mhurhangee/ep-ind-claims huggingface dataset:
A dialysis device, comprising at least a first membrane and a second membrane, wherein: a first chamber formed by the first membrane is configured to receive a first fluid; a second chamber formed by the second membrane is configured to receive a second fluid; a third chamber formed in between a common housing, the first membrane and the second membrane is configured to receive a third fluid; and wherein the dialysis device is configured such that the first fluid flowing through the first membrane can be indirectly communicated with the second fluid flowing through the second membrane via the third fluid, characterized in that the first membrane and the second membrane each are a membrane formed by hollow fibers, wherein the first membrane and the second membrane as individual hollow fibers are disposed within the common housing so that the third fluid is filled between the individual hollow fibers. a first chamber formed by the first membrane is configured to receive a first fluid; a second chamber formed by the second membrane is configured to receive a second fluid; a third chamber formed in between a common housing, the first membrane and the second membrane is configured to receive a third fluid; and wherein the dialysis device is configured such that the first fluid flowing through the first membrane can be indirectly communicated with the second fluid flowing through the second membrane via the third fluid, characterized in that the first membrane and the second membrane each are a membrane formed by hollow fibers, wherein the first membrane and the second membrane as individual hollow fibers are disposed within the common housing so that the third fluid is filled between the individual hollow fibers.
An article having uniform grain size, produced by a process consisting essentially of, in sequence: heating a casting to a first temperature of 732°C (1350°F) for a first time period of approximately 12 hours, the casting being made from a spinodal alloy, wherein the as-cast spinodal alloy is a copper-nickel-tin alloy comprising from 8 to 20 wt% nickel and from 5 to 11 wt% tin, with the balance being copper; performing a first hot work reduction of the casting, wherein the first hot work reduction reduces the area of the casting by at least 30%; air cooling the casting to a first ambient temperature; heating the casting to a second temperature of 927°C (1700°F) for a second time period of from 16 hours to 48 hours; heating the casting to a third temperature of 954°C (1750°F) for a third time period of 4 hours; performing a second hot work reduction of the casting, wherein the second hot work reduction reduces the area of the casting by at least 30%; and air cooling the casting to a final ambient temperature to produce the article with uniform grain size; wherein the process does not include a homogenization step; and wherein the grain size is from 40 μm to 60 μm. heating a casting to a first temperature of 732°C (1350°F) for a first time period of approximately 12 hours, the casting being made from a spinodal alloy, wherein the as-cast spinodal alloy is a copper-nickel-tin alloy comprising from 8 to 20 wt% nickel and from 5 to 11 wt% tin, with the balance being copper; performing a first hot work reduction of the casting, wherein the first hot work reduction reduces the area of the casting by at least 30%; air cooling the casting to a first ambient temperature; heating the casting to a second temperature of 927°C (1700°F) for a second time period of from 16 hours to 48 hours; heating the casting to a third temperature of 954°C (1750°F) for a third time period of 4 hours; performing a second hot work reduction of the casting, wherein the second hot work reduction reduces the area of the casting by at least 30%; and air cooling the casting to a final ambient temperature to produce the article with uniform grain size; wherein the process does not include a homogenization step; and wherein the grain size is from 40 μm to 60 μm.
A blood reservoir comprising: a housing having a venous inlet and a vent inlet; a venous tube in fluid communication with the venous inlet; at least one vent tube in fluid communication with the vent inlet for directing blood to a blood-handling assembly that surrounds a portion of the venous tube; and the blood-handling assembly positioned within the housing and including a blood-collection chamber and a guide surface, the blood-collection chamber defining drainage holes for directing blood to the guide surface, the blood reservoir being characterized in that the guide surface defines an outer diameter, and wherein an outer diameter at a top of the guide surface near the blood collector is smaller than an outer diameter of the guide surface at a bottom of the guide surface. a housing having a venous inlet and a vent inlet; a venous tube in fluid communication with the venous inlet; at least one vent tube in fluid communication with the vent inlet for directing blood to a blood-handling assembly that surrounds a portion of the venous tube; and the blood-handling assembly positioned within the housing and including a blood-collection chamber and a guide surface, the blood-collection chamber defining drainage holes for directing blood to the guide surface, the blood reservoir being characterized in that the guide surface defines an outer diameter, and wherein an outer diameter at a top of the guide surface near the blood collector is smaller than an outer diameter of the guide surface at a bottom of the guide surface.
A heat diffuser for use with an electrically-operated aerosol-generating device, the heat diffuser being configured to be removably couplable to the aerosol-generating device and comprising a non-combustible porous body for absorbing heat from an electric heating element, wherein the porous body is thermally conductive such that, in use, air drawn through the porous body is heated by the heat absorbed by the porous body, and wherein the porous body has a surface area-to-volume ratio of at least 20 to 1.
