mhurhangee/ep-ind-claims huggingface dataset:
A method of electrochemically polishing turbomachines of refractory metal using laser beam heating, comprising: immersing a surface of a component within a fluid held in a tank during a finishing process wherein the finishing process comprises electrochemical polishing; and heating fluid near the surface during the finishing process to create a convection current within the fluid that carries a byproduct of the finishing process away from the surface, and said step of heating comprising directing a laser beam at a target location within the fluid, the target location in an area of the tank other than the surface. immersing a surface of a component within a fluid held in a tank during a finishing process wherein the finishing process comprises electrochemical polishing; and heating fluid near the surface during the finishing process to create a convection current within the fluid that carries a byproduct of the finishing process away from the surface, and said step of heating comprising directing a laser beam at a target location within the fluid, the target location in an area of the tank other than the surface.
A tissue sampling device comprising: a flexible sheath; a needle tube which is inserted into the sheath so as to advance and retreat and with which biological tissue is punctured; and an operating unit which is provided on a proximal side of the sheath and is used for operating the advancing and retreating of the needle tube, wherein the needle tube has a distal portion provided with a slit extending toward the proximal side from a distal opening, and when the distal portion is in a state of protruding from a distal end of the sheath, at least a part of the distal portion is positioned further on a radially outside than an inner surface of the sheath when viewed from an axial direction of the needle tube, characterized in that the proximal side of the slit is formed in a spiral shape with respect to the axial direction of the needle tube. a flexible sheath; a needle tube which is inserted into the sheath so as to advance and retreat and with which biological tissue is punctured; and an operating unit which is provided on a proximal side of the sheath and is used for operating the advancing and retreating of the needle tube, wherein the needle tube has a distal portion provided with a slit extending toward the proximal side from a distal opening, and when the distal portion is in a state of protruding from a distal end of the sheath, at least a part of the distal portion is positioned further on a radially outside than an inner surface of the sheath when viewed from an axial direction of the needle tube, characterized in that the proximal side of the slit is formed in a spiral shape with respect to the axial direction of the needle tube.
A compound of formula: wherein: R 1 is independently selected from -R 4, -OH, -OR 4, -O R 4, monohydrogen phosphate, -F, -Cl, -Br and -I; n is selected from 0, 1, 2, 3 or 4; R 2 is C( x H) 3; R 3 is C( x H) 3; each R 4 is independently selected from C 1 -C 4 alkyl; each x H is independently protium or deuterium; and each y H is deuterium, wherein a ratio of deuterium: protium in a C( x H) 3 moiety in the compound is greater than that found naturally in hydrogen, wherein one or both of R 2 and R 3 are CD 3, or a pharmaceutically acceptable salt thereof. R 1 is independently selected from -R 4, -OH, -OR 4, -O R 4, monohydrogen phosphate, -F, -Cl, -Br and -I; n is selected from 0, 1, 2, 3 or 4; R 2 is C( x H) 3; R 3 is C( x H) 3; each R 4 is independently selected from C 1 -C 4 alkyl; each x H is independently protium or deuterium; and each y H is deuterium, wherein a ratio of deuterium: protium in a C( x H) 3 moiety in the compound is greater than that found naturally in hydrogen, wherein one or both of R 2 and R 3 are CD 3, or a pharmaceutically acceptable salt thereof.
A navigation system for determining a location of a trackable instrument assembly relative to an anatomy, comprising: the trackable instrument assembly having, an elongated guide defining a first bore extending from a first proximal end to a first distal end; an elongated sleeve defining a second bore extending from a second proximal end to a second distal end, the elongated sleeve configured to be positionable in the first bore; a tracking sensor attached to the elongated sleeve; and a tool extending from a third proximal end to a third distal end, the tool configured to be positionable in the second bore; and a tracking system operable to track said tracking sensor; wherein the tracking sensor is configured to be used to track a selected portion of the tool, when said tool is positioned in the second bore; and wherein said first distal end is adapted to allow for operation of said third distal end when said tool is positioned in said elongated sleeve and said elongated sleeve is positioned in said elongated guide. the trackable instrument assembly having, an elongated guide defining a first bore extending from a first proximal end to a first distal end; an elongated sleeve defining a second bore extending from a second proximal end to a second distal end, the elongated sleeve configured to be positionable in the first bore; a tracking sensor attached to the elongated sleeve; and a tool extending from a third proximal end to a third distal end, the tool configured to be positionable in the second bore; and a tracking system operable to track said tracking sensor; wherein the tracking sensor is configured to be used to track a selected portion of the tool, when said tool is positioned in the second bore; and wherein said first distal end is adapted to allow for operation of said third distal end when said tool is positioned in said elongated sleeve and said elongated sleeve is positioned in said elongated guide.
