mhurhangee/patent-ind-claim-en huggingface dataset:
A baby crib provided with a continuously height adjustable mattress support , comprising: a side unit and end unit ; a horizontal mattress support ; two solely vertically displaceable driven components each connected to an opposite end unit of the baby crib and connected to, or being in supporting relation with, the horizontal mattress support ; two drive units (56A 56B) for applying a vertical force to the two driven components , said driven components being two pneumatically actuated pistons , each piston being connected to a respective drive unit ; at least one stabilizing means connected to the baby crib side unit or end unit and to said mattress support directly for stabilizing said mattress support , said stabilizing means being a vertically oriented linear bearing ; at least one actuator associated with two drive units for setting and continuously adjusting a height of said mattress support above a floor surface; wherein the baby crib comprises two L-shaped attachment plates that are connected to one of said pistons and to said linear bearing respectively. a side unit and end unit ; a horizontal mattress support ; two solely vertically displaceable driven components each connected to an opposite end unit of the baby crib and connected to, or being in supporting relation with, the horizontal mattress support ; two drive units (56A 56B) for applying a vertical force to the two driven components , said driven components being two pneumatically actuated pistons , each piston being connected to a respective drive unit ; at least one stabilizing means connected to the baby crib side unit or end unit and to said mattress support directly for stabilizing said mattress support , said stabilizing means being a vertically oriented linear bearing ; at least one actuator associated with two drive units for setting and continuously adjusting a height of said mattress support above a floor surface; wherein the baby crib comprises two L-shaped attachment plates that are connected to one of said pistons and to said linear bearing respectively.
An X-ray imageable polymer particle comprising bismuth as a radiopacifying agent, wherein the polymer has covalently bound thereto a compound of Formula or Formula : wherein: A is covalent bond or a functional group; L is a C 1 -C 12 linking group; G is a residue of a functional group; n is an integer corresponding to one less than the valence of L, and is 1 to 6; and * is a point of covalent attachment to the polymer. A is covalent bond or a functional group; L is a C 1 -C 12 linking group; G is a residue of a functional group; n is an integer corresponding to one less than the valence of L, and is 1 to 6; and * is a point of covalent attachment to the polymer.
A secure element (SC) including first and second profiles (PR1, PR2) comprising files organized in respective first and second logical tree structures, characterized in that said first logical tree structure includes a first root file (RF1) and said second logical tree structure includes a second root file (RF2), in that said root files (RF1, RF2) have identifiers whose values are different from 0x3F00 and in that said secure element (SC) is configured to enable browsing of the logical tree structure comprising a targeted root file in response to the receipt of a Select file command aiming at selecting said targeted root file.
Method for assembling an aircraft pylon, said aircraft pylon comprising: - a primary structure comprising upper and lower longerons , transverse frames connecting the upper and lower longerons , and a first and a second lateral panel arranged on either side of the transverse frames , - a secondary structure which encloses the primary structure, - at least one internal system that is at least partially positioned inside the primary structure , - and at least one external system that is positioned outside the primary structure , the assembly method comprising the following steps, in chronological order: - assembling the primary structure with the exception of at least one of the first and second lateral panels so as to obtain a primary structure having at least one lateral face left open, - installing the internal system inside the primary structure from the open lateral face of the primary structure , and - securing the first and/or second lateral panel in order to close each lateral face that was previously open. - a primary structure comprising upper and lower longerons , transverse frames connecting the upper and lower longerons , and a first and a second lateral panel arranged on either side of the transverse frames , - a secondary structure which encloses the primary structure, - at least one internal system that is at least partially positioned inside the primary structure , - and at least one external system that is positioned outside the primary structure , - assembling the primary structure with the exception of at least one of the first and second lateral panels so as to obtain a primary structure having at least one lateral face left open, - installing the internal system inside the primary structure from the open lateral face of the primary structure , and - securing the first and/or second lateral panel in order to close each lateral face that was previously open.
