mhurhangee/ep-ind-claims huggingface dataset:
A method for transmitting broadcast service data in a digital broadcasting communication system, the method comprising: mapping (502, 504, 506) first broadcast service data of a plurality of services of a first type to a first zone, and mapping(502, 504, 506) second broadcast service data of a plurality of services of a second type to a second zone; and transmitting a frame comprising the first zone and the second zone, wherein each of the plurality of services of the first type is sliced into at least one sub-slice according to a first number allocated for the first zone, wherein each of the plurality of services of the second type is sliced into a plurality of sub-slices according to a second number allocated for the second zone; wherein the sub-slices per service have a same length, and wherein the first number and the second number are transmitted through control information included in the frame, and the first number is less than the second number; characterized in that said length is transmitted through the control information for each service. mapping (502, 504, 506) first broadcast service data of a plurality of services of a first type to a first zone, and mapping(502, 504, 506) second broadcast service data of a plurality of services of a second type to a second zone; and transmitting a frame comprising the first zone and the second zone, wherein each of the plurality of services of the first type is sliced into at least one sub-slice according to a first number allocated for the first zone, wherein each of the plurality of services of the second type is sliced into a plurality of sub-slices according to a second number allocated for the second zone; wherein the sub-slices per service have a same length, and wherein the first number and the second number are transmitted through control information included in the frame, and the first number is less than the second number; characterized in that said length is transmitted through the control information for each service.
A programmable integrated circuit device comprising: an input for configuration data for said programmable integrated circuit device, wherein an original portion of the configuration data is at least partially encrypted according to a first encryption scheme and an additional portion of said configuration data is at least partially encrypted according to second encryption scheme, wherein said second encryption scheme is different from the first encryption scheme; a plurality of key stores (201, 202, 203) operable to store a plurality of keys for said first and second encryption schemes; control circuitry operable to identify respective required keys from said at least partially encrypted original portion and additional portion of said configuration data and to generate respective key selection signals; and key selection circuitry responsive to said key selection signals, wherein the key selection circuitry is operable to read said plurality of key stores (201, 202, 203) and to provide said respective required keys to said control circuitry; wherein said control circuitry includes decryption circuitry operable to decrypt said at least partially encrypted original portion and additional portion of said configuration data using said respective required keys; wherein said programmable integrated circuit device is partially reconfigurable by writing said additional portion of said configuration data into said input. an input for configuration data for said programmable integrated circuit device, wherein an original portion of the configuration data is at least partially encrypted according to a first encryption scheme and an additional portion of said configuration data is at least partially encrypted according to second encryption scheme, wherein said second encryption scheme is different from the first encryption scheme; a plurality of key stores (201, 202, 203) operable to store a plurality of keys for said first and second encryption schemes; control circuitry operable to identify respective required keys from said at least partially encrypted original portion and additional portion of said configuration data and to generate respective key selection signals; and key selection circuitry responsive to said key selection signals, wherein the key selection circuitry is operable to read said plurality of key stores (201, 202, 203) and to provide said respective required keys to said control circuitry; wherein said control circuitry includes decryption circuitry operable to decrypt said at least partially encrypted original portion and additional portion of said configuration data using said respective required keys; wherein said programmable integrated circuit device is partially reconfigurable by writing said additional portion of said configuration data into said input.
A pen needle assembly, comprising: a hub; and a needle fixed to said hub, said needle having proximal and distal ends (16, 18) with a lumen extending therebetween; wherein said needle extends distally from said hub to define an exposed length between said distal end of said needle and said hub in the range of about 5.0 mm to 9.0 mm; and wherein said hub defines a post formed about said needle, said post having a distally-facing first skin engaging surface, said exposed length of said needle extending distally from said first skin engaging surface; and wherein said hub defines an annular wall defining a radially facing surface and a distally-facing second skin engaging surface which at least partially circumscribes said first skin engaging surface, said second skin engaging surface being located proximally of said first skin engaging surface; wherein said second skin engaging surface is continuous; wherein said second skin engaging surface is radially displaced from said first skin engaging surface, wherein said hub defines a cavity between said first skin engaging surface and said second skin engaging surface, the cavity comprising a distally facing surface located proximally of said second skin engaging surface, and a rigid shell; characterized in that the assembly further comprises at least one snap formed on one of the radially facing surface or the rigid shell, adapted to be received and retained in a snap recess formed in the other of the radially facing surface or the rigid shell. a hub; and a needle fixed to said hub, said needle having proximal and distal ends (16, 18) with a lumen extending therebetween; wherein said needle extends distally from said hub to define an exposed length between said distal end of said needle and said hub in the range of about 5.0 mm to 9.0 mm; and wherein said hub defines a post formed about said needle, said post having a distally-facing first skin engaging surface, said exposed length of said needle extending distally from said first skin engaging surface; and wherein said hub defines an annular wall defining a radially facing surface and a distally-facing second skin engaging surface which at least partially circumscribes said first skin engaging surface, said second skin engaging surface being located proximally of said first skin engaging surface; wherein said second skin engaging surface is continuous; wherein said second skin engaging surface is radially displaced from said first skin engaging surface, wherein said hub defines a cavity between said first skin engaging surface and said second skin engaging surface, the cavity comprising a distally facing surface located proximally of said second skin engaging surface, and a rigid shell; characterized in that the assembly further comprises at least one snap formed on one of the radially facing surface or the rigid shell, adapted to be received and retained in a snap recess formed in the other of the radially facing surface or the rigid shell.
