mhurhangee/ep-ind-claims huggingface dataset:
A cathode material for a secondary battery containing a cathode active material represented by a general formula Li n FePO 4 (wherein n represents a number from 0 to 1) as a primary component, characterized in that the cathode material further comprises: one or more metal elements selected from the group consisting of vanadium, chromium (Cr), copper (Cu), zinc (Zn), indium (In), tin (Sn), and titanium (Ti), the total content of which is in the range of 0.1 to 5 mol%, in terms of element ratio, based on iron in the cathode active material, and a halogen element in an amount of 0.1 mol% or more based on P. one or more metal elements selected from the group consisting of vanadium, chromium (Cr), copper (Cu), zinc (Zn), indium (In), tin (Sn), and titanium (Ti), the total content of which is in the range of 0.1 to 5 mol%, in terms of element ratio, based on iron in the cathode active material, and a halogen element in an amount of 0.1 mol% or more based on P.
A compression system comprising: a garment configured to wrap around at least a portion of a body, the garment comprising: a plurality of pressure applying regions, each configured to apply pressure to the portion of the body, wherein the plurality of pressure applying regions comprises a plurality of compartments configured to receive a fluid; a lacing system comprising: a plurality of spaced apart lacing guide members, each lacing guide member positioned at a location on the garment; and at least one lace guided by the plurality of lacing guide members; a tightening apparatus coupled to the at least one lace, wherein the tightening apparatus is configured to apply tension on the at least one lace and thereby move at least one portion of the garment relative to another portion of the garment, to tighten the garment about the portion of the body; and a controller configured to control the pressure applied to the portion of the body by each of the pressure applying regions of the garment by controlling fluid flow into each of the plurality of compartments to apply pressure to a portion of the body corresponding to a pressure applying region. a garment configured to wrap around at least a portion of a body, the garment comprising: a plurality of pressure applying regions, each configured to apply pressure to the portion of the body, wherein the plurality of pressure applying regions comprises a plurality of compartments configured to receive a fluid; a lacing system comprising: a plurality of spaced apart lacing guide members, each lacing guide member positioned at a location on the garment; and at least one lace guided by the plurality of lacing guide members; a plurality of spaced apart lacing guide members, each lacing guide member positioned at a location on the garment; and at least one lace guided by the plurality of lacing guide members; a tightening apparatus coupled to the at least one lace, wherein the tightening apparatus is configured to apply tension on the at least one lace and thereby move at least one portion of the garment relative to another portion of the garment, to tighten the garment about the portion of the body; and a controller configured to control the pressure applied to the portion of the body by each of the pressure applying regions of the garment by controlling fluid flow into each of the plurality of compartments to apply pressure to a portion of the body corresponding to a pressure applying region.
A method for controlled atmosphere stunning of poultry comprising the steps of: (i) loading one or more batches of poultry in a stunning chamber; (ii) sealably enclosing the one or more batches of poultry in the stunning chamber to isolate the atmosphere proximate the poultry; (iii) introducing a gaseous mixture to the isolated atmosphere to stun the one or more batches of poultry; wherein the introduction of gaseous mixture is done in three to five stages with each successive stage having a greater concentration of stunning gas (iv) forcibly exhausting the gaseous mixture from the isolated atmosphere; and (v) advancing the stunned poultry from the stunning chamber. (i) loading one or more batches of poultry in a stunning chamber; (ii) sealably enclosing the one or more batches of poultry in the stunning chamber to isolate the atmosphere proximate the poultry; (iii) introducing a gaseous mixture to the isolated atmosphere to stun the one or more batches of poultry; wherein the introduction of gaseous mixture is done in three to five stages with each successive stage having a greater concentration of stunning gas (iv) forcibly exhausting the gaseous mixture from the isolated atmosphere; and (v) advancing the stunned poultry from the stunning chamber.
