mhurhangee/patent-ind-claim-en huggingface dataset:
A modular fuselage for an unmanned aerial vehicle, UAV, comprising: a battery module for housing a battery to power the UAV; an avionics module that houses flight control circuitry of the UAV; and a mission payload module that houses equipment associated with a mission of the UAV, wherein the battery module, the avionics module, and the mission payload module are detachable from each other and mechanically securable to each other to contiguously form at least a portion of the modular fuselage of the UAV. a battery module for housing a battery to power the UAV; an avionics module that houses flight control circuitry of the UAV; and a mission payload module that houses equipment associated with a mission of the UAV, wherein the battery module, the avionics module, and the mission payload module are detachable from each other and mechanically securable to each other to contiguously form at least a portion of the modular fuselage of the UAV.
System for the distribution of wireless signals in telecommunication networks, configured for providing a baseband unit functionally integrated with a distributed antenna system, comprising: - a central server provided with a plurality of baseband units , wherein said baseband units are realized via a BBU pooling software configured for the virtualization of the baseband units ; characterized in that it comprises: - a point of interface network connected with said central server via an interface link and provided with a plurality of point of interface units , wherein said interface network is connected with a distributed antenna system and configured to distribute the signal received from said plurality of baseband units in areas with high density of users. - a central server provided with a plurality of baseband units , wherein said baseband units are realized via a BBU pooling software configured for the virtualization of the baseband units ; - a point of interface network connected with said central server via an interface link and provided with a plurality of point of interface units , wherein said interface network is connected with a distributed antenna system and configured to distribute the signal received from said plurality of baseband units in areas with high density of users.
An engine system (100; 100A, 100B) of an aircraft , the engine system comprising: an energy storage system (16; 218); a gas turbine engine comprising a low spool , a high spool , a low-spool generator operably coupled to the low spool, and a high-spool electric motor operably coupled to the high spool; and a controller configured to: detect a braking condition of the aircraft ; determine a storage capacity state of the energy storage system (16; 218); transfer power from the low-spool generator to the energy storage system based on the storage capacity state of the energy storage system; transfer power to the high spool through the high-spool electric motor to support combustion in the gas turbine engine while a rotational speed of the low spool is reduced responsive to the low-spool generator extracting energy from the low spool; and split energy output of the low-spool generator between the energy storage system (16; 218) and the high-spool electric motor based on the storage capacity state and a target speed of the high spool , wherein the storage capacity state indicates a capacity to receive a power surge from the low-spool generator. an energy storage system (16; 218); a gas turbine engine comprising a low spool , a high spool , a low-spool generator operably coupled to the low spool, and a high-spool electric motor operably coupled to the high spool; and a controller configured to: detect a braking condition of the aircraft ; determine a storage capacity state of the energy storage system (16; 218); transfer power from the low-spool generator to the energy storage system based on the storage capacity state of the energy storage system; transfer power to the high spool through the high-spool electric motor to support combustion in the gas turbine engine while a rotational speed of the low spool is reduced responsive to the low-spool generator extracting energy from the low spool; and split energy output of the low-spool generator between the energy storage system (16; 218) and the high-spool electric motor based on the storage capacity state and a target speed of the high spool , wherein the storage capacity state indicates a capacity to receive a power surge from the low-spool generator. detect a braking condition of the aircraft ; determine a storage capacity state of the energy storage system (16; 218); transfer power from the low-spool generator to the energy storage system based on the storage capacity state of the energy storage system; transfer power to the high spool through the high-spool electric motor to support combustion in the gas turbine engine while a rotational speed of the low spool is reduced responsive to the low-spool generator extracting energy from the low spool; and split energy output of the low-spool generator between the energy storage system (16; 218) and the high-spool electric motor based on the storage capacity state and a target speed of the high spool , wherein the storage capacity state indicates a capacity to receive a power surge from the low-spool generator.
