mhurhangee/ep-ind-claims huggingface dataset:
An aircraft cabin blower system having a hydraulic circuit comprising a first hydraulic device and a second hydraulic device, wherein the first hydraulic device is mechanically coupled to a cabin blower compressor and the second hydraulic device is arranged in use to be mechanically coupled to a spool of a gas turbine engine and where further the first hydraulic device is capable of performing as a hydraulic motor and the second hydraulic device is capable of performing as a hydraulic pump, such that when, in use, the system is operating in a cabin blower configuration, a driving force supplied by the spool of the gas turbine causes the second hydraulic device to pump liquid provided in the hydraulic circuit and thereby to drive the first hydraulic device, which in turn rotates the cabin blower compressor, characterised in that the first hydraulic device is capable of performing as a hydraulic pump and the second hydraulic device is capable of performing as a hydraulic motor such that when, in use, the system is operating in an engine start configuration, a driving force supplied by the cabin blower compressor acting as a turbine causes the first hydraulic device to pump the liquid provided in the hydraulic circuit and thereby to drive the second hydraulic device, which in turn rotates the spool of the gas turbine engine, and the hydraulic circuit comprises a valve assembly actuatable between a first position when the system is in the cabin blower configuration and a second position when the system is in the engine start configuration, whereby the first and second positions give rise to different porting of liquid in the hydraulic circuit such that the flow direction through the second hydraulic device is the same regardless of whether the system is operating in the cabin blower configuration or the engine start configuration and such that the flow direction through the first hydraulic device reverses in dependence upon whether the system is operating in the cabin blower configuration or the engine start configuration.
A required time of arrival performance graphic display system for a vehicle, said system comprising: a processor programmed to receive predetermined parameters associated with a required time of arrival; and a first visual display communicatively coupled to said processor, said display comprising an RTA graphic comprising: a dial comprising an axis; a first marker indicative of a current estimated time of arrival at a predetermined waypoint; a second marker indicative of a value of the RTA relative to the current ETA value and a selected RTA time tolerance value; a first indication (210, 220) representing a first time the vehicle can attain the predetermined waypoint; a second indication (212, 222) representing a last time the vehicle can attain the predetermined waypoint; a third indication representing an uncertainty of the ETA in an early arrival direction; and a fourth indication representing an uncertainty of the ETA in a late arrival direction. a processor programmed to receive predetermined parameters associated with a required time of arrival; and a first visual display communicatively coupled to said processor, said display comprising an RTA graphic comprising: a dial comprising an axis; a first marker indicative of a current estimated time of arrival at a predetermined waypoint; a second marker indicative of a value of the RTA relative to the current ETA value and a selected RTA time tolerance value; a first indication (210, 220) representing a first time the vehicle can attain the predetermined waypoint; a second indication (212, 222) representing a last time the vehicle can attain the predetermined waypoint; a third indication representing an uncertainty of the ETA in an early arrival direction; and a fourth indication representing an uncertainty of the ETA in a late arrival direction. a dial comprising an axis; a first marker indicative of a current estimated time of arrival at a predetermined waypoint; a second marker indicative of a value of the RTA relative to the current ETA value and a selected RTA time tolerance value; a first indication (210, 220) representing a first time the vehicle can attain the predetermined waypoint; a second indication (212, 222) representing a last time the vehicle can attain the predetermined waypoint; a third indication representing an uncertainty of the ETA in an early arrival direction; and a fourth indication representing an uncertainty of the ETA in a late arrival direction.
A three-dimensional flexible nail sticker for decorating and styling nails, wherein the three-dimensional flexible nail sticker has shape memory and comprises a film of thickness between 30 and 140 μm, and the three-dimensional shape memory nail sticker is placed on a the base layer, and the film, from the base layer side, has a self-adhesive coating, and the film together with the self-adhesive coating and the base layer is in a form of three-dimensional protrusion, and wherein the protrusion mirrors an anatomic nail shape essentially of a the whole nail plate, and wherein the three-dimensional shape memory nail sticker protrusion shape is convex that is a section of a sphere that mirrors the three-dimensional anatomic shape of the nail, and wherein three-dimensional shape memory nail sticker is formed together with the base layer on a matrix, thereby forming permanently formed flexible three-dimensional nail sticker placed on the base layer, and the film layer together with the self-adhesive coating is cut around the perimeter of the protrusion, and wherein the three-dimensional flexible nail sticker during placing the sticker on the nail plate starting from the nail lunula curls back to restore its initial anatomic shape, and wherein the three-dimensional shape of the flexible shape memory nail sticker does not tend to deform and maintains its three-dimensional form, anatomically adapted to the nail shape.