Body of a motor vehicle, comprising at least one first modular component and at least one second modular component, wherein the first modular component and the second modular component are connected to each other, wherein, in order to connect the modular components to one another, the first modular component has at least one connection extension, and the second modular component has at least one connection opening, wherein the connection extension of the first modular component is plugged through a connection opening of the second modular component, characterized in that the connection extension is of arcuate design, and the geometry of the connection opening is adapted in a manner corresponding to the arc shape of the connection extension, and therefore the connection extension can be pivoted in the connection opening.
An ultrasound probe (40; 56; 200; 330; 464; 546; 600; 620; 700; 802) mountable to the moveable member of a coordinate positioning apparatus, comprising; a transducer (92; 210; 248; 260) for transmitting and receiving ultrasound, and a coupling element (42; 104; 208; 270; 462; 548; 622; 702) for contacting and acoustically coupling to an object (62; 218; 272; 450) to be inspected, wherein the ultrasound probe (40; 56; 200; 330; 464; 546; 600; 620; 700; 802) comprises an analyser arranged to analyse the ultrasound signal received by the transducer (92; 210; 248; 260) and thereby determine if there is contact between the coupling element (42; 104; 208; 270; 462; 548; 622; 702) and the surface of said object (62; 218; 272; 450), the ultrasound probe (40; 56; 200; 330; 464; 546; 600; 620; 700; 802) being arranged for outputting a trigger signal that indicates when the analyser has determined the coupling element (42; 104; 208; 270; 462; 548; 622; 702) is in contact with said object (62; 218; 272; 450).
Compounds of the formula in which A represents an optionally C 1 -C 4 -alkyl-substituted C 1 -C 4 -alkanediyl group or represents optionally C 1 -C 4 -alkyl-substituted C 5 -C 8 -cycloalkyl in which optionally one methylene group is replaced by oxygen, B represents optionally halogen-substituted C 2 -C 8 -alkenyl, C 1 -C 6 -alkoxy, C 1 -C 6 -alkoxy-C 1 -C 4 -alkyloxy, represents optionally halogen-, C 1 -C 6 -alkyl-, C 1 -C 6 -alkoxy-, C 1 -C 4 -haloalkyl-, C 1 -C 4 -haloalkoxy, cyano- or nitro-substituted phenyl, represents optionally halogen-, C 1 -C 4 -alkyl- or C 1 -C 2 -haloalkyl-substituted pyridyl, pyrimidyl, thiazolyl or thienyl or represents optionally halogen-, C 1 -C 4 -alkyl-, C 1 -C 4 -alkoxy- or C 1 -C 2 -haloalkyl-substituted C 3 -C 8 -cycloalkyl in which optionally one or two not directly adjacent methylene groups are replaced by oxygen or three methylene groups are replaced by the radical -O-CO-O-, R 8 represents alkyl. A represents an optionally C 1 -C 4 -alkyl-substituted C 1 -C 4 -alkanediyl group or represents optionally C 1 -C 4 -alkyl-substituted C 5 -C 8 -cycloalkyl in which optionally one methylene group is replaced by oxygen, B represents optionally halogen-substituted C 2 -C 8 -alkenyl, C 1 -C 6 -alkoxy, C 1 -C 6 -alkoxy-C 1 -C 4 -alkyloxy, represents optionally halogen-, C 1 -C 6 -alkyl-, C 1 -C 6 -alkoxy-, C 1 -C 4 -haloalkyl-, C 1 -C 4 -haloalkoxy, cyano- or nitro-substituted phenyl, represents optionally halogen-, C 1 -C 4 -alkyl- or C 1 -C 2 -haloalkyl-substituted pyridyl, pyrimidyl, thiazolyl or thienyl or represents optionally halogen-, C 1 -C 4 -alkyl-, C 1 -C 4 -alkoxy- or C 1 -C 2 -haloalkyl-substituted C 3 -C 8 -cycloalkyl in which optionally one or two not directly adjacent methylene groups are replaced by oxygen or three methylene groups are replaced by the radical -O-CO-O-, R 8 represents alkyl.
