mhurhangee/ep-ind-claims huggingface dataset:
A fuel cell anode catalyst in which a platinum and ruthenium alloy is supported on a carbon material, such that the molar ratio of platinum to ruthenium (Pt:Ru) in the alloy falls within a range of from 1:1 to 1:5; when the numbers of Pt atom coordination sites and the number of Ru atom coordination sites of the atom sites in the alloy, as measured by means of the X-ray absorption fine structure, are denoted as N(Pt) and N(Ru), respectively, N(Ru)/(N(Pt)+N(Ru)) at platinum sites falls within a range of 0.8 to 1.1 times the theoretical value, and N(Pt)/(N(Ru)+N(Pt)) at Ru sites falls within a range of 0.8 to 1.1 times the theoretical value; the average particle diameter of the alloy falls within a range of 1 to 5 nm; and the standard deviation in the particle diameter falls within a range of 2 nm and below.
A fungicidal composition containing a carboxylic acid amide derivative of the formula or a salt thereof as an active ingredient: wherein A is phenyl which may be substituted by X, benzodioxolanyl which may be substituted by X, or benzodioxanyl which may be substituted by X; B is 2- or 3-pyridyl which may be substituted by halogen, alkyl, haloalkyl, alkoxy or haloalkoxy; each of R 1 and R 2 is alkyl, or R 1 and R 2 may together form a 3- to 6-membered saturated carbon ring; X is halogen, alkyl, haloalkyl, alkenyl, haloalkenyl, alkynyl, haloalkynyl, hydroxy, alkoxy, haloalkoxy, alkenyloxy, haloalkenyloxy, alkynyloxy, haloalkynyloxy, cycloalkyloxy, alkylthio, haloalkylthio, alkenylthio, haloalkenylthio, alkynylthio, haloalkynylthio, alkylsulfonyloxy, haloalkylsulfonyloxy, alkoxyalkoxy, haloalkoxyalkoxy, alkoxyhaloalkoxy, haloalkoxyhaloalkoxy, alkoxyalkyl, haloalkoxyalkyl, alkylthioalkyl, haloalkylthioalkyl, phenyl which may be substituted by Y, phenoxy which may be substituted by Y, benzyloxy which may be substituted Y, pyridyl which may be substituted by Y, or pyridyloxy which may be substituted by Y; and Y is halogen, alkyl, haloalkyl, alkenyl, haloalkenyl, alkynyl, haloalkynyl, alkoxy or haloalkoxy, provided that when B is 3-pyridyl which may be substituted, A is phenyl which is substituted by at least two X (such a plurality of X may be the same or different).
A drum comprising: - a sound box; - a counter-disk structurally separated from said sound box; - at least one releasable securing bracket of said counter-disk to said sound box; and - tensioning means configured to secure a batter head to said counter-disk by tensioning said batter head. and characterized in that - said counter-disk comprises a plurality of mutually securable modules; - wherein said module comprises bases each of which is configured to engage said tensioning means and said at least one releasable securing bracket and connections configured to secure each of said bases between two adjoining of said bases. - a sound box; - a counter-disk structurally separated from said sound box; - at least one releasable securing bracket of said counter-disk to said sound box; and - tensioning means configured to secure a batter head to said counter-disk by tensioning said batter head. - said counter-disk comprises a plurality of mutually securable modules; - wherein said module comprises bases each of which is configured to engage said tensioning means and said at least one releasable securing bracket and connections configured to secure each of said bases between two adjoining of said bases.
A pharmaceutical composition comprising liposomes composed of non-charged vesicle-forming lipids, optionally including not more than 10 mole percent of negatively charged vesicle- forming lipids and/or not more than 10 mole percent of PEGylated lipids, the liposomes having a selected mean particle diameter in the size range of 40-200 nm and comprising a first corticosteroid in water soluble form, for use in a method for the treatment of an inflammatory disorder in a human at a dose of at most 5 mg/kg body weight of prednisolone or an equipotent dose of a corticosteroid other than prednisolone, wherein said composition is administered intravenously and wherein said treatment has a treatment frequency of at most once per two weeks and a long lasting therapeutic effect of two weeks or longer.