Road reflector with anti-condensation and anti-frost heating system, the reflector being fundamentally constituted by a support with a hinged fastening holding a convex mirror with a heating system by means of electrical resistance either wired or screen printed or sputtered and an insulating system, a thermal sensor, a hygrometric sensor, a heating control system of PWM type and an electrical energy source (7, 7'), wherein the heating control is obtained modulating the PWM power by means of a PID control whose proportional mode P is 1/Δt or whose derivative mode D is - Δt/Δτ (-dt/dτ) and whose integrative mode I is adjusted by means of a trimmer; where Δt (dt) is the difference between the ambient temperature tA and the corresponding dew or frost temperature tS obtained through a microprocessor elaborating the signals of the thermal sensor and hygrometric sensor by means of an algorithm containing the relationship of the psychrometric diagram J-X of the humid air and where Δτ (dτ) is the corresponding variation on time.
A mower conditioner implement comprising: a cutting system operable to cut crop material; a crop conditioning system operable to receive the cut crop material from the cutting system and condition the cut crop material; an image sensor positioned to sense an image of the crop material, the image having a color spectrum; a computing device having a processor and a memory having a crop analysis algorithm stored thereon, wherein the processor is operable to execute the crop analysis algorithm to: determine at least one of an ash content in the cut crop material or a degree of stem conditioning of the cut crop material; and adjust at least one of the cutting system or the crop conditioning system based on at least one of the determined ash content or the determined degree of stem conditioning characterized in that the determination of at least one of the ash content in the cut crop material or the degree of stem conditioning of the cut crop material is executed by comparing the color spectrum of the image to a calibrated color measurement; and in that the mower conditioner further comprises a light source associated with the image sensor, wherein the light source is operable to emit light immediately prior to the image sensor sensing the image, such that the color spectrum of the image includes reflected light emitted from the light source. a cutting system operable to cut crop material; a crop conditioning system operable to receive the cut crop material from the cutting system and condition the cut crop material; an image sensor positioned to sense an image of the crop material, the image having a color spectrum; a computing device having a processor and a memory having a crop analysis algorithm stored thereon, wherein the processor is operable to execute the crop analysis algorithm to: determine at least one of an ash content in the cut crop material or a degree of stem conditioning of the cut crop material; and adjust at least one of the cutting system or the crop conditioning system based on at least one of the determined ash content or the determined degree of stem conditioning determine at least one of an ash content in the cut crop material or a degree of stem conditioning of the cut crop material; and adjust at least one of the cutting system or the crop conditioning system based on at least one of the determined ash content or the determined degree of stem conditioning characterized in that the determination of at least one of the ash content in the cut crop material or the degree of stem conditioning of the cut crop material is executed by comparing the color spectrum of the image to a calibrated color measurement; and in that the mower conditioner further comprises a light source associated with the image sensor, wherein the light source is operable to emit light immediately prior to the image sensor sensing the image, such that the color spectrum of the image includes reflected light emitted from the light source.
A method for controlling use of carriers for aggregation in a wireless communication system, comprising determining a set of carriers available for use in carrier aggregation; characterized by: determining at least one carrier of the set of carriers that can become unavailable for use by a communication device; sending to the communication device an indication of a configuration type of the at least one carrier (51, 64), the configuration type being indicative of different behavior during a period of unavailability, wherein different behavior comprises ceasing scheduling of resources on the at least one carrier; and maintaining the at least one carrier in the set of carriers during said period. determining at least one carrier of the set of carriers that can become unavailable for use by a communication device; sending to the communication device an indication of a configuration type of the at least one carrier (51, 64), the configuration type being indicative of different behavior during a period of unavailability, wherein different behavior comprises ceasing scheduling of resources on the at least one carrier; and maintaining the at least one carrier in the set of carriers during said period.
Laser communication system for an aircraft (4, 52), comprising - a plurality of optical head units (6, 54), - at least one separate laser transmitting unit, - at least one laser receiving unit, - at least one optical fiber for each optical head unit (6, 54), - at least one optical switching device for selectively coupling at least one of the optical head units (6, 54) and at least one of the at least one separate laser transmitting unit, and - a central control unit, wherein the optical head units (6, 54) are connected to the at least one optical switching device through the at least one optical fiber, wherein the optical head units (6, 54) each comprise an optical axis, parallel to which light is emitted or received, wherein the optical head units (6, 54) each comprise at least one optical pointing mechanism for adjusting the respective optical axis, wherein the at least one separate laser transmitting unit comprises a laser and an optical amplifier, and wherein the control unit is coupled with the at least one optical switching device, the at least one laser transmitting unit, the at least one laser receiving unit and the optical head units (6, 54) and is adapted to control a laser based data communication through coupling at least one of the optical head units (6, 54), which is in a free line of sight to at least one target outside the aircraft, to the at least one separate laser transmitting unit and to modulate the operation of the at least one separate laser transmitting unit for emitting a signal. - a plurality of optical head units (6, 54), - at least one separate laser transmitting unit, - at least one laser receiving unit, - at least one optical fiber for each optical head unit (6, 54), - at least one optical switching device for selectively coupling at least one of the optical head units (6, 54) and at least one of the at least one separate laser transmitting unit, and - a central control unit, wherein the optical head units (6, 54) are connected to the at least one optical switching device through the at least one optical fiber, wherein the optical head units (6, 54) each comprise an optical axis, parallel to which light is emitted or received, wherein the optical head units (6, 54) each comprise at least one optical pointing mechanism for adjusting the respective optical axis, wherein the at least one separate laser transmitting unit comprises a laser and an optical amplifier, and wherein the control unit is coupled with the at least one optical switching device, the at least one laser transmitting unit, the at least one laser receiving unit and the optical head units (6, 54) and is adapted to control a laser based data communication through coupling at least one of the optical head units (6, 54), which is in a free line of sight to at least one target outside the aircraft, to the at least one separate laser transmitting unit and to modulate the operation of the at least one separate laser transmitting unit for emitting a signal.
