mhurhangee/ep-ind-claims huggingface dataset:
A wireless device, comprising: an antenna configured to facilitate wireless communications of the wireless device; and a location core (112, 114, 116) communicatively coupled to the antenna and configured to receive, when the wireless device is operational in a first wireless network, first location-related aid information from a first aid-data source in the first wireless network, initiate tracking and acquiring one or more satellites (106a, 106b, 106x) according to a first configuration corresponding to the first location-related aid information, receive, when the wireless device is operational in a second wireless network, second location-related aid information from a second aid-data source in the second wireless network, generate integrated location-related aid information based on a combination of the first location-related aid information and the second location-related aid information, and update the tracking and acquiring of the one or more satellites according to a second configuration corresponding to the integrated location-related aid information. an antenna configured to facilitate wireless communications of the wireless device; and a location core (112, 114, 116) communicatively coupled to the antenna and configured to receive, when the wireless device is operational in a first wireless network, first location-related aid information from a first aid-data source in the first wireless network, initiate tracking and acquiring one or more satellites (106a, 106b, 106x) according to a first configuration corresponding to the first location-related aid information, receive, when the wireless device is operational in a second wireless network, second location-related aid information from a second aid-data source in the second wireless network, generate integrated location-related aid information based on a combination of the first location-related aid information and the second location-related aid information, and update the tracking and acquiring of the one or more satellites according to a second configuration corresponding to the integrated location-related aid information.
A reusable logistical transport package for transporting an object comprising: - a box having a stowage volume defined by a bottom and a peripheral rim substantially perpendicular to the bottom; - a lid able to occupy a position closing the box in which the stowage volume is sealed, the lid being movable between an open position and a closed position and vice versa; - a tray housed in the stowage volume and movable with respect to the bottom between a rest position in which it is located in proximity to the bottom and an operating position in which it is separated from the bottom and holds the object against the lid; - means for returning the tray to its operating position, in which the package is of the foldable type and in which the return means comprise: - a cross-brace movable between a flattened position in which it is crushed between the tray and the bottom, and a deployed position in which it pushes back the tray with respect to the bottom; - a return member secured to the cross-brace and tending to position the cross-brace in its deployed position from its flattened position. - a box having a stowage volume defined by a bottom and a peripheral rim substantially perpendicular to the bottom; - a lid able to occupy a position closing the box in which the stowage volume is sealed, the lid being movable between an open position and a closed position and vice versa; - a tray housed in the stowage volume and movable with respect to the bottom between a rest position in which it is located in proximity to the bottom and an operating position in which it is separated from the bottom and holds the object against the lid; - means for returning the tray to its operating position, in which the package is of the foldable type and in which the return means comprise: - a cross-brace movable between a flattened position in which it is crushed between the tray and the bottom, and a deployed position in which it pushes back the tray with respect to the bottom; - a return member secured to the cross-brace and tending to position the cross-brace in its deployed position from its flattened position. - a cross-brace movable between a flattened position in which it is crushed between the tray and the bottom, and a deployed position in which it pushes back the tray with respect to the bottom; - a return member secured to the cross-brace and tending to position the cross-brace in its deployed position from its flattened position.
A powder conveying chamber (2, 2') for a dense phase powder pump for conveying powder, in particular coating powder, wherein the powder conveying chamber (2, 2') comprises at least one air exchange opening which is in particular designed and formed separately from a cleaning air outlet of the end region for alternately connecting fluidly to a vacuum line or vacuum source, respectively, or to a compressed air supply line or compressed air source, respectively for drawing powder into the powder conveying chamber (2, 2'), or, respectively, pneumatically expelling a portion of powder present within the powder conveying chamber (2, 2'), wherein the powder conveying chamber (2, 2') comprises an end region via which the powder conveying chamber (2, 2') is fluidly connected or connectable to a powder line, wherein the end region of the powder conveying chamber (2, 2') is configured as a transition region and designed to reduce an effective sectional area of flow of the powder conveying chamber (2, 2') to an effective sectional area of flow of the powder line and/or to an effective sectional area of flow of a valve (6, 7), in particular a pinch valve, arranged between the powder conveying chamber (2, 2') and the powder line, wherein the end region is allocated a cleaning system via which cleaning air in the form of compressed air can be supplied to the end region, particularly as necessary, in order to keep the end region free of powder deposits or to remove powder deposits at the end region, characterized in that a wall area of the end region forming the end region of the powder conveying chamber (2, 2') is designed at least partly as a porous wall area permeable to compressed air but not permeable to powder.
