mhurhangee/ep-ind-claims huggingface dataset:
A landing gear arrangement comprising: a landing gear component: a cylindrical composite member formed by: a first composite layer having an outer surface and a cylindrical geometry; and a second composite layer wherein the first composite layer and second composite layer comprise the landing gear component; a metallic load transfer member comprising an inner surface having a constant diameter, the metallic load transfer member perimetrically surrounding at least a portion of the first composite layer, wherein the constant diameter and a diameter of the outer surface are substantially equal; the second composite layer perimetrically surrounding at least a portion of the metallic load transfer member; characterized in that the metallic load transfer member comprises a metallic connecting tab extending away from the metallic load transfer member in at least one of a radial, axial, and tangential direction, and extending through the second composite layer, and in that at least a portion of the metallic connecting tab is located further radially outward than the second composite layer. a cylindrical composite member formed by: a first composite layer having an outer surface and a cylindrical geometry; and a second composite layer a first composite layer having an outer surface and a cylindrical geometry; and a second composite layer wherein the first composite layer and second composite layer comprise the landing gear component; a metallic load transfer member comprising an inner surface having a constant diameter, the metallic load transfer member perimetrically surrounding at least a portion of the first composite layer, wherein the constant diameter and a diameter of the outer surface are substantially equal; the second composite layer perimetrically surrounding at least a portion of the metallic load transfer member; characterized in that the metallic load transfer member comprises a metallic connecting tab extending away from the metallic load transfer member in at least one of a radial, axial, and tangential direction, and extending through the second composite layer, and in that at least a portion of the metallic connecting tab is located further radially outward than the second composite layer.
Time arbitration circuit comprising: • a comparator comprising at least first and second inputs and configured to provide at least a first data item relative to a synchronization status of signals (C1, C2, Ci) present on the first and second inputs, • a clock signal generator connected to an output terminal of the time arbitration circuit and delivering an output clock signal (C O), • a control circuit configured to enable or disable delivery of the output clock signal (C O) on the output terminal according to the at least a first data item from the comparator and/or to deliver data relative to the synchronization status according to the at least a first data item, • the first input of the comparator is connected to a first input terminal of the time arbitration circuit designed to be connected to a first source delivering a first clock signal, • the second input of the comparator is designed to be connected to a second source (S2, G) delivering a second clock signal (C2, Ci), time arbitration circuit characterized in that the comparator or the control circuit is configured to calculate variation of a time difference between the signals (C1, C2, Ci) present on the first and second inputs and/or the time difference variation rate on a predetermined time period, the at least a first data item being obtained by means of the variation of the time difference and/or the time difference variation rate. • a comparator comprising at least first and second inputs and configured to provide at least a first data item relative to a synchronization status of signals (C1, C2, Ci) present on the first and second inputs, • a clock signal generator connected to an output terminal of the time arbitration circuit and delivering an output clock signal (C O), • a control circuit configured to enable or disable delivery of the output clock signal (C O) on the output terminal according to the at least a first data item from the comparator and/or to deliver data relative to the synchronization status according to the at least a first data item, • the first input of the comparator is connected to a first input terminal of the time arbitration circuit designed to be connected to a first source delivering a first clock signal, • the second input of the comparator is designed to be connected
A method of performing image cytometry, comprising: a. obtaining a sample containing rare cells from blood or other fluids; b. labeling said rare cells with a fluorophore; c. manipulating said rare cells towards a collection surface; d. illuminating said collected rare cells with a laser having a beam homogenizer with a rotating diffuser and microlens array, wherein said illuminating is homogenous across said rare cells; and e. imaging said rare cells by fluorescent microscopy wherein said fluorescent microscopy produces a homogeneous fluorescent image. a. obtaining a sample containing rare cells from blood or other fluids; b. labeling said rare cells with a fluorophore; c. manipulating said rare cells towards a collection surface; d. illuminating said collected rare cells with a laser having a beam homogenizer with a rotating diffuser and microlens array, wherein said illuminating is homogenous across said rare cells; and e. imaging said rare cells by fluorescent microscopy wherein said fluorescent microscopy produces a homogeneous fluorescent image.