An infusion device for infusion of a fluid from a reservoir (2, 4) into a body, the infusion device being connectable to an infusion set adaptor at a connecting site, the infusion device comprising: a drive mechanism (40, 45, 50, 51, 52, 53, 55, 56) to operatively couple with at least a portion of the reservoir (2,4); a housing (5, 6) comprising at least two compartments, at least one of which being sized to contain at least a portion of the reservoir (2, 4), wherein the drive mechanism is at least partially or fully contained within another one of the compartments; a sealing device (54, 54a, 57, 58) that permits the passage of air into and out of a first housing compartment or within the housing and inhibits the passage of liquids through the sealing device between the first compartment and a neighbouring compartment or within the housing; characterized by that the sealing device (54, 54a, 57, 58) is arranged at a location between the first compartment and the neighbouring compartment, wherein such location is part of a path for movement of air between compartments of or within the housing, wherein such movement equalises pressure between such compartments, and wherein the housing does not contain a vent port being an aperture of the housing. a drive mechanism (40, 45, 50, 51, 52, 53, 55, 56) to operatively couple with at least a portion of the reservoir (2,4); a housing (5, 6) comprising at least two compartments, at least one of which being sized to contain at least a portion of the reservoir (2, 4), wherein the drive mechanism is at least partially or fully contained within another one of the compartments; a sealing device (54, 54a, 57, 58) that permits the passage of air into and out of a first housing compartment or within the housing and inhibits the passage of liquids through the sealing device between the first compartment and a neighbouring compartment or within the housing; characterized by that the sealing device (54, 54a, 57, 58) is arranged at a location between the first compartment and the neighbouring compartment, wherein such location is part of a path for movement of air between compartments of or within the housing, wherein such movement equalises pressure between such compartments, and wherein the housing does not contain a vent port being an aperture of the housing.
Anchor module for anchoring to a casing, comprising: - an inner mandrel having a through bore; - a slips device provided radially outside the inner mandrel; - upper and lower slips supports (71, 72) for supporting the slips device in a run state, in which the slips device is radially retracted, and for supporting the slips device in a set state, in which the slips device is radially expanded; - a spring device provided radially outside of the inner mandrel, where the slips device is biased to its run state by means of the spring device; - a fluid actuation system configured to counteract the biasing force provided by the spring device, thereby causing the slips device to move from its run state to its set state; where the fluid actuation system comprises a lower piston axially displaceable within a lower fluid chamber, where a lower fluid line is provided between the bore and the lower fluid chamber, where the lower piston is a part of or is connected to the lower slips device; characterized in that: - the fluid actuation system further comprises an upper piston axially displaceable within an upper fluid chamber, where an upper fluid line is provided between the bore and the upper fluid chamber, where the upper piston is connected to the lower slips device; - the fluid actuation system further comprises a fluid restriction provided in the bore, where a cross sectional area of the fluid bore at the entrance of the upper fluid line is smaller than the cross sectional area of the fluid bore at the entrance of the lower fluid line. - an inner mandrel having a through bore; - a slips device provided radially outside the inner mandrel; - upper and lower slips supports (71, 72) for supporting the slips device in a run state, in which the slips device is radially retracted, and for supporting the slips device in a set state, in which the slips device is radially expanded; - a spring device provided radially outside of the inner mandrel, where the slips device is biased to its run state by means of the spring device; - a fluid actuation system configured to counteract the biasing force provided by the spring device, thereby causing the slips device to move from its run state to its set state; - the fluid actuation system further comprises an upper piston axially displaceable within an upper fluid chamber, where an upper fluid line is provided between the bore and the upper fluid chamber, where the upper piston is connected to the lower slips device; - the fluid actuation system further comprises a fluid restriction provided in the bore, where a cross sectional area of the fluid bore at the entrance of the upper fluid line is smaller than the cross sectional area of the fluid bore at the entrance of the lower fluid line.
Apparatus for enhancing an input signal (s), comprising a sparse approximator configured to generate, using sparse approximation, an approximated signal (a) approximating the input signal; a high frequency portion extractor configured to extract a high frequency portion (h) from the approximated signal (a) wherein the high frequency portion extractor is a high pass filter or is configured to extract the high frequency portion from the approximated signal by estimating (50, 60) a low frequency portion of the approximated signal and subtracting the low frequency portion from the approximated signal; and a combiner configured to combine the input signal (s) and the extracted high frequency portion (h) extracted from approximated signal by adding the input signal and the high frequency portion of the approximated signal, wherein the sparse approximator is configured to perform the sparse approximation by sequentially performing a forward transformation by using shearlets to obtain transform coefficients, thresholding the transform coefficients to obtain thresholded transform coefficients and performing an inverse transform onto the thresholded transform coefficients.
