mhurhangee/ep-ind-claims huggingface dataset:
A fastening tool comprising: a housing; a nosepiece assembly carried by the housing, the nosepiece assembly including a nose portion having first end adjacent to the housing and a second end opposite to the housing, a pair of hooks integrally formed on the nose portion, a door arranged opposite the nose portion and a fastener drive track disposed therebetween; a magazine for feeding fasteners successively to the fastener drive track of the nosepiece assembly; an engine carried by the housing and configured to drive a fastener out of the fastener drive track and into a workpiece during a drive stroke; and characterised by a latch mechanism arranged to cover the nosepiece assembly, the latch mechanism including: a latch cover; a latch plate disposed between the latch cover and the door; and a latch member connecting the latch plate to the latch cover. a housing; a nosepiece assembly carried by the housing, the nosepiece assembly including a nose portion having first end adjacent to the housing and a second end opposite to the housing, a pair of hooks integrally formed on the nose portion, a door arranged opposite the nose portion and a fastener drive track disposed therebetween; a magazine for feeding fasteners successively to the fastener drive track of the nosepiece assembly; an engine carried by the housing and configured to drive a fastener out of the fastener drive track and into a workpiece during a drive stroke; and characterised by a latch mechanism arranged to cover the nosepiece assembly, the latch mechanism including: a latch cover; a latch plate disposed between the latch cover and the door; and a latch member connecting the latch plate to the latch cover. a latch cover; a latch plate disposed between the latch cover and the door; and a latch member connecting the latch plate to the latch cover.
Pendulum damping device comprising: - a support that is rotatable about an axis, - at least one pendulum body that is movable with respect to the support, and - stabilizing members for this pendulum body, each stabilizing member making it possible to connect this pendulum body to another pendulum body or to the support, and each stabilizing member exerting a force on a circumferential end (7, 8) of this pendulum body, each stabilizing member being movable such that the angle (α, β), defined from the centre of gravity of this stabilizing member, between: - the orthoradial direction at this centre of gravity and - the direction of the force that this stabilizing member exerts on the circumferential end (7, 8) of the pendulum body can vary during the movement of the pendulum body with respect to the support, characterized in that each stabilizing member comprises at least one weight connected by a wire to a circumferential end (7, 8) of the pendulum body and to the opposing circumferential end (8, 7) of a circumferentially adjacent pendulum body or to the support, or in that each stabilizing member is formed by at least one roller, the outer contour of which rolls over all or part of the circumferential end (7, 8) of the pendulum body and over all or part of the opposing circumferential end (8, 7) of a circumferentially adjacent pendulum body or over the support. - a support that is rotatable about an axis, - at least one pendulum body that is movable with respect to the support, and - stabilizing members for this pendulum body, each stabilizing member making it possible to connect this pendulum body to another pendulum body or to the support, and each stabilizing member exerting a force on a circumferential end (7, 8) of this pendulum body, - the orthoradial direction at this centre of gravity and - the direction of the force that this stabilizing member exerts on the circumferential end (7, 8) of the pendulum body can vary during the movement of the pendulum body with respect to the support,
A surgical stapler comprising: a first jaw including an anvil; a second jaw including a cartridge including a plurality of staples and a corresponding set of staple pushers situated in a plurality of staple pockets, the staple pushers being actuatable to eject the staples from the staple pockets through interaction with a set of fins on a slider moving longitudinally within the cartridge, the first jaw movable towards and away from the second jaw; characterised by a cartridge lift disposed between the second jaw and the cartridge, the lift arranged to move the cartridge towards the first jaw in a direction transverse to a longitudinal direction while the lift is movable in the longitudinal direction. a first jaw including an anvil; a second jaw including a cartridge including a plurality of staples and a corresponding set of staple pushers situated in a plurality of staple pockets, the staple pushers being actuatable to eject the staples from the staple pockets through interaction with a set of fins on a slider moving longitudinally within the cartridge, the first jaw movable towards and away from the second jaw; characterised by a cartridge lift disposed between the second jaw and the cartridge, the lift arranged to move the cartridge towards the first jaw in a direction transverse to a longitudinal direction while the lift is movable in the longitudinal direction.