A method in which a flowable agent for lightening and dyeing human hair is prepared by mixing and applied to human hair, the agent is left in the hair for a period of from 2 to 60 min, and then the hair is rinsed with water and/or a commercially available shampoo, characterized in that the agent is prepared by mixing i. at least one oxidizing agent preparation (A) containing at least one oxidizing agent in a liquid cosmetic carrier, ii. at least one bleaching powder (B) containing at least one bleach booster and at least one solid alkalizing agent, and iii. at least one dye preparation (C) containing, in a liquid cosmetic carrier, at least one halogenated direct dye, selected from the group consisting of tetrabromophenol blue and Acid Red 92, and additionally at least one complexing agent, at a pH of less 10, characterized in that the total amount of direct dyes is 0.0001 to 2.5 wt.%, based on the total weight of the ready-to-use agent, the terms "flowable," "solid" and "liquid" relating to a temperature in the range between 15 and 40 °C. i. at least one oxidizing agent preparation (A) containing at least one oxidizing agent in a liquid cosmetic carrier, ii. at least one bleaching powder (B) containing at least one bleach booster and at least one solid alkalizing agent, and iii. at least one dye preparation (C) containing, in a liquid cosmetic carrier, at least one halogenated direct dye, selected from the group consisting of tetrabromophenol blue and Acid Red 92, and additionally at least one complexing agent, at a pH of less 10, characterized in that the total amount of direct dyes is 0.0001 to 2.5 wt.%, based on the total weight of the ready-to-use agent, the terms "flowable," "solid" and "liquid" relating to a temperature in the range between 15 and 40 °C.
A sensor for transcutaneously measuring the partial pressure of oxygen at a measuring site of a patient, comprising: - a heating element, for heating a skin of the patient at the measuring site, - a control unit for controlling the temperature of the heating element, processing of the sensor signals, and controlling communication between the sensor and a monitor, - said control unit comprising an analogue to digital converter, the control unit further being adapted to control the heating element to cycle the temperature of the skin at the measuring site between a lower and a higher temperature by; - adjust and maintain, by the controller and the heating element, the measuring site at a temperature close to body core temperature in a first time interval so that the skin temperature at the measuring site is maintained at the lower temperature, which is between 35°C - 42°C, and - increase and maintain, by the controller and the heating element, the temperature at the measuring site in a second time interval so that the skin temperature at the measuring site is maintained at the higher temperature, which is at least 43 °C, wherein the controller and the heating element are configured so that the first time interval is longer than the second time interval, and the sequence of first and second time intervals is repeated for performing the cycling of the temperature of the skin at the measuring site; wherein the controller and the heating element are configured so that in the second time interval, the increasing and maintaining of the temperature at the measuring site comprises at least 10 minutes of heating up the skin followed by 5 minutes of measuring the oxygen partial pressure; wherein the 5 minutes of measuring the oxygen partial pressure are within the second time interval when the skin temperature is maintained at the higher temperature. - a heating element, for heating a skin of the patient at the measuring site, - a control unit for controlling the temperature of the heating element, processing of the sensor signals, and controlling communication between the sensor and a monitor, - said control unit comprising an analogue to digital converter, - adjust and maintain, by the controller and the heating element, the measuring site at a temperature close to body core temperature in a first time interval so that the skin temperature at the measuring site is maintained at the lower temperature, which is between 35°C - 42°C, and - increase and maintain, by the controller and the heating element, the temperature at the measuring site in a second time interval so that the skin temperature at the measuring site is maintained at the higher temperature, which is at least 43 °C,
A method performed by a transmitting device for handling communication in a wireless communications network, wherein the transmitting device comprises at least two radio link control, RLC, entities and is configured with a split bearer to a receiving device , the method comprising: - identifying that a last transmitted protocol data unit, PDU, of one of the at least two RLC entities, is lacking a poll indicator requesting a status of one or more transmitted PDUs; when identifying that the last transmitted PDU lacks the poll indicator, - transmitting to the receiving device , a PDU comprising a poll indicator, wherein identifying that the last transmitted PDU is lacking the poll indicator is performed in the event that transmission on one or more of the at least two RLC entities is stopped or switched to another RLC entity while data still awaits in higher layers associated to a first RLC entity. - identifying that a last transmitted protocol data unit, PDU, of one of the at least two RLC entities, is lacking a poll indicator requesting a status of one or more transmitted PDUs; when identifying that the last transmitted PDU lacks the poll indicator, - transmitting to the receiving device , a PDU comprising a poll indicator, wherein identifying that the last transmitted PDU is lacking the poll indicator is performed in the event that transmission on one or more of the at least two RLC entities is stopped or switched to another RLC entity while data still awaits in higher layers associated to a first RLC entity.