A catalysed ion-conducting membrane comprising an ion-conducting membrane, an electrocatalyst layer having two opposing faces, and a layer A, wherein: the layer A and the ion-conducting membrane are adjacent to opposite faces of the electrocatalyst layer; the layer A comprises an ion-conducting material I A and a carbon containing material C A; the electrocatalyst layer comprises an ion-conducting material I B and an electrocatalyst; wherein the layer A does not comprise an electrocatalyst; and the layer A has a permeability, k 1, of greater than 20 nm 2; and the electrocatalyst layer has a permeability, k 2, of no more than 20 nm 2; and the weight ratio of ion-conducting material I A to carbon containing material C A in layer A is in the range of and including 2:1 to 1:2; wherein permeability is calculated from mercury intrusion porosimetry measurements in accordance with the procedure set out in the examples section in which mercury pressure is increased from ~3.0 to 60,000 psia during a measurement, and the porosity at <1 micron and >3 nm pore diameter is used for calculating porosity characteristics. the layer A and the ion-conducting membrane are adjacent to opposite faces of the electrocatalyst layer; the layer A comprises an ion-conducting material I A and a carbon containing material C A; the electrocatalyst layer comprises an ion-conducting material I B and an electrocatalyst; wherein the layer A does not comprise an electrocatalyst; and the layer A has a permeability, k 1, of greater than 20 nm 2; and the electrocatalyst layer has a permeability, k 2, of no more than 20 nm 2; and the weight ratio of ion-conducting material I A to carbon containing material C A in layer A is in the range of and including 2:1 to 1:2; wherein permeability is calculated from mercury intrusion porosimetry measurements in accordance with the procedure set out in the examples section in which mercury pressure is increased from ~3.0 to 60,000 psia during a measurement, and the porosity at <1 micron and >3 nm pore diameter is used for calculating porosity characteristics.
A method comprising: providing a three-dimensional printer (100, 200) having an extruder with a first input port, a second input port, an extrusion port, and a chamber coupling the first input port, the second input port, and the extrusion port in fluid communication; driving a first build material through the first input port until the first build material extrudes through the extrusion port; withdrawing the first build material through the first input port of the extruder a predetermined amount, wherein the predetermined amount is at least enough to move a material transition region out of the chamber and into the first input port, the material transition region being a region of mixing between the first build material and a second build material; and driving the second build material through the second input port until the second build material extrudes through the extrusion port. providing a three-dimensional printer (100, 200) having an extruder with a first input port, a second input port, an extrusion port, and a chamber coupling the first input port, the second input port, and the extrusion port in fluid communication; driving a first build material through the first input port until the first build material extrudes through the extrusion port; withdrawing the first build material through the first input port of the extruder a predetermined amount, wherein the predetermined amount is at least enough to move a material transition region out of the chamber and into the first input port, the material transition region being a region of mixing between the first build material and a second build material; and driving the second build material through the second input port until the second build material extrudes through the extrusion port.