Electronic control system for controlling the speed of an internal combustion engine and an electric motor, which are arranged as drive motors in a hybrid vehicle, wherein associated motor-specific control parameters are used for each of the two drive motors, wherein the differential speed (n diff) between a predefined target speed (n soll) and an actual speed (n ist) of each drive motor are considered as system value for determining motor-specific control parameters that influence the speed control, and wherein as additional system value the differential speed gradient (gradn diff) is considered in terms of magnitude and direction for determining the motor-specific control parameters, characterised in that in addition to determining the motor-specific control parameters as further system values the changing speed of the target speed (n soll) and/or the actual speed (n ist) are taken into account, and in that the system values are transmitted to a processor, which from a parameter engine characteristic memory, in which motor-specific control parameters assigned to all possible system value combinations are stored, reads the associated motor-specific control parameters for system value combinations and transmits the latter to a motor control unit of the drive motors.
Boat drive for driving a boat, comprising a drive unit with an electric motor and a propeller driven by means of the electric motor, comprising a water detector, which is arranged to detect whether the propeller is immersed in water, wherein a control unit is provided for controlling the power and/or the speed and/or the torque of the electric motor, wherein the control unit communicates with the water detection and the control unit, upon detection of a propeller not immersed in water, retains and/or limits and/or reduces the power and/or speed of the electric motor and/or the torque of the electric motor or stops the electric motor, characterized in that the control unit, after limiting and/or retaining and/or reducing power and/or speed and/ or torque and/or after stopping the electric motor, is configured to enable a renewed increase in power and/or speed and/or torque or to enable the electric motor to be started only if a driving stage adjuster for setting a driving stage has been moved to a lower driving stage or to a zero position.
A lubrication system comprising: a lubrication tank; a gearbox driven pump; an electrically driven pump located in parallel with the gearbox driven pump; a gearbox for driving the gearbox driven pump; and a tower shaft; characterised by: a first control valve for selectively connecting the electrically driven pump or the gearbox driven pump with the lubrication tank; a second control valve located downstream of an output to the gearbox driven pump and an output to the electrically driven pump; a third control valve located downstream of the second control valve for selectively directing lubrication between at least one of a speed change mechanism on a gas turbine engine and rotor support bearings on the gas turbine engine; and the tower shaft mechanically connecting the gearbox with a high speed spool. a lubrication tank; a gearbox driven pump; an electrically driven pump located in parallel with the gearbox driven pump; a gearbox for driving the gearbox driven pump; and a tower shaft; characterised by: a first control valve for selectively connecting the electrically driven pump or the gearbox driven pump with the lubrication tank; a second control valve located downstream of an output to the gearbox driven pump and an output to the electrically driven pump; a third control valve located downstream of the second control valve for selectively directing lubrication between at least one of a speed change mechanism on a gas turbine engine and rotor support bearings on the gas turbine engine; and the tower shaft mechanically connecting the gearbox with a high speed spool. a first control valve for selectively connecting the electrically driven pump or the gearbox driven pump with the lubrication tank; a second control valve located downstream of an output to the gearbox driven pump and an output to the electrically driven pump; a third control valve located downstream of the second control valve for selectively directing lubrication between at least one of a speed change mechanism on a gas turbine engine and rotor support bearings on the gas turbine engine; and the tower shaft mechanically connecting the gearbox with a high speed spool.
