mhurhangee/patent-ind-claim-en huggingface dataset:
A catalyst layer forming method of forming a catalyst layer on a surface of an electrolyte membrane of a fuel cell, the method comprising the steps of: (a) transporting an electrolyte membrane having a support film attached to a first surface thereof; (b) applying a catalyst ink to part of a second surface of said electrolyte membrane ; (c) heating said electrolyte membrane applied with said catalyst ink at a first temperature to evaporate a solvent contained in said catalyst ink to 30% or less of that before heating; and (d) heating said electrolyte membrane at a second temperature higher than said first temperature and drying said catalyst ink to form a catalyst layer after said step (c), said second temperature being higher than a glass transition temperature of said catalyst layer and being lower than a melting point of said catalyst layer ; wherein said first temperature being equal to or higher than a boiling point of said solvent of said catalyst ink and lower than a glass transition temperature of said electrolyte membrane . (a) transporting an electrolyte membrane having a support film attached to a first surface thereof; (b) applying a catalyst ink to part of a second surface of said electrolyte membrane ; (c) heating said electrolyte membrane applied with said catalyst ink at a first temperature to evaporate a solvent contained in said catalyst ink to 30% or less of that before heating; and (d) heating said electrolyte membrane at a second temperature higher than said first temperature and drying said catalyst ink to form a catalyst layer after said step (c), said second temperature being higher than a glass transition temperature of said catalyst layer and being lower than a melting point of said catalyst layer ; wherein
A receiver , configured to receive and process a radio signal received via a radio channel from a transmitter employing a plurality of antenna ports, determine, based on the received signal, complex precoder coefficients and delays of respective space-delay precoders for each layer and transmit beam at the transmitter so as to achieve a predefined property for a communication over the radio channel , each space-delay precoder comprising a double-stage precoding structure, the double-stage precoding structure including a beamforming matrix that contains PU vectors to form PU spatial beams, U = total number of vectors per polarization, and P = number of polarizations, where P = 1 for co-polarized antenna arrays at the transmitter and P = 2 for dual-polarized antenna arrays at the transmitter , wherein the double-stage precoding structure further includes a space-delay-domain combining coefficient vector or matrix including complex delay-domain combining-coefficients associated with the beams and the delays, feed back to the transmitter the determined delays and the determined complex precoder coefficients, the complex precoder coefficients including the complex delay-domain combining-coefficients, wherein the feedback includes a precoding matrix identifier, PMI, the PMI indicating a number of indices of the vectors associated with the spatial beams, the respective complex delay-domain combining-coefficients, and a number of indices of the delays associated with respective column vectors of a codebook matrix.
A pharmaceutical composition comprising an adenovirus having European Collection of Cell Cultures (ECACC) deposit designation number 13021201, wherein said composition comprises a buffer.
Multiplex analysis method allowing the detection of a signal corresponding to the presence of an analyte to be improved, comprising the following steps: a) providing a solid support comprising at least two compartments, said compartments comprising at least two spots for detection of an analyte, b) bringing a sample to be analysed into contact with the spots of a compartment, c) bringing at least one ligand for detection of an analyte into contact with the spots of said compartment, said ligand for detection of an analyte being coupled to a direct or indirect detection marker, d) when said detection marker is an indirect marker, bringing a reporter of the indirect detection marker coupled to said detection ligand into contact with the spots of said compartment, e) when the reporter used in step d) is coupled to an indirect marker, bringing a reporter of the indirect detection marker coupled to said reporter into contact with the spots of said compartment, f) bringing at least one dye into contact with the spots of said compartment, said dye or dyes being contained in a liquid phase in contact with the spots of said compartment and said at least one dye being tartrazine, and g) detecting a signal corresponding to the presence of an analyte in the region of the spots of said compartment, in the presence of the liquid phase comprising said dye or dyes, said method further comprising one or more washing steps allowing the compounds that are not bound to the spots or to the various compounds bound directly or indirectly to the spots to be removed, no washing step being carried out between step f) and step g). a) providing a solid support comprising at least two compartments, said compartments comprising at least two spots for detection of an analyte, b) bringing a sample to be analysed into contact with the spots of a compartment, c) bringing at least one ligand for detection of an analyte into contact with the spots of said compartment, said ligand for detection of an analyte being coupled to a direct or indirect detection marker, d) when said detection marker is an indirect marker, bringing a reporter of the indirect detection marker coupled to said detection ligand into contact with the spots of said compartment, e) when the reporter used in step d) is coupled to an indirect marker, bringing a reporter of the indirect detection marker coupled to said reporter into contact with the spots of said compartment, f) bringing at least one dye into contact with the spots of said compartment, said dye or dyes being contained in a liquid phase in contact with the spots of said compartment and said at least one dye being tartrazine, and g) detecting a signal corresponding to the presence of an analyte in the region of the spots of said compartment, in the presence of the liquid phase comprising said dye or dyes,
