mhurhangee/ep-ind-claims huggingface dataset:
A target launching machine comprising a base on which an assembly comprising a launching mechanism and a rotary launcher for storing targets is arranged, the assembly being configured to be movable relative to the base, the machine comprising a tilting device ensuring movability of the assembly relative to the base, the tilting device comprising on the one hand a first part connected to the base and comprising one of a curved slide and a guide element of the slide along a single tilting degree of freedom along the slide, and on the other hand a second part connected to the assembly and comprising the other of the slide and the guide element, the machine comprising a pivot connection along an axis of rotation A2 between the second part and the assembly, the pivot connection comprising a fixed base relative to the second part and a turret rotatably adjustable on the fixed base, one of the fixed base and the turret comprising at least one oblong hole, and the other of the fixed base and the turret comprising at least one guided finger in the at least one oblong hole.
Apparatus for allowing radio frequency selectivity for use in a wireless communication system for the passage of one or more receiving and/or transmission frequency signals therethrough, said apparatus including at least a first set of first and second 90 degree phase shift coupling means, and at least one pair of resonating means (236, 238) coupled between the at least first and second 90 degree phase shift coupling means, wherein at least one further set of first and second 90 degree phase shift coupling means are cascaded, either directly or indirectly, with said at least first set of first and second 90 degree phase shift coupling means, with or without at least one pair of resonating means (236, 238) located between the first and second 90 degree phase shift coupling means of the at least one further set, characterised in that the 90 degree phase shift coupling means is in the form of a transmission line with an electrical length of 90 degrees, or a quarter wavelength transmission line (232, 234), such that said quarter wavelength transmission line (232, 234) is provided at either side of the at least one pair of resonating means (236, 238), with each quarter wavelength transmission line (232, 234) having one end coupled to one of the resonating means (236, 238) of the pair of resonating means and the other end of the quarter wavelength transmission line (232, 234) coupled to the other resonating means (236, 238) of the pair of resonating means, and coupling is provided between the pair of resonating means (236, 238).
Leading-edge slat for an aircraft, comprising a slat body having a front skin, a back skin, a spar and an air inlet, wherein the front skin is curved about at least 120° around a spanwise axis to form a bottom section and a top section, wherein a leading edge of the slat body is arranged between the bottom section and the top section, and wherein the spar extends from the bottom section to the top section, wherein a first portion of the back skin is attached to the spar at a distance to the bottom section, wherein a second portion of the back skin is attached to the top section, wherein the back skin is bent away from the spar and comprises a directly adjacent outlet portion that extends in a spanwise direction and directly faces the bottom section, wherein the front skin, the back skin and the spar enclose at least one air chamber (24, 34) that is in fluid communication with the air inlet, and wherein the outlet portion comprises a plurality of air outlets for letting air from the at least one air chamber (24, 34) exhaust through the air outlets. wherein the front skin is curved about at least 120° around a spanwise axis to form a bottom section and a top section, wherein a leading edge of the slat body is arranged between the bottom section and the top section, and wherein the spar extends from the bottom section to the top section, wherein a first portion of the back skin is attached to the spar at a distance to the bottom section, wherein a second portion of the back skin is attached to the top section, wherein the back skin is bent away from the spar and comprises a directly adjacent outlet portion that extends in a spanwise direction and directly faces the bottom section, wherein the front skin, the back skin and the spar enclose at least one air chamber (24, 34) that is in fluid communication with the air inlet, and wherein the outlet portion comprises a plurality of air outlets for letting air from the at least one air chamber (24, 34) exhaust through the air outlets.
A dissection prosthesis system comprising: a first prosthesis having a generally tubular shape, a radially compressed delivery configuration and a radially expanded deployed configuration, the first prosthesis comprising; a first stent ring; a second stent ring; a first graft material band connecting the first stent ring to the second stent ring; the first graft material band disposed between the first stent ring and the second stent ring; a third stent ring; and a second graft material band connecting the second stent ring to the third stent ring, the second graft material band disposed between the second stent ring and the third stent ring; wherein the second stent ring includes a plurality of openings to enable fluid flow from a lumen of the first prosthesis through the plurality of openings; and a second prosthesis having a generally tubular shape, a radially compressed delivery configuration and a radially expanded deployed configuration, the second prosthesis comprising a stent and a graft material coupled to the stent; and wherein the second prosthesis is configured to be disposed within the lumen of the first prosthesis. a first prosthesis having a generally tubular shape, a radially compressed delivery configuration and a radially expanded deployed configuration, the first prosthesis comprising; a first stent ring; a second stent ring; a first graft material band connecting the first stent ring to the second stent ring; the first graft material band disposed between the first stent ring and the second stent ring; a third stent ring; and a second graft material band connecting the second stent ring to the third stent ring, the second graft material band disposed between the second stent ring and the third stent ring; wherein the second stent ring includes a plurality of openings to enable fluid flow from a lumen of the first prosthesis through the plurality of openings; and a second prosthesis having a generally tubular shape, a radially compressed delivery configuration and a radially expanded deployed configuration, the second prosthesis comprising a stent and a graft material coupled to the stent; and wherein the second prosthesis is configured to be disposed within the lumen of the first prosthesis.
