mhurhangee/patent-ind-claim-en huggingface dataset:
Bellows element of a bellows for forming a tunnel-shaped transition protection between two vehicle members interconnected in an articulated manner, wherein the bellows element comprises, at least in sections, a cross-sectional profile which is open at one side, which cross-sectional profile comprises a central section and two mutually opposite side sections projecting from the central section , wherein the bellows element comprises a plurality of frame bellows elements , which frame bellows elements are connected to one another in a frame-like manner, wherein a connecting arch connecting two frame bellows elements to one another along a longitudinal arch axis is formed between every two frame bellows elements , wherein the connecting arches each comprise a central arch segment and two side arch segments fastened to the central arch segment , wherein the central arch segment extends in the central section of the cross-sectional profile which is open at one side and the two side arch segments extend in the side sections , wherein the central arch segment and the two side arch segments overlap in a central overlap region , characterized in that at least one of the connecting arches has a central arch segment with a sleeve section arranged at the end, wherein the sleeve section extends up into the side sections of the cross-sectional profile which is open at one side, so that additional lateral overlap regions are formed in the sleeve section between the side arch segments and the central arch segment .
A drive shaft for selectively connecting a drive input to an output , said drive shaft comprising: a tubular portion (32; 260; 304); a first diaphragm member (28, 252; 300); and a second diaphragm member displaced axially along the drive shaft from the first diaphragm member, said first and second diaphragm members each being formed with two axial ends and at least one undulation extending radially of said ends, and the tubular portion connecting said first and second diaphragm members, said first and second diaphragm members and said tubular portion being formed of fiber-reinforced polymer matrix composites, and said first and second diaphragm members connected to first and second axial ends of said tubular portion through a mechanical connection at joints ; and characterised in that said mechanical connection includes welding of said axial ends of each of said first and second diaphragms to said tubular portion, wherein said mechanical connection receives reinforcement; and wherein said reinforcement includes teeth on said first and second diaphragms interfitting with teeth at said axial ends of said tubular portion, wherein said teeth on said first and second diaphragms are circumferentially spaced with said teeth at said ends of said tubular portion. a tubular portion (32; 260; 304); a first diaphragm member (28, 252; 300); and a second diaphragm member displaced axially along the drive shaft from the first diaphragm member, said first and second diaphragm members each being formed with two axial ends and at least one undulation extending radially of said ends, and the tubular portion connecting said first and second diaphragm members, said first and second diaphragm members and said tubular portion being formed of fiber-reinforced polymer matrix composites, and said first and second diaphragm members connected to first and second axial ends of said tubular portion through a mechanical connection at joints ; and characterised in that said mechanical connection includes welding of said axial ends of each of said first and second diaphragms to said tubular portion, wherein said mechanical connection receives reinforcement; and wherein said reinforcement includes teeth on said first and second diaphragms interfitting with teeth at said axial ends of said tubular portion, wherein said teeth on said first and second diaphragms are circumferentially spaced with said teeth at said ends of said tubular portion.
A hybrid gas turbine engine system (201; 301) of a hybrid electric aircraft (200; 300), the hybrid gas turbine engine system comprising: a gas turbine engine ; an electric motor operable to perform an electric taxiing of the hybrid electric aircraft; and a controller operable to: prevent fuel flow to the gas turbine engine during at least a portion of the electric taxiing; monitor for a powered warm-up request during the electric taxiing; initiate a powered warm-up state of the gas turbine engine based on detecting the powered warm-up request, wherein the powered warm-up state adds heat to one or more components of the gas turbine engine prior to transitioning to a takeoff power state; and transition the gas turbine engine from the powered warm-up state to the takeoff power state after reaching a target temperature of the one or more components in the powered warm-up state; characterised in that the powered warm-up state comprises enabling one or more electric heaters , and/or the controller is configured to command a combination of vane positions and power setting of the gas turbine engine that reduces a compressor efficiency of the gas turbine engine to increase temperature at or below idle thrust in the powered warm-up state . a gas turbine engine ; an electric motor operable to perform an electric taxiing of the hybrid electric aircraft; and a controller operable to: prevent fuel flow to the gas turbine engine during at least a portion of the electric taxiing; monitor for a powered warm-up request during the electric taxiing; initiate a powered warm-up state of the gas turbine engine based on detecting the powered warm-up request, wherein the powered warm-up state adds heat to one or more components of the gas turbine engine prior to transitioning to a takeoff power state; and transition the gas turbine engine from the powered warm-up state to the takeoff power state after reaching a target temperature of the one or more components in the powered warm-up state; characterised in that prevent fuel flow to the gas turbine engine during at least a portion of the electric taxiing; monitor for a powered warm-up request during the electric taxiing; initiate a powered warm-up state of the gas turbine engine based on detecting the powered warm-up request, wherein the powered warm-up state adds heat to one or more components of the gas turbine engine prior to transitioning to a takeoff power state; and transition the gas turbine engine from the powered warm-up state to the takeoff power state after reaching a target temperature of the one or more components in the powered warm-up state; characterised in that the powered warm-up state comprises enabling one or more electric heaters , and/or the controller is configured to command a combination of vane positions and power setting of the gas turbine engine that reduces a compressor efficiency of the gas turbine engine to increase temperature at or below idle thrust in the powered warm-up state .