Element of an aircraft , said element having: - a leading edge forming a box structure delimited by a wall and a skin that constitutes a pressure face and a suction face of the element and is pierced with holes , wherein the wall connects an inner face of the pressure face to an inner face of the suction face, wherein the skin has an electrically conductive inner wall , an electrically conductive outer wall and an intermediate wall that is disposed between the inner wall and the outer wall and is electrically insulating, - a pump provided to pump out the air present in the box structure and/or to inject air into the box structure , said element being characterized in that each hole is equipped with an anti-clogging system that has: - an electrically conductive base that is electrically continuous with the inner wall , - a needle made of a piezoelectric material and housed in the hole , and one end of which is secured to the base , - an electric generator intended to generate an electric current in the needle , wherein the shape of the needle is such that a space is created between the needle and the edges of the hole , and wherein the base has a recess in the continuation of the space . - a leading edge forming a box structure delimited by a wall and a skin that constitutes a pressure face and a suction face of the element and is pierced with holes , wherein the wall connects an inner face of the pressure face to an inner face of the suction face, wherein the skin has an electrically conductive inner wall , an electrically conductive outer wall and an intermediate wall that is disposed between the inner wall and the outer wall and is electrically insulating, - a pump provided to pump out the air present in the box structure and/or to inject air into the box structure , - an electrically conductive base that is electrically continuous with the inner wall , - a needle made of a piezoelectric material and housed in the hole , and one end of which is secured to the base , - an electric generator intended to generate an electric current in the needle ,
A saddle-ride type vehicle comprising: a vehicle body frame ; a rear wheel unit swingably supported on the vehicle body frame ; an electric motor for driving a rear wheel (WR); a fuel cell unit supported on the vehicle body frame ; a fuel tank extending rearwardly from the fuel cell unit over the rear wheel unit ; a secondary cell that is charged with electric power from the fuel cell unit and disposed below the fuel cell unit and the fuel tank , and a controller for controlling electric power supplied to the electric motor generating a drive force for the rear wheel (WR), the controller being disposed below the fuel tank and behind the secondary cell ; characterized in that the controller is disposed below the fuel cell unit , and the controller and the secondary cell are assembled and fixed to an electrical component cover mounted on the vehicle body frame, such that after the controller and the secondary cell are assembled on the electrical component cover , the electrical component cover which is part of a vehicle body cover can be installed together with the fuel cell unit on the vehicle body frame . a vehicle body frame ; a rear wheel unit swingably supported on the vehicle body frame ; an electric motor for driving a rear wheel (WR); a fuel cell unit supported on the vehicle body frame ; a fuel tank extending rearwardly from the fuel cell unit over the rear wheel unit ; a secondary cell that is charged with electric power from the fuel cell unit and disposed below the fuel cell unit and the fuel tank , and a controller for controlling electric power supplied to the electric motor generating a drive force for the rear wheel (WR), the controller being disposed below the fuel tank and behind the secondary cell ; characterized in that the controller is disposed below the fuel cell unit , and the controller and the secondary cell are assembled and fixed to an electrical component cover mounted on the vehicle body frame, such that after the controller and the secondary cell are assembled on the electrical component cover , the electrical component cover which is part of a vehicle body cover can be installed together with the fuel cell unit on the vehicle body frame .
Manually tearable textile adhesive tape, having a woven carrier strip, at least one side of which is coated with an adhesive, wherein the carrier strip is constructed from longitudinal threads and transverse threads, characterized in that - individual threads have a tear resistance that is reduced by 5 % to 60 %, determined according to DIN EN 14 410, which has been adjusted by a treatment with a treatment fluid to reduce the tear resistance prior to the weaving, wherein - all or selected longitudinal threads of the carrier strip have been treated and exhibit the reduced tear resistance, whereas - the transverse threads are untreated threads with unchanged tear resistance in comparison therewith. - individual threads have a tear resistance that is reduced by 5 % to 60 %, determined according to DIN EN 14 410, which has been adjusted by a treatment with a treatment fluid to reduce the tear resistance prior to the weaving, wherein - all or selected longitudinal threads of the carrier strip have been treated and exhibit the reduced tear resistance, whereas - the transverse threads are untreated threads with unchanged tear resistance in comparison therewith.