Device for supporting a bearing spring of a wheel suspension for a motor vehicle, which bearing spring can be supported by means of a spring disc component (30; 44) on a base wall, comprising a recess, of a longitudinal beam of the bodywork, the longitudinal beam having, on its lower wall facing toward the bearing spring, an indentation which is configured in the shape of a dome and in which the base wall with the recess is formed in a set-back fashion, characterised in that either the spring disc component is configured with an adjustment spring disc of an actuator, which can be driven by an electric motor, for level adjustment of the bodywork, or in that, if the motor vehicle is configured without height adjustment, the spring disc component is an adapter having a spring support (30c; 40c) which is fixed in a height direction, the indentation of the longitudinal beam being configured so that the adjustment spring disc can be inserted into the indentation in such a way that it is arranged at least partially inside the indentation, and the electric motor extending through the recess of the base wall into the longitudinal beam.
A reverse flow gas turbine engine (10;110) comprising: a propulsor section (14;114) includes a propulsor compressor section and a propulsor turbine section, wherein the propulsor section (14;114) includes a fan section and a geared architecture, the fan section driven by the propulsor turbine section; wherein a core section is arranged fluidly between the propulsor compressor section and the propulsor turbine section, the core section includes a reverse flow duct (64; 164) that reverses a core flow through the core section, wherein at least one of the propulsor section (14;114) and the core section has a two-spool arrangement; and an intercooler is arranged upstream from the reverse flow duct (64; 164) and downstream from the propulsor compressor section (14;114); characterised in that: the intercooler is a tube heat exchanger; and the intercooler provides the reverse flow duct (64; 164). a propulsor section (14;114) includes a propulsor compressor section and a propulsor turbine section, wherein the propulsor section (14;114) includes a fan section and a geared architecture, the fan section driven by the propulsor turbine section; wherein a core section is arranged fluidly between the propulsor compressor section and the propulsor turbine section, the core section includes a reverse flow duct (64; 164) that reverses a core flow through the core section, wherein at least one of the propulsor section (14;114) and the core section has a two-spool arrangement; and an intercooler is arranged upstream from the reverse flow duct (64; 164) and downstream from the propulsor compressor section (14;114); characterised in that: the intercooler is a tube heat exchanger; and the intercooler provides the reverse flow duct (64; 164). the intercooler is a tube heat exchanger; and the intercooler provides the reverse flow duct (64; 164).
A porous ceramic honeycomb body, comprising: a primary cordierite ceramic phase; a total porosity %P of at least 40%; and a thermal shock parameter of at least 450°C, wherein TSP is (MOR 25°C /E 25°C)(CTE 500 - 900°C) -1, MOR 25°C is the modulus of rupture strength at 25°C, E 25°C is the Young's elastic modulus at 25°C, and CTE 500 - 900°C is the high temperature thermal expansion coefficient at 500°C to 900°C, all as measured in the axial direction of the honeycomb; characterized in that after exposure to a temperature of 1050°C for 100 hours, the honeycomb body exhibits at least one of: an elastic modulus ratio E ratio ≤ 0.99, and a microcrack parameter Nb 3 ≤ 0.07, wherein E ratio = E 900°C /E 25°C where E 900°C is the elastic modulus at 900°C measured during heating, wherein the honeycomb body comprises a strain tolerance of at least 0.14 x 10 -2 where the strain tolerance = (MOR 25°C / E 25°C). a primary cordierite ceramic phase; a total porosity %P of at least 40%; and a thermal shock parameter of at least 450°C, wherein an elastic modulus ratio E ratio ≤ 0.99, and a microcrack parameter Nb 3 ≤ 0.07,
A device for growth of blue-green algae, said device being a photobioreactor, comprising at least one vacuum-rated and solar receiver hosting the cultivation medium, and filling completely said solar receiver, a head vessel system, located above the solar receiver, partially filled with the cultivation medium and partially filled with inert gas, a culture medium feed system for the feed of decarbonated or non-decarbonate culture medium, a carbon dioxide feed system, allowing the insertion of the carbon dioxide, which enables the photosynthesis of the blue-green algae, a harvesting system for the collection of a cultivation medium matured as final product ready for processing for extraction of the blue-green algae, a gas loop, characterized by comprising an "inert gas-push" system comprising at least a circuit connection line, a circuit isolation valve, a gas shutoff valve, a downcomer, apt to open/interrupt the recirculation path of the cultivation medium by opening/closing said valves (202,204) and such as to allow, alternatively and in a cyclical pattern, the flow of cultivation medium through valve or the rapid insertion in the vertical portion of the downcomer below the vertical circuit connection line and below valve of said system a volume of inert gas, the inert gas push system being thus able to force the recirculation of the cultivation medium while minimizing the stress and shear on the molecules of blue-green algae and avoiding introduction of dissolved oxygen.