Use of the isolated fraction of the STIM1 protein localized to the plasma membrane of the cells in a method for screening in vitro candidate molecules for treating chronic lymphatic leukaemia and/or systemic lupus erythematosus, wherein the cells are isolated entire cells.
A control assembly comprising: a lock assembly including a vent valve having a sensing sleeve and a sensing piston, said sensing sleeve defining a sensing chamber for receiving said sensing piston and defining a vent channel for venting fluid out of said sensing chamber; wherein said sensing piston is moveable within said sensing chamber between an open position and a closed position, said sensing piston allowing flow of said fluid into said vent channel during movement of said sensing piston between said open and closed positions; characterised in that said sensing piston is configured to restrict flow of said fluid into said vent channel in at least one of said open and closed positions. a lock assembly including a vent valve having a sensing sleeve and a sensing piston, said sensing sleeve defining a sensing chamber for receiving said sensing piston and defining a vent channel for venting fluid out of said sensing chamber; wherein said sensing piston is moveable within said sensing chamber between an open position and a closed position, said sensing piston allowing flow of said fluid into said vent channel during movement of said sensing piston between said open and closed positions; characterised in that said sensing piston is configured to restrict flow of said fluid into said vent channel in at least one of said open and closed positions.
A piston ring having a TiN coating having a thickness of 10 - 60 μm on a peripheral sliding surface, characterized in that a plane of TiN in the X-ray diffraction of a surface of said TiN coating has a maximum diffraction intensity, the texture coefficient of a plane of TiN is 1.1 - 1.8, larger than those of and planes of TiN, said texture coefficient being defined as Texture coefficient = I(hkl)/I 0 (hkl) [1/3(I /I 0 + I /I 0 + I /I 0)] -1, wherein I(hkl) represents an X-ray diffraction intensity of three types of, and planes, which is converted to a relative value with the maximum X-ray diffraction intensity measured as 100, and I 0 (hkl) represents a standard X-ray diffraction intensity of three types of, and planes described in JCPDS File No. 38-1420, i.e. 72 for I 0, 100 for I 0 and 45 for I 0; and said TiN coating is formed in a nitrogen atmosphere consisting of N 2 gas.
A processor-implemented method of determining a bias for an axis of a gyroscope, the method comprising: observing a temperature reading; maintaining a plurality of bias estimators (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h) for the axis, each bias estimator associated with a temperature and configured to estimate a bias at the associated temperature, the plurality of bias estimators including a number of short term bias estimators storing data for estimating biases for recently observed temperatures and a number of long term bias estimators storing data for estimating biases for temperatures observed over an earlier period of time; and determining a bias for the axis of the gyroscope based on the temperature reading and one or more of the bias estimators (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h); wherein maintaining a plurality of bias estimators (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h) for the axis comprises: storing the short term bias estimators in a least recently used cache; and determining that the temperature reading defines a temperature that does not have a bias estimator (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h) associated therewith and, in response, replacing one of the short term bias estimators with a new short term bias estimator associated with the temperature defined by the temperature reading. observing a temperature reading; maintaining a plurality of bias estimators (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h) for the axis, each bias estimator associated with a temperature and configured to estimate a bias at the associated temperature, the plurality of bias estimators including a number of short term bias estimators storing data for estimating biases for recently observed temperatures and a number of long term bias estimators storing data for estimating biases for temperatures observed over an earlier period of time; and determining a bias for the axis of the gyroscope based on the temperature reading and one or more of the bias estimators (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h); wherein maintaining a plurality of bias estimators (298a, 298b, 298c, 298d, 298e, 298f, 298g, 298h) for the axis comprises:
A mobile terminal comprising: a window (151a, 251a, 351a, 451a, 551a) disposed on a surface of a terminal body; a liquid crystal display, LCD, (151b, 251b, 351b, 451b, 551b) disposed on a rear surface of the window (151a, 251a, 351a, 451a, 551a) and configured to output visual information through the window (151a, 251a, 351a, 451a, 551a); a frame (101, 201, 301, 401, 501, 601, 701, 801) formed in a curved shape and including a window mounting portion (101a, 201a, 301a, 501a, 601a, 701a, 801a), on which the window (151a, 251a, 351a, 451a, 551a) is mounted and to which at least part of the window (151a, 251a, 351a, 451a, 551a) is coupled; and a reinforcing member (305, 405) disposed below a rear surface of the display (151b, 251b, 351b, 451b, 551b) and coupled to the frame to form a space (301") with the frame for accommodating the display (151b, 251b, 351b, 451b, 551b), the reinforcing member (305, 405) being