An operating fluid container for a motor vehicle for accommodating an operating fluid, wherein the operating fluid container has a compensation container that is at least indirectly fluidically connected to the atmosphere, wherein the operating fluid container has the following features: - the compensation container is situated within the operating fluid container in such a way that an outer surface of a compensation container upper shell is situated opposite from an inner surface of an operating fluid container upper shell; - in the event of positive pressure in the operating fluid container relative to the atmosphere, a compensation container volume decreases; and - in the event of negative pressure in the operating fluid container relative to the atmosphere, the compensating container volume increases; - the compensation container upper shell opposite from the operating fluid container upper shell has a shape, at least in sections, that is complementary to the operating fluid container upper shell, wherein the operating fluid container is characterized by the following features: - the compensation container upper shell and/or the compensation container lower shell have/has a barrier layer that is impermeable to gaseous components of the operating fluid; and - the compensation container upper shell and/or the compensation container lower shell have/has a multilayer structure. - the compensation container is situated within the operating fluid container in such a way that an outer surface of a compensation container upper shell is situated opposite from an inner surface of an operating fluid container upper shell; - in the event of positive pressure in the operating fluid container relative to the atmosphere, a compensation container volume decreases; and - in the event of negative pressure in the operating fluid container relative to the atmosphere, the compensating container volume increases; - the compensation container upper shell opposite from the operating fluid container upper shell has a shape, at least in sections, that is complementary to the operating fluid container upper shell, - the compensation container upper shell and/or the compensation container lower shell have/has a barrier layer that is impermeable to gaseous components of the operating fluid; and - the compensation container upper shell and/or the compensation container lower shell have/has a multilayer structure.
Coated substrate for packaging applications comprising - a recrystallisation annealed single reduced steel substrate or - a double reduced steel substrate which was subjected to recrystallisation annealing between the first and second cold rolling treatment, wherein one or both sides of the substrate is coated with an iron-tin alloy layer which contains at least 80 weight percent (wt.%) of FeSn (50 at.% iron and 50 at.% tin) and wherein the iron-tin alloy layer or layers are provided with a chromium metal - chromium oxide coating layer produced by a trivalent chromium electroplating process, and wherein the thickness of the chromium metal - chromium oxide coating layer corresponds to at least 20 mg Cr/m 2. - a recrystallisation annealed single reduced steel substrate or - a double reduced steel substrate which was subjected to recrystallisation annealing between the first and second cold rolling treatment,
A center air jet burner comprising: an axial zone concentrically surrounded by a first annular zone, the first annular zone concentrically surrounded by a second annular zone, and the second annular zone concentrically surrounded by a third annular zone, where in the axial zone, the first annular zone, the second annular zone and the third annular zone are separated by an axial pipe, an annular pipe, and a barrel, respectively, a feeder duct radially interposed between a portion of the first annular zone and the axial zone, wherein the feeder duct provides a gas comprising oxygen to the axial zone, a means for regulating flow of the gas through the feeder duct a means for providing the first annular zone with a combustible fuel, a means for providing air to the second annular zone, and a means for providing air to the third annular zone, wherein the axial zone and the second and third annular zones provide secondary air for combustion, and wherein the gas comprising oxygen exits the axial zone to form the center air jet. an axial zone concentrically surrounded by a first annular zone, the first annular zone concentrically surrounded by a second annular zone, and the second annular zone concentrically surrounded by a third annular zone, where in the axial zone, the first annular zone, the second annular zone and the third annular zone are separated by an axial pipe, an annular pipe, and a barrel, respectively, a feeder duct radially interposed between a portion of the first annular zone and the axial zone, wherein the feeder duct provides a gas comprising oxygen to the axial zone, a means for regulating flow of the gas through the feeder duct a means for providing the first annular zone with a combustible fuel, a means for providing air to the second annular zone, and a means for providing air to the third annular zone, wherein the axial zone and the second and third annular zones provide secondary air for combustion, and wherein the gas comprising oxygen exits the axial zone to form the center air jet.