A method of model predictive control of a sheet making system that comprises: assigning a target for one or more manipulated variables MVs ; selecting delays and ramps for the one or more MVs for which targets have been assigned; assigning a target for one or more controlled variable CVs ; selecting delays and ramps rates for the one or more CVs; calculating trajectories for the one or more MVs for which targets have been assigned based on the target and the selected delays and ramps; calculating trajectories for at least one controlled variable based on the target and on the selected delays and ramps; calculating moves for any MVs that do not have pre-assigned targets by minimizing a cost function that penalizes deviations of the CVs from the calculated trajectories and also penalizes MV movements; generating a reference trajectory by allowing a time delay and creation of a ramp from an initial setpoint to a final setpoint at a pre-selected ramp rate, for a grade change, wherein the generated reference trajectory is represented as: Y ref k = P yref z − 1 r k where the P yref (z -1 ) is (ny × Hp) × ny matrix of transfer functions that generates the reference trajectory and H p is the prediction horizon; r(k) represents the current setpoint; and implementing the grade change using the reference trajectory and the calculated MV moves minimizing the cost function so as to transition from the production of the product having a first grade to production of a product having a second grade. assigning a target for one or more manipulated variables MVs ; selecting delays and ramps for the one or more MVs for which targets have been assigned; assigning a target for one or more controlled variable CVs ; selecting delays and ramps rates for the one or more CVs; calculating trajectories for the one or more MVs for which targets have been assigned based on the target and the selected delays and ramps; calculating trajectories for at least one controlled variable based on the target and on the selected delays and ramps; calculating moves for any MVs that do not have pre-assigned targets by minimizing a cost function that penalizes deviations of the CVs from the calculated trajectories and also penalizes MV movements; generating a reference trajectory by allowing a time delay and creation of a ramp from an initial setpoint to a final setpoint at a pre-selected ramp rate, for a grade change, wherein the generated reference trajectory is represented as: Y ref k = P yref z − 1 r k where the P yref (z -1 ) is (ny × Hp) × ny matrix of transfer functions that generates the reference trajectory and H p is the prediction horizon; r(k) represents the current setpoint; and implementing the grade change using the reference trajectory and the calculated MV moves minimizing the cost function so as to transition from the production of the product having a first grade to production of a product having a second grade.
An inductor coil for induction welding of a packaging material having at least one layer of metal foil, the inductor coil being configured to induce an alternating current in the metal foil for inductive heating of the packaging material, the inductor coil comprises a base layer material , characterized in that the inductor coil comprises a top layer material bonded to the base layer material to form an irreversible bonding interface comprising a mixture of the base layer material and the top layer material.
An image intensifier comprising: a vacuum package assembly ; a photocathode sealingly attached to the vacuum package assembly to thereby define a vacuum chamber, the photocathode having a bottom face comprising a photo-emissive surface ; an anode positioned inside the vacuum chamber, the anode having a front surface comprising an electron sensitive surface, wherein the electron sensitive surface is oriented to face the photo-emissive surface ; characterized in that : a resilient spring assembly is attached in part to the vacuum package assembly and in part to a back surface of the anode . a vacuum package assembly ; a photocathode sealingly attached to the vacuum package assembly to thereby define a vacuum chamber, the photocathode having a bottom face comprising a photo-emissive surface ; an anode positioned inside the vacuum chamber, the anode having a front surface comprising an electron sensitive surface, wherein the electron sensitive surface is oriented to face the photo-emissive surface ; characterized in that : a resilient spring assembly is attached in part to the vacuum package assembly and in part to a back surface of the anode .
A composition comprising: A) serine and/or glycine; B) N-acetyl cysteine, cysteine and/or cystine; C) optionally carnitine, deoxycarnitine, gamma-butyrobetaine, 4-trimethylammoniobutanal, 3-hydroxy-N6,N6,N6-trimethyl-L-lysine, N6,N6,N6-trimethyl-L-lysine and/or lysine; and D) nicotinamide riboside, wherein the molar ratio of A) to D) is between 250:1 and 1.5:1 and the molar ratio of A) to B) is between 16:1 and 1:4. A) serine and/or glycine; B) N-acetyl cysteine, cysteine and/or cystine; C) optionally carnitine, deoxycarnitine, gamma-butyrobetaine, 4-trimethylammoniobutanal, 3-hydroxy-N6,N6,N6-trimethyl-L-lysine, N6,N6,N6-trimethyl-L-lysine and/or lysine; and D) nicotinamide riboside, wherein the molar ratio of A) to D) is between 250:1 and 1.5:1 and the molar ratio of A) to B) is between 16:1 and 1:4.
