mhurhangee/ep-ind-claims huggingface dataset:
An anaerobic curable composition comprising: (a) a (meth)acrylate component; (b) an anaerobic cure-inducing composition; and (c) a cure accelerator embraced by wherein X is CH 2, O, S, NR 4, CR 5 R 6 or C=O; R is hydrogen, alkyl, alkenyl, alkynl, hydroxyalkyl, hydroxyalkenyl, or hydroxyalkynl; R 1 - R 6 are each individually selected from hydrogen, halogen, amino, carboxyl, nitro, alkyl, alkenyl, alkynyl, hydroxyalkyl, hydroxyalkenyl, hydroxyalkynyl, or alkaryl; R 7 is hydrogen or CHR 8 R 9, wherein R 8 and R 9 are each individually selected from hydrogen, halogen, amino, carboxyl, nitro, alkyl, alkenyl, alkynyl, hydroxyalkyl, hydroxyalkenyl, hydroxyalkynyl, or alkaryl; and n is 0 or 1. (a) a (meth)acrylate component; (b) an anaerobic cure-inducing composition; and (c) a cure accelerator embraced by
A cannula for providing respiratory therapy to a patient, the cannula comprising: a first nasal prong having a proximal end attached to a cannula body, and a distal end for insertion into a nare of the patient; and the first nasal prong defining a lumen for a flow of breathing gas from a source of breathing gas to the nare of the patient; wherein the first nasal prong is configured to have a variable geometry such that a cross-sectional area of the lumen at the distal end of the first nasal prong varies with a flow rate of breathing gas, wherein the distal end of the first nasal prong is shaped as a dome having a plurality of slits, and wherein the slits are configured to be closed at no flow through the first nasal prong and the slits are configured to be open at a first flow rate to create an opening at the distal end through which the breathing gas can flow. a first nasal prong having a proximal end attached to a cannula body, and a distal end for insertion into a nare of the patient; and the first nasal prong defining a lumen for a flow of breathing gas from a source of breathing gas to the nare of the patient; wherein the first nasal prong is configured to have a variable geometry such that a cross-sectional area of the lumen at the distal end of the first nasal prong varies with a flow rate of breathing gas, wherein the distal end of the first nasal prong is shaped as a dome having a plurality of slits, and wherein the slits are configured to be closed at no flow through the first nasal prong and the slits are configured to be open at a first flow rate to create an opening at the distal end through which the breathing gas can flow.
A winter tyre tread band comprising: a number of longitudinal and transverse grooves (3, 4) defining a number of blocks, each projecting radially upwards from a base surface of the tread band; and a number of sipes formed in at least some of the blocks, and each of which extends radially inwards of a corresponding block, from a top surface forming the rolling surface of the tread band; wherein, in section, each sipe has a first wave pattern which is constant when the block is sectioned along a first plane defined by the longitudinal axis (x) and transverse axis (y); wherein, along the radial axis (z), the first wave pattern of each sipe shifts along the longitudinal axis (x) in a second wave pattern which is a piecewise linear; and wherein, along the radial axis (z), in addition to shifting along the longitudinal axis (x) in the second wave pattern, the first wave pattern of each sipe also shifts along the transverse axis (y) in a third wave pattern; the tread band being characterized in that the second wave pattern of the sipes comprises a half-wave originating from a top surface of the corresponding block; and two successive whole waves (B, C) following the half-wave. a number of longitudinal and transverse grooves (3, 4) defining a number of blocks, each projecting radially upwards from a base surface of the tread band; and a number of sipes formed in at least some of the blocks, and each of which extends radially inwards of a corresponding block, from a top surface forming the rolling surface of the tread band;
A turbine arrangement comprising a turbo unit, said turbo unit including a turbine shaft supporting a turbine, and a bearing housing enclosing said turbine shaft, said bearing housing comprising means for fastening the turbo unit to a first engine unit, wherein a fluid port of the bearing housing is configured to be in fluid communication with a fluid port of the first engine unit when the turbo unit is attached to the first engine unit, wherein the fluid being cooling water or lubrication oil, characterized in that the turbine arrangement further comprises a valve for opening and closing at least one of the fluid ports (102, 202) wherein said valve is configured to ensure that the fluid port(s) (102, 202) is closed unless the turbo unit is securely attached to the first engine unit.
A promoter ladder comprising at least three promoter polynucleotide sequences selected from the group consisting of SEQ ID NOs: 1 to 8, wherein said promoter ladder comprises a plurality of promoters with incrementally increasing levels of promoter activity.