Compounds of the general formula, in which Z 1 represents 1-halogenated cyclopropyl; Z 2 represents -S 0-2 -(C 1 -C 2)-alkyl, (C 1 -C 2)-halogenalkyl, or nitro (NO 2); Z 3 represents (C 1 -C 2)-alkyl; R 1 represents hydrogen or (C 1 -C 2)-alkyl; R 2 represents H or cyano; R 3 represents CH 3 or chlorine; A 1 represents CH or nitrogen. Z 1 represents 1-halogenated cyclopropyl; Z 2 represents -S 0-2 -(C 1 -C 2)-alkyl, (C 1 -C 2)-halogenalkyl, or nitro (NO 2); Z 3 represents (C 1 -C 2)-alkyl; R 1 represents hydrogen or (C 1 -C 2)-alkyl; R 2 represents H or cyano; R 3 represents CH 3 or chlorine; A 1 represents CH or nitrogen.
Method for introducing a drill pipe into the ground with directional accuracy, in which - an alignment of the position of the drill pipe is determined at least at the beginning of the introduction, - the alignment of the drill pipe is adjusted by means of a positioning means which is controlled by a control means and - the drill pipe is drilled down into the ground by means of a drilling device, characterized in that - on a head region of the drill pipe a marking element is arranged and axially opposite the marking element a measuring means is arranged which is independent of the drill pipe and has at least two distance measuring units, - by means of the at least two distance measuring units the axial distance to the marking element is measured regularly while the drill pipe is being drilled down, wherein the distance measuring units each provide independent measured distance values, and - in that the measured distance values of the at least two distance measuring units are compared in the control means and used to adjust the drill pipe during drilling. - an alignment of the position of the drill pipe is determined at least at the beginning of the introduction, - the alignment of the drill pipe is adjusted by means of a positioning means which is controlled by a control means and - the drill pipe is drilled down into the ground by means of a drilling device, - on a head region of the drill pipe a marking element is arranged and axially opposite the marking element a measuring means is arranged which is independent of the drill pipe and has at least two distance measuring units, - by means of the at least two distance measuring units the axial distance to the marking element is measured regularly while the drill pipe is being drilled down, wherein the distance measuring units each provide independent measured distance values, and - in that the measured distance values of the at least two distance measuring units are compared in the control means and used to adjust the drill pipe during drilling.
A front-end monitoring device, comprising: a Bluetooth low energy, BLE, module, configured to establish a BLE link between the front-end monitoring device and a back-end monitoring device; a universal asynchronous receiver/transmitter, UART, configured to receive, by using the BLE link, a first body temperature value sent by the back-end monitoring device, wherein the first body temperature value is obtained by the back-end monitoring device by measuring body temperature of a monitored person; a thermistor sensor, configured to measure body temperature of a monitoring person to obtain a second body temperature value; and a processing module, configured to determine, according to a variation of the first body temperature value relative to the second body temperature value, whether first prompt information needs to be generated. a Bluetooth low energy, BLE, module, configured to establish a BLE link between the front-end monitoring device and a back-end monitoring device; a universal asynchronous receiver/transmitter, UART, configured to receive, by using the BLE link, a first body temperature value sent by the back-end monitoring device, wherein the first body temperature value is obtained by the back-end monitoring device by measuring body temperature of a monitored person; a thermistor sensor, configured to measure body temperature of a monitoring person to obtain a second body temperature value; and a processing module, configured to determine, according to a variation of the first body temperature value relative to the second body temperature value, whether first prompt information needs to be generated.
A gas turbine engine comprising: a compressor section; a turbine section operably coupled to the compressor section; a means (1200; 1202) for selectively releasing a cooling fluid flow produced at a cryogenic temperature; and a plumbing system in fluid communication with the means for selectively releasing the cooling fluid flow, the plumbing system configured to route the cooling fluid flow to the compressor section, and characterized in that the plumbing system is also configured to route the cooling fluid flow to the turbine section. a compressor section; a turbine section operably coupled to the compressor section; a means (1200; 1202) for selectively releasing a cooling fluid flow produced at a cryogenic temperature; and a plumbing system in fluid communication with the means for selectively releasing the cooling fluid flow, the plumbing system configured to route the cooling fluid flow to the compressor section, and characterized in that the plumbing system is also configured to route the cooling fluid flow to the turbine section.