A wafer container comprising: a top housing and a bottom housing; the top housing having a base with at least one rib that extends perpendicular from the base of the top housing in an essentially circular orientation; the bottom housing having a base with at least one rib that extends perpendicular from the base of the bottom housing, wherein the at least one rib on the bottom housing is arranged concentric and at a different radius from the at least one rib that extends perpendicular from the base of the top housing (50, the at least one rib on the bottom housing having an arc angle of <360°; the bottom housing having at least one latch that extends essentially perpendicular from the base of the bottom housing; the wafer container being characterized in that the distance between the base of the bottom housing to the top surface of the latch is less than the distance between the base of the bottom housing and the top of the at least one rib on the bottom housing; the wafer container being further characterized by the top housing having at least one latch well, the latch well having a bottom surface and a rim around the well, wherein the bottom surface is located below the surface of the base of the top housing, and wherein when the top housing is joined with the bottom housing, the top surface of the latch is lower than the rim around the well, and wherein the latch well comprises a notch configured to receive the at least one latch on the bottom housing. a top housing and a bottom housing; the top housing having a base with at least one rib that extends perpendicular from the base of the top housing in an essentially circular orientation; the bottom housing having a base with at least one rib that extends perpendicular from the base of the bottom housing, wherein the at least one rib on the bottom housing is arranged concentric and at a different radius from the at least one rib that extends perpendicular from the base of the top housing (50, the at least one rib on the bottom housing having an arc angle of <360°; the bottom housing having at least one latch that extends essentially perpendicular from the base of the bottom housing; the wafer container being characterized in that the distance between the base of the bottom housing to the top surface of the latch is less than the distance between the base of the bottom housing and the top of the at least one rib on the bottom housing; the wafer container being further characterized by the top housing having at least one latch well, the latch well having a bottom surface and a rim around the well, wherein the bottom surface is located below the surface of the base of the top housing, and wherein when the top housing is joined with the bottom housing, the top surface of the latch is lower than the rim around the well, and wherein the latch well comprises a notch configured to receive the at least one latch on the bottom housing.
A method of operating a printer for printing an image, the method comprising: printing over a print swath for reproducing a portion of the image, wherein based on an estimate of an amount of print fluid to be printed in an outstanding image portion via a set of nozzles, the print swath is printed by ejecting only imaging droplets of the print fluid via the set of nozzles, if ejection of imaging droplets of a print fluid via the set of nozzles for printing the outstanding image portion is above a selected droplet number; and printing the print swath includes ejecting purging droplets of the print fluid via the set of nozzles, if ejection of imaging droplets of the print fluid for printing an outstanding image portion is below the selected droplet number. the print swath is printed by ejecting only imaging droplets of the print fluid via the set of nozzles, if ejection of imaging droplets of a print fluid via the set of nozzles for printing the outstanding image portion is above a selected droplet number; and printing the print swath includes ejecting purging droplets of the print fluid via the set of nozzles, if ejection of imaging droplets of the print fluid for printing an outstanding image portion is below the selected droplet number.
Method of manufacturing torsion boxes of wings, empennages, control elements and highlift systems of aircraft comprising the steps of - providing a first rigid mould, - depositing reinforcing fibres on this rigid mould, - providing at least one further rigid mould tool, - depositing reinforcing fibres on these rigid mould tools, - fixing the mould tools with the reinforcing fibres so that the reinforcing fibres partially contact the reinforcing fibres and form a hollow structure which can be formed with at least one further mould tool, - providing at least one rigid core, - inserting this or these rigid cores each into a flexible tool, - positioning reinforcing fibres on the tools, - removing the rigid cores, - providing at least one further rigid core, - inserting this or these further rigid cores each into a further flexible tool, - optionally positioning further reinforcing fibres 10 on the further tools, - removing the further rigid cores, - inserting the reinforcing fibres on the tools and optionally the further reinforcing fibres on the further tools 9 into the preformed hollow structure, - sealing the preformed hollow structure with at least one final mould covered with reinforcing fibres, - inflating the flexible moulds and the further flexible moulds to form an internal support structure which braces the hollow structure formed from the reinforcing fibres, and - consolidating the reinforcing fibres. - providing a first rigid mould, - depositing reinforcing fibres on this rigid mould, - providing at least one further rigid mould tool, - depositing reinforcing fibres on these rigid mould tools, - fixing the mould tools with the reinforcing fibres so that the reinforcing fibres partially contact the reinforcing fibres and form a hollow structure which can be formed with at least one further mould tool, - providing at least one rigid core, - inserting this or these rigid cores each into a flexible tool, - positioning reinforcing fibres on the tools, - removing the rigid cores, - providing at least one further rigid core, - inserting this or these further rigid cores each into a further flexible tool, - optionally positioning further reinforcing fibres 10 on the further tools, - removing the further rigid cores, - inserting the reinforcing fibres on the tools and optionally the further reinforcing fibres on the further tools 9 into the preformed hollow structure, - sealing the preformed hollow structure with at least one final mould covered with reinforcing fibres, - inflating the flexible moulds and the further flexible moulds to form an internal support structure which braces the hollow structure formed from the reinforcing fibres, and - consolidating the reinforcing fibres.