A chemical injection valve for use in a subterranean well, the chemical injection valve comprising: a tubular housing assembly; a valve stem reciprocably disposed relative to the housing assembly, the valve stem being displaceable relative to the housing assembly between closed and open positions, and flow from a first flow passage section to a second flow passage section being selectively prevented and permitted in the respective closed and open positions, in which the valve stem displaces to the open position in response to an increase in pressure in the first flow passage section to at least a predetermined level; a resilient primary seal that prevents flow through an annular gap between the valve stem and the housing assembly in the closed position of the valve stem; and a lateral bypass passage in communication with the annular gap and the second flow passage section in the closed position of the valve stem, and the bypass passage being in communication with the first flow passage section in the open position of the valve stem, characterised in that the chemical injection valve receives chemical treatment fluid via at least one inlet port formed radially through the housing assembly. a tubular housing assembly; a valve stem reciprocably disposed relative to the housing assembly, the valve stem being displaceable relative to the housing assembly between closed and open positions, and flow from a first flow passage section to a second flow passage section being selectively prevented and permitted in the respective closed and open positions, in which the valve stem displaces to the open position in response to an increase in pressure in the first flow passage section to at least a predetermined level; a resilient primary seal that prevents flow through an annular gap between the valve stem and the housing assembly in the closed position of the valve stem; and a lateral bypass passage in communication with the annular gap and the second flow passage section in the closed position of the valve stem, and the bypass passage being in communication with the first flow passage section in the open position of the valve stem, characterised in that the chemical injection valve receives chemical treatment fluid via at least one inlet port formed radially through the housing assembly.
A drying machine, comprising: a housing; an outer vessel supported in the housing; a drum configured to accommodate clothing; a heat pump device including a heat exchanger configured to dry the clothing in the drum; a blower configured to blow dry air; a circulatory ventilation flue connecting the outer vessel with the heat exchanger to define a circulation path through which the dry air from the blower circulates; a filter disposed in the circulatory ventilation flue and configured to prevent infiltration of dust components into the heat exchanger, and the heat exchanger includes a dehumidifier configured to absorb heat from the dry air with the refrigerant and a radiator configured to heat the dry air with the refrigerant, a recovery structure that is configured to recover a water component condensed at the dehumidifier and is disposed below the dehumidifier, wherein the filter, the heat exchanger and the blower are disposed in sequence along a flow direction of the dry air, the filter and the heat exchanger are disposed above the outer vessel formed in the housing, characterized in that at least one concave part is formed on the recovery structure. a housing; an outer vessel supported in the housing; a drum configured to accommodate clothing; a heat pump device including a heat exchanger configured to dry the clothing in the drum; a blower configured to blow dry air; a circulatory ventilation flue connecting the outer vessel with the heat exchanger to define a circulation path through which the dry air from the blower circulates; a filter disposed in the circulatory ventilation flue and configured to prevent infiltration of dust components into the heat exchanger, and the heat exchanger includes a dehumidifier configured to absorb heat from the dry air with the refrigerant and a radiator configured to heat the dry air with the refrigerant, a recovery structure that is configured to recover a water component condensed at the dehumidifier and is disposed below the dehumidifier, wherein the filter, the heat exchanger and the blower are disposed in sequence along a flow direction of the dry air, the filter and the heat exchanger are disposed above the outer vessel formed in the housing, characterized in that at least one concave part is formed on the recovery structure.
A shale shaker for separating solids from solids laden drilling fluid, the shale shaker comprising a base, a basket isolated from the base and a vibratory mechanism, the basket having a feed end, a solids discharge end and sides (105,106) therebetween, the basket comprising a scalping deck, an upper deck and a lower deck, the upper deck and lower deck having a feed end and a solids discharge end, the upper deck and lower deck at an uphill angle from the feed end to the discharge end, wherein a trough is arranged in the basket at said discharge end of said upper deck and a diverter plate for facilitating flow of solids discharged from the discharge end of the upper deck into said trough, the trough having a floor which slopes towards respective side openings (154, 154') of the trough.
