mhurhangee/ep-ind-claims huggingface dataset:
Part (10, 40) for guiding and locking a predefined gas- and/or spring-operated cylinder comprising a piston and a tube comprising an axial recess wherein the piston can slide, this part comprising, in a casing: - a mounting receptacle for the tube, configured to receive, in its interior, an extremity of the tube in free movement for exiting from the receptacle; and - a mounting receptacle for the piston, coaxial with the receptacle for the tube and in the extension of the receptacle for the tube, configured to receive, in its interior, the piston in free translation along the common axis of the receptacles; characterised in that it also comprises - on the side with the mounting receptacle for the tube, relative to a plane perpendicular to the axis of the receptacles and passing by the bottom of the mounting receptacle for the tube, a projection (14, 26) extending beyond the mounting receptacle for the tube, configured to penetrate to the inside of the tube. - a mounting receptacle for the tube, configured to receive, in its interior, an extremity of the tube in free movement for exiting from the receptacle; and - a mounting receptacle for the piston, coaxial with the receptacle for the tube and in the extension of the receptacle for the tube, configured to receive, in its interior, the piston in free translation along the common axis of the receptacles; characterised in that it also comprises - on the side with the mounting receptacle for the tube, relative to a plane perpendicular to the axis of the receptacles and passing by the bottom of the mounting receptacle for the tube, a projection (14, 26) extending beyond the mounting receptacle for the tube, configured to penetrate to the inside of the tube.
A closure arrangement (20, 420) for a base liquid container for a base liquid, the closure arrangement comprising: a reservoir (24, 24A, 24B) for an additive liquid (28, 28A, 28B); and a passage (54, 76) for flow of liquid from the base liquid container to a user, the passage including a mixing space for mixing the additive liquid from the reservoir and the base liquid; characterized in that the reservoir (24, 24A, 24B) is collapsible such that the reservoir volume decreases as additive liquid flows out of the reservoir. a reservoir (24, 24A, 24B) for an additive liquid (28, 28A, 28B); and a passage (54, 76) for flow of liquid from the base liquid container to a user, the passage including a mixing space for mixing the additive liquid from the reservoir and the base liquid; characterized in that the reservoir (24, 24A, 24B) is collapsible such that the reservoir volume decreases as additive liquid flows out of the reservoir.
A load hook substructure for purposes of attachment onto or into the cabin structure of a helicopter, comprising a housing in which a shaft with hook attachment means is mounted, such that a load hook can be connected with the shaft and thereby with the load hook substructure, characterised in that, the shaft passes through the interior of the housing in the longitudinal direction between a housing end wall and a housing wall, such that it can move linearly, and a return spring device is arranged between a damping plate arranged on the shaft and the housing end wall, and a damping device is arranged between the damping plate and the lower housing wall, wherein the damping device comprises at least one flexibly compressible damping element, which develops a damping action in the event of a linear movement of the shaft.
An electric light candle comprising a luminous body of an elongated shape and a light source, wherein the luminous body is in the form of opal glass, wherein the opaqueness is achieved by opacifying agents arranged in the luminous body, characterised in that the luminous body is of such a material thickness, at least in a direction of propagation of the light emitted by the light source, that a colour conversion visible to the human eye of the luminous body irradiated by the light source is effected as a consequence of the scattering of the light emitted by the light source by the opacifying agents serving as scattering centres in said propagation direction in the luminous body, wherein the opacifying agents serving as scattering centres have a particle size of between 10 nm and 100 nm.
A wound dressing comprising a wound contact layer in the form of a textile, a film or a foam and an absorption layer, the absorption layer being attached to the wound contact layer by an adhesive, wherein the wound contact layer comprises at least one antimicrobial agent dispersed across the wound contact layer and wherein the wound contact layer is compressed.
A connection device of a partition wall, in particular a shower partition wall which comprises at least one pane (2, 4), comprising a connecting body (34, 35) and a plate connected to the pane (2, 4), wherein an adhesive adapter is provided, which comprises on the one hand the plate and on the other hand a coupling body, wherein the plate is connected by means of an adhesive to the pane (2, 4), wherein the connecting body (34, 35) further comprises a recess and the coupling body disposed on the other side of the plate engages into the recess of the connecting body (34, 35) and is fixed in the latter by means of a fixing element constituted as a screw or cylindrical head screw, characterised in that the coupling body is constituted dove-tailed and comprises at least one V-shaped recess and that, in the recess of the connecting element (34, 35), and more precisely opposite to the fixing element, a triangular or tooth-like projection is provided, which engages into the V-shaped recess of the coupling body.