Lining element of a duct, conveying hot gas, of an intermediate turbine housing of a gas turbine, in particular an aircraft gas turbine, having a first connection portion (12; 112) which is axially at the front relative to a machine axis of the gas turbine, a second connection portion (14; 114) which is axially at the rear, and a central portion (16; 116) which is connected to the first connection portion (12; 112) and the second connection portion (14; 114) and is arranged therebetween in the axial direction (AR), the central portion (16; 116) having an outer surface (20; 120) facing away from the duct, and it being possible to couple the first connection portion (12; 112) to axially forward components of the intermediate turbine housing or the gas turbine, and it being possible to couple the second connection portion (14; 114) to axially rear components of the intermediate turbine housing or the gas turbine, the central portion (16; 116) having at least one first reinforcement portion (24; 124) that protrudes away from the duct and extends substantially in a straight line between an axially forward end and an axially rear end, a second reinforcement portion (26; 126) that protrudes away from the duct being connected to at least one of the two axial ends, which second reinforcement portion is inclined or curved relative to the straight extension of the first reinforcement portion (24; 124), the first reinforcement portion (24; 124) and the second reinforcement portion (26; 126) together forming a reinforcement element (22; 122), the reinforcement element (22; 122) being at a distance from the first connection portion (12; 112) and from the second connection portion (14; 114), characterized in that the reinforcement element (22; 122) is at a distance in the circumferential direction (UR) from lateral edge portions (18; 118) of the lining element (10; 110) which protrude from the outer surface (20; 120) of the central portion (16; 116) at least in the radial direction (RR), such that the entire reinforcement element (22; 122) is arranged within the outer surface (20; 120) of the central portion (16; 116) and is not directly connected to the connection portions and the lateral edge portions of the lining element.
Method for operating a plurality of vehicles, - wherein navigation data for autonomous navigation of the first vehicle in a carpark are transmitted to a first vehicle via a communication network, - wherein the first vehicle is assigned as a lead vehicle to a second vehicle, which first vehicle the second vehicle is to follow autonomously by means of its driving assistance systems, wherein - while the second vehicle follows the lead vehicle autonomously during the autonomous navigation of the lead vehicle in the carpark, a target signal is transmitted to the second vehicle via the communication network, said signal causing the second vehicle to break off the following process and to stop at a target position. - wherein navigation data for autonomous navigation of the first vehicle in a carpark are transmitted to a first vehicle via a communication network, - wherein the first vehicle is assigned as a lead vehicle to a second vehicle, which first vehicle the second vehicle is to follow autonomously by means of its driving assistance systems, wherein - while the second vehicle follows the lead vehicle autonomously during the autonomous navigation of the lead vehicle in the carpark, a target signal is transmitted to the second vehicle via the communication network, said signal causing the second vehicle to break off the following process and to stop at a target position.
