mhurhangee/ep-ind-claims huggingface dataset:
A method of operating a terminal device (406, 408) to perform measurement event evaluation for measurement reporting in respect of a downlink carrier operating in a wireless telecommunications system, the method comprising: determining that measurement event evaluation for the downlink carrier should be undertaken from a start time; obtaining measurements of a parameter associated with radio channel conditions for frequency resources used by the downlink carrier during an evaluation period beginning at the start time; establishing the extent to which the downlink carrier is being transmitted during the evaluation period; and evaluating whether to send a measurement report to network infrastructure equipment by taking account of both the measurements of the parameter during the evaluation period and the extent to which the downlink carrier is being transmitted during the evaluation period; wherein the terminal device is in downlink communication with the network infrastructure equipment using a primary downlink component carrier operating on frequency resources within a first frequency band, and the downlink carrier for which measurement event evaluation is performed is a secondary component carrier using frequency resources within a second frequency band; and wherein the second frequency band comprises radio resources which are shared with wireless communication devices that are not part of the wireless telecommunications system. determining that measurement event evaluation for the downlink carrier should be undertaken from a start time; obtaining measurements of a parameter associated with radio channel conditions for frequency resources used by the downlink carrier during an evaluation period beginning at the start time; establishing the extent to which the downlink carrier is being transmitted during the evaluation period; and evaluating whether to send a measurement report to network infrastructure equipment by taking account of both the measurements of the parameter during the evaluation period and the extent to which the downlink carrier is being transmitted during the evaluation period; wherein the terminal device is in downlink communication with the network infrastructure equipment using a primary downlink component carrier operating on frequency resources within a first frequency band, and the downlink carrier for which measurement event evaluation is performed is a secondary component carrier using frequency resources within a second frequency band; and wherein the second frequency band comprises radio resources which are shared with wireless communication devices that are not part of the wireless telecommunications system.
Method for manufacturing semi-finished fibre composites, comprising the steps: a) producing film strips, comprising the steps of a1) providing a film material; a2) slitting the film material to produce said film strips; a3) stretching the film strips by applying a defined tension and/or a defined temperature; b) providing reinforcing fibres; characterized in that c) the arrangement of film strips and reinforcing fibres takes place in such a manner that said reinforcing fibres run unidirectionally and that the film strips stabilise the reinforcing fibres in their position within the semi-finished fibre composite, wherein said semi-finished fibre composite is formed as a tissue with the reinforcing fibres as warp threads and the film strips as weft threads, or as a laid fabric with reinforcing fibres running essentially parallel, which are tangled with a counter layer of film strips, or as a braided fabric in which the reinforcing fibres are guided in a first direction and the film strips are guided in a second direction opposite to said first direction. a) producing film strips, comprising the steps of a1) providing a film material; a2) slitting the film material to produce said film strips; a3) stretching the film strips by applying a defined tension and/or a defined temperature; a1) providing a film material; a2) slitting the film material to produce said film strips; a3) stretching the film strips by applying a defined tension and/or a defined temperature; b) providing reinforcing fibres; characterized in that c) the arrangement of film strips and reinforcing fibres takes place in such a manner that said reinforcing fibres run unidirectionally and that the film strips stabilise the reinforcing fibres in their position within the semi-finished fibre composite,
A support system arranged for a crown area of an aircraft, the system comprising: a crown integration panel, CIP, comprising a honeycomb panel and sheet metal, wherein the CIP provides a mounting surface for a plurality of aircraft equipment and provides an electrical ground for at least one of the aircraft equipment of the plurality of aircraft equipment; a first attachment and a second attachment attached to the CIP, wherein the first attachment and the second attachment are configured to attach to an airframe of the aircraft and to provide support for the CIP; and a crown raceway support, CRS, having a first end and a second end, wherein the first end of the CRS is attached to a first end of the CIP, and wherein the second end of the CRS is configured to attach to an outboard rail of the aircraft. a crown integration panel, CIP, comprising a honeycomb panel and sheet metal, wherein the CIP provides a mounting surface for a plurality of aircraft equipment and provides an electrical ground for at least one of the aircraft equipment of the plurality of aircraft equipment; a first attachment and a second attachment attached to the CIP, wherein the first attachment and the second attachment are configured to attach to an airframe of the aircraft and to provide support for the CIP; and a crown raceway support, CRS, having a first end and a second end, wherein the first end of the CRS is attached to a first end of the CIP, and wherein the second end of the CRS is configured to attach to an outboard rail of the aircraft.