A fiber reinforced plastic material, characterized by comprising: a fiber layer comprising a plurality of continuous carbon fiber reinforced thermoplastic sheets; a veil layer comprising fibers selected from at least one of glass fiber and carbon fiber, the fibers of the veil layer preferably being non-woven; and a resin layer comprising a resin film,, wherein the veil layer is impregnated by at least a portion of the resin film, the fiber reinforced plastic material being characterized in that the resin film comprises a polyphenylene sulfide resin, and in that the carbon fibers of the continuous carbon fiber reinforced thermoplastic sheets are bundled into carbon fiber bundles. a fiber layer comprising a plurality of continuous carbon fiber reinforced thermoplastic sheets; a veil layer comprising fibers selected from at least one of glass fiber and carbon fiber, the fibers of the veil layer preferably being non-woven; and a resin layer comprising a resin film,, wherein the veil layer is impregnated by at least a portion of the resin film, the fiber reinforced plastic material being characterized in that the resin film comprises a polyphenylene sulfide resin, and in that the carbon fibers of the continuous carbon fiber reinforced thermoplastic sheets are bundled into carbon fiber bundles.
AIRCRAFT RUDDER AUTHORITY CONTROL SYSTEM, for a rudder comprising a reversible mechanical system having stop parts and an actuator, said stop parts commanded or moved by an actuator that works based on control/command signals, the aircraft rudder authority control system being characterized by having at least two stop parts (M, M') movable inside of the field of movement of the actuator and interfering in the movement of said actuator; the mentioned control signals being based on one or more of the following aircraft information: - Traction of the engines, pressure of the engines, temperature of the engines, axis rotation speed, traction asymmetry between the engines of the aircraft; - Flight speed; - Altitude; - Skidding angle; and - Aircraft on the ground. - Traction of the engines, pressure of the engines, temperature of the engines, axis rotation speed, traction asymmetry between the engines of the aircraft; - Flight speed; - Altitude; - Skidding angle; and - Aircraft on the ground.
Transport system for conveying objects along a repeatedly redirected conveying route, comprising at least one conveying element, which consists of a multiplicity of chain links connected together in an articulated manner by chain joints to form a closed loop and which can be driven circulating in a timed manner by means of at least one chain wheel in at least one conveying direction, wherein the conveying element is constituted by means of the at least one chain wheel (4, 5) and at least two further direction changes (U1, U2, U3) as a closed and repeatedly redirected loop with a free middle region, wherein the chain links are configured as conveyor pallets, wherein chain wheel engagement or driver regions are provided on the at least one chain wheel at a predetermined separation angle, in which guiding or bearing units (32, 33) provided at the chain joints of the conveyor pallets engage as the chain wheel circulates in each case on at least one pitch circle (8.1), on which the conveyor pallets are guided radially at least in sections about the at least one chain wheel and/or the at least two direction changes (U1, U2, U3) between a conveyor pallet inlet (11.1, 12.1, 13.1, 14.1) and a conveyor pallet outlet (11.2, 12.2, 13.2, 14.2), wherein conveyor pallets guides (30, 31) for the linear guiding of the driver and guiding elements (19, 20) of the conveyor pallets are each provided between the at least one chain wheel and the associated direction changes (U1, U2, U3), characterised in that, relative to the conveying direction, respectively between the conveyor pallet inlet (11.1, 12.1, 13.1, 14.1, 15.1, 16.1, 17.1, 18.1) and the corresponding linear guide by means of the conveyor pallet guides (30, 31) and between a conveyor outlet (11.2, 12.2, 13.2, 14.2, 15.2, 16.2, 17.2, 18.2) and the corresponding linear guide by means of conveyor pallet guides (30, 31), a compensation curve (28, 28a) is provided in each case, along which the guiding and bearing units (32, 33) of the conveyor pallets are guided for a polygon compensation, wherein the compensation curves (28, 28a) each extend over an angle range (α, β), which corresponds to half the separation angle of the chain wheel engagement or driver regions, wherein the rectilinear sections (15, 16, 17, 18) each following one another in the conveying direction between the chain wheel and/or one of the direction changes (U1, U2, U3) are provided at an angle (μ) equal to 90° and wherein the repeatedly redirected loop of the conveying element is constituted in plan view essentially as a rectangle with the free middle region between the chain wheel and the further direction changes (U1, U2, U3).