A composition comprising: a) ( rac)-4-(3-amino-1-(isoquinolin-6-ylamino)-1-oxopropan-2-yl)benzyl 2,4-dimethylbenzoate dimesylate; and b) a prostaglandin selected from the group consisting of: latanoprost; bimatoprost; travoprost; tafluprost; AR-102; cloprostenol isopropyl ester; 13,14-dihydrocloprostenol isopropyl ester; latanoprostene bunod; unoprostone; PGF 1α isopropyl ester; PGF 2α isopropyl ester; PGF 3α isopropyl ester; fluprostenol isopropyl ester; or a pharmaceutically acceptable salt thereof. a) ( rac)-4-(3-amino-1-(isoquinolin-6-ylamino)-1-oxopropan-2-yl)benzyl 2,4-dimethylbenzoate dimesylate; and b) a prostaglandin selected from the group consisting of: latanoprost; bimatoprost; travoprost; tafluprost; AR-102; cloprostenol isopropyl ester; 13,14-dihydrocloprostenol isopropyl ester; latanoprostene bunod; unoprostone; PGF 1α isopropyl ester; PGF 2α isopropyl ester; PGF 3α isopropyl ester; fluprostenol isopropyl ester; or a pharmaceutically acceptable salt thereof.
A tubular ventilation sleeve for a turbomachine distributor, in particular for an aircraft, the sleeve having a generally elongated shape along an axis (A-A) and comprising a tubular wall perforated around this axis, one of the axial ends of the sleeve being open and the other being closed by a bottom wall, said sleeve further comprising support beams when the sleeve is made by additive manufacturing, said support beams extending inside the sleeve, perforations in the tubular wall being provided between the support beams, said sleeve being characterized in that the beams extend between the tubular wall and the bottom wall and have a longitudinal cross-section with a generally triangular shape, two sides of which are respectively connected to the tubular wall and to the bottom wall, and the last side of which is free and extends inside the sleeve.
A process for preparing a 3-((2S,5S)-4-methylene-5-(3-oxopropyl)tetrahydrofuran-2-yl)propanol derivative of the following formula, which comprises the steps of: (i) reacting a compound of the following formula with allyl bromide to obtain a compound of the following formula; (ii) reacting the compound of the following formula with an arylsulfonyl azide to obtain a triazole compound of the following formula; (iii) subjecting the triazole compound of the following formula to denitrification and rearrangement followed by hydrolysis to obtain a tetrahydrofuran compound of the following formula; (iv) subjecting the tetrahydrofuran compound of the following formula to Wittig reaction to obtain a compound of the following formula; (v) subjecting the compound of the following formula to hydroboration followed by oxidation to obtain a compound of the following formula; and (vi) oxidizing a hydroxyl group of the compound of the following formula: wherein, R is an arylsulfonyl group substituted or unsubstituted with C 1 -C 6 alkyl group, and PG represents a protecting group. (i) reacting a compound of the following formula with allyl bromide to obtain a compound of the following formula; (ii) reacting the compound of the following formula with an arylsulfonyl azide to obtain a triazole compound of the following formula; (iii) subjecting the triazole compound of the following formula to denitrification and rearrangement followed by hydrolysis to obtain a tetrahydrofuran compound of the following formula; (iv) subjecting the tetrahydrofuran compound of the following formula to Wittig reaction to obtain a compound of the following formula; (v) subjecting the compound of the following formula to hydroboration followed by oxidation to obtain a compound of the following formula; and (vi) oxidizing a hydroxyl group of the compound of the following formula: wherein, R is an arylsulfonyl group substituted or unsubstituted with C 1 -C 6 alkyl group, and PG represents a protecting group.
A system, comprising: a free-radical ignition system (12,122), comprising: a pre-combustion chamber configured to combust a first fuel-air mixture to generate a flame, a shockwave, and free radicals; injection passages configured to inject the free radicals driven by the shock wave from the pre-combustion chamber toward a combustion chamber; and a quench system configured to extinguish the flame in the pre-combustion chamber or the injection passages, characterized in that the quench system comprises a coolant chamber containing coolant, the injection passages being completely surrounded by the coolant in the coolant chamber and having a helical, spiral or winding shape. a free-radical ignition system (12,122), comprising: a pre-combustion chamber configured to combust a first fuel-air mixture to generate a flame, a shockwave, and free radicals; injection passages configured to inject the free radicals driven by the shock wave from the pre-combustion chamber toward a combustion chamber; and a quench system configured to extinguish the flame in the pre-combustion chamber or the injection passages, a pre-combustion chamber configured to combust a first fuel-air mixture to generate a flame, a shockwave, and free radicals; injection passages configured to inject the free radicals driven by the shock wave from the pre-combustion chamber toward a combustion chamber; and a quench system configured to extinguish the flame in the pre-combustion chamber or the injection passages,
A heater comprising: a tower; a head at the top of the tower, wherein the head comprises a heating element and a heat shield; a head cover coupled to the head, wherein the head cover has a top and a bottom with the heating element positioned therebetween, and wherein the top and bottom of the head cover are open; wherein the head cover at least partially surround the heat shield, and wherein the head cover completely overlaps the heat shield and the heating element in a longitudinal direction of the heater, a base; and a frame that connects the head cover to the heat shield; characterized in that the heater further comprises a tower cover removably attached to the tower and a base cover moveable from a first position substantially encircling the base to a second position vertically overlapping the tower cover, and that the head cover is cylindrical or partially conical thereby comprising a cone shape, wherein an angle of the cone shape with respect to the longitudinal axis of the heater is 0 to 25 degrees. a tower; a head at the top of the tower, wherein the head comprises a heating element and a heat shield; a head cover coupled to the head, wherein the head cover has a top and a bottom with the heating element positioned therebetween, and wherein the top and bottom of the head cover are open; wherein the head cover at least partially surround the heat shield, and wherein the head cover completely overlaps the heat shield and the heating element in a longitudinal direction of the heater, a base; and a frame that connects the head cover to the heat shield; characterized in that the heater further comprises a tower cover removably attached to the tower and a base cover moveable from a first position substantially encircling the base to a second position vertically overlapping the tower cover, and that the head cover is cylindrical or partially conical thereby comprising a cone shape, wherein an angle of the cone shape with respect to the longitudinal axis of the heater is 0 to 25 degrees.