Production plant for producing a chemical and/or pharmaceutical product, having at least two process modules (P1,..., Pn), which can be connected to one another for production purposes, and a communication network, wherein each process module (P1,..., Pn) has an electronic device, in particular a control and/or regulating device, which can be used to connect the respective process module (P1,..., Pn) to the communication network for communication purposes and is set up to control and/or regulate the respective process module (P1,..., Pn) to independently carry out a particular process section of production, wherein the electronic devices are set up in such a manner that process modules (P1,..., Pn) connected to the communication network for communication purposes can automatically communicate with one another at least in such a manner that at least one process module (P1,..., Pn) automatically requests information from at least one further process module (P1,..., Pn), wherein the requestable information comprises at least information in the form of given and/or expected process parameters with regard to the process section carried out or to be carried out by the process module (P1,..., Pn) providing this information, wherein each electronic device of a process module (P1,..., Pn) is set up to use the information obtained from a further process module (P1,..., Pn) to control and/or regulate the process module (P1,..., Pn) assigned to it, wherein at least one process module (P1,..., Pn) is modular and comprises a housing allowing simple transport of the process module (P1,..., Pn) and at least two process submodules (p1,..., pm) which are suitable for carrying out the desired process section, can be connected to one another for process engineering purposes and can be connected to the communication network for communication purposes, and are arranged in the housing.
An assembly for an aircraft propulsion system, comprising: a core of a gas turbine engine; a nacelle inner structure comprising an internal compartment and a cowl; the internal compartment configured to house the core of the gas turbine engine; the cowl configured to form an outer radial periphery of the internal compartment, and the cowl further configured to form an outer radial periphery of a compartment exhaust for the internal compartment at an aft end of the cowl; and a deflection limiter attached to the cowl, the deflection limiter configured to limit radial outward movement of the cowl; wherein the deflection limiter extends radially between an inner end and an outer end, characterized in that: the deflection limiter comprises an outer mounting aperture at the outer end; an outer fastener is mated with the outer mounting aperture to attach the deflection limiter to the cowl; the outer mounting aperture comprises a slot; and the outer fastener is configured to move radially within the slot. a core of a gas turbine engine; a nacelle inner structure comprising an internal compartment and a cowl; the internal compartment configured to house the core of the gas turbine engine; the cowl configured to form an outer radial periphery of the internal compartment, and the cowl further configured to form an outer radial periphery of a compartment exhaust for the internal compartment at an aft end of the cowl; and a deflection limiter attached to the cowl, the deflection limiter configured to limit radial outward movement of the cowl; wherein the deflection limiter extends radially between an inner end and an outer end, characterized in that: the deflection limiter comprises an outer mounting aperture at the outer end; an outer fastener is mated with the outer mounting aperture to attach the deflection limiter to the cowl; the outer mounting aperture comprises a slot; and the outer fastener is configured to move radially within the slot. the deflection limiter comprises an outer mounting aperture at the outer end; an outer fastener is mated with the outer mounting aperture to attach the deflection limiter to the cowl; the outer mounting aperture comprises a slot; and the outer fastener is configured to move radially within the slot.
An apparatus comprising: a processor having secure enclave support, wherein the processor is to establish a secure enclave using the secure enclave support; and an input/output (I/O) controller including an integrated trusted I/O device, characterized in that the trusted I/O device is to receive an unencrypted request to configure the trusted I/O device via a default control endpoint of the trusted I/O device, configure a command endpoint and a response endpoint to block topology change notifications to system software and direct the topology change notifications to the secure enclave instead in response to receipt of the unencrypted request, receive an encrypted command from the secure enclave via the command endpoint, perform a device management operation related to the I/O controller in response to receipt of the encrypted command; and transmit an encrypted response to the secure enclave via the response endpoint in response to performance of the device management operation. a processor having secure enclave support, wherein the processor is to establish a secure enclave using the secure enclave support; and an input/output (I/O) controller including an integrated trusted I/O device, characterized in that the trusted I/O device is to receive an unencrypted request to configure the trusted I/O device via a default control endpoint of the trusted I/O device, configure a command endpoint and a response endpoint to block topology change notifications to system software and direct the topology change notifications to the secure enclave instead in response to receipt of the unencrypted request, receive an encrypted command from the secure enclave via the command endpoint, perform a device management operation related to the I/O controller in response to receipt of the encrypted command; and transmit an encrypted response to the secure enclave via the response endpoint in response to performance of the device management operation.