Sprayable, stable composition, containing - at least one organopolysiloxane containing hydroxyl groups and/or hydrolyzable groups, - at least one cross-linking agent based on a functionalized silane, - at least one filler based on silica and - at least one condensation catalyst, characterized in that the composition is free of water and/or solvents. - at least one organopolysiloxane containing hydroxyl groups and/or hydrolyzable groups, - at least one cross-linking agent based on a functionalized silane, - at least one filler based on silica and - at least one condensation catalyst, characterized in that the composition is free of water and/or solvents.
A compound having Formula I wherein: R 1 is selected from the group consisting of aryl, alkyl, silyl, and deuterated analogs thereof; R 2 is selected from the group consisting of aryl, alkyl, silyl, and deuterated analogs thereof; R 3 is selected from the group consisting of D, alkyl, silyl, deuterated alkyl, and deuterated silyl; and R 4 is the same or different at each occurrence and is H, D, aryl, alkyl, silyl, deuterated aryl, deuterated alkyl, and deuterated silyl, provided that the compound is not compound G1: R 1 is selected from the group consisting of aryl, alkyl, silyl, and deuterated analogs thereof; R 2 is selected from the group consisting of aryl, alkyl, silyl, and deuterated analogs thereof; R 3 is selected from the group consisting of D, alkyl, silyl, deuterated alkyl, and deuterated silyl; and R 4 is the same or different at each occurrence and is H, D, aryl, alkyl, silyl, deuterated aryl, deuterated alkyl, and deuterated silyl,
A combustor for a turbine engine comprising: an outer liner having a row of circumferentially distributed outer combustion air holes including at least a major outer air hole having a first outer air hole size, an intermediate outer air hole having a second outer air hole size, and a minor outer air hole having a third outer air hole size, wherein said first, said second, and said third outer air hole sizes are all different from each other; and an inner liner circumscribed by said outer liner and having a row of circumferentially distributed inner combustion air holes including at least a major inner air hole having a first inner air hole size, an intermediate inner air hole having a second inner air hole size, and a minor inner air hole having a third inner air hole size, wherein said first, said second, and said third inner air hole sizes are all different from each other; characterised in that said major inner air hole is at least partially aligned in a radial direction with one of said minor outer air holes or said intermediate air hole from said outer liner. an outer liner having a row of circumferentially distributed outer combustion air holes including at least a major outer air hole having a first outer air hole size, an intermediate outer air hole having a second outer air hole size, and a minor outer air hole having a third outer air hole size, wherein said first, said second, and said third outer air hole sizes are all different from each other; and an inner liner circumscribed by said outer liner and having a row of circumferentially distributed inner combustion air holes including at least a major inner air hole having a first inner air hole size, an intermediate inner air hole having a second inner air hole size, and a minor inner air hole having a third inner air hole size, wherein said first, said second, and said third inner air hole sizes are all different from each other; characterised in that said major inner air hole is at least partially aligned in a radial direction with one of said minor outer air holes or said intermediate air hole from said outer liner.
A gas phase surface treatment for treating carbon fiber, comprising: a) exposing a carbon fiber to a gaseous oxidizing atmosphere to form a modified carbon fiber with an oxidized fiber surface; followed by b) exposing the oxidized fiber surface to a gaseous nitrogen-containing atmosphere to form a modified carbon fiber with a nitrogen-enriched surface, wherein the gaseous nitrogen-containing atmosphere comprises at least 50% by volume of ammonia gas and the nitrogen-enriched surface exhibits an increase in surface nitrogen to surface carbon (N/C) ratio as compared to the surface of the carbon fiber prior to exposure at (a), and wherein steps (a) and (b) are carried out continuously without any additional intervening surface treatment and are performed at a temperature in the range of 100°C to 200°C. a) exposing a carbon fiber to a gaseous oxidizing atmosphere to form a modified carbon fiber with an oxidized fiber surface; followed by b) exposing the oxidized fiber surface to a gaseous nitrogen-containing atmosphere to form a modified carbon fiber with a nitrogen-enriched surface, wherein the gaseous nitrogen-containing atmosphere comprises at least 50% by volume of ammonia gas and the nitrogen-enriched surface exhibits an increase in surface nitrogen to surface carbon (N/C) ratio as compared to the surface of the carbon fiber prior to exposure at (a), and
Sealing system for fluids comprising: - a packing-type sealing gasket, - a housing and containing track which develops on a plane and is adapted to house said packing-type sealing gasket comprising at least one internal wall and one external wall, housing and containing track comprising a first part having a substantially constant width and a second part having a width greater than the width of the first part, the second part of the housing and containing track being composed of sections of the internal wall and/or of the external wall of the housing and containing track on which a recess is machined, characterized in that the packing-type sealing gasket is inserted in the housing and containing track with a first end and a second end of the sealing gasket inside the second part having greater width, mutually juxtaposed anc either overlapped, or with at least one section of packing interposed - a packing-type sealing gasket, - a housing and containing track which develops on a plane and is adapted to house said packing-type sealing gasket comprising at least one internal wall and one external wall, housing and containing track comprising a first part having a substantially constant width and a second part having a width greater than the width of the first part, the second part of the housing and containing track being composed of sections of the internal wall and/or of the external wall of the housing and containing track on which a recess is machined, characterized in that the packing-type sealing gasket is inserted in the housing and containing track with a first end and a second end of the sealing gasket inside the second part having greater width, mutually juxtaposed anc either overlapped, or with at least one section of packing interposed