A sensor package comprising: an inertial sensor, wherein the inertial sensor comprises a sensing structure (204; 306; 408; 512; 612) formed in a material layer (202; 300; 400) and one or more further material layers arranged to seal the sensing structure to form a hermetically sealed inertial sensor unit (210; 520; 620); a support structure (214; 302; 402; 516; 616); one or more springs (212; 304; 404; 514; 614) flexibly fixing the hermetically sealed inertial sensor unit to the support structure; wherein the one or more springs are formed in the same material layer as the sensing structure of the inertial sensor unit; one or more external package wall(s) (216, 220; 524; 624) encapsulating the inertial sensor unit, the support structure, and the one or more springs, wherein the support structure is fixed to at least one of the package wall(s); and characterised in that the sensor package further comprises: a squeeze film damping structure arranged between the hermetically sealed inertial sensor unit and the support structure, wherein the squeeze film damping structure is formed in the same material layer (202; 300; 400) as the sensing structure (204; 306; 408; 512; 612) of the inertial sensor unit (210; 520; 620) and the spring(s) (212; 304; 404; 514; 614). an inertial sensor, wherein the inertial sensor comprises a sensing structure (204; 306; 408; 512; 612) formed in a material layer (202; 300; 400) and one or more further material layers arranged to seal the sensing structure to form a hermetically sealed inertial sensor unit (210; 520; 620); a support structure (214; 302; 402; 516; 616); one or more springs (212; 304; 404; 514; 614) flexibly fixing the hermetically sealed inertial sensor unit to the support structure; wherein the one or more springs are formed in the same material layer as the sensing structure of the inertial sensor unit; one or more external package wall(s) (216, 220; 524; 624) encapsulating the inertial sensor unit, the support structure, and the one or more springs, wherein the support structure is fixed to at least one of the package wall(s); and characterised in that the sensor package further comprises: a squeeze film damping structure arranged between the hermetically sealed inertial sensor unit and the support structure, wherein the squeeze film damping structure is formed in the same material layer (202; 300; 400) as the sensing structure (204; 306; 408; 512; 612) of the inertial sensor unit (210; 520; 620) and the spring(s) (212; 304; 404; 514; 614).
An aqueous oxidizing composition having a pH in the range of 1 to 6 comprising: a) hydrogen peroxide at a concentration of more than 5% by weight, calculated to the total weight of the composition, and b) one or more compound(s) according to the following structure: wherein R 1 , R 2 , and R 3 are independently selected from H and CH 3 , and/or their mixtures. a) hydrogen peroxide at a concentration of more than 5% by weight, calculated to the total weight of the composition, and b) one or more compound(s) according to the following structure:
Laminated polyethylene based film structure having barrier properties comprising one oriented first film being at least oriented in machine direction (MDO film) which comprises a) at least one layer A based on polyethylene polymer having a density of 890 to 980 kg/m 3 and b) optionally at least one layer B of high density polyethylene (HDPE) having a density of 940 up to 970 kg/m 3 or a medium density polyethylene (MDPE) having a density of 925 up to 940 kg/m 3 or a linear low density polyethylene (LLDPE) having a density of 910 up to 950 kg/m 3 whereby the oriented first film is at least oriented in machine direction in a draw ratio of 1:1.5 to 1:12 and having a film thickness after orientation of 10 to 50 μm and whereby the oriented first film is coated by a thin vapour deposited barrier ceramic or metal layer on one surface of the oriented first film a second film, having c) at least one sealant layer C based on polyethylene polymer d) optionally in combination with a high density polyethylene (HDPE) barrier layer D, the oriented first film being laminated with the coated surface to a second film and wherein in the laminated film structures other polymers than ethylene based polymers are substantially absent. one oriented first film being at least oriented in machine direction (MDO film) which comprises a) at least one layer A based on polyethylene polymer having a density of 890 to 980 kg/m 3 and b) optionally at least one layer B of high density polyethylene (HDPE) having a density of 940 up to 970 kg/m 3 or a medium density polyethylene (MDPE) having a density of 925 up to 940 kg/m 3 or a linear low density polyethylene (LLDPE) having a density of 910 up to 950 kg/m 3 whereby the oriented first film is at least oriented in machine direction in a draw ratio of 1:1.5 to 1:12 and having a film thickness after orientation of 10 to 50 μm and whereby the oriented first film is coated by a thin vapour deposited barrier ceramic or metal layer on one surface of the oriented first film a) at least one layer A based on polyethylene polymer having a density of 890 to 980 kg/m 3 and b) optionally at least one layer B of high density polyethylene (HDPE) having a density of 940 up to 970 kg/m 3 or a medium density polyethylene (MDPE) having a density of 925 up to 940 kg/m 3 or a linear low density polyethylene (LLDPE) having a density of 910 up to 950 kg/m 3 a second film, having c) at least one sealant layer C based on polyethylene polymer d) optionally in combination with a high density polyethylene (HDPE) barrier layer D, the oriented first film being laminated with the coated surface to a second film and wherein in the laminated film structures other polymers than ethylene based polymers are substantially absent. c) at least one sealant layer C based on polyethylene polymer d) optionally in combination with a high density polyethylene (HDPE) barrier layer D,
A pharmaceutical composition comprising ezetimibe, or a pharmaceutically acceptable salt thereof, and curcumin for use in a method of treating a cancer in a patient in need thereof, wherein the cancer is characterized by overexpression of Mdm2.