A rear nacelle assembly for a turbojet engine comprising at least one thrust reverser device adapted to redirect an air flow circulating from upstream to downstream in a flow path of the turbojet engine and a mast designed to connect the nacelle on the structure of the aircraft, the nacelle extending longitudinally from front to back along an axis, the thrust reverser device comprising at least: - a cowl which is movably mounted in longitudinal translation from front to back in a direction substantially parallel to the axis of the nacelle, between a closed position in which the cowl ensures the aerodynamic continuity of the nacelle, and an open position in which the cowl opens a passage in the nacelle, - at least one sliding thrust reverser cascade which is driven by the movable cowl between a retracted position between a fan casing and an outer envelope of the nacelle, corresponding to the closed position of the cowl, and a thrust reversal position corresponding to the open position of the cowl, position in which the sliding cascade is displaced downstream so as to be able to extend through said passage opened by the cowl, and - cradle which is fastened on the mast and which includes a first spar and a second spar extending generally longitudinally on either side of the mast, said spars each carrying means (40a, 40b, 44a, 44b) for slidably guiding the movable cowl and the sliding cascade, characterized in that a rear portion of the cradle includes a first front fastening means on the mast and a second rear fastening means on the mast, said fastening means being spaced longitudinally, and in that the cradle includes a front portion, forming a suspension, which extends longitudinally cantilevered beyond said fastening means (60, 62). - a cowl which is movably mounted in longitudinal translation from front to back in a direction substantially parallel to the axis of the nacelle, between a closed position in which the cowl ensures the aerodynamic continuity of the nacelle, and an open position in which the cowl opens a passage in the nacelle, - at least one sliding thrust reverser cascade which is driven by the movable cowl between a retracted position between a fan casing and an outer envelope of the nacelle, corresponding to the closed position of the cowl, and a thrust reversal position corresponding to the open position of the cowl, position in which the sliding cascade is displaced downstream so as to be able to extend through said passage opened by the cowl, and - cradle which is fastened on the mast and which includes a first spar and a second spar extending generally longitudinally on either side of the mast, said spars each carrying means (40a, 40b, 44a, 44b) for slidably guiding the movable cowl and the sliding cascade,
A static mixer which is provided for a connection to a dispensing cartridge or to a dispensing device for a plurality of components, comprising - a mixing element; - a mixer housing; - an intermediate piece; and - a coupling element, wherein the mixing element is arranged within the mixer housing and the intermediate piece is arranged within the coupling element; the coupling element is provided for fastening the mixer to the dispensing cartridge or to the dispensing device and the intermediate piece has a first passage for a first component and a second passage for a second component; wherein the first passage passes through the intermediate piece separately from the second passage; wherein a first inlet opening is provided which opens into the first passage and a second inlet opening is provided which opens into the second passage; and wherein at least one encoding means (16, 60) is provided by means of which a correct positioning of the intermediate piece on the dispensing cartridge or dispensing device can be carried out, characterized in that the intermediate piece has a first connection element which is intended for receiving the mixer housing and which has a positioning element for aligning the mixer housing with respect to the connection element. - a mixing element; - a mixer housing; - an intermediate piece; and - a coupling element,
Aircraft comprising a lighting system, the lighting system comprising: - a light source configured to emit light, - at least one refractive optical element; wherein the at least one refractive optical element is configured for receiving light from the light source and for redirecting the light received from the light source to produce a plurality of light beams for illuminating simultaneously different surfaces of the aircraft and/or areas surrounding the aircraft; wherein the lighting system is installed in the fuselage of the aircraft; wherein at least one refractive optical element is a single complex lens comprising a light reception side and a light emitting side, wherein the light reception side comprises: - a planar surface configured to let part of the received light pass through the lens towards the light emitting side without modifying its direction; and - a plurality of lobes configured to gather and focus part of the received light in a particular direction towards the light emitting side; wherein the light emitting side is a flat surface and wherein the planar surface is parallel to the light emitting side. - a light source configured to emit light, - at least one refractive optical element; wherein the at least one refractive optical element is configured for receiving light from the light source and for redirecting the light received from the light source to produce a plurality of light beams for illuminating simultaneously different surfaces of the aircraft and/or areas surrounding the aircraft; wherein the lighting system is installed in the fuselage of the aircraft; wherein at least one refractive optical element is a single complex lens comprising a light reception side and a light emitting side, wherein the light reception side comprises: - a planar surface configured to let part of the received light pass through the lens towards the light emitting side without modifying its direction; and - a plurality of lobes configured to gather and focus part of the received light in a particular direction towards the light emitting side; - a planar surface configured to let part of the received light pass through the lens towards the light emitting side without modifying its direction; and - a plurality of lobes configured to gather and focus part of the received light in a particular direction towards the light emitting side; wherein the light emitting side is a flat surface and wherein the planar surface is parallel to the light emitting side.