Compound needle for knitting machines, having the following features: a) a needle , which extends substantially in the needle's longitudinal direction (x) and has a hook at its front end in the needle's longitudinal direction (x), b) a slider , - which also extends substantially in the needle's longitudinal direction (x), - which is adapted to the needle in such a way that, within the slider's working portion , relative movement between needle and slider is possible - and which has a closing lip for closing the hook of the needle , c) wherein the needle has a fork comprising at least two fork arms , which are mutually offset in the needle's height direction (y) and extend beside each other in the needle's longitudinal direction (x), d) wherein at least one fork arm is a guiding element for the slider during relative movement between needle and slider , e) and wherein the slider has at least one functional element which keeps it within its working portion during relative movement between needle and slider characterised in that f) the needle has at least one hole with which the at least one functional element of the slider engages. a) a needle , which extends substantially in the needle's longitudinal direction (x) and has a hook at its front end in the needle's longitudinal direction (x), b) a slider , - which also extends substantially in the needle's longitudinal direction (x), - which is adapted to the needle in such a way that, within the slider's working portion , relative movement between needle and slider is possible - and which has a closing lip for closing the hook of the needle , - which also extends substantially in the needle's longitudinal direction (x), - which is adapted to the needle in such a way that, within the slider's working portion , relative movement between needle and slider is possible - and which has a closing lip for closing the hook of the needle , c) wherein the needle has a fork comprising at least two fork arms , which are mutually offset in the needle's height direction (y) and extend beside each other in the needle's longitudinal direction (x), d) wherein at least one fork arm is a guiding element for the slider during relative movement between needle and slider , e) and wherein the slider has at least one functional element which keeps it within its working portion during relative movement between needle and slider characterised in that f) the needle has at least one hole with which the at least one functional element of the slider engages.
A method of manufacturing semiconductor devices , the method comprising: - providing a plastic material substrate having at least one die mounting location for a semiconductor die , wherein said plastic material substrate comprises laser direct structuring material, - forming metallic traces on selected areas of said plastic material substrate , wherein said metallic traces provide electrically-conductive paths for coupling to said semiconductor die , and wherein forming said metallic traces on selected areas of said plastic material substrate comprises laser activating said laser direct structuring material, - attaching said semiconductor die onto said at least one die mounting location , - bonding said semiconductor die attached onto said at least one die mounting location to selected ones of said metallic traces formed on the plastic material substrate , - molding package material onto said semiconductor die attached onto said at least one die mounting location . - providing a plastic material substrate having at least one die mounting location for a semiconductor die , wherein said plastic material substrate comprises laser direct structuring material, - forming metallic traces on selected areas of said plastic material substrate , wherein said metallic traces provide electrically-conductive paths for coupling to said semiconductor die , and wherein forming said metallic traces on selected areas of said plastic material substrate comprises laser activating said laser direct structuring material, - attaching said semiconductor die onto said at least one die mounting location , - bonding said semiconductor die attached onto said at least one die mounting location to selected ones of said metallic traces formed on the plastic material substrate , - molding package material onto said semiconductor die attached onto said at least one die mounting location .
Method for operating a digital web printing press , comprising: selecting a frequency (F) for actuating a digital printing head at the frequency (F) to output printing ink onto a print web , ascertaining a specified conveying speed (vs) for conveying the print web on the basis of the selected frequency (F) and printing data (D), controlling a motor (M1) driving a first roller and/or a motor (M2) driving a second roller on the basis of the specified conveying speed (vs) such that the print web between the first roller and the second roller , in particular directly below the digital printing head , is conveyed at the specified conveying speed (vs), and actuating the digital printing head at the selected frequency (F) and on the basis of the printing data (D). selecting a frequency (F) for actuating a digital printing head at the frequency (F) to output printing ink onto a print web , ascertaining a specified conveying speed (vs) for conveying the print web on the basis of the selected frequency (F) and printing data (D), controlling a motor (M1) driving a first roller and/or a motor (M2) driving a second roller on the basis of the specified conveying speed (vs) such that the print web between the first roller and the second roller , in particular directly below the digital printing head , is conveyed at the specified conveying speed (vs), and actuating the digital printing head at the selected frequency (F) and on the basis of the printing data (D).