Hub of intermediate casing for aircraft turbojet engine, comprising: - an inner annular shroud that will firstly delimit the exterior of a core engine flow space of a core engine gas flow in the turbojet engine, and secondly on the interior, the upstream part at least one inter-flow area, the inner annular shroud being provided with at least one primary air passage orifice, - an outer annular shroud that will firstly delimit the interior of a fan flow space of a fan gas flow in the turbojet engine, and secondly the exterior of said at least one inter-flow area, the outer annular shroud being provided with at least one secondary air passage orifice, - at least one variable bleed valve, comprising at least one mobile gate capable of drawing off air circulating in the core engine flow space through said at least one primary orifice and sending air thus drawn off to said at least one inter-flow area towards at least one corresponding discharge inlet orifice of at least one outlet pipe of the hub of the intermediate case shaped to allow an air passage from said at least one discharge inlet orifice to said at least one secondary orifice to send air drawn off through said at last one variable bleed valve into the fan flow space, said at least one outlet pipe being fixed to the outer annular shroud at said at least one secondary orifice, characterised in that at least one gasket for sealing against air and fire is installed between said at least one outlet pipe and the outer annular shroud, and in that said at least one outlet pipe is made of a composite material and comprises a draped composite wall (30a, 30b) composed of a plurality of plies impregnated with resin. - an inner annular shroud that will firstly delimit the exterior of a core engine flow space of a core engine gas flow in the turbojet engine, and secondly on the interior, the upstream part at least one inter-flow area, the inner annular shroud being provided with at least one primary air passage orifice, - an outer annular shroud that will firstly delimit the interior of a fan flow space of a fan gas flow in the turbojet engine, and secondly the exterior of said at least one inter-flow area, the outer annular shroud being provided with at least one secondary air passage orifice, - at least one variable bleed valve, comprising at least one mobile gate capable of drawing off air circulating in the core engine flow space through said at least one primary orifice and sending air thus drawn off to said at least one inter-flow area towards at least one corresponding discharge inlet orifice of at least one outlet pipe of the hub of the intermediate case shaped to allow an air passage from said at least one discharge inlet orifice to said at least one secondary orifice to send air drawn off through said at last one variable bleed valve into the fan flow space,
Modular soundproof cabin comprising a perimeter wall having perimeter panels (21, 22, 23, 24, 25), an upper ceiling having ceiling panels and a lower floor having floor panels, where the panels (3a, 4a, 21, 22, 23, 24, 25) have acoustic insulation properties, where the perimeter panels (21, 22, 23, 24, 25) comprise frames on their inner side, comprising intermediate horizontal struts provided between horizontal lines (90, 91) of perimeter panels (21, 22, 23, 24, 25), and end horizontal struts provided between the perimeter wall and the upper ceiling and lower floor; comprising mechanical fixation means, at least, between the frames and the horizontal struts (6, 7), and between the ceiling panels and the floor panels and the end horizontal struts, characterized in that: the horizontal struts (6, 7) are divided into segments (6a, 7a) that comprise end dovetails, where each segment (6a, 7a) overlaps, at least, a connection between horizontally adjacent perimeter panels (21, 22, 23, 24, 25), further comprising vertical struts for being laterally inserted straight between the perimeter panels (21, 22, 23, 24, 25), where the vertical struts comprise a solid inner square portion and an outer soundproof portion which is recessed with respect to the lateral edges of the square portion, where the outer soundproof portion projects up and down from the inner square portion enough length for overlapping the horizontal struts (6, 7), and where the perimeter panels (21, 22, 23, 24, 25) project from the frames enough length for overlapping the horizontal struts (6, 7) and/or the solid inner square portion. the horizontal struts (6, 7) are divided into segments (6a, 7a) that comprise end dovetails, where each segment (6a, 7a) overlaps, at least, a connection between horizontally adjacent perimeter panels (21, 22, 23, 24, 25), further comprising vertical struts for being laterally inserted straight between the perimeter panels (21, 22, 23, 24, 25), where the vertical struts comprise a solid inner square portion and an outer soundproof portion which is recessed with respect to the lateral edges of the square portion, where the outer soundproof portion projects up and down from the inner square portion enough length for overlapping the horizontal struts (6, 7), and where the perimeter panels (21, 22, 23, 24, 25) project from the frames enough length for overlapping the horizontal struts (6, 7) and/or the solid inner square portion.
A seat tube assembly for bicycle, the seat tube assembly comprising: a seat tube; a seat post, being telescoped and an axially movable in the seat tube; a regulating valve, having a valve seat and a valve stem, wherein the valve seat is fixed in the seat post and the valve stem is received in the seat tube so that an upper end thereof is inserted and axially movable in the valve seat; and a controlling component, having a trigger lever, a driving arm, an auxiliary pusher, a cable, and a control switch; the trigger lever abutting against a lower end of the valve stem of the regulating valve, one end of the auxiliary pusher being pivotally connected to the trigger lever, one end of the cable being connected to an end of the driving arm, and an opposite end of the cable being connected to the control switch; characterized in that: the opposite end of the driving arm is pivotally connected to the trigger lever. a seat tube; a seat post, being telescoped and an axially movable in the seat tube; a regulating valve, having a valve seat and a valve stem, wherein the valve seat is fixed in the seat post and the valve stem is received in the seat tube so that an upper end thereof is inserted and axially movable in the valve seat; and a controlling component, having a trigger lever, a driving arm, an auxiliary pusher, a cable, and a control switch; the trigger lever abutting against a lower end of the valve stem of the regulating valve, one end of the auxiliary pusher being pivotally connected to the trigger lever, one end of the cable being connected to an end of the driving arm, and an opposite end of the cable being connected to the control switch; characterized in that: the opposite end of the driving arm is pivotally connected to the trigger lever. the opposite end of the driving arm is pivotally connected to the trigger lever.
