mhurhangee/ep-ind-claims huggingface dataset:
An inlet duct for an auxiliary power unit comprising: an inlet door to be pivotable between open and closed positions, and at an upstream end of an inlet duct body; said inlet duct body extending from an inlet end to an outlet end; and a plurality of splitters (34,40) positioned within said inlet duct body and between said inlet and said outlet ends to sub-divide an interior of said inlet duct body into plural flow paths, and characterised by said plurality of splitters including acoustic deadening material. an inlet door to be pivotable between open and closed positions, and at an upstream end of an inlet duct body; said inlet duct body extending from an inlet end to an outlet end; and a plurality of splitters (34,40) positioned within said inlet duct body and between said inlet and said outlet ends to sub-divide an interior of said inlet duct body into plural flow paths, and characterised by said plurality of splitters including acoustic deadening material.
A storage assembly comprising: a delivery device including a shaft having an implant loaded thereto; an inner container surrounding the implant and sealed to the shaft; wherein the inner container contains sterilizing fluid; and an outer container surrounding the inner container and sealed to the shaft; wherein the outer container contains aqueous water. a delivery device including a shaft having an implant loaded thereto; an inner container surrounding the implant and sealed to the shaft; wherein the inner container contains sterilizing fluid; and an outer container surrounding the inner container and sealed to the shaft; wherein the outer container contains aqueous water.
Method implemented by a processor for processing a reference seismic image of a medium and a control seismic image of said medium, the reference seismic image comprising at least one seismic trace described in a depth scale and the control seismic image comprising at least one seismic trace described in the depth scale, the method comprising the following steps: a) receiving the reference seismic image and the control seismic image; and b) defining at least one first planar capture level situated on one of the traces from among the seismic trace of the reference image and the seismic trace of the control image, and at least one second planar capture level on the seismic trace of the reference image; and c) transforming a continuous portion of the seismic trace of the control image by demigration on the first capture level by means of an original velocity model, into a transformed control seismic trace described in a time scale; and d) transforming a continuous portion of the seismic trace of the reference image comprising the second capture level by demigration on the second capture level by means of a current velocity model, into a transformed reference seismic trace portion described in the time scale; and e) correcting the portion of the transformed control seismic trace by calibration on the second capture level by means of the current velocity model in a new transformed control seismic trace portion described in the time scale; and f) determining an optimised current velocity model by the addition, to the current velocity model, of a correction factor for the current velocity model determined from an offset in time between the portion of the transformed reference seismic trace and the new transformed control seismic trace portion. a) receiving the reference seismic image and the control seismic image; and b) defining at least one first planar capture level situated on one of the traces from among the seismic trace of the reference image and the seismic trace of the control image, and at least one second planar capture level on the seismic trace of the reference image; and c) transforming a continuous portion of the seismic trace of the control image by demigration on the first capture level by means of an original velocity model, into a transformed control seismic trace described in a time scale; and d) transforming a continuous portion of the seismic trace of the reference image comprising the second capture level by demigration on the second capture level by means of a current velocity model, into a transformed reference seismic trace portion described in the time scale; and e) correcting the portion of the transformed control seismic trace by calibration on the second capture level by means of the current velocity model in a new transformed control seismic trace portion described in the time scale; and f) determining an optimised current velocity model by the addition, to the current velocity model, of a correction factor for the current velocity model determined from an offset in time between the portion of the transformed reference seismic trace and the new transformed control seismic trace portion.
Induction sealing device for heat sealing of packaging material, said sealing device comprising a coil conductor partly encapsulated in a supporting body, said coil conductor being adapted for cooperation with the packaging material during sealing, said coil conductor has a reduced cross sectional area at at least one position along the coil conductor so as to concentrate the magnetic flux induced by the coil conductor at said at least one position, wherein said reduced cross sectional area is achieved by reducing the width and height of the coil conductor and wherein said at least one position is placed to match a packaging material overlap in the area that is arranged to be sealed by the induction sealing device.
A gas barrier layered product comprising a base material and a layer stacked on at least one surface of the base material, wherein the layer is formed of a composition that includes: a hydrolyzed and condensed product of at least one compound containing a metal atom to which at least one characteristic group selected from a halogen atom and an alkoxy group has been bonded; and a neutralized product of a polymer containing at least one functional group selected from a carboxyl group and a carboxylic anhydride group, and at least a part of -COO- group contained in the at least one functional group has been neutralized with a metal ion having a valence of two or more, wherein the compound is composed of at least one compound expressed by the following chemical formula and at least one compound expressed by the following chemical formula: M 1 (OR 1) n X 1 k Z 1 m-n-k..., where M 1 denotes Si; R 1 indicates an alkyl group; X 1 indicates a halogen atom; Z 1 denotes an alkyl group substituted by a functional group having reactivity to a carboxyl group; m is equal to a valence of M 1; n denotes an integer of 0 to (m-1); k indicates an integer of 0 to (m-1); and 1 ≤ n + k ≤ (m-1), M 2 (OR 2) q R 3 p-q-r X 2 r... where M 2 denotes Si; R 2 indicates an alkyl group; R 3 denotes an alkyl group, an aralkyl group, an aryl group, or an alkenyl group; X 2 indicates a halogen atom; p is equal to a valence of M 2; q denotes an integer of 0 to p; r indicates an integer of 0 to p; and 1 ≤ q + r ≤ p, and a mole ratio of the compound / the compound is in a range of 0.5 / 99.5 to 40 / 60.