An injector, comprising: an injector housing; an intraocular lens disposed within said housing, said intraocular lens having first and second interconnected, coaxial viewing elements (202,204); a lens carrier, said lens carrier being operable to move said intraocular lens from a home position of said intraocular lens along a continuously longitudinal path, said continuously longitudinal path extending distally from said home position, past a single-element engagement surface located distal of said home position, and between opposed lens-compacting surfaces (131,133) located distal of said single-element engagement surface. an injector housing; an intraocular lens disposed within said housing, said intraocular lens having first and second interconnected, coaxial viewing elements (202,204); a lens carrier, said lens carrier being operable to move said intraocular lens from a home position of said intraocular lens along a continuously longitudinal path, said continuously longitudinal path extending distally from said home position, past a single-element engagement surface located distal of said home position, and between opposed lens-compacting surfaces (131,133) located distal of said single-element engagement surface.
A portable level sensor for a flexible bag for collecting a fluid and/or a solid, wherein the flexible bag is a stoma bag or a urine collection bag and the sensor comprises a flexible resistor element, having an electrical resistance that changes in dependence upon its degree of flexing; means (12, 13) for attaching the resistor element to an outside surface of the flexible bag; and means (17, 18) for periodically polling the electrical resistance of the resistor element and transmitting to a receiver a signal which varies in dependence on the said electrical resistance.
A process for preparing a carbon molecular sieve membrane from a polyimide for separation of hydrogen and ethylene from one another comprising sequential steps as follows: a) placing a membrane fabricated from hollow fibers of a polyimide which is 6FDA/BPDA-DAM in contact with an oxygen-containing atmosphere or gas at a temperature within a range of from 340 °C to 380 °C and for a time within that temperature range of from five minutes up to 200 hours to produce a pre-oxidized and pre-carbonized polymeric membrane that is insoluble in N-methylpyrrolidone at a temperature of 110 °C and free of substructure collapse; wherein 6FDA is 5,5'-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione, BPDA is 3,3',4,4'-biphenyl tetracarboxylic dianhydride, and DAM is 2,4,6-trimethyl-1,3-phenylene diamine, wherein 6FDA and BPDA are present in a molar ratio in a range of from 10:1 to 1:10, wherein the polyimide i) has a glass transition temperature (T g) of at least 400 °C and ii) includes a bridged phenyl compound; and b) pyrolyzing the pre-oxidized and pre-carbonized polymeric membrane in the presence of a purge gas at a temperature within a range of from 450 °C to 1000 °C and for a time within a range of from 1 minute to 100 hours, to yield a carbon molecular sieve membrane that has at least one of a hydrogen permeance and a hydrogen/ethylene selectivity greater than that of a carbon molecular sieve membrane prepared from the same membrane using only pyrolysis as in step b). a) placing a membrane fabricated from hollow fibers of a polyimide which is 6FDA/BPDA-DAM in contact with an oxygen-containing atmosphere or gas at a temperature within a range of from 340 °C to 380 °C and for a time within that temperature range of from five minutes up to 200 hours to produce a pre-oxidized and pre-carbonized polymeric membrane that is insoluble in N-methylpyrrolidone at a temperature of 110 °C and free of substructure collapse; wherein 6FDA is 5,5'-[2,2,2-trifluoro-1-(trifluoromethyl)ethylidene]bis-1,3-isobenzofurandione, BPDA is 3,3',4,4'-biphenyl tetracarboxylic dianhydride, and DAM is 2,4,6-trimethyl-1,3-phenylene diamine, wherein 6FDA and BPDA are present in a molar ratio in a range of from 10:1 to 1:10, wherein the polyimide i) has a glass transition temperature (T g) of at least 400 °C and ii) includes a bridged phenyl compound; and i) has a glass transition temperature (T g) of at least 400 °C and ii) includes a bridged phenyl compound; b) pyrolyzing the pre-oxidized and pre-carbonized polymeric membrane in the presence of a purge gas at a temperature within a range of from 450 °C to 1000 °C and for a time within a range of from 1 minute to 100 hours, to yield a carbon molecular sieve membrane that has at least one of a hydrogen permeance and a hydrogen/ethylene selectivity greater than that of a carbon molecular sieve membrane prepared from the same membrane using only pyrolysis as in step b).
A rocker plate assembly (800; 900) adapted to be coupled to a circular fixator to be positioned around the tibia and foot of a patient, the rocker plate assembly comprising a body including a first side member having a first end, a second side member having a second end, and a connecting portion attached to the first side member opposite the first end and attached to the second side member opposite the second end, characterized in that the first and second side members each have at least one slot (804, 810) extending from a top surface of the body into the body, and in that the rocker plate assembly further comprises a plurality of sliders slidably retained in the slots of the first and second side members.