A method for recharging batteries (12A, 12B, 12C), wherein: a first energy converter (100A, 100B, 100C) is used to recharge a first battery (12A, 12B, 12C); and the first energy converter (100A, 100B, 100C) is bypassed in order to recharge from the first battery (12A, 12B, 12C), one or more second batteries (12A, 12B, 12C), the first battery being intended to be mounted on a first vehicle and each second battery (12B, 12C) being intended to be mounted on a second vehicle (1B, 1C). a first energy converter (100A, 100B, 100C) is used to recharge a first battery (12A, 12B, 12C); and the first energy converter (100A, 100B, 100C) is bypassed in order to recharge from the first battery (12A, 12B, 12C), one or more second batteries (12A, 12B, 12C), the first battery being intended to be mounted on a first vehicle and each second battery (12B, 12C) being intended to be mounted on a second vehicle (1B, 1C).
A device, comprising: a holder mountable to a manipulator; a processing machine with a tool; a linear actuator coupled to the processing machine for adjusting a relative position of the tool relative to the holder; characterized by a maintenance unit having a bracket pivotally mounted to the holder such that the maintenance unit can be positioned at least partially in front of the tool by pivoting the bracket. a holder mountable to a manipulator; a processing machine with a tool; a linear actuator coupled to the processing machine for adjusting a relative position of the tool relative to the holder; characterized by a maintenance unit having a bracket pivotally mounted to the holder such that the maintenance unit can be positioned at least partially in front of the tool by pivoting the bracket.
A quenching chamber for a circuit interrupter comprising a space, and at least two walls at least partially enclosing the space and positioned on opposite sides of the space, wherein the quenching chamber is configured to comprise, in the space, a switch having a fixed contact and a movable contact, between which contacts (2, 3) an arc can be generated, each wall of the quenching chamber comprises one or more levels (a) of wall units, whereby the wall unit within one level (a) extend over a width (w) of the wall along a first axis (x) and extend along a part or whole length of the wall along a second axis (y) being perpendicular to the first axis, and whereby each wall unit comprises quenching material, and characterised in that the wall units on opposite sides of the space within the same level (a) comprise quenching material having different quenching capabilities.
An undercutting tool for producing a blind hole in flowable, curable batch mixtures, comprising - a connecting piece for connecting the undercutting tool with a mould, - a plug supported in the connecting piece so as to be slideable along an operating direction, - a cap that covers the plug in the operating direction; - a jacket that consists of a material reversibly deformable under pressure and completely encloses the plug on the outside between the connecting piece and the cup, - the jacket being provided with at least one cavity that surrounds the plug and has a defined geometry, - with the geometry of the cavity being specified in such a way that the jacket, when under pressure exerted along the operating direction, locally bulges out in the region of the cavity, whereby a blind hole can be formed in the batch mixture surrounding the jacket, the said blind hole having a shape corresponding to the jacket in its bulged-out state. - a connecting piece for connecting the undercutting tool with a mould, - a plug supported in the connecting piece so as to be slideable along an operating direction, - a cap that covers the plug in the operating direction; - a jacket that consists of a material reversibly deformable under pressure and completely encloses the plug on the outside between the connecting piece and the cup, - the jacket being provided with at least one cavity that surrounds the plug and has a defined geometry, - with the geometry of the cavity being specified in such a way that the jacket, when under pressure exerted along the operating direction, locally bulges out in the region of the cavity, whereby a blind hole can be formed in the batch mixture surrounding the jacket, the said blind hole having a shape corresponding to the jacket in its bulged-out state.
A disposal system comprising: a shredder that shreds input material to produce shredded material; a carbonization furnace that combusts the shredded material from the shredder to generate combustion exhaust gas and carbonized matter; and a gasification furnace that places the carbonized matter generated in the carbonization furnace and water vapor in contact with each other while heating with the combustion exhaust gas generated in the carbonization furnace so as to react to generate combustible generated gas. a shredder that shreds input material to produce shredded material; a carbonization furnace that combusts the shredded material from the shredder to generate combustion exhaust gas and carbonized matter; and a gasification furnace that places the carbonized matter generated in the carbonization furnace and water vapor in contact with each other while heating with the combustion exhaust gas generated in the carbonization furnace so as to react to generate combustible generated gas.