A contact lens comprising: a. a hydrogel lens body having a Young s modulus (M); and b. a non-expandable object having a surface energy (SE) embedded within the hydrogel lens body, wherein the hydrogel of the hydrogel lens body is a silicone hydrogel; the hydrogel lens body is formed from a polymerisable composition comprising at least 10 wt% hydrophilic N-vinyl amide-containing monomer that contains a single N-vinyl polymerizable group and no other polymerizable group, the hydrogel lens body comprises an N-vinyl amide component, which is a polymer or copolymer of the hydrophilic N-vinyl amide-containing monomer; and wherein the hydrogel lens body is characterized by a bonding factor, X, of 0.01 to 1.0, wherein X is calculated using Equation I: X = SE / M ∗ 100 wherein M is in units of megapascal (MPa) and is determined using the ANSI Z80.20 standard method described in Example 1 of the description, and SE is in units of millinewton per meter (mN/m) and is determined using the Owens-Wendt method as described in Example 2 of the description. a. a hydrogel lens body having a Young s modulus (M); and b. a non-expandable object having a surface energy (SE) embedded within the hydrogel lens body,
A system that uses log based replication to transfer data between a database system that uses binary log files , and another type of database or system , comprising: a vendor access module, VAM, comprising: a first part of the VAM configured to recognize event data as recorded in a binary log file by a first or source database, convert the event data into data records in a format ready to send and store the data records in a limited size queue ; and a second part of the VAM configured to fetch a data record from the limited size queue and send the data record to an application program interface, API, of the VAM in response to a request from the VAM API, wherein the VAM API communicates with an extract process to process the data records and to generate an output containing the processed data, for use in applying the processed data to a second or target database or system . a vendor access module, VAM, comprising: a first part of the VAM configured to recognize event data as recorded in a binary log file by a first or source database, convert the event data into data records in a format ready to send and store the data records in a limited size queue ; and a second part of the VAM configured to fetch a data record from the limited size queue and send the data record to an application program interface, API, of the VAM in response to a request from the VAM API, a first part of the VAM configured to recognize event data as recorded in a binary log file by a first or source database, convert the event data into data records in a format ready to send and store the data records in a limited size queue ; and a second part of the VAM configured to fetch a data record from the limited size queue and send the data record to an application program interface, API, of the VAM in response to a request from the VAM API, wherein the VAM API communicates with an extract process to process the data records and to generate an output containing the processed data, for use in applying the processed data to a second or target database or system .
A gas barrier laminate comprising a base, a gas barrier layer and a protective layer laminated directly or via another layer in this order, wherein: a content rate of oxygen atoms is 20 to 70%, a content rate of nitrogen atoms is 0 to 30% and a content rate of silicon atoms is 25 to 50% relative to the total content of oxygen atoms, nitrogen atoms and silicon atoms in a surface layer part on a protective layer side of the gas barrier layer; a Young's modulus at 25°C of the protective layer is not less than 5 × 10 9 Pa and not more than 1 × 10 12 Pa; and characterized in that : at least one material comprised in the protective layer is a silicon-containing polymer compound. a content rate of oxygen atoms is 20 to 70%, a content rate of nitrogen atoms is 0 to 30% and a content rate of silicon atoms is 25 to 50% relative to the total content of oxygen atoms, nitrogen atoms and silicon atoms in a surface layer part on a protective layer side of the gas barrier layer; a Young's modulus at 25°C of the protective layer is not less than 5 × 10 9 Pa and not more than 1 × 10 12 Pa; and characterized in that : at least one material comprised in the protective layer is a silicon-containing polymer compound.
A display device comprising: a substrate on which light sources are disposed; a display plate that is disposed to face the substrate ; a tubular panel that surrounds and holds a periphery of the substrate and a periphery of the display plate ; and a lens that is disposed between the substrate and the display plate and guides light emitted from the light sources ; wherein the lens has at least one slide groove and at least one claw portion disposed adjacent to the at least one slide groove , characterised in that the tubular panel has at least one rib protruding from an inner peripheral surface thereof, wherein the slide groove is configured to receive the at least one rib , such that when the lens is assembled into the tubular panel , in a state where the rib of the panel enters the slide groove of the lens , the lens is configured to be slid forward, which is a first direction of the lens towards the display plate , till a rear surface of the rib abuts on a front surface of the base portion of the lens and then the lens is configured to be slid to a lateral direction, different to the first direction, and the at least one claw portion is positioned between the at least one rib and the display plate in an assembled state. a substrate on which light sources are disposed; a display plate that is disposed to face the substrate ; a tubular panel that surrounds and holds a periphery of the substrate and a periphery of the display plate ; and a lens that is disposed between the substrate and the display plate and guides light emitted from the light sources ; wherein the lens has at least one slide groove and at least one claw portion disposed adjacent to the at least one slide groove , characterised in that the tubular panel has at least one rib protruding from an inner peripheral surface thereof, wherein the slide groove is configured to receive the at least one rib , such that when the lens is assembled into the tubular panel , in a state where the rib of the panel enters the slide groove of the lens , the lens is configured to be slid forward, which is a first direction of the lens towards the display plate , till a rear surface of the rib abuts on a front surface of the base portion of the lens and then the lens is configured to be slid to a lateral direction, different to the first direction, and the at least one claw portion is positioned between the at least one rib and the display plate in an assembled state.