An outdoor unit of an air-conditioning apparatus, the outdoor unit comprising: an outer casing having a back portion and a side portion , the outer casing including a body in which a first opening is formed to be continuous in the side portion and the back portion , and a first panel that covers the first opening , wherein the first panel includes a side panel that covers a part formed in the side portion of the first opening , a back panel that covers a part formed in the back portion of the first opening , and a plurality of claw portions, one of the plurality of claw portions is a first claw portion that has a plate-like shape and that protrudes upward from an upper end portion of the back panel , the back portion of the body includes a first plate having a lower end portion in which a cutout is formed, characterized in that the cross section of the first panel has an L shape, the back portion of the outer casing further includes a second plate disposed forward of the first plate with a predetermined distance between the first plate and the second plate , and when the first claw portion is inserted into the cutout , and the first panel is moved in a direction in which the side panel approaches the side portion , the first claw portion is disposed between the first plate and the second plate . an outer casing having a back portion and a side portion , the outer casing including a body in which a first opening is formed to be continuous in the side portion and the back portion , and a first panel that covers the first opening , wherein the first panel includes a side panel that covers a part formed in the side portion of the first opening , a back panel that covers a part formed in the back portion of the first opening , and a plurality of claw portions, a body in which a first opening is formed to be continuous in the side portion and the back portion , and a first panel that covers the first opening , wherein the first panel includes a side panel that covers a part formed in the side portion of the first opening , a back panel that covers a part formed in the back portion of the first opening , and a plurality of claw portions, a side panel that covers a part formed in the side portion of the first opening , a back panel that covers a part formed in the back portion of the first opening , and a plurality of claw portions, one of the plurality of claw portions is a first claw portion that has a plate-like shape and that protrudes upward from an upper end portion of the back panel , the back portion of the body includes a first plate having a lower end portion in which a cutout is formed, characterized in that the cross section of the first panel has an L shape, the back portion of the outer casing further includes a second plate disposed forward of the first plate with a predetermined distance between the first plate and the second plate , and when the first claw portion is inserted into the cutout , and the first panel is moved in a direction in which the side panel approaches the side portion , the first claw portion is disposed between the first plate and the second plate .
Printhead for the additive manufacturing of a fibre reinforced material, comprising fibre reinforcement in a polymer matrix, comprising: - an infiltration unit for mixing and/or infiltrating a fibre roving with a molten polymer; - at least one feeder for a polymer and/or a fibre roving to the infiltration unit ; - a heating element, for at least partial melting of the polymer within the infiltration unit ; - at least one deflecting element within the infiltration unit ; and - an outlet of the infiltration unit for the resulting fibre reinforced material from the infiltration unit , wherein the molten polymer and the fibre roving can be guided within the infiltration unit along a channel between the feeder and the outlet , and the fibre roving can be deflected within the channel by the deflecting element , area by area, transversely and/or obliquely to a straight-line movement between the feeder and the outlet , characterized in that the infiltration unit has at least one material overflow for the polymer. - an infiltration unit for mixing and/or infiltrating a fibre roving with a molten polymer; - at least one feeder for a polymer and/or a fibre roving to the infiltration unit ; - a heating element, for at least partial melting of the polymer within the infiltration unit ; - at least one deflecting element within the infiltration unit ; and - an outlet of the infiltration unit for the resulting fibre reinforced material from the infiltration unit , wherein the molten polymer and the fibre roving can be guided within the infiltration unit along a channel between the feeder and the outlet , and the fibre roving can be deflected within the channel by the deflecting element , area by area, transversely and/or obliquely to a straight-line movement between the feeder and the outlet , characterized in that the infiltration unit has at least one material overflow for the polymer. wherein the molten polymer and the fibre roving can be guided within the infiltration unit along a channel between the feeder and the outlet , and the fibre roving can be deflected within the channel by the deflecting element , area by area, transversely and/or obliquely to a straight-line movement between the feeder and the outlet , characterized in that the infiltration unit has at least one material overflow for the polymer.