An electronic device comprising: a display, a memory and a processor, wherein the processor is configured to: display, on the display, a folder icon that includes execution icons of a plurality of applications; in response to a first user input selecting the folder icon, display a user interface including the execution icons of the plurality of applications, and when an application is added to a folder corresponding to the folder icon, collectively set a notification pattern of the added application as a notification pattern for the plurality of applications included in the folder wherein the user interface includes at least one object for collectively controlling notifications for the plurality of applications. a display, a memory and a processor, wherein the processor is configured to: display, on the display, a folder icon that includes execution icons of a plurality of applications; in response to a first user input selecting the folder icon, display a user interface including the execution icons of the plurality of applications, and when an application is added to a folder corresponding to the folder icon, collectively set a notification pattern of the added application as a notification pattern for the plurality of applications included in the folder wherein the user interface includes at least one object for collectively controlling notifications for the plurality of applications. display, on the display, a folder icon that includes execution icons of a plurality of applications; in response to a first user input selecting the folder icon, display a user interface including the execution icons of the plurality of applications, and when an application is added to a folder corresponding to the folder icon, collectively set a notification pattern of the added application as a notification pattern for the plurality of applications included in the folder wherein the user interface includes at least one object for collectively controlling notifications for the plurality of applications.
Apparatus (10, 50), including a diaphragm valve, comprising: a valve body (12, 52) configured with a passage to be opened to allow fluid to pass through the valve body and to be closed to prevent fluid from passing through the valve body; a bonnet assembly (14, 54) having a compressor, a pressure ring, and a diaphragm, the pressure ring configured to load and unload the diaphragm based at least partly on a first spring constant to seal a peripheral portion of the diaphragm, and the compressor configured to close or open the passage of the valve body; the valve body and the bonnet assembly are substantially fixed together with a second spring constant that is substantially higher than and independent from the first spring constant, characterized in that, the valve body and bonnet assembly being configured with a rotational connection that allows the bonnet assembly and valve body to be rotated. a valve body (12, 52) configured with a passage to be opened to allow fluid to pass through the valve body and to be closed to prevent fluid from passing through the valve body; a bonnet assembly (14, 54) having a compressor, a pressure ring, and a diaphragm, the pressure ring configured to load and unload the diaphragm based at least partly on a first spring constant to seal a peripheral portion of the diaphragm, and the compressor configured to close or open the passage of the valve body; the valve body and the bonnet assembly are substantially fixed together with a second spring constant that is substantially higher than and independent from the first spring constant, the valve body and bonnet assembly being configured with a rotational connection that allows the bonnet assembly and valve body to be rotated.
A compound of formula I wherein R 1 is a) -H, b) -C -R 3, c) -C 1 -C 6 alkyl, or d) -CN; R 2 is a) -C 1 -C 6 alkyl optionally substituted with one to three halo, or b) cyclopropyl, cyclobutyl, cyclopentyl or cyclohexyl; R 3 is -C 1 -C 6 alkyl; W is a) or b) absent; X and Y are each independently halo; Z is a) -C 1 -C 2 alkyl-, b) cyclopropyl or cyclobutyl, or c) absent; or a pharmaceutical acceptable salt thereof. wherein R 1 is a) -H, b) -C -R 3, c) -C 1 -C 6 alkyl, or d) -CN; a) -H, b) -C -R 3, c) -C 1 -C 6 alkyl, or d) -CN; R 2 is a) -C 1 -C 6 alkyl optionally substituted with one to three halo, or b) cyclopropyl, cyclobutyl, cyclopentyl or cyclohexyl; a) -C 1 -C 6 alkyl optionally substituted with one to three halo, or b) cyclopropyl, cyclobutyl, cyclopentyl or cyclohexyl; R 3 is -C 1 -C 6 alkyl; W is a) or b) absent; a) or b) absent; X and Y are each independently halo; Z is a) -C 1 -C 2 alkyl-, b) cyclopropyl or cyclobutyl, or c) absent; a) -C 1 -C 2 alkyl-, b) cyclopropyl or cyclobutyl, or c) absent; or a pharmaceutical acceptable salt thereof.