configured to reinforce rigidity of the frame (301, 401), and, wherein: - the frame (101, 201, 301, 401, 501, 601, 701, 801) is configured to apply a bending force to conform the window (151a, 251a, 351a, 451a, 551a) to the curved shape of the frame (101, 201, 301, 401, 501, 601, 701, 801), - the frame (101, 201, 301, 401, 501, 601, 701, 801) is formed to enclose the window (151a, 251a, 351a, 451a, 551a), - the reinforcing member (305, 405) is formed of a metal and integrally formed with the frame (101, 201, 301, 401, 501, 601, 701, 801), and - the frame (101, 201, 301, 401, 501, 601, 701, 801) is formed of a synthetic resin. a window (151a, 251a, 351a, 451a, 551a) disposed on a surface of a terminal body; a liquid crystal display, LCD, (151b, 251b, 351b, 451b, 551b) disposed on a rear surface of the window (151a, 251a, 351a, 451a, 551a) and configured to output visual information through the window (151a, 251a, 351a, 451a, 551a); a frame (101, 201, 301, 401, 501, 601, 701, 801) formed in a curved shape and including a window mounting portion (101a, 201a, 301a, 501a, 601a, 701a, 801a), on which the window (151a, 251a, 351a, 451a, 551a) is mounted and to which at least part of the window (151a, 251a, 351a, 451a, 551a) is coupled; and a reinforcing member (305, 405) disposed below a rear surface of the display (151b, 251b, 351b, 451b, 551b) and coupled to the frame to form a space (301") with the frame for accommodating the display (151b, 251b, 351b, 451b, 551b), the reinforcing member (305, 405) being configured to reinforce rigidity of the frame (301, 401), and, - the frame (101, 201, 301, 401, 501, 601, 701, 801) is configured to apply a bending force to conform the window (151a, 251a, 351a, 451a, 551a) to the curved shape of the frame (101, 201, 301, 401, 501, 601, 701, 801), - the frame (101, 201, 301, 401, 501, 601, 701, 801) is formed to enclose the window (151a, 251a, 351a, 451a, 551a), - the reinforcing member (305, 405) is formed of a metal and integrally formed with the frame (101, 201, 301, 401, 501, 601, 701, 801), and - the frame (101, 201, 301, 401, 501, 601, 701, 801) is formed of a synthetic resin.
A centrifugal impeller for a turbomachine comprising a plurality of blades which form between them a plurality of aerodynamic vanes; the aerodynamic vanes being the empty spaces between adjacent blades, and through which vanes a working fluid passes during use of the impeller; the aerodynamic vanes each further comprising first and second walls (13S, 13I) between adjacent blades, each of the vanes having internal walls comprising the lateral walls of said blades, and said first and second walls (13S, 13I), and on each of which internal walls is associated a first fabric element; and wherein a second fabric element is configured to surround alternately a first wall of a vane and a second wall of an adjacent vane passing along the respective blade therebetween; the fabric comprising fibrous structures woven into a pattern, or an assembly of layers; and said fabric elements (1A; 1B) being impregnated with a filling material.
A bypass turbine engine for an aircraft, said turbine engine comprising: - a hollow nacelle of longitudinal axis (L-L) provided, at the front, with an air inlet and, at the rear, with an air outlet; - a central hot-stream generator, positioned axially in said nacelle; - a fan positioned axially in said nacelle forward of said central generator and able to generate the cold stream for said turbine engine; - an outer fairing borne internally by said nacelle and an inner fairing surrounding said central generator, said outer and inner fairings between them delimiting a fan duct of annular cross section for said cold stream; and - a precooler comprising an inlet for a current of hot air bled from said central generator and an outlet for a current of hot air cooled using said cold stream, characterized in that said precooler is positioned inside at least a portion of said rear part of the inner fairing around said longitudinal axis (L-L) and in thermal contact with said rear part of the inner fairing so as to be cooled by said cold stream blown onto said rear part of the inner fairing. - a hollow nacelle of longitudinal axis (L-L) provided, at the front, with an air inlet and, at the rear, with an air outlet; - a central hot-stream generator, positioned axially in said nacelle; - a fan positioned axially in said nacelle forward of said central generator and able to generate the cold stream for said turbine engine; - an outer fairing borne internally by said nacelle and an inner fairing surrounding said central generator, said outer and inner fairings between them delimiting a fan duct of annular cross section for said cold stream; and - a precooler comprising an inlet for a current of hot air bled from said central generator and an outlet for a current of hot air cooled using said cold stream,
Securing device for an anchor rail having a T-head bolt and a retaining plate which is fixed to the T-head bolt and has a plurality of teeth for engagement with a toothing on the anchor rail, and an opening through which a threaded bolt of the T-head bolt is passed, wherein at least one latching web projecting into the opening of the retaining plate is provided on the retaining plate, by means of which the retaining plate can be latched to the threaded bolt of the T-head bolt, wherein the at least one latching web is integrally formed with a plate-shaped latching element with an opening for passing through the threaded bolt of the T-head bolt, characterized in that the retaining plate has teeth on opposite sides which are at least partially covered by a projection of the latching element.