Cream dispenser for topically dispensing liquid on the skin of a user, having the following features: a. the cream dispenser possesses a liquid reservoir having an outlet port; and b. the cream dispenser possesses an applicator head having an outlet duct and an applicator opening at the end of the outlet duct; and c. the applicator head has an end wall which is penetrated by the outlet duct and in which the applicator opening is provided; and d. the applicator head possesses a hinged cover which in a closed state closes the applicator opening; and e. the hinged cover on an internal side has a bulged closure face of which the size is larger than the cross-sectional area of the applicator opening, wherein the bulged closure face in the closed state of the hinged cover in the region of an annular contact face surrounding the applicator opening bears on the end wall, characterized by the following additional features: f. the closure face is formed by a face which lies opposite the applicator opening and which in the closed state bulges in the direction of the applicator opening; and g. the closure face has a curvature radius which at least in the region of the annular contact face is between 4 cm and 25 cm; and h. the hinged cover has a periphery and a covering wall which is bordered by this periphery, wherein the bulged closure face occupies at least 80% of an internal side of the covering wall. a. the cream dispenser possesses a liquid reservoir having an outlet port; and b. the cream dispenser possesses an applicator head having an outlet duct and an applicator opening at the end of the outlet duct; and c. the applicator head has an end wall which is penetrated by the outlet duct and in which the applicator opening is provided; and d. the applicator head possesses a hinged cover which in a closed state closes the applicator opening; and e. the hinged cover on an internal side has a bulged closure face of which the size is larger than the cross-sectional area of the applicator opening, wherein the bulged closure face in the closed state of the hinged cover in the region of an annular contact face surrounding the applicator opening bears on the end wall, f. the closure face is formed by a face which lies opposite the applicator opening and which in the closed state bulges in the direction of the applicator opening; and g. the closure face has a curvature radius which at least in the region of the annular contact face is between 4 cm and 25 cm; and h. the hinged cover has a periphery and a covering wall which is bordered by this periphery, wherein the bulged closure face occupies at least 80% of an internal side of the covering wall.
A method for validating a propeller control unit associated with a propeller having blades, the method comprising: commanding, by a controller (110, 120), actuation of a control valve of the propeller control unit to achieve a predetermined degree of openness or closedness of the control valve in order to cause a change in a flow of fluid to the propeller to alter a pitch angle of the blades to a commanded pitch angle and to control a rotational speed of the propeller to a commanded rotational speed; determining, at the controller (110, 120) and via a sensing system at the propeller, one of an actual pitch angle of the blades and an actual rotational speed of the propeller after a predetermined time delay has elapsed from the commanding of the actuation of the control valve, the predetermined time delay commensurate with an expected time required for the control valve to achieve the predetermined degree of openness or closedness; comparing, at the controller (110, 120), the one of the actual pitch angle of the blades and the actual rotational speed of the propeller to a corresponding one of a pitch angle threshold and a rotational speed threshold, the pitch angle threshold and the rotational speed threshold based on the commanded pitch angle; and issuing, by the controller (110, 120), a warning signal in response to determining one of the actual pitch angle failing to meet the pitch angle threshold and the actual rotational speed failing to meet the rotational speed threshold. commanding, by a controller (110, 120), actuation of a control valve of the propeller control unit to achieve a predetermined degree of openness or closedness of the control valve in order to cause a change in a flow of fluid to the propeller to alter a pitch angle of the blades to a commanded pitch angle and to control a rotational speed of the propeller to a commanded rotational speed; determining, at the controller (110, 120) and via a sensing system at the propeller, one of an actual pitch angle of the blades and an actual rotational speed of the propeller after a predetermined time delay has elapsed from the commanding of the actuation of the control valve, the predetermined time delay commensurate with an expected time required for the control valve to achieve the predetermined degree of openness or closedness; comparing, at the controller (110, 120), the one of the actual pitch angle of the blades and the actual rotational speed of the propeller to a corresponding one of a pitch angle threshold and a rotational speed threshold, the pitch angle threshold and the rotational speed threshold based on the commanded pitch angle; and issuing, by the controller (110, 120), a warning signal in response to determining one of the actual pitch angle failing to meet the pitch angle threshold and the actual rotational speed failing to meet the rotational speed threshold.
A device for collecting oil to collect oil among ice, the device including a lifting device suitable to be supported to a vessel, a separating cage to be lowered into water among the ice by the lifting device and formed by a casing that lets water and oil but substantially no ice through, and an oil collector to collect oil on the surface of water in the space defined by the separating cage, the casing of the separating cage is formed by a trough surface consisting of parallel ribs that are transverse relative to the longitudinal direction of the trough surface and disposed at a distance form one another and the separating cage includes a swinging suspension for supporting it to the lifting device to turn the separating cage in the longitudinal direction of the ribs, characterized in that the lifting device is a gantry crane that extends in the rear part of the vessel substantially over the entire width thereof to be turned over the stern, the separating cage extending over the entire width of the gantry crane.