A method for controlling a physical layer state, comprising: receiving , by a base station, a notification sent from a radio network controller, RNC, wherein the notification is sent by the RNC according to capability information of a terminal and access layer version information of the terminal, wherein the capability information of the terminal and the access layer version information of the terminal are sent by the terminal to the RNC, and the capability information of the terminal is that the terminal is supporting a dual-cell high speed downlink packet access, DC-HSDPA, feature; and sending, by the base station according to the notification, a high speed shared control channel, HS-SCCH, order to the terminal for controlling a DC-HSDPA physical layer state of the terminal when the access layer version information of the terminal is a universal mobile telecommunications system, UMTS, release 9, R9, or a universal mobile telecommunications system, UMTS, version later than UMTS R9; or not sending, by the base station according to the notification, a high speed shared control channel, HS-SCCH, order to the terminal for controlling a DC-HSDPA physical layer state of the terminal when the access layer version information of the terminal is a universal mobile telecommunications system, UMTS, release 8, R8, or a universal mobile telecommunications system, UMTS, version earlier than UMTS R8. receiving , by a base station, a notification sent from a radio network controller, RNC, wherein the notification is sent by the RNC according to capability information of a terminal and access layer version information of the terminal, wherein the capability information of the terminal and the access layer version information of the terminal are sent by the terminal to the RNC, and the capability information of the terminal is that the terminal is supporting a dual-cell high speed downlink packet access, DC-HSDPA, feature; and sending, by the base station according to the notification, a high speed shared control channel, HS-SCCH, order to the terminal for controlling a DC-HSDPA physical layer state of the terminal when the access layer version information of the terminal is a universal mobile telecommunications system, UMTS, release 9, R9, or a universal mobile telecommunications system, UMTS, version later than UMTS R9; or not sending, by the base station according to the notification, a high speed shared control channel, HS-SCCH, order to the terminal for controlling a DC-HSDPA physical layer state of the terminal when the access layer version information of the terminal is a universal mobile telecommunications system, UMTS, release 8, R8, or a universal mobile telecommunications system, UMTS, version earlier than UMTS R8.
A method for operating a gas turbine engine comprising a fan, a core in flow communication with the fan, and a nacelle assembly enclosing the fan and at least a portion of the core to define a bypass passage with the core, the nacelle assembly including a thrust reverser system moveable between a fully stowed position and a fully deployed position, the method comprising: operating at the fan at a fan pressure ratio of less than two ; characterized in moving at the thrust reverser system from the fully stowed position to a partially deployed position, the partially deployed position located between the fully stowed position and the fully deployed position, wherein moving the thrust reverser system from the fully stowed position to the partially deployed position comprises translating a transcowl aftward and moving each cascade segment of a cascade system aftward with the transcowl; and holding at the thrust reverser system in the partially deployed position to allow an additional amount of airflow to exit the bypass passage. operating at the fan at a fan pressure ratio of less than two ; characterized in moving at the thrust reverser system from the fully stowed position to a partially deployed position, the partially deployed position located between the fully stowed position and the fully deployed position, wherein moving the thrust reverser system from the fully stowed position to the partially deployed position comprises translating a transcowl aftward and moving each cascade segment of a cascade system aftward with the transcowl; and holding at the thrust reverser system in the partially deployed position to allow an additional amount of airflow to exit the bypass passage.
A method of coating a metal substrate comprising steel, the method comprising disposing the metal substrate as an anode in an electrolytic circuit comprising an aqueous alkaline liquid electrolyte, and applying an electrical voltage differential to the metal substrate and a cathode; disposing the anodic alkaline electrolytically-treated metal substrate as an anode in an electrolytic circuit comprising a liquid electrolyte that comprises an ionic liquid, and applying an electrical voltage differential to the metal substrate and a cathode; subjecting the anodic ionic electrolytically-treated metal substrate to ultrasonic cleaning; and disposing the ultrasonically cleaned metal substrate as a cathode in an electrolytic circuit comprising a liquid electrolyte that comprises an ionic liquid and an aluminum salt, and applying an electrical voltage differential to the metal substrate and an anode to form a layer comprising aluminum on the metal substrate. disposing the metal substrate as an anode in an electrolytic circuit comprising an aqueous alkaline liquid electrolyte, and applying an electrical voltage differential to the metal substrate and a cathode; disposing the anodic alkaline electrolytically-treated metal substrate as an anode in an electrolytic circuit comprising a liquid electrolyte that comprises an ionic liquid, and applying an electrical voltage differential to the metal substrate and a cathode; subjecting the anodic ionic electrolytically-treated metal substrate to ultrasonic cleaning; and disposing the ultrasonically cleaned metal substrate as a cathode in an electrolytic circuit comprising a liquid electrolyte that comprises an ionic liquid and an aluminum salt, and applying an electrical voltage differential to the metal substrate and an anode to form a layer comprising aluminum on the metal substrate.