A mold for injection molding, the mold comprising: three or more cavity rows (22a, 22b, 22c), each cavity row having a plurality of cavities; and a cooling flow path configured to allow a cooling medium to flow through the cooling flow path, the cooling medium cooling the cavities, the cooling flow path including: at least one supply port; a distribution conduit communicated with the supply port; a supply conduit communicated with the distribution conduit; a cavity cooling portion communicated with the supply conduit and provided to an outer periphery of the cavities; a discharge conduit communicated with the cavity cooling portion; a collecting conduit communicated with the discharge conduit; and at least one discharge port communicated with the collecting conduit, characterized in that the supply conduit and the discharge conduit are parallel to the cavity rows, and at least one supply conduit and at least one discharge conduit are provided for each cavity row. three or more cavity rows (22a, 22b, 22c), each cavity row having a plurality of cavities; and a cooling flow path configured to allow a cooling medium to flow through the cooling flow path, the cooling medium cooling the cavities, the cooling flow path including: at least one supply port; a distribution conduit communicated with the supply port; a supply conduit communicated with the distribution conduit; a cavity cooling portion communicated with the supply conduit and provided to an outer periphery of the cavities; a discharge conduit communicated with the cavity cooling portion; a collecting conduit communicated with the discharge conduit; and at least one discharge port communicated with the collecting conduit, at least one supply port; a distribution conduit communicated with the supply port; a supply conduit communicated with the distribution conduit; a cavity cooling portion communicated with the supply conduit and provided to an outer periphery of the cavities; a discharge conduit communicated with the cavity cooling portion; a collecting conduit communicated with the discharge conduit; and at least one discharge port communicated with the collecting conduit, characterized in that the supply conduit and the discharge conduit are parallel to the cavity rows, and at least one supply conduit and at least one discharge conduit are provided for each cavity row.
A space debris removing device for removing space debris undergoing an irregular tumbling motion from an orbit by capturing and decelerating the space debris, comprising: a propulsion device for performing approach and attitude control to a target debris which is the space debris to be removed; a capture device having a harpoon which can be ejected toward the target debris; an observation device for observing a motion of the target debris and calculating a capture position and a capture attitude at which the harpoon can be driven into a portion of the target debris; a deceleration device directly or indirectly connected to the harpoon, for decelerating the target debris; and a body part on which the propulsion device, the capture device, the observation device and the deceleration device are mounted, wherein the portion of the target debris into which the harpoon can be driven is hollow; characterised in that the harpoon includes a pointed end part having a barb part that can be locked to the target debris, a stopper part to be in contact with a surface of the target debris, a thrust generation part for ejecting the harpoon, and a wire for connecting the harpoon to the body part, and the harpoon includes an elastic body (47, 47') disposed so as to cover the pointed end part on a front surface of the stopper part, and by compressing the elastic body (47, 47') between the target debris surface and the stopper part when the pointed end part is locked to the target debris, scattering of broken pieces generated when the harpoon passes through is suppressed. a propulsion device for performing approach and attitude control to a target debris which is the space debris to be removed; a capture device having a harpoon which can be ejected toward the target debris; an observation device for observing a motion of the target debris and calculating a capture position and a capture attitude at which the harpoon can be driven into a portion of the target debris; a deceleration device directly or indirectly connected to the harpoon, for decelerating the target debris; and a body part on which the propulsion device, the capture device, the observation device and the deceleration device are mounted, wherein the portion of the target debris into which the harpoon can be driven is hollow; characterised in that the harpoon includes a pointed end part having a barb part that can be locked to the target debris, a stopper part to be in contact with a surface of the target debris, a thrust generation part for ejecting the harpoon, and a wire for connecting the harpoon to the body part, and the harpoon includes an elastic body (47, 47') disposed so as to cover the pointed end part on a front surface of the stopper part, and by compressing the elastic body (47, 47') between the target debris surface and the stopper part when the pointed end part is locked to the target debris, scattering of broken pieces generated when the harpoon passes through is suppressed.
A pivot actuator, comprising: a housing; a piston that is supported in the housing and displaceable along a longitudinal axis of the housing; a drive shaft that protrudes from the housing wherein the piston engages the drive shaft by form locking so that the drive shaft is pivoted about a drive axis by a pivot angle between two end positions through a displacement of the piston; and a switching cam that is fixed torque proof at the drive shaft and configured to contact a stop element at the housing with a respective contact surface of the switch cam in the two end positions, characterized in that the switching cam includes two discs that are arranged on top of each other along the drive axis, wherein one respective contact surface of the two contact surfaces is arranged at each of the two discs respectively, and wherein the pivot angle can be adjusted by pivoting the two discs relative to each other along the drive axis in different angular orientations. a housing; a piston that is supported in the housing and displaceable along a longitudinal axis of the housing; a drive shaft that protrudes from the housing wherein the piston engages the drive shaft by form locking so that the drive shaft is pivoted about a drive axis by a pivot angle between two end positions through a displacement of the piston; and a switching cam that is fixed torque proof at the drive shaft and configured to contact a stop element at the housing with a respective contact surface of the switch cam in the two end positions, characterized in that the switching cam includes two discs that are arranged on top of each other along the drive axis, wherein one respective contact surface of the two contact surfaces is arranged at each of the two discs respectively, and wherein the pivot angle can be adjusted by pivoting the two discs relative to each other along the drive axis in different angular orientations.