A method of managing resource usage by multiple entities (106, 108; 406, 408, 416) in a computer system, wherein each entity (106, 108; 406, 408, 416) is configured to consume one or more resources (110;410), the method comprising: continuously determining whether a resource (110; 410) has reached a critical level in which an available resource amount falls below a predetermined level or a usage amount of the resource rises above a predetermined level: and when it is determined that a resource (110; 410) has reached a critical level: selecting a first entity (106, 108; 406, 416) from said multiple entities based on one or more criteria, wherein the one or more criteria include a priority value for each entity (106, 108; 406, 408, 416) and whether the selected resource entity has a lower priority than other entities (106, 108; 406, 408, 416) that are not selected, and requesting the selected entity (106, 108; 406, 408, 416) to change its resource consumption state to a more restrictive state in which the selected entity consumes or is likely to consume less resource. continuously determining whether a resource (110; 410) has reached a critical level in which an available resource amount falls below a predetermined level or a usage amount of the resource rises above a predetermined level: and when it is determined that a resource (110; 410) has reached a critical level: selecting a first entity (106, 108; 406, 416) from said multiple entities based on one or more criteria, wherein the one or more criteria include a priority value for each entity (106, 108; 406, 408, 416) and whether the selected resource entity has a lower priority than other entities (106, 108; 406, 408, 416) that are not selected, and requesting the selected entity (106, 108; 406, 408, 416) to change its resource consumption state to a more restrictive state in which the selected entity consumes or is likely to consume less resource. selecting a first entity (106, 108; 406, 416) from said multiple entities based on one or more criteria, wherein the one or more criteria include a priority value for each entity (106, 108; 406, 408, 416) and whether the selected resource entity has a lower priority than other entities (106, 108; 406, 408, 416) that are not selected, and requesting the selected entity (106, 108; 406, 408, 416) to change its resource consumption state to a more restrictive state in which the selected entity consumes or is likely to consume less resource.
A turbine engine comprising: a turbine section with at least one turbine stage (100, 100a, 100b) having a stationary vane assembly and a rotating blade assembly, where combustion gases flow through the at least one turbine stage (100, 100a, 100b) in a fore to aft direction; wherein the stationary vane assembly terminates in a hanger, the hanger including at least one rim; an outer casing surrounding the at least one turbine stage (100, 100a, 100b); an interface between a portion of the outer casing and a portion of the stationary vane assembly including a fore interface defining a leak flow path; and a seal (132, 138) coupled to one of the stationary vane assembly and the outer casing to retard combustion gases in the leak flow path; wherein the seal (132, 138) is a fore seal at the fore interface, wherein said fore seal abuts at least a portion of the hanger at the at least one rim and the outer casing, characterised in said fore seal comprising a plurality of discrete spacers extending along the fore seal to form an annular set of discrete spacers, the discrete spacers defining an insulating air gap between the outer casing and the fore seal, the insulating air gap providing an insulation barrier to minimize heat transfer by convection between the outer casing and the hot combustion airflow in the turbine housing. a turbine section with at least one turbine stage (100, 100a, 100b) having a stationary vane assembly and a rotating blade assembly, where combustion gases flow through the at least one turbine stage (100, 100a, 100b) in a fore to aft direction; wherein the stationary vane assembly terminates in a hanger, the hanger including at least one rim; an outer casing surrounding the at least one turbine stage (100, 100a, 100b); an interface between a portion of the outer casing and a portion of the stationary vane assembly including a fore interface defining a leak flow path; and a seal (132, 138) coupled to one of the stationary vane assembly and the outer casing to retard combustion gases in the leak flow path; wherein the seal (132, 138) is a fore seal at the fore interface, wherein said fore seal abuts at least a portion of the hanger at the at least one rim and the outer casing, characterised in said fore seal comprising a plurality of discrete spacers extending along the fore seal to form an annular set of discrete spacers, the discrete spacers defining an insulating air gap between the outer casing and the fore seal, the insulating air gap providing an insulation barrier to minimize heat transfer by convection between the outer casing and the hot combustion airflow in the turbine housing.