A surface cooler (2; 90; 170) comprising: a base plate (6; 95; 172) having an outer surface ; and at least one fin element (9, 10; 99, 100; 177, 178) extending from the base plate, the at least one fin element having an outer surface portion (18, 22, 24, 39, 42, 45; 109, 113, 117, 134, 138, 142; 188, 192, 196, 209, 213, 217) that is configured and disposed to be in direct contact with a first fluid and an inner surface portion (19, 23, 25, 40, 43, 46; 110, 114, 118, 135, 139, 143; 189, 193, 197, 210, 214, 218) that is configured and disposed to be in direct contact with a second fluid, the at least one fin element defining a primary heat exchange member that is configured and disposed to facilitate an exchange of heat between the first and second fluids, characterised in that the outer surface of the the base plate and the inner surface portion of the at least one fin element are formed to define a fluid channel that is configured to pass the second fluid through an interior of the at least one fin element. a base plate (6; 95; 172) having an outer surface ; and at least one fin element (9, 10; 99, 100; 177, 178) extending from the base plate, the at least one fin element having an outer surface portion (18, 22, 24, 39, 42, 45; 109, 113, 117, 134, 138, 142; 188, 192, 196, 209, 213, 217) that is configured and disposed to be in direct contact with a first fluid and an inner surface portion (19, 23, 25, 40, 43, 46; 110, 114, 118, 135, 139, 143; 189, 193, 197, 210, 214, 218) that is configured and disposed to be in direct contact with a second fluid, the at least one fin element defining a primary heat exchange member that is configured and disposed to facilitate an exchange of heat between the first and second fluids, characterised in that the outer surface of the the base plate and the inner surface portion of the at least one fin element are formed to define a fluid channel that is configured to pass the second fluid through an interior of the at least one fin element.
An impact absorber comprising a three-dimensional structure, the three-dimensional structure including: a closed top surface located at the upper portion of the impact absorber disposed at a position to contact on an object to be packaged; an open bottom located at the lower portion of the impact absorber; a hollow inside; and a recess within an outline of the top surface, characterised in that the upper portion and lower portion are configured such that upon the application of an impact to the impact absorber, the lower portion of the impact absorber deforms to generate a compressed and crushed portion and a buckled portion such that the upper portion sinks to a lower position while maintaining a constant shape. a closed top surface located at the upper portion of the impact absorber disposed at a position to contact on an object to be packaged; an open bottom located at the lower portion of the impact absorber; a hollow inside; and a recess within an outline of the top surface, characterised in that the upper portion and lower portion are configured such that upon the application of an impact to the impact absorber, the lower portion of the impact absorber deforms to generate a compressed and crushed portion and a buckled portion such that the upper portion sinks to a lower position while maintaining a constant shape.
An improved process for preparation of Sugammadex sodium comprising the steps of: (i) reacting gamma-cyclodextrin having the Formula-I, with phosphorous halide of Formula PX 5 or PX 3 in an organic solvent to obtain 6-perdeoxy-6-per-halo gamma cyclodextrin of Formula-II, wherein X is Cl; (ii) reacting the 6-perdeoxy-6-per-halo gamma cyclodextrin of Formula-II with 3-mercapto propionic acid in presence of 30% sodium methoxide in an organic solvent to obtain Sugammadex sodium. (i) reacting gamma-cyclodextrin having the Formula-I, with phosphorous halide of Formula PX 5 or PX 3 in an organic solvent to obtain 6-perdeoxy-6-per-halo gamma cyclodextrin of Formula-II, wherein X is Cl; (ii) reacting the 6-perdeoxy-6-per-halo gamma cyclodextrin of Formula-II with 3-mercapto propionic acid in presence of 30% sodium methoxide in an organic solvent to obtain Sugammadex sodium.