A unit converting kinetic energy from wind or water into mechanical energy, comprising: - a scaffold which forms the main structure of the unit and carries a system, - at least one shaft mounted to the scaffold, - a plurality of motion elements, each of the motion elements rotating the at least one +4e- shaft by moving in the direction of the wind or water flow or in the opposite direction thereof, - a plurality of single direction moving fitments positioned inside the at least one shaft, each single direction moving fitment allows each motion element to be mounted to the at least one shaft and rotate idly in one direction, and allowing said motion element to actuate the at least one shaft to rotate by moving in the other direction, wherein the single direction moving fitments allow transferring the single direction movement generated by each motion element collectively to the at least one shaft. - a scaffold which forms the main structure of the unit and carries a system, - at least one shaft mounted to the scaffold, - a plurality of motion elements, each of the motion elements rotating the at least one +4e- shaft by moving in the direction of the wind or water flow or in the opposite direction thereof, - a plurality of single direction moving fitments positioned inside the at least one shaft, each single direction moving fitment allows each motion element to be mounted to the at least one shaft and rotate idly in one direction, and allowing said motion element to actuate the at least one shaft to rotate by moving in the other direction, wherein the single direction moving fitments allow transferring the single direction movement generated by each motion element collectively to the at least one shaft.
An aircraft management system comprising: a sensor configured to be loaded onto an aircraft; a diagnosis executor configured to diagnose health of a part of the aircraft on a basis of output from the sensor while the aircraft is flying; an outputter configured to output a predetermined recommendation information to an outside of the aircraft through wireless communication, in a case where the part satisfies a preset maintenance recommendation condition as a result of diagnosis of the health, characterized in that the predetermined recommendation information includes one or both of routine maintenance information and non-routine maintenance information, the aircraft management system further comprises a maintenance management server including a storage, an operation unit, a communication unit, a controller and a display, the storage includes a draft plan of routine maintenance of the aircraft, wherein maintenance items of the routine maintenance are decided in accordance with an upper limit of a maintenance interval that is set for each part of the aircraft, the controller adds, in the case where the predetermined recommendation information includes the routine maintenance information, maintenance of the part indicated by the routine maintenance information to the maintenance items of the draft plan of the routine maintenance to change the draft plan of the routine maintenance, and the controller generates, in the case where the predetermined recommendation information includes the non-routine maintenance information, a draft plan of non-routine maintenance of the aircraft. a sensor configured to be loaded onto an aircraft; a diagnosis executor configured to diagnose health of a part of the aircraft on a basis of output from the sensor while the aircraft is flying; an outputter configured to output a predetermined recommendation information to an outside of the aircraft through wireless communication, in a case where the part satisfies a preset maintenance recommendation condition as a result of diagnosis of the health, characterized in that the predetermined recommendation information includes one or both of routine maintenance information and non-routine maintenance information, the aircraft management system further comprises a maintenance management server including a storage, an operation unit, a communication unit, a controller and a display, the storage includes a draft plan of routine maintenance of the aircraft, wherein maintenance items of the routine maintenance are decided in accordance with an upper limit of a maintenance interval that is set for each part of the aircraft, the controller adds, in the case where the predetermined recommendation information includes the routine maintenance information, maintenance of the part indicated by the routine maintenance information to the maintenance items of the draft plan of the routine maintenance to change the draft plan of the routine maintenance, and the controller generates, in the case where the predetermined recommendation information includes the non-routine maintenance information, a draft plan of non-routine maintenance of the aircraft.
A method of machining an airfoil characterised by comprising the steps of: providing first and second cutting tools (140;40) respectively having first and second cutting contours (142;42) that are different than one another; cutting a blank with the first cutting tool to provide a first airfoil surface on a first blade; cutting the blank with the second cutting tool to provide a second airfoil surface on a second blade; and producing an airfoil having the first and second blades (24a,24b). providing first and second cutting tools (140;40) respectively having first and second cutting contours (142;42) that are different than one another; cutting a blank with the first cutting tool to provide a first airfoil surface on a first blade; cutting the blank with the second cutting tool to provide a second airfoil surface on a second blade; and producing an airfoil having the first and second blades (24a,24b).