A sterilization apparatus for sterilizing receptacle closures comprising: - a treatment chamber having an inlet station and an outlet station; - conveying means apt to convey the receptacle closures through the treatment chamber from the inlet station to the outlet station; and - sterilization agent injection means adapted to inject a sterilization agent into said treatment chamber; characterized in that the sterilization apparatus further comprises: - feeding means apt to feed a succession of receptacle closures to the inlet station by means of a flow of air; and - deflector means arranged within the area of the inlet station and configured to restrict the flow of air feeding the receptacle closures to the inlet station within the area of the inlet station. - a treatment chamber having an inlet station and an outlet station; - conveying means apt to convey the receptacle closures through the treatment chamber from the inlet station to the outlet station; and - sterilization agent injection means adapted to inject a sterilization agent into said treatment chamber; characterized in that the sterilization apparatus further comprises: - feeding means apt to feed a succession of receptacle closures to the inlet station by means of a flow of air; and - deflector means arranged within the area of the inlet station and configured to restrict the flow of air feeding the receptacle closures to the inlet station within the area of the inlet station. - feeding means apt to feed a succession of receptacle closures to the inlet station by means of a flow of air; and - deflector means arranged within the area of the inlet station and configured to restrict the flow of air feeding the receptacle closures to the inlet station within the area of the inlet station.
A computer-implemented method for determination of real subsoil geological formation characterized in that the method comprises: /a/ receiving a model representing the real subsoil, said model being based on the real geographical coordinates of the subsoil and said model comprising a stratigraphic layer, said stratigraphic layer comprising a shore line dividing the stratigraphic layer into a continental zone and a marine zone; /b/ receiving a first flow speed field representative of a continental domain for the stratigraphic layer, said first flow speed field being based on at least one geological constraint; /c/ receiving a second flow speed field representative of a marine domain for the stratigraphic layer; /d/ determining a weighted combination, named global flow speed field, of the first flow speed field and the second flow speed field for each position in the stratigraphic layer, weights of the combination are based on a distance of said position to the shore line and the fact that the position is within the continental zone or the marine zone; /e/ determining a real subsoil geological formation for the stratigraphic layer based on the determined global flow speed field for each position; /f/ determining at least one reservoir of hydrocarbon to exploit based on the determined real subsoil geological formation for the stratigraphic layer. /a/ receiving a model representing the real subsoil, said model being based on the real geographical coordinates of the subsoil and said model comprising a stratigraphic layer, said stratigraphic layer comprising a shore line dividing the stratigraphic layer into a continental zone and a marine zone; /b/ receiving a first flow speed field representative of a continental domain for the stratigraphic layer, said first flow speed field being based on at least one geological constraint; /c/ receiving a second flow speed field representative of a marine domain for the stratigraphic layer; /d/ determining a weighted combination, named global flow speed field, of the first flow speed field and the second flow speed field for each position in the stratigraphic layer, weights of the combination are based on a distance of said position to the shore line and the fact that the position is within the continental zone or the marine zone; /e/ determining a real subsoil geological formation for the stratigraphic layer based on the determined global flow speed field for each position; /f/ determining at least one reservoir of hydrocarbon to exploit based on the determined real subsoil geological formation for the stratigraphic layer.
A drug delivery device configured to be at least partially implanted in an eye, the device comprising: a retention structure positioned near a proximal end region of the device; a penetrable element coupled to and extending within at least a portion of the retention structure; a porous drug release mechanism positioned in fluid communication with an outlet of the device; an elongated core element having a longitudinal axis; and a reservoir positioned around the elongated core element, the reservoir having a volume configured to contain one or more therapeutic agents and to be in fluid communication with the outlet through the porous drug release mechanism, wherein the device is configured to be at least partially inserted into the eye along an axis of insertion, and wherein the reservoir is configured to enlarge from an insertion configuration having a first three-dimensional shape to an expanded configuration having a second three-dimensional shape, characterized in that the second three-dimensional shape is eccentrically positioned relative to the longitudinal axis of the elongated core element. a retention structure positioned near a proximal end region of the device; a penetrable element coupled to and extending within at least a portion of the retention structure; a porous drug release mechanism positioned in fluid communication with an outlet of the device; an elongated core element having a longitudinal axis; and a reservoir positioned around the elongated core element, the reservoir having a volume configured to contain one or more therapeutic agents and to be in fluid communication with the outlet through the porous drug release mechanism, wherein the device is configured to be at least partially inserted into the eye along an axis of insertion, and wherein the reservoir is configured to enlarge from an insertion configuration having a first three-dimensional shape to an expanded configuration having a second three-dimensional shape, characterized in that the second three-dimensional shape is eccentrically positioned relative to the longitudinal axis of the elongated core element.