A method for forming a non-oxygen silicon-based film on at least one surface of a substrate, the method comprising: providing at least one surface of the substrate in a reaction chamber; providing at least one organosilicon precursor having at least two SiH 3 groups with at least one C 2-3 linkage between silicon atoms in the reaction chamber; and forming the non-oxygen silicon-based film on the at least one surface by a deposition process comprising chemical vapor deposition, low pressure chemical vapor deposition (LPCVD), plasma enhanced chemical vapor deposition (PECVD), cyclic chemical vapor deposition (CCVD), plasma enhanced cyclic chemical vapor deposition (PECCVD), atomic layer deposition, or plasma enhanced atomic layer deposition (PEALD), wherein the deposition step is conducted at one or more temperatures ranging from 100°C to 650°C, and wherein the non-oxygen silicon-based film comprises greater than 50 atomic percent silicon as measured by X-ray photoelectron spectroscopy and 2 atomic percent or less of oxygen as measured by XPS. providing at least one surface of the substrate in a reaction chamber; providing at least one organosilicon precursor having at least two SiH 3 groups with at least one C 2-3 linkage between silicon atoms in the reaction chamber; and forming the non-oxygen silicon-based film on the at least one surface by a deposition process comprising chemical vapor deposition, low pressure chemical vapor deposition (LPCVD), plasma enhanced chemical vapor deposition (PECVD), cyclic chemical vapor deposition (CCVD), plasma enhanced cyclic chemical vapor deposition (PECCVD), atomic layer deposition, or plasma enhanced atomic layer deposition (PEALD), wherein the deposition step is conducted at one or more temperatures ranging from 100°C to 650°C, and wherein the non-oxygen silicon-based film comprises greater than 50 atomic percent silicon as measured by X-ray photoelectron spectroscopy and 2 atomic percent or less of oxygen as measured by XPS.
A control device for controlling a refrigerant circuit including a compressor configured to compress a refrigerant, a first outdoor heat exchanger configured to liquefy the refrigerant, a second outdoor heat exchanger during operation stop configured not to function as either a condenser or an evaporator, an expansion valve configured to lower the pressure of the liquefied refrigerant, and an indoor heat exchanger configured to evaporate the low-pressure refrigerant, the control device comprising: a control switching program which is configured to, when a valve opening degree of the expansion valve of the refrigerant circuit becomes equal to or larger than a predetermined threshold value, determine that the refrigerant has accumulated in the second outdoor heat exchanger, and switch from a normal operation to a refrigerant recovery operation; characterised by a refrigerant recovery operation control program which is configured to, when the control switching program switches to the refrigerant recovery operation, increase a rotational speed of the compressor and controls the pressure on a suction side of the compressor to be lower than the pressure of the second outdoor heat exchanger. a control switching program which is configured to, when a valve opening degree of the expansion valve of the refrigerant circuit becomes equal to or larger than a predetermined threshold value, determine that the refrigerant has accumulated in the second outdoor heat exchanger, and switch from a normal operation to a refrigerant recovery operation; characterised by a refrigerant recovery operation control program which is configured to, when the control switching program switches to the refrigerant recovery operation, increase a rotational speed of the compressor and controls the pressure on a suction side of the compressor to be lower than the pressure of the second outdoor heat exchanger.
An anti-S100A8 antibody comprising a heavy chain variable region consisting of SEQ ID NO: 4, and a light chain variable region consisting of SEQ ID NO: 6.
A lighting apparatus comprising: a first substrate comprising a lighting portion, a first outer portion disposed at an outer edge of the lighting portion, and a second outer portion (NA3, NA4) disposed along a second direction perpendicular to the first outer portion; an organic light emitting device comprising a first electrode, an organic light emitting layer, and a second electrode arranged in the lighting portion and in a partial region of the first and second outer portions (NA1, NA3) on the first substrate; and a first pad and a second pad disposed on the first outer portion and connected to the first electrode and the second electrode to apply a voltage to the first electrode and the second electrode, wherein the organic light emitting layer and the second electrode are not formed in a partial region of the first outer portion in which the first pad and the second pad are disposed to not expose the organic light emitting layer and the second electrode to an outside along the first outer portion and are formed over the entire second outer portion to expose the organic light emitting layer and the second electrode to the outside through a lateral end surface of the second outer portion, and an open region is formed on the second electrode and the organic light emitting layer in a region spaced apart from the lateral end surface by a predetermined distance along the lateral end surface of the second outer portion to disconnect the organic light emitting layer. a first substrate comprising a lighting portion, a first outer portion disposed at an outer edge of the lighting portion, and a second outer portion (NA3, NA4) disposed along a second direction perpendicular to the first outer portion; an organic light emitting device comprising a first electrode, an organic light emitting layer, and a second electrode arranged in the lighting portion and in a partial region of the first and second outer portions (NA1, NA3) on the first substrate; and a first pad and a second pad disposed on the first outer portion and connected to the first electrode and the second electrode to apply a voltage to the first electrode and the second electrode, wherein the organic light emitting layer and the second electrode are not formed in a partial region of the first outer portion in which the first pad and the second pad are disposed to not expose the organic light emitting layer and the second electrode to an outside along the first outer portion and are formed over the entire second outer portion to expose the organic light emitting layer and the second electrode to the outside through a lateral end surface of the second outer portion, and an open region is formed on the second electrode and the organic light emitting layer in a region spaced apart from the lateral end surface by a predetermined distance along the lateral end surface of the second outer portion to disconnect the organic light emitting layer.
