electric field of alternating polarity to subject particles within the fuel and/or lubricant to dielectrophoresis as the fuel and/or lubricant passes through the electric field to prevent deposits from forming on the engine component (101;201), wherein the engine component (101;201) is a filter screen (101;201) configured to filter the fuel and/or lubricant to subject particles within the fuel and/or lubricant to dielectrophoresis as the fuel and/or lubricant passes through the filter screen (101;201).