Cosmetic composition comprising, in a physiologically acceptable medium: - at least water, preferably at least 5% by weight of water; - at least alkylcellulose, the alkyl residue of which comprises between 1 and 6 carbon atoms, preferably between 2 and 6 carbon atoms and preferably between 2 and 3 carbon atoms, preferably ethylcellulose; - at least one first hydrocarbon-based non-volatile oil, chosen from: - C 10 -C 26 alcohols, preferably monoalcohols; - optionally hydroxylated monoesters, diesters or triesters of an optionally hydroxylated C 2 -C 8 monocarboxylic or polycarboxylic acid and of a C 2 -C 8 alcohol; - esters of a C 2 -C 8 polyol and of one or more C 2 -C 8 carboxylic acids; - at least one second non-volatile oil chosen from silicone oils and/or fluoro oils or hydrocarbon-based oils other than the said first oil; - at least one wax; - at least one hydrophilic gelling agent chosen from nonionic associative polymers of polyurethane type, preferably polyoxyethylenated; - preferably at least one surfactant, preferably nonionic. - at least water, preferably at least 5% by weight of water; - at least alkylcellulose, the alkyl residue of which comprises between 1 and 6 carbon atoms, preferably between 2 and 6 carbon atoms and preferably between 2 and 3 carbon atoms, preferably ethylcellulose; - at least one first hydrocarbon-based non-volatile oil, chosen from: - C 10 -C 26 alcohols, preferably monoalcohols; - optionally hydroxylated monoesters, diesters or triesters of an optionally hydroxylated C 2 -C 8 monocarboxylic or polycarboxylic acid and of a C 2 -C 8 alcohol; - esters of a C 2 -C 8 polyol and of one or more C 2 -C 8 carboxylic acids; - C 10 -C 26 alcohols, preferably monoalcohols; - optionally hydroxylated monoesters, diesters or triesters of an optionally hydroxylated C 2 -C 8 monocarboxylic or polycarboxylic acid and of a C 2 -C 8 alcohol; - esters of a C 2 -C 8 polyol and of one or more C 2 -C 8 carboxylic acids; - at least one second non-volatile oil chosen from silicone oils and/or fluoro oils or hydrocarbon-based oils other than the said first oil; - at least one wax; - at least one hydrophilic gelling agent chosen from nonionic associative polymers of polyurethane type, preferably polyoxyethylenated; - preferably at least one surfactant, preferably nonionic.
Method for vulcanizing a tyre, comprising at least the following steps: - introducing the tyre into a vulcanizing chamber and carrying out a main vulcanizing process by treating the tyre with pressure and heat, whereby the tyre is brought into its final form and a curing of the material of the tyre takes place, - carrying out a temperature-controlling process after completion of the main vulcanizing process, wherein for this a temperature-controlling element is used for acting thermally on the tyre in order to post-cure the tyre, wherein - the temperature-controlling element is placed against the tyre, at least in certain regions, and the temperature of the tyre is specifically influenced in certain regions by the temperature-controlling element for the specific post-curing of the tyre, characterized in that the temperature-controlling element acts thermally on the tyre with multiple temperature-controlling segments (12.i) and adjacent temperature-controlling segments (12.i) influence the temperature of the tyre to differing degrees, wherein the multiple temperature-controlling segments (12.i) adjoin one another in the axial direction with respect to the tyre and can act on the temperature of the tyre independently of one another. - introducing the tyre into a vulcanizing chamber and carrying out a main vulcanizing process by treating the tyre with pressure and heat, whereby the tyre is brought into its final form and a curing of the material of the tyre takes place, - carrying out a temperature-controlling process after completion of the main vulcanizing process, wherein for this a temperature-controlling element is used for acting thermally on the tyre in order to post-cure the tyre, wherein - the temperature-controlling element is placed against the tyre, at least in certain regions, and the temperature of the tyre is specifically influenced in certain regions by the temperature-controlling element for the specific post-curing of the tyre, characterized in that
Monolithic membrane made of glass, - in particular designed as - a vertical membrane suspended on one or both sides and/or as - a micromechanical bending structure suspended on one or both sides, in particular designed as a deflectable spring beam suspended on one or both sides, wherein - the membrane has been released from a glass substrate by laser-induced modification of the glass substrate and subsequent wet-chemical etching, and - the membrane is designed as a vertical membrane, so that a plane of the vertical membrane extends transversely to a substrate plane of the glass substrate, characterized in that - at least one surface of the vertical membrane is bounded by a blind hole which was produced by means of laser-induced modification of the glass substrate and subsequent wet-chemical etching. - in particular designed as - a vertical membrane suspended on one or both sides and/or as - a micromechanical bending structure suspended on one or both sides, in particular designed as a deflectable spring beam suspended on one or both sides, wherein - a vertical membrane suspended on one or both sides and/or as - a micromechanical bending structure suspended on one or both sides, in particular designed as a deflectable spring beam suspended on one or both sides, wherein - the membrane has been released from a glass substrate by laser-induced modification of the glass substrate and subsequent wet-chemical etching, and - the membrane is designed as a vertical membrane, so that a plane of the vertical membrane extends transversely to a substrate plane of the glass substrate, - at least one surface of the vertical membrane is bounded by a blind hole which was produced by means of laser-induced modification of the glass substrate and subsequent wet-chemical etching.