Use of mixtures of triisopentyl esters of trimellitic acid comprising isomeric pentyl radicals, wherein at least 20 mol% of the isomeric pentyl radicals incorporated in the ester mixture are branched, and at the same time more than 10 mol% of the isomeric pentyl radicals incorporated in the ester mixture are linear, as plasticizer, or as part of a plasticizer composition comprising at least one further polymer-plasticizing compound in addition to the mixtures of triisopentyl esters of trimellitic acid, for PVC or vinyl chloride-containing copolymers.
A display panel with pressure sensor comprising: a display panel including an image forming panel configured to control light emitted to a front face side to form a displayed image, and a front polarizing plate disposed on the front face side of the image forming panel; and a pressure sensor including a piezoelectric film formed of only a single film of chiral polymer, wherein the chiral polymer forming the piezoelectric film is polylactic acid and the polylactic acid is uniaxially drawn, characterised in that the pressure sensor is disposed relative to the display panel such that the uniaxial drawing direction of the piezoelectric film is parallel to or orthogonal to a polarizing direction of the front polarizing plate. a display panel including an image forming panel configured to control light emitted to a front face side to form a displayed image, and a front polarizing plate disposed on the front face side of the image forming panel; and a pressure sensor including a piezoelectric film formed of only a single film of chiral polymer, wherein the chiral polymer forming the piezoelectric film is polylactic acid and the polylactic acid is uniaxially drawn, characterised in that the pressure sensor is disposed relative to the display panel such that the uniaxial drawing direction of the piezoelectric film is parallel to or orthogonal to a polarizing direction of the front polarizing plate.
A method for manufacturing a superconducting wire having a plurality of superconducting filaments which are arranged within an electrically conducting but not superconducting matrix, wherein at least some of the superconducting filaments are twisted around the wire axis in a range of twist angles, characterized in that the filaments of an Nb 3 Sn wire are twisted so that a) the majority of the filaments comes to lie at an angle of twist of 58° ± 2° relative to the wire axis and the wire is not surrounded by a steel jacket or that b) the Nb 3 SN wire is surrounded by a steel jacket and the twist angle of the filaments relative to the wire axis is 55° ± 5°, thereby reducing the dependency of the critical current of the superconducting wire on an external axial strain of the wire. a) the majority of the filaments comes to lie at an angle of twist of 58° ± 2° relative to the wire axis and the wire is not surrounded by a steel jacket or that b) the Nb 3 SN wire is surrounded by a steel jacket and the twist angle of the filaments relative to the wire axis is 55° ± 5°, thereby reducing the dependency of the critical current of the superconducting wire on an external axial strain of the wire.
A vehicle having a dimethyl ether fuel storage and delivery system for an internal combustion engine, the vehicle comprising: a DME fuel filter in the DME fuel storage and delivery system, the DME fuel filter configured to collect ferrous particulates; a DME fuel pump having a fuel inlet downstream of the DME fuel filter, the pump being operable to draw DME fuel through the DME fuel filter to the inlet; characterized in that it further comprises at least one sensor having at least one transducer, the at least one transducer being disposed at the DME fuel filter and having an electrical property responsive to an amount of ferrous particulate collected at the DME fuel filter, the at least one sensor being operable to detect a change in the at least one electrical property of the at least one transducer and to generate a signal indicative of DME fuel quality according to the electrical property of the transducer. a DME fuel filter in the DME fuel storage and delivery system, the DME fuel filter configured to collect ferrous particulates; a DME fuel pump having a fuel inlet downstream of the DME fuel filter, the pump being operable to draw DME fuel through the DME fuel filter to the inlet; characterized in that it further comprises at least one sensor having at least one transducer, the at least one transducer being disposed at the DME fuel filter and having an electrical property responsive to an amount of ferrous particulate collected at the DME fuel filter, the at least one sensor being operable to detect a change in the at least one electrical property of the at least one transducer and to generate a signal indicative of DME fuel quality according to the electrical property of the transducer.