A method comprising: receiving user traffic in a satellite communication system from terminals (270, 280, 290) of different types through a common physical layer; identifying a type associated with each terminal (270, 280, 290); routing the user traffic to a multi-protocol stack based, at least in part, on the terminal type; and forwarding the user traffic from the multi-protocol stack to a core network corresponding to the terminal type, wherein the terminal type (270, 280, 290) is determined based on utilization of a current generation protocol or a legacy protocol of at least one prior generation. receiving user traffic in a satellite communication system from terminals (270, 280, 290) of different types through a common physical layer; identifying a type associated with each terminal (270, 280, 290); routing the user traffic to a multi-protocol stack based, at least in part, on the terminal type; and forwarding the user traffic from the multi-protocol stack to a core network corresponding to the terminal type, wherein the terminal type (270, 280, 290) is determined based on utilization of a current generation protocol or a legacy protocol of at least one prior generation.
A lighting device (1, 1a) having a front-rear direction and comprising: a case made from a material allowing light to penetrate therethrough and having a cylinder shape with a closed bottom in a front end and an opening in a rear end; a substrate including a light emitter configured to emit light; and a cover made from a rigid material, wherein the cover includes a cover body, a pair of cover side walls, and a pair of arms, and press-fitted and installed in the substrate in the tip end portion, the tip end portion being on the side of the front end of the case so as to cover the light emitter, and installed inside the case together with the substrate, wherein the central portion of the substrate in a transverse direction at the forward end of the substrate is sandwiched by and between the pair of cover side walls and the pair of arms in a longitudinal direction, wherein a direction perpendicular to the front-rear direction of the lighting device (1, 1a) is referred to as a longitudinal direction, and a direction perpendicular to the front-rear direction and the longitudinal direction is referred to as a transverse direction, and wherein the thickness direction of the substrate in which the light emitter is installed and which has a thin flat plate shape is the longitudinal direction. a case made from a material allowing light to penetrate therethrough and having a cylinder shape with a closed bottom in a front end and an opening in a rear end; a substrate including a light emitter configured to emit light; and a cover made from a rigid material, wherein the cover includes a cover body, a pair of cover side walls, and a pair of arms, and press-fitted and installed in the substrate in the tip end portion, the tip end portion being on the side of the front end of the case so as to cover the light emitter, and installed inside the case together with the substrate, wherein the central portion of the substrate in a transverse direction at the forward end of the substrate is sandwiched by and between the pair of cover side walls and the pair of arms in a longitudinal direction, wherein a direction perpendicular to the front-rear direction of the lighting device (1, 1a) is referred to as a longitudinal direction, and a direction perpendicular to the front-rear direction and the longitudinal direction is referred to as a transverse direction, and wherein the thickness direction of the substrate in which the light emitter is installed and which has a thin flat plate shape is the longitudinal direction.
A luminous module for a motor vehicle, said luminous module comprising: - a support plate; - a light source disposed on said support plate; - a control module for said light source arranged on said support plate; - a light guide adapted to cooperate with said light source; - a reception shaft for said light guide integral with said support plate comprising: - a first opening adapted to receive said light guide; - at least one slot adapted to receive an anchoring tongue (25A, 25B) of a locking part; - said locking piece comprising: - a main body; - at least one anchoring tongue (25A, 25B) projecting from the main body and adapted to block the light guide in said receiving barrel, said light module further comprising a jumper disposed on said support plate upstream of the reception barrel and adapted to serve as a support for said locking piece. - a support plate; - a light source disposed on said support plate; - a control module for said light source arranged on said support plate; - a light guide adapted to cooperate with said light source; - a reception shaft for said light guide integral with said support plate comprising: - a first opening adapted to receive said light guide; - at least one slot adapted to receive an anchoring tongue (25A, 25B) of a locking part; - a first opening adapted to receive said light guide; - at least one slot adapted to receive an anchoring tongue (25A, 25B) of a locking part; - said locking piece comprising: - a main body; - at least one anchoring tongue (25A, 25B) projecting from the main body and adapted to block the light guide in said receiving barrel, said light module further comprising a jumper disposed on said support plate upstream of the reception barrel and adapted to serve as a support for said locking piece. - a main body; - at least one anchoring tongue (25A, 25B) projecting from the main body and adapted to block the light guide in said receiving barrel,
Method for joint-welding coated metal sheets (1, 2) in a butt joint, characterised in that at least one pulverulent welding additive in the form of a gas-powder flow is added to the weld melt via at least one flow duct, in such a way that the gas-powder flow leaving the flow duct is directed towards the weld melt and has an output speed of at least 2 m/s, in such a way the welding additive is mixed together turbulently with the weld melt, flow eddies forming in the weld melt during said mixing.