A method of treating a formation, comprising: emplacing a gel into a region of the formation; emplacing an oxidizing breaker into the region of the formation; and allowing sufficient time for the oxidizing breaker to degrade the gel; wherein the gel comprises at least one of a lignin, a lignosulfonate, a tannin, a tannic acid, a modified lignin, a modified lignosulfonate, a modified tannin, a modified tannic acid, and combinations thereof crosslinked with a crosslinking agent, or at least one of a polyurea or polyurethane gel; and wherein the crosslinking agent comprises at least one of ethylene glycol diglycidyl ether, propylene glycol diglycidyl ether, butylene glycol diglycidyl ether, trimethylolpropane triglycidyl ether, sorbitol polyglycidyl ether, diglycidyl ether of neopentyl glycol, epoxidized 1,6-hexanediol, aziridine derivatives, carbodiimides, blocked isocyanates, epoxy functionalized polyalkalene glycols, an oxidized starch, a polymeric dialdehyde, an aldehyde adduct, a tetra methoxy propane, a hydrolized acetal, and combinations thereof. emplacing a gel into a region of the formation; emplacing an oxidizing breaker into the region of the formation; and allowing sufficient time for the oxidizing breaker to degrade the gel; wherein the gel comprises at least one of a lignin, a lignosulfonate, a tannin, a tannic acid, a modified lignin, a modified lignosulfonate, a modified tannin, a modified tannic acid, and combinations thereof crosslinked with a crosslinking agent, or at least one of a polyurea or polyurethane gel; and wherein the crosslinking agent comprises at least one of ethylene glycol diglycidyl ether, propylene glycol diglycidyl ether, butylene glycol diglycidyl ether, trimethylolpropane triglycidyl ether, sorbitol polyglycidyl ether, diglycidyl ether of neopentyl glycol, epoxidized 1,6-hexanediol, aziridine derivatives, carbodiimides, blocked isocyanates, epoxy functionalized polyalkalene glycols, an oxidized starch, a polymeric dialdehyde, an aldehyde adduct, a tetra methoxy propane, a hydrolized acetal, and combinations thereof.
An espresso machine comprising: a pump; a pump power modification module (500, 550) operatively associated with the pump, wherein the power modification module (500, 550) is configured for providing preinfusion; characterized in that the power modification module (500, 550) enables pressure profiling during an espresso production cycle, the pressure profile being configurable via a user interface, wherein the pressure profiling takes the form of a power-time profile indicative of electrical power delivered to the pump. a pump; a pump power modification module (500, 550) operatively associated with the pump, wherein the power modification module (500, 550) is configured for providing preinfusion; characterized in that the power modification module (500, 550) enables pressure profiling during an espresso production cycle, the pressure profile being configurable via a user interface, wherein the pressure profiling takes the form of a power-time profile indicative of electrical power delivered to the pump.
Stamping device with at least one oscillating machine part, which has at least one piezoelectric sensor, characterized in that the piezoelectric sensor is electrically connected to at least one first coil attached to the oscillating machine part and inductively coupled to at least one second stationary coil.