A method in a data processing system for creating data structures for parallel programming, comprising: forming, by one or more processors, one or more data structures, each data structure comprising one or more global containers and a first plurality of local containers, wherein each of the one or more global containers is accessible by all of a plurality of threads in a multi-thread parallel processing environment, wherein each of the first plurality of local containers is accessible only by a corresponding one of the plurality of threads, wherein a local container of the first plurality of local containers comprises a trace identifier, tid, a start index, and an end index, the start index and the end index corresponds to a global container of the one or more global containers; splitting the global container into a second plurality of local containers when items are going to be processed in parallel; performing parallel processing with the plurality of threads accessing the global container, wherein during the parallel processing, each of the plurality of threads accesses a corresponding local container, wherein the global container and the local container are implemented as common data structure, and a data region of the common data structure is identified by the start index and the end index in the local container, the corresponding one of the plurality of threads is identified by the tid; and merging two or more of the first plurality local containers into a single global container when the plurality of threads synchronize the items. forming, by one or more processors, one or more data structures, each data structure comprising one or more global containers and a first plurality of local containers, wherein each of the one or more global containers is accessible by all of a plurality of threads in a multi-thread parallel processing environment, wherein each of the first plurality of local containers is accessible only by a corresponding one of the plurality of threads, wherein a local container of the first plurality of local containers comprises a trace identifier, tid, a start index, and an end index, the start index and the end index corresponds to a global container of the one or more global containers; splitting the global container into a second plurality of local containers when items are going to be processed in parallel; performing parallel processing with the plurality of threads accessing the global container, wherein during the parallel processing, each of the plurality of threads accesses a corresponding local container, wherein the global container and the local container are implemented as common data structure, and a data region of the common data structure is identified by the start index and the end index in the local container, the corresponding one of the plurality of threads is identified by the tid; and merging two or more of the first plurality local containers into a single global container when the plurality of threads synchronize the items.
An aircraft landing gear assembly comprising: a first body having a first side, a second side and a bearing face extending between the sides; a second body having a first side, a second side and a bearing face extending between the sides, the bodies being positioned relative to one another such that the bearing faces are adjacent to one another and the first side of each body is closer to the first side of the other body than it is to the second side of the other body; characterised by a flexible coupling arranged to limit separation of the bearing faces while permitting relative rotational movement between the bodies in a movement plane so as to define a joint between the bodies, the flexible coupling comprising: one or more flexible straps arranged in a first configuration in which the straps are coupled to the first side of the first body and coupled to the second side of the second body; and one or more flexible straps arranged in a second configuration in which the straps are coupled to the second side of the first body and coupled to the first side of the second body, the straps of the first and second configurations being arranged in parallel across the joint. a first body having a first side, a second side and a bearing face extending between the sides; a second body having a first side, a second side and a bearing face extending between the sides, the bodies being positioned relative to one another such that the bearing faces are adjacent to one another and the first side of each body is closer to the first side of the other body than it is to the second side of the other body; characterised by a flexible coupling arranged to limit separation of the bearing faces while permitting relative rotational movement between the bodies in a movement plane so as to define a joint between the bodies, the flexible coupling comprising: one or more flexible straps arranged in a first configuration in which the straps are coupled to the first side of the first body and coupled to the second side of the second body; and one or more flexible straps arranged in a second configuration in which the straps are coupled to the second side of the first body and coupled to the first side of the second body, the straps of the first and second configurations being arranged in parallel across the joint. one or more flexible straps arranged in a first configuration in which the straps are coupled to the first side of the first body and coupled to the second side of the second body; and one or more flexible straps arranged in a second configuration in which the straps are coupled to the second side of the first body and coupled to the first side of the second body, the straps of the first and second configurations being arranged in parallel across the joint.