Refrigerator, in particular domestic refrigerator, having a machine compartment and having components (13, 14, 15, 22, 34, 39, 40) in a refrigerant circuit, which are received in the machine compartment, wherein assembly sites (16, 18, 21; 34; 37, 38) for the components (13, 14, 15, 22, 34, 39, 40) are provided in the machine compartment, wherein at least one unoccupied assembly site (16, 18, 21; 34; 37, 38) is blocked by a component assembled in another assembly site (16, 18, 21; 34; 37, 38), characterised in that a wall of the machine compartment is clad with a wall panel (10; 11) upon which the assembly sites (16, 18, 21; 34; 37, 38) are formed.
A non-aqueous liquid foul release coating composition for controlling aqueous biofouling on man-made objects comprising: i) a moisture curable polysiloxane comprising repeating units of formula and at least one terminal or pendant group of formula wherein R 1 and R 2 are, independently, organic groups having 1 to 20 carbon atoms; R 3 and R 4 are, independently, organic groups having 1 to 20 carbon atoms; A is an organic group having 1 to 50 carbon groups; R 5 is, independently, selected from organic groups having 1 to 20 carbon atoms and groups of the formula O-R 6 wherein R 6 is an organic group having 1 to 20 carbon atoms, with the proviso that at least one R 5 is a group of the formula O-R 6; and ii) at least one of a marine biocide or a non-volatile component comprising units selected from hydrocarbyl, heterocarbyl, halocarbyl, ether, ester, amide, ketone, siloxane, urethane or urea groups. i) a moisture curable polysiloxane comprising repeating units of formula and at least one terminal or pendant group of formula wherein R 1 and R 2 are, independently, organic groups having 1 to 20 carbon atoms; R 3 and R 4 are, independently, organic groups having 1 to 20 carbon atoms; A is an organic group having 1 to 50 carbon groups; R 5 is, independently, selected from organic groups having 1 to 20 carbon atoms and groups of the formula O-R 6 wherein R 6 is an organic group having 1 to 20 carbon atoms, with the proviso that at least one R 5 is a group of the formula O-R 6; and ii) at least one of a marine biocide or a non-volatile component comprising units selected from hydrocarbyl, heterocarbyl, halocarbyl, ether, ester, amide, ketone, siloxane, urethane or urea groups.
A method of removing a wellbore isolation device comprising: introducing the isolation device into the wellbore, wherein the wellbore isolation device comprises: a first material forming a matrix of a portion of the isolation device; a second material, disposed within the first material, selected from the group consisting of a cathode of a galvanic system, a filler material, a strengthening material, an electrolytic compound, a buffering agent, and any combination thereof; and a coating, wherein the coating: (i) completely surrounds at least the first material prior to introduction of the isolation device into the wellbore; and (ii) comprises at least an anode of the galvanic system comprising the anode, a cathode, and an electrolyte, wherein the anode undergoes galvanic dissolution after introduction of the isolation device into the wellbore; and causing or allowing the first material to undergo a phase transformation in the wellbore. introducing the isolation device into the wellbore, wherein the wellbore isolation device comprises: a first material forming a matrix of a portion of the isolation device; a second material, disposed within the first material, selected from the group consisting of a cathode of a galvanic system, a filler material, a strengthening material, an electrolytic compound, a buffering agent, and any combination thereof; and a coating, wherein the coating: (i) completely surrounds at least the first material prior to introduction of the isolation device into the wellbore; and (ii) comprises at least an anode of the galvanic system comprising the anode, a cathode, and an electrolyte, wherein the anode undergoes galvanic dissolution after introduction of the isolation device into the wellbore; and a first material forming a matrix of a portion of the isolation device; a second material, disposed within the first material, selected from the group consisting of a cathode of a galvanic system, a filler material, a strengthening material, an electrolytic compound, a buffering agent, and any combination thereof; and a coating, wherein the coating: (i) completely surrounds at least the first material prior to introduction of the isolation device into the wellbore; and (ii) comprises at least an anode of the galvanic system comprising the anode, a cathode, and an electrolyte, wherein the anode undergoes galvanic dissolution after introduction of the isolation device into the wellbore; and (i) completely surrounds at least the first material prior to introduction of the isolation device into the wellbore; and (ii) comprises at least an anode of the galvanic system comprising the anode, a cathode, and an electrolyte, causing or allowing the first material to undergo a phase transformation in the wellbore.