A lighting module comprising: - a light exit window and a phosphor coating arranged on an inner surface, in view of the optical path (101, 102, 103), of the light exit window; - a light source arranged to provide light having an optical path (101, 102, 103) through the light exit window; characterised in that said light exit window is engraved thereby increasing the amount of light backscattered to the phosphor coating. - a light exit window and a phosphor coating arranged on an inner surface, in view of the optical path (101, 102, 103), of the light exit window; - a light source arranged to provide light having an optical path (101, 102, 103) through the light exit window; characterised in that said light exit window is engraved thereby increasing the amount of light backscattered to the phosphor coating.
A film coated tablet for oral administration which contains deferasirox or a pharmaceutically acceptable salt thereof present in an amount of from 45% to 60% by weight based on the total weight of the tablet, and wherein the tablet contains 90 mg, 180 mg or 360 mg of deferasirox or a pharmaceutically acceptable salt thereof, wherein the tablet further comprises, (i) at least one filler in a total amount of 10% to 40 % by weight based on total weight of the tablet, wherein the filler is microcrystalline cellulose; (ii) at least one disintegrant in a total amount of 1% to 10% by weight based on the total weight of the tablet, wherein the disintegrant is cross-linked polyvinylpyrrolidone (crospovidone); (iii) at least one binder in a total amount of 1% to 5% by weight based on the total weight of the tablet, wherein the binder is polyvinylpyrrolidone; (iv) optionally, at least one surfactant in a total amount of 0.0% to 2% by weight based on the total weight of the tablet, wherein the surfactant is poloxamer; (v) at least one glidant in a total amount of 0.1% to 1% by weight based on the total weight of the tablet, wherein the glidant is colloidal silicon dioxide; (vi) at least one lubricant in a total amount of less than 0.1% to 2% by weight based on the total weight of the tablet, wherein the lubricant is magnesium stearate; and (vii) a coating. (i) at least one filler in a total amount of 10% to 40 % by weight based on total weight of the tablet, wherein the filler is microcrystalline cellulose; (ii) at least one disintegrant in a total amount of 1% to 10% by weight based on the total weight of the tablet, wherein the disintegrant is cross-linked polyvinylpyrrolidone (crospovidone); (iii) at least one binder in a total amount of 1% to 5% by weight based on the total weight of the tablet, wherein the binder is polyvinylpyrrolidone; (iv) optionally, at least one surfactant in a total amount of 0.0% to 2% by weight based on the total weight of the tablet, wherein the surfactant is poloxamer; (v) at least one glidant in a total amount of 0.1% to 1% by weight based on the total weight of the tablet, wherein the glidant is colloidal silicon dioxide; (vi) at least one lubricant in a total amount of less than 0.1% to 2% by weight based on the total weight of the tablet, wherein the lubricant is magnesium stearate; and (vii) a coating.
A piston, comprising: a piston body made of an aluminum alloy serving as a base material; a piston ring groove formed at the piston body; an electrolytic oxidation ceramic coating at a portion of a surface of the piston body, the portion being the piston ring groove, the electrolytic oxidation ceramic coating including a most outer layer and an inner layer which is arranged close to the piston body relative to the most outer layer, the inner layer being richer in aluminum oxide than the most outer layer and the most outer layer being richer in titanium oxide or a total of titanium oxide and zirconium oxide than the inner layer; and a piston ring attached to the piston ring groove, wherein a surface roughness Ra of the electrolytic oxidation ceramic coating is specified to be equal to or smaller than 0.7 μm, and an average hardness of the electrolytic oxidation ceramic coating is equal to or smaller than HV 600 and is greater than an average hardness of the piston body. a piston body made of an aluminum alloy serving as a base material; a piston ring groove formed at the piston body; an electrolytic oxidation ceramic coating at a portion of a surface of the piston body, the portion being the piston ring groove, the electrolytic oxidation ceramic coating including a most outer layer and an inner layer which is arranged close to the piston body relative to the most outer layer, the inner layer being richer in aluminum oxide than the most outer layer and the most outer layer being richer in titanium oxide or a total of titanium oxide and zirconium oxide than the inner layer; and a piston ring attached to the piston ring groove, wherein a surface roughness Ra of the electrolytic oxidation ceramic coating is specified to be equal to or smaller than 0.7 μm, and an average hardness of the electrolytic oxidation ceramic coating is equal to or smaller than HV 600 and is greater than an average hardness of the piston body.