A stapler for endoscopic tissue fastening comprising: a tubular member having and extending between a proximate end and a remote end; a rod at least partially disposed within the tubular member, extending in the same direction as the tubular member, and movable in the direction of extension of the tubular member relative to the tubular member; and a staple having a first segment of a first length, a first hook which is a part of the first segment, a second segment of a second length greater than the first length, a second hook which is part of the second segment, and a connection portion connecting the first segment to the second segment, wherein the staple is configured such that the staple may be removably attached to the rod and may be folded such that at least the first hook and the second hook are disposable within the tubular member with the first segment and the second segment extending from the connection portion such that the distances from the first segment and the second segment to the proximate end are each less than the distance from the connection portion to the proximate end. a tubular member having and extending between a proximate end and a remote end; a rod at least partially disposed within the tubular member, extending in the same direction as the tubular member, and movable in the direction of extension of the tubular member relative to the tubular member; and a staple having a first segment of a first length, a first hook which is a part of the first segment, a second segment of a second length greater than the first length, a second hook which is part of the second segment, and a connection portion connecting the first segment to the second segment, wherein the staple is configured such that the staple may be removably attached to the rod and may be folded such that at least the first hook and the second hook are disposable within the tubular member with the first segment and the second segment extending from the connection portion such that the distances from the first segment and the second segment to the proximate end are each less than the distance from the connection portion to the proximate end.
A knitting method of a knitted fabric for knitting a set-up portion connecting a one side knitted fabric portion, which is mainly knitted on one needle bed, and an other side knitted fabric portion, which is mainly knitted on an other needle bed, using a flat knitting machine including at least one front needle bed and one back needle bed, in which at least one of the front and back needle beds (FB, BB) can be racked in a transverse direction and stitches can be transferred between the front and back needle beds (FB, BB); assuming a direction in which the set-up portion is sequentially formed in a longitudinal direction of the needle beds (FB, BB) is a forming direction and an opposite direction is a starting end direction, the knitting method characterized by forming the set-up portion by repeating: a step 0 of forming a one side stitch (9, 11) on one needle bed (FB, BB) and forming an other side stitch (10, 12) on an other needle bed (BB, FB); a step α of transferring the one side stitch held on one needle bed (FB, BB) to a knitting needle (1 to 8) in the forming direction, and forming a new one side stitch following in a wale direction of the moved one side stitch; a step β of forming a one side widening stitch on an empty needle (1 to 8) on the starting end direction side of the new one side stitch formed in the step α; a step γ of transferring the other side stitch held on the other needle bed (BB, FB) to a knitting needle (1 to 8) in the forming direction and forming a new other side stitch following in a wale direction of the moved other side stitch after the step β; and a step δ of forming an other side widening stitch on an empty needle (1 to 8) on the starting end direction side of the new other side stitch formed in the step γ, whereby the steps α to δ are performed consecutively with a same yarn feeder. a step 0 of forming a one side stitch (9, 11) on one needle bed (FB, BB) and forming an other side stitch (10, 12) on an other needle bed (BB, FB); a step α of transferring the one side stitch held on one needle bed (FB, BB) to a knitting needle (1 to 8) in the forming direction, and forming a new one side stitch following in a wale direction of the moved one side stitch; a step β of forming a one side widening stitch on an empty needle (1 to 8) on the starting end direction side of the new one side stitch formed in the step α; a step γ of transferring the other side stitch held on the other needle bed (BB, FB) to a knitting needle (1 to 8) in the forming direction and forming a new other side stitch following in a wale direction of the moved other side stitch after the step β; and a step δ of forming an other side widening stitch on an empty needle (1 to 8) on the starting end direction side of the new other side stitch formed in the step γ,
A composition of matter comprising a first IPN or semi-IPN comprising a hydrophobic thermoset or thermoplastic polymer T and a non-ionic polymer P and a second IPN or semi-IPN comprising the same said hydrophobic thermoset or thermoplastic polymer T and a hydrophilic interpenetrating polymer S, the composition including at least two concentration gradients, wherein the non-ionic polymer P forms a first concentration gradient from a first portion of the composition to a second portion of the composition and the hydrophilic interpenetrating polymer S forms a second concentration gradient from a third portion of the composition to a fourth portion of the composition.