Evaporation device for evaporating thaw water from a refrigerator, in particular from a household refrigerator, having a condenser arranged in a coolant circuit of the refrigerator as a heat source and having an evaporation container designed on the condenser for receiving the thaw water, wherein a housing surrounding the condenser is provided, wherein the evaporation container is formed integrally with a housing wall of the housing, wherein an air flow generation facility is provided for generating an air flow across a surface of the thaw water received in the evaporation container, characterised in that the air flow generation facility is arranged in the housing wall.
A system for applying reduced pressure to a tissue site, the system comprising: a reduced-pressure source operable to supply reduced pressure; a bioabsorbable membrane (170, 270), wherein a membrane wall thickness associated with the membrane is substantially uniform throughout the membrane, the membrane having a plurality of projections on a first, tissue-facing surface and a plurality of substantially matched recesses on a second surface of the membrane, the plurality of projections at least partially defining at least one channel operable to transfer the reduced pressure along the tissue-facing surface; and a delivery tube coupled to the membrane, the delivery tube operable to deliver the reduced pressure to the tissue-facing surface of the membrane. a reduced-pressure source operable to supply reduced pressure; a bioabsorbable membrane (170, 270), wherein a membrane wall thickness associated with the membrane is substantially uniform throughout the membrane, the membrane having a plurality of projections on a first, tissue-facing surface and a plurality of substantially matched recesses on a second surface of the membrane, the plurality of projections at least partially defining at least one channel operable to transfer the reduced pressure along the tissue-facing surface; and a delivery tube coupled to the membrane, the delivery tube operable to deliver the reduced pressure to the tissue-facing surface of the membrane.
An engine comprising: a rocket combustion chamber for the combustion of fuel and oxidant; an air-breathing combustion chamber for the combustion of fuel and oxidant; a compressor for pressurizing air for supply to said air-breathing combustion chamber; a first fuel delivery system for delivering fuel to said rocket combustion chamber; a second fuel delivery system for delivering fuel to said air-breathing combustion chamber; an oxidant delivery system for delivering oxidant to said rocket combustion chamber; wherein the air-breathing combustion chamber and the rocket combustion chamber are configured to be operated independently with the engine being, above a predetermined velocity, switchable from an air-breathing mode to a full rocket mode; and. wherein the engine further comprises: a first heat exchanger arrangement (29, 30) having an inlet and an outlet arranged for cooling air to be supplied to said compressor using a heat transfer medium before compression by said compressor; a heat transfer medium loop for said heat transfer medium; and a second heat exchanger arrangement (34, 35, 36) configured for cooling of said heat transfer medium by fuel delivered by the first or second fuel delivery system. a rocket combustion chamber for the combustion of fuel and oxidant; an air-breathing combustion chamber for the combustion of fuel and oxidant; a compressor for pressurizing air for supply to said air-breathing combustion chamber; a first fuel delivery system for delivering fuel to said rocket combustion chamber; a second fuel delivery system for delivering fuel to said air-breathing combustion chamber; an oxidant delivery system for delivering oxidant to said rocket combustion chamber; wherein the air-breathing combustion chamber and the rocket combustion chamber are configured to be operated independently with the engine being, above a predetermined velocity, switchable from an air-breathing mode to a full rocket mode; and. a first heat exchanger arrangement (29, 30) having an inlet and an outlet arranged for cooling air to be supplied to said compressor using a heat transfer medium before compression by said compressor; a heat transfer medium loop for said heat transfer medium; and a second heat exchanger arrangement (34, 35, 36) configured for cooling of said heat transfer medium by fuel delivered by the first or second fuel delivery system.
An inductor for a welding power supply, comprising: an L shaped core element, having a short side core section and a long side core section; a T shaped core element, the T shaped core element having a central extension core section with an end disposed adjacent to the short side of the L shaped core element and a top core section disposed adjacent to the long side of the L shaped core element; combs disposed about the central extension of the T shaped core element; and a winding disposed in the combs and spaced from the core elements (62, 64), characterized by spacers disposed between the L and T shaped core elements (62, 64) at locations where their core sections approach one another; connection pieces welded on opposite sides of the inductor between the T shaped core element and the L shaped core element. an L shaped core element, having a short side core section and a long side core section; a T shaped core element, the T shaped core element having a central extension core section with an end disposed adjacent to the short side of the L shaped core element and a top core section disposed adjacent to the long side of the L shaped core element; combs disposed about the central extension of the T shaped core element; and a winding disposed in the combs and spaced from the core elements (62, 64), characterized by spacers disposed between the L and T shaped core elements (62, 64) at locations where their core sections approach one another; connection pieces welded on opposite sides of the inductor between the T shaped core element and the L shaped core element.