A method of preparing a high-protein, acidified, liquid dairy product, comprising the steps of a) providing a liquid composition - comprising a total amount of whey protein of at least 4% (w/w) of which at least 30%(w/w) is in the form of insoluble particles of denatured whey protein, - having volume weighted mean particle diameter, D[4,3], of at most 50 micron, measured according to Example 1.1 - wherein at least 90% (w/w) of the total protein is whey protein, b) subjecting the liquid composition of step a) to at least one acidification step using an acidifying agent and to at least one heat-treatment step in any order, thereby obtaining an acidified heat-treated liquid composition, c) optionally, homogenizing the acidified heat-treated liquid composition, and d) optionally, packaging an acidified dairy product derived from the acidified, heat-treated liquid composition of step b) or step c), wherein Ca 2+ and Mg 2+ cations are present prior to step b and/or added during or after step b) in an amount sufficient to obtain a weight ratio between the total amount of protein and the total amount of Ca 2+ and Mg 2+ cations of at most 100 in the acidified, heat-treated, liquid composition and wherein the acidifying agent reduces pH of the liquid composition of step b) to a pH of at most 5.5. a) providing a liquid composition - comprising a total amount of whey protein of at least 4% (w/w) of which at least 30%(w/w) is in the form of insoluble particles of denatured whey protein, - having volume weighted mean particle diameter, D[4,3], of at most 50 micron, measured according to Example 1.1 - wherein at least 90% (w/w) of the total protein is whey protein, - comprising a total amount of whey protein of at least 4% (w/w) of which at least 30%(w/w) is in the form of insoluble particles of denatured whey protein, - having volume weighted mean particle diameter, D[4,3], of at most 50 micron, measured according to Example 1.1 - wherein at least 90% (w/w) of the total protein is whey protein, b) subjecting the liquid composition of step a) to at least one acidification step using an acidifying agent and to at least one heat-treatment step in any order, thereby obtaining an acidified heat-treated liquid composition, c) optionally, homogenizing the acidified heat-treated liquid composition, and d) optionally, packaging an acidified dairy product derived from the acidified, heat-treated liquid composition of step b) or step c),
A drone comprising: - a frame comprising an engagement portion, said engagement portion being a strip having a predetermined geometry; - a plurality of propulsion elements; said frame being configured, in use, for engaging each propulsion element in a removable way to said engagement portion at any point of said strip, in such a way to easily change the number and the arrangement of said propulsion elements present on said engagement portion, characterized in that said frame comprises actuating means arranged to automatically cause the sliding of said propulsion elements on said strip. - a frame comprising an engagement portion, said engagement portion being a strip having a predetermined geometry; - a plurality of propulsion elements;
A method for orienting a workpiece on an assembly line to prepare the workpiece for an operation, wherein the assembly line includes a tray in order to aid and support the workpiece from being transported from one station of an assembly line to another, wherein the tray is disposed on a mechanism for providing movement, said method comprising: positioning a flexible fixture, implemented on the tray, on the assembly line, wherein the flexible fixture has a base and at least one adjustable component being moveable relative to the base; positioning a workpiece on the flexible fixture; detecting a first orientation of the workpiece relative to the flexible fixture with a detection device and transmitting the detected first orientation from the detection device to a calibrator; determining a difference between the detected first orientation of the workpiece and a predetermined fixture orientation with the calibrator and transmitting instructions from the calibrator to the flexible fixture to move the workpiece from the detected first orientation to the predetermined fixture orientation with the at least one adjustable component of the flexible fixture based on the determined difference; and moving the workpiece with the at least one adjustable component from the detected first orientation to the predetermined fixture orientation and fixedly holding the workpiece in the predetermined fixture orientation with the adjustable component. positioning a flexible fixture, implemented on the tray, on the assembly line, wherein the flexible fixture has a base and at least one adjustable component being moveable relative to the base; positioning a workpiece on the flexible fixture; detecting a first orientation of the workpiece relative to the flexible fixture with a detection device and transmitting the detected first orientation from the detection device to a calibrator; determining a difference between the detected first orientation of the workpiece and a predetermined fixture orientation with the calibrator and transmitting instructions from the calibrator to the flexible fixture to move the workpiece from the detected first orientation to the predetermined fixture orientation with the at least one adjustable component of the flexible fixture based on the determined difference; and moving the workpiece with the at least one adjustable component from the detected first orientation to the predetermined fixture orientation and fixedly holding the workpiece in the predetermined fixture orientation with the adjustable component.