An amorphous form of vilanterol trifenatate, characterised by the X-ray powder diffraction (XRPD) pattern, obtained using copper K-alpha1 radiation, depicted in Figure 1.
- A method for measuring the energy behavior of a transport network comprising a set of substation(s) for supplying electrical energy and a fleet of vehicles electrically supplied by said substations, said vehicles following predefined trajectories and comprising an environmental data capture unit comprising at least one temperature sensor, one humidity sensor and one CO 2 sensor, said method comprising the following steps implemented by an electronic system for measuring the energy behavior of the transport network comprising a memory and a processor : - the collection of environmental data captured by the sensor(s) of the capture unit during the movement of vehicles on their trajectory, with each environmental data being associated with its respective capture time,; - the collection of data characterizing the dynamic state of vehicles during the movement of vehicles on their trajectory; - determination of electrical consumption values of the vehicles at sampling times - the calculation of at least one indicator of energy performance indicator of the network according to said determined electrical values; where the electrical consumption values at said sampling times of at least some of said vehicles are determined by an algorithmic model, said algorithmic model being stored in the memory of the electronic measuring system and executed on the processor of said system, the electrical consumption values at said sampling times of each of said vehicles being calculated by the algorithmic model based on the captured environmental data and the associated capture times collected during the travel of the vehicle along said trajectory, as well as data characterizing the dynamic state of the vehicle on the predefined trajectory at the sampling times, the electrical consumption values of a substation being determined at said sampling times during the passage of a vehicle while solely supplied by said substation ; electrical consumption values of said vehicle being deduced from said determined electrical consumption values of a substation and the validity of the algorithmic model being evaluated by comparing said deduced electrical consumption values of said vehicle with said determined electrical consumption values of said vehicles. - the collection of environmental data captured by the sensor(s) of the capture unit during the movement of vehicles on their trajectory, with each environmental data being associated with its respective capture time,; - the collection of data characterizing the dynamic state of vehicles during the movement of vehicles on their trajectory; - determination of electrical consumption values of the vehicles at sampling times - the calculation of at least one indicator of energy performance indicator of the network according to said determined electrical values;
An axial turbine for an exhaust-gas-driven turbocharger, the turbine being statorless, and comprising: an axial turbine wheel comprising a hub and a plurality of blades extending generally radially outward from the hub, and a turbine housing assembly that houses the turbine wheel; the turbine housing assembly comprising a sector-divided turbine housing, the sector-divided turbine housing defining a plurality of separate exhaust gas inlets into the turbine housing, each exhaust gas inlet for receiving a separate exhaust gas stream from an internal combustion engine, the sector-divided turbine housing further defining a plurality of separate angular sector passageways each of which occupies a fractional part of a circumference surrounding the turbine wheel, the angular sector passageways succeeding one another in a circumferential direction, each angular sector passageway being supplied with exhaust gas by a respective one of the plurality of exhaust gas inlets, each angular sector passageway having a convergent cross-section that spirals inward and converges to accelerate the exhaust gas; the turbine housing assembly defining a separate sector outlet for each angular sector passageway through which the respective exhaust gas stream is fed into an inlet side of the turbine wheel generally in an axial direction of the turbine wheel; and being characterised in that the turbine housing assembly comprises the sector-divided turbine housing and a separately formed heat shroud , and the sector outlets are formed at least in part by the heat shroud. an axial turbine wheel comprising a hub and a plurality of blades extending generally radially outward from the hub, and a turbine housing assembly that houses the turbine wheel; the turbine housing assembly comprising a sector-divided turbine housing, the sector-divided turbine housing defining a plurality of separate exhaust gas inlets into the turbine housing, each exhaust gas inlet for receiving a separate exhaust gas stream from an internal combustion engine, the sector-divided turbine housing further defining a plurality of separate angular sector passageways each of which occupies a fractional part of a circumference surrounding the turbine wheel, the angular sector passageways succeeding one another in a circumferential direction, each angular sector passageway being supplied with exhaust gas by a respective one of the plurality of exhaust gas inlets, each angular sector passageway having a convergent cross-section that spirals inward and converges to accelerate the exhaust gas; the turbine housing assembly defining a separate sector outlet for each angular sector passageway through which the respective exhaust gas stream is fed into an inlet side of the turbine wheel generally in an axial direction of the turbine wheel; and being characterised in that the turbine housing assembly comprises the sector-divided turbine housing and a separately formed heat shroud , and the sector outlets are formed at least in part by the heat shroud.