A fiber optic ribbon, comprising: optical fibers, each optical fiber comprising a core surrounded by a cladding; edge bonding rigidly connecting the optical fibers to one another in a side-by-side arrangement; characterized in that the fiber optic ribbon comprises: a stress-isolation layer surrounding the optical fibers and the edge bonding, wherein the edge bonding limits independent movement of the optical fibers relative to one another within the stress-isolation layer; and a hardened shell surrounding the optical fibers, the edge bonding, and the stress-isolation layer, the hardened shell defining an exterior of the fiber optic ribbon, wherein, at 25° Celsius and at sea level, the Young's modulus of elasticity of the hardened shell is, on average, at least twice that of the stress-isolation layer and the Young's modulus of elasticity of the edge bonding is, on average, at least twice that of the stress-isolation layer. optical fibers, each optical fiber comprising a core surrounded by a cladding; edge bonding rigidly connecting the optical fibers to one another in a side-by-side arrangement; characterized in that the fiber optic ribbon comprises: a stress-isolation layer surrounding the optical fibers and the edge bonding, wherein the edge bonding limits independent movement of the optical fibers relative to one another within the stress-isolation layer; and a hardened shell surrounding the optical fibers, the edge bonding, and the stress-isolation layer, the hardened shell defining an exterior of the fiber optic ribbon, a stress-isolation layer surrounding the optical fibers and the edge bonding, wherein the edge bonding limits independent movement of the optical fibers relative to one another within the stress-isolation layer; and a hardened shell surrounding the optical fibers, the edge bonding, and the stress-isolation layer, the hardened shell defining an exterior of the fiber optic ribbon, wherein, at 25° Celsius and at sea level, the Young's modulus of elasticity of the hardened shell is, on average, at least twice that of the stress-isolation layer and the Young's modulus of elasticity of the edge bonding is, on average, at least twice that of the stress-isolation layer.
Protection device for joining the end of a power cable, the power cable (3, 33) comprising a central conductor, an insulation around the conductor based on paper impregnated with a material based on an impregnation oil, and a sheath around the insulation, a first portion of the cable being stripped of the sheath, an adjacent portion of the cable being stripped of both insulation and sheath, the central conductor penetrating a connector, the protection device comprising an external protection extending at least over the first and the adjacent portions of cable and over the connector, and comprising a continuous barrier layer placed in contact with the insulation, the continuous barrier layer being made of an elastomer material that is impermeable to the impregnation oil, the continuous barrier covering the first stripped portion of the oil impregnated paper insulation and extending axially to the stripped end of said insulation which is close to the connector, a mastic material filling an axial space extending along the adjacent portion of the cable, the mastic material having a high permittivity and separating the stripped end of the insulation and the opposite end of the connector, characterized in that the continuous barrier layer is either a helically wound tape or a sheet wound with overlapping edges around the cable, the elastomer material of the continuous barrier layer being chosen from the group of butadiene nitrile rubbers, chlorinated polyethylene, chlorosulfonated polyethylene, epichlorhydrine, butyl-type polymers or a blend thereof, having a Mooney viscosity of between 12 and 90 at 100°C, and preferably of between 15 and 60 at 100°C, and a water vapour permeation of less than 3.123 x 10 -15 Kg/m.s.Pa (1.5 x 10 -8 g/cm.h.mmHg) at 60°C and/or less than 4.165 x 10 -16 Kg/m.s.Pa (2 x 10 -9 g/cm.h.mmHg) at 25°C.
A gas turbine engine system comprising: a compressor configured to compress a first working medium; a heater configured to heat the compressed first working medium utilizing an external heat source; a turbine configured to output power from the first working medium; an intermediate cooler provided at the compressor and configured to cool the first working medium compressed by a low-pressure compression part of the compressor and supply the first working medium to a high-pressure compression part of the compressor; an exhaust heat boiler using as a heating medium an exhaust gas discharged from the turbine; and a Rankine cycle engine using the intermediate cooler and the exhaust heat boiler as a heat source and a cooling medium of the intermediate cooler as a second working medium; characterized in that the exhaust heat boiler and the intermediate cooler are provided in series in this order and are configured to cool the first working medium compressed by the low-pressure compression part. a compressor configured to compress a first working medium; a heater configured to heat the compressed first working medium utilizing an external heat source; a turbine configured to output power from the first working medium; an intermediate cooler provided at the compressor and configured to cool the first working medium compressed by a low-pressure compression part of the compressor and supply the first working medium to a high-pressure compression part of the compressor; an exhaust heat boiler using as a heating medium an exhaust gas discharged from the turbine; and a Rankine cycle engine using the intermediate cooler and the exhaust heat boiler as a heat source and a cooling medium of the intermediate cooler as a second working medium; characterized in that the exhaust heat boiler and the intermediate cooler are provided in series in this order and are configured to cool the first working medium compressed by the low-pressure compression part.