An optical device (100; 200; 300; 400) to perform nonlinear optical processes, the optical device comprises a nonlinear optical medium (107; 206; 307; 407) having an entrance surface and an exit surface, and an angular dispersive element (105; 205; 306; 405) in direct optical coupling with the nonlinear optical medium (107; 206; 307; 407) with no imaging optics inserted between the nonlinear optical medium (107; 206; 307; 407) and the angular dispersive element (105; 205; 306; 405), characterized in that the angular dispersive element (105; 205; 306; 405) directs each frequency component of a broadband incident light beam (102; 202; 302; 402) into its respective phase matching direction within the nonlinear medium (107; 206; 307; 407).
A spherical bearing comprising a metal first bearing element made of steel, which is coated at least in part by means of a coating, and a metal second bearing element made of steel, which is coated with a PTFE-containing sliding lining, wherein the coating and the sliding lining are in sliding contact, and wherein the coating comprises at least one first layer deposited on the first bearing element by means of a PVD, CVD or PECVD method; characterised in that the coating further comprises at least one further layer arranged on the at least one first layer and facing away from the first bearing element, wherein the at least one further layer, which adjoins the at least one first layer, which is arranged facing away from the first bearing element, forms a second layer, which differs in respect of its composition from the adjoining first layer and is formed by means of a PVD, CVD or PECVD method, a) the first layer is formed from chromium and the second layer is formed from chromium nitride, or b) a first layer is formed from chromium, a further first layer is formed from tungsten carbide, and the second layer is a hydrogen-containing tungsten-doped amorphous carbon layer of the type a-C:H:W, or c) the first layer adjoining the second layer is formed from molybdenum nitride and the second layer is formed from copper, or d) the first layer is a silicon-doped amorphous carbon layer of the type a-C:H: Si and the second layer is an amorphous carbon layer of the type a-C:H or an amorphous carbon layer of the type a-C:H:Si with different silicon doping. a metal first bearing element made of steel, which is coated at least in part by means of a coating, and a metal second bearing element made of steel, which is coated with a PTFE-containing sliding lining, wherein the coating and the sliding lining are in sliding contact, and wherein the coating comprises at least one first layer deposited on the first bearing element by means of a PVD, CVD or PECVD method; characterised in that the coating further comprises at least one further layer arranged on the at least one first layer and facing away from the first bearing element, wherein the at least one further layer, which adjoins the at least one first layer, which is arranged facing away from the first bearing element, forms a second layer, which differs in respect of its composition from the adjoining first layer and is formed by means of a PVD, CVD or PECVD method, a) the first layer is formed from chromium and the second layer is formed from chromium nitride, or b) a first layer is formed from chromium, a further first layer is formed from tungsten carbide, and the second layer is a hydrogen-containing tungsten-doped amorphous carbon layer of the type a-C:H:W, or c) the first layer adjoining the second layer is formed from molybdenum nitride and the second layer is formed from copper, or d) the first layer is a silicon-doped amorphous carbon layer of the type a-C:H: Si and the second layer is an amorphous carbon layer of the type a-C:H or an amorphous carbon layer of the type a-C:H:Si with different silicon doping.
A cooking oven including a swing oven door and a closure system (10, 12) for said swing oven door, wherein - the closure system comprises a hook element attached at the cooking oven, - the closure system comprises a hook seat element attached at the cooking oven, - the hook seat element includes an opening for receiving a hook projecting from the hook element, - the hook element and the hook seat element are detachably connectable by a latching mechanism, - the hook element is attached at an oven frame of an oven chassis, and - the hook seat element is attached at a door frame of an oven door of the cooking oven, characterized in, that the hook seat element is inserted in a recess of the door frame, so that the hook seat element forms an integrated part of the door frame, wherein the cross sections of the hook seat element and the door frame have at least partially the same shape. - the closure system comprises a hook element attached at the cooking oven, - the closure system comprises a hook seat element attached at the cooking oven, - the hook seat element includes an opening for receiving a hook projecting from the hook element, - the hook element and the hook seat element are detachably connectable by a latching mechanism, - the hook element is attached at an oven frame of an oven chassis, and - the hook seat element is attached at a door frame of an oven door of the cooking oven, characterized in, that the hook seat element is inserted in a recess of the door frame, so that the hook seat element forms an integrated part of the door frame, wherein the cross sections of the hook seat element and the door frame have at least partially the same shape.