A structure, comprising: a first body formed from a first material; and a second body disposed on or embedded within the first body; the second body comprising a shape memory alloy configured to exert a first stress to the first body in at least one first state and a second stress to the first body in at least one second state, wherein the shape memory alloy is configured to transition between the first and second state as a function of an applied activation energy, wherein the second stress is greater than the first stress; characterized in that the structure is a landing gear strut, and the second body is formed within a lug of the landing gear strut at a maximum stress location to provide stress relief to prevent cracking of the lug. a first body formed from a first material; and a second body disposed on or embedded within the first body; the second body comprising a shape memory alloy configured to exert a first stress to the first body in at least one first state and a second stress to the first body in at least one second state, wherein the shape memory alloy is configured to transition between the first and second state as a function of an applied activation energy, wherein the second stress is greater than the first stress; characterized in that the structure is a landing gear strut, and the second body is formed within a lug of the landing gear strut at a maximum stress location to provide stress relief to prevent cracking of the lug.
An interlayer film for laminated glass, comprising a polyvinyl acetal resin and a second resin component with a glass transition temperature higher than or equal to -15°C and lower than or equal to 5°C; and the content of the polyvinyl acetal resin being greater than or equal to 10% by weight and less than or equal to 50% by weight and the content of the second resin component being greater than or equal to 50% by weight and less than or equal to 90% by weight, in 100% by weight of the total of the polyvinyl acetal resin and the second resin component, and the polyvinyl acetal resin and the second resin component forming a sea-island structure in the interlayer film.
A gas storage system, comprising: a first flow path configured to be in pneumatic communication with a port of a vessel; a first burst disc disposed in the first flow path such that the gas flow in the first flow path is prevented by the first burst disc, and the first burst disc configured to permit gas flow at a first burst pressure; a second flow path in pneumatic communication with the first flow path, downstream from the first burst disc with respect to the gas flow; and a second burst disc disposed in the second flow path such that gas flow in the second flow path is prevented by the second burst disc, the second burst disc configured to permit gas flow at a second burst pressure, wherein the second burst pressure is less than the first burst pressure. a first flow path configured to be in pneumatic communication with a port of a vessel; a first burst disc disposed in the first flow path such that the gas flow in the first flow path is prevented by the first burst disc, and the first burst disc configured to permit gas flow at a first burst pressure; a second flow path in pneumatic communication with the first flow path, downstream from the first burst disc with respect to the gas flow; and a second burst disc disposed in the second flow path such that gas flow in the second flow path is prevented by the second burst disc, the second burst disc configured to permit gas flow at a second burst pressure, wherein the second burst pressure is less than the first burst pressure.
Internal combustion engine, preferably for a motor vehicle, comprising - at least one cylinder, which encloses a combustion chamber and in which a piston capable of stroking displacement is located, - at least one injector per cylinder for injecting fuel into the combustion chamber, the respective injector having a plurality of injection ports (9, 10), through which the fuel is discharged from the injector and enters the combustion chamber in the respective injection process, - wherein the respective injector comprises in a first port plane extending transversely to its longitudinal central axis a first row of ports with a plurality of first injection ports and in a second port plane extending transversely to its longitudinal central axis a second row of ports with a plurality of second injection ports, characterised in that the first injection ports and the second injection ports are arranged relative to one another in such a way that, during an injection process, first injection jets of the first injection ports reach the piston substantially without contact with second injection jets of the second injection ports, and in that the respective piston has on the side facing the combustion chamber a piston trough with a trough contour having a deflection geometry for the second injection jets which deflects the second injection jets towards the first injection jets, and in that the trough contour for the first injection jets has a jet splitter geometry which splits the first injection jets into first sub-jets and second sub-jets, wherein the first sub-jets are deflected into a region facing the second injection jets and the second sub-jets are deflected into a region remote from the second injection jets, and wherein the trough contour has a further deflection contour which deflects the first sub-jets towards the first injection jets. - at least one cylinder, which encloses a combustion chamber and in which a piston capable of stroking displacement is located, - at least one injector per cylinder for injecting fuel into the combustion chamber, the respective injector having a plurality of injection ports (9, 10), through which the fuel is discharged from the injector and enters the combustion chamber in the respective injection process, - wherein the respective injector comprises in a first port plane extending transversely to its longitudinal central axis a first row of ports with a plurality of first injection ports and in a second port plane extending transversely to its longitudinal central axis a second row of ports with a plurality of second injection ports,
A single piece sheath for a fan airfoil, for a gas turbine engine, having a leading edge, a trailing edge, a tip, a root, a suction side and a pressure side, the single piece sheath comprising: a solid portion to wrap around the airfoil to cover all of the leading edge and the airfoil tip; and means for securing the solid portion to the airfoil. a solid portion to wrap around the airfoil to cover all of the leading edge and the airfoil tip; and means for securing the solid portion to the airfoil.