A method of treating the skin comprising a glycosaminoglycan-containing mixture of substances for use in a method of dermatological treatment of the skin, characterized in that astragaloside IV is included, wherein the glycosaminoglycan has substantially cross-chain hyaluron chains, wherein the glycosaminoglycan has a concentration of from 0.2% to 5% by weight and the astragaloside IV has a concentration of from 0.1% to 5% by weight. astragaloside IV is included, wherein the glycosaminoglycan has substantially cross-chain hyaluron chains, wherein the glycosaminoglycan has a concentration of from 0.2% to 5% by weight and the astragaloside IV has a concentration of from 0.1% to 5% by weight.
A pressure transducer comprising: a Bourdon tube mechanism of amorphous quartz having a tube with a closed end and an open end, the open end of the tube being configured to be placed in fluid communication with a fluid and to receive the fluid into the tube, the closed end of the tube being configured to flex in response to a change in pressure in the tube; a support structure of amorphous quartz molecularly bonded to the open end of the tube of the Bourdon tube mechanism without an adhesive material; and a crystalline quartz sensor coupled between the closed end of the tube and the support structure and configured to detect a force associated with the flexing of the tube, wherein the crystalline quartz sensor is pre-tensioned or pre-compressed such that the crystalline quartz sensor is pre-stressed or pre-compressed at atmospheric pressure and remains in tension or compression for the entire operating range of the pressure transducer, wherein the crystalline quartz sensor has a longitudinal axis that is parallel with a tangent of a curving motion of the closed end of the Bourdon tube. a Bourdon tube mechanism of amorphous quartz having a tube with a closed end and an open end, the open end of the tube being configured to be placed in fluid communication with a fluid and to receive the fluid into the tube, the closed end of the tube being configured to flex in response to a change in pressure in the tube; a support structure of amorphous quartz molecularly bonded to the open end of the tube of the Bourdon tube mechanism without an adhesive material; and a crystalline quartz sensor coupled between the closed end of the tube and the support structure and configured to detect a force associated with the flexing of the tube, wherein the crystalline quartz sensor is pre-tensioned or pre-compressed such that the crystalline quartz sensor is pre-stressed or pre-compressed at atmospheric pressure and remains in tension or compression for the entire operating range of the pressure transducer, wherein the crystalline quartz sensor has a longitudinal axis that is parallel with a tangent of a curving motion of the closed end of the Bourdon tube.
A cooling device for cooling a charger for charging a battery with use of power supply received from a power source, comprising: a compressor for circulating a cooling agent; a condenser for condensing said cooling agent; a decompressor for decompressing said cooling agent condensed by said condenser; an evaporator for evaporating said cooling agent decompressed by said decompressor; characterized by further comprising: a cooling portion for cooling said charger with use of said cooling agent flowing from said condenser, said cooling portion being provided on a path of the said cooling agent flowing from said condenser to said decompressor; and a communication passage for allowing communication between a path of said cooling agent flowing from said cooling portion to said decompressor and a path of said cooling agent flowing from said compressor to said condenser, said cooling portion being arranged below said condenser in the vertical direction perpendicular to ground. a compressor for circulating a cooling agent; a condenser for condensing said cooling agent; a decompressor for decompressing said cooling agent condensed by said condenser; an evaporator for evaporating said cooling agent decompressed by said decompressor; characterized by further comprising: a cooling portion for cooling said charger with use of said cooling agent flowing from said condenser, said cooling portion being provided on a path of the said cooling agent flowing from said condenser to said decompressor; and a communication passage for allowing communication between a path of said cooling agent flowing from said cooling portion to said decompressor and a path of said cooling agent flowing from said compressor to said condenser, said cooling portion being arranged below said condenser in the vertical direction perpendicular to ground. a cooling portion for cooling said charger with use of said cooling agent flowing from said condenser, said cooling portion being provided on a path of the said cooling agent flowing from said condenser to said decompressor; and a communication passage for allowing communication between a path of said cooling agent flowing from said cooling portion to said decompressor and a path of said cooling agent flowing from said compressor to said condenser, said cooling portion being arranged below said condenser in the vertical direction perpendicular to ground.