An ophthalmic surgical system , comprising: an intraocular pressure controller; an imaging device configured to acquire a first image of a fundus of an eye ; a hemorrhage detecting unit comprising a processor configured to: receive the first fundus image from the imaging device ; analyze the first fundus image to detect a hemorrhage in the eye ; and in response to detecting the hemorrhage, send a signal to said intraocular pressure controller ; the intraocular pressure controller comprising a processor configured to: receive the signal from the hemorrhage detecting unit ; in response to the received signal, determine if a current intraoperative pressure of the eye is below a predetermined threshold; and in response to determining the current intraoperative pressure of the eye is below the predetermined threshold, generate a signal to increase the intraoperative pressure of the eye . an intraocular pressure controller; an imaging device configured to acquire a first image of a fundus of an eye ; a hemorrhage detecting unit comprising a processor configured to: receive the first fundus image from the imaging device ; analyze the first fundus image to detect a hemorrhage in the eye ; and in response to detecting the hemorrhage, send a signal to said intraocular pressure controller ; receive the first fundus image from the imaging device ; analyze the first fundus image to detect a hemorrhage in the eye ; and in response to detecting the hemorrhage, send a signal to said intraocular pressure controller ; the intraocular pressure controller comprising a processor configured to: receive the signal from the hemorrhage detecting unit ; in response to the received signal, determine if a current intraoperative pressure of the eye is below a predetermined threshold; and in response to determining the current intraoperative pressure of the eye is below the predetermined threshold, generate a signal to increase the intraoperative pressure of the eye . receive the signal from the hemorrhage detecting unit ; in response to the received signal, determine if a current intraoperative pressure of the eye is below a predetermined threshold; and in response to determining the current intraoperative pressure of the eye is below the predetermined threshold, generate a signal to increase the intraoperative pressure of the eye .
An assembly for an aircraft with a gas turbine engine , the assembly comprising: a nacelle comprising an inlet nose lip ; and a thermal management system including a duct , a pressure regulator and a flow restrictor , the thermal management system configured to direct a flow of bleed gas through the duct from the gas turbine engine to the inlet nose lip for heating at least a portion of the inlet nose lip ; and the pressure regulator configured to regulate a pressure of the bleed gas downstream of the pressure regulator ; characterised in that the flow restrictor is configured to selectively restrict the regulated flow of bleed gas through the duct when a temperature of the flow of bleed gas is greater than a threshold temperature (T threshold ), wherein the flow restrictor is a passively actuated flow restrictor and is fluidly coupled between the pressure regulator and the inlet nose lip . a nacelle comprising an inlet nose lip ; and a thermal management system including a duct , a pressure regulator and a flow restrictor , the thermal management system configured to direct a flow of bleed gas through the duct from the gas turbine engine to the inlet nose lip for heating at least a portion of the inlet nose lip ; and the pressure regulator configured to regulate a pressure of the bleed gas downstream of the pressure regulator ; characterised in that the flow restrictor is configured to selectively restrict the regulated flow of bleed gas through the duct when a temperature of the flow of bleed gas is greater than a threshold temperature (T threshold ), wherein the flow restrictor is a passively actuated flow restrictor and is fluidly coupled between the pressure regulator and the inlet nose lip .
Hydraulic boom crane assembly for a working machine with multiple sections movable relative to each other, comprising: a hydraulic tool attachment movably connected to one end of the boom crane , a hydraulic joint with a rotation axis , further comprising at least two joint sections connected to each other, which are movable relative to each other, and which are hydraulically connected to each other, whereas the joint sections are rotatable around the rotation axis , and the joint sections each have at least one hydraulic connector , able to connect to a hydraulic line , so that hydraulic pressure is transferable from one hydraulic connector on one joint section to another hydraulic connector on another joint section , wherein the hydraulic connectors are oriented 90° to the rotation axis wherein the hydraulic joint is mounted between two movable sections of the boom crane or between the boom crane and the tool attachment wherein the hydraulic connectors are movable relative to each other in a plane perpendicular to the rotation axis . a hydraulic tool attachment movably connected to one end of the boom crane , a hydraulic joint with a rotation axis , further comprising at least two joint sections connected to each other, which are movable relative to each other, and which are hydraulically connected to each other, whereas the joint sections are rotatable around the rotation axis , and the joint sections each have at least one hydraulic connector , able to connect to a hydraulic line , so that hydraulic pressure is transferable from one hydraulic connector on one joint section to another hydraulic connector on another joint section , wherein the hydraulic connectors are oriented 90° to the rotation axis wherein the hydraulic joint is mounted between two movable sections of the boom crane or between the boom crane and the tool attachment wherein the hydraulic connectors are movable relative to each other in a plane perpendicular to the rotation axis .
An antenna , comprising: an optically transparent substrate layer having a first surface and an opposing second surface; a radiating element having a first mesh structure and disposed on the first surface of the substrate layer; a ground plane having a second mesh structure formed on the second surface of the substrate layer; at least two feed lines configured to connect the radiating element to an external circuit; and at least two stubs connected to the radiating element, characterized in that the at least two feed lines are substantially parallel or perpendicular to each other, and each of the at least two feed lines has a third mesh structure. an optically transparent substrate layer having a first surface and an opposing second surface; a radiating element having a first mesh structure and disposed on the first surface of the substrate layer; a ground plane having a second mesh structure formed on the second surface of the substrate layer; at least two feed lines configured to connect the radiating element to an external circuit; and at least two stubs connected to the radiating element, characterized in that the at least two feed lines are substantially parallel or perpendicular to each other, and each of the at least two feed lines has a third mesh structure.