A method for adapting the velocity of a vehicle during driving of the vehicle along a route of travel, comprising the steps of: prescribing velocity in the form of a velocity profile comprising retardations along the route of travel of the vehicle based on the occurrence of velocity-limiting factors along the route of travel of the vehicle; prescribing a target velocity associated with a velocity-limiting factor, and controlling the vehicle velocity so that a velocity associated with said target velocity is permitted to be higher than the target velocity by a given offset, characterized in that said offset is adapted so that a relatively larger offset is permitted in connection with a non-safety-critical velocity-limiting factor and a relatively smaller offset is permitted in connection with a safety-critical velocity-limiting factor.
Raw meal delivery device for the delivery of raw meal into a gas line, such as a riser (112', 113') of a heat exchanger cyclone (112, 113), or into a reactor, such as a calciner, of a layout for production of cement clinker, comprising - a connection line for connecting a raw meal line to the gas line or the reactor, - an inclined raw meal chute, which is situated inside the connection line and by which raw meal gets from the raw meal line into the gas line or the reactor, wherein at the foot of the raw meal chute there is arranged a baffle slide, which protrudes into the path of the raw meal flowing along the raw meal chute and deflects the incoming raw meal, characterized in that a substantially convex displacement body is arranged on the baffle slide, which lies in the path of the incoming raw meal and disperses the flow of raw meal. - a connection line for connecting a raw meal line to the gas line or the reactor, - an inclined raw meal chute, which is situated inside the connection line and by which raw meal gets from the raw meal line into the gas line or the reactor, wherein at the foot of the raw meal chute there is arranged a baffle slide, which protrudes into the path of the raw meal flowing along the raw meal chute and deflects the incoming raw meal, characterized in that a substantially convex displacement body is arranged on the baffle slide, which lies in the path of the incoming raw meal and disperses the flow of raw meal.
A factor H binding protein (fHbp) comprising: an amino acid sequence having at least 80% sequence identity to SEQ ID NO:1 (fHbp ID1) and an amino acid substitution at position R130 of SEQ ID NO:1, and wherein said fHbp has a lower affinity for human factor H (fH) than the fHbp ID1 and elicits bactericidal antibodies against Neisseria meningitidis (N. meningitidis). an amino acid sequence having at least 80% sequence identity to SEQ ID NO:1 (fHbp ID1) and an amino acid substitution at position R130 of SEQ ID NO:1, and wherein said fHbp has a lower affinity for human factor H (fH) than the fHbp ID1 and elicits bactericidal antibodies against Neisseria meningitidis (N. meningitidis).
A diterminally silanol-modified perfluoropolyether compound of general formula below wherein each R 1 is independently an unsubstituted divalent hydrocarbon group of 1 to 10 carbon atoms, each R 2 is independently a substituted or unsubstituted monovalent hydrocarbon group of 1 to 10 carbon atoms, Rf is a perfluoropolyether group, and the subscript 'n' is independently at each occurrence an integer from 0 to 8.
A pressure-propelled contact system for gas circuit breaker interrupter, comprising: an insulating chamber for storage of gas; a pressure-propelled fixed arcing contact and a moveable arcing contact; a compression spring configured to restore the fixed arcing contact to its initial position after a process of current interruption, characterised in that it further comprises: a metallic blast cylinder having a moveable piston configured to pressurise gas supplied from the insulating chamber; an insulating nozzle configured to blow the pressurised gas over an arc formed between the fixed arcing contact and the moveable arcing contact; wherein movement of the fixed arcing contact is configured to be effected by a discharge of pressurised gas from the metallic blast cylinder during a process of current interruption, in a direction opposite to that of the moveable arcing contact and against the compression spring. an insulating chamber for storage of gas; a pressure-propelled fixed arcing contact and a moveable arcing contact; a compression spring configured to restore the fixed arcing contact to its initial position after a process of current interruption, characterised in that it further comprises: a metallic blast cylinder having a moveable piston configured to pressurise gas supplied from the insulating chamber; a metallic blast cylinder having a moveable piston configured to pressurise gas supplied from the insulating chamber; an insulating nozzle configured to blow the pressurised gas over an arc formed between the fixed arcing contact and the moveable arcing contact; wherein movement of the fixed arcing contact is configured to be effected by a discharge of pressurised gas from the metallic blast cylinder during a process of current interruption, in a direction opposite to that of the moveable arcing contact and against the compression spring.
A recombinant protein wherein the amino acid sequence of the recombinant protein is represented by SEQ ID NO: 1; or a derivative of the recombinant protein that is: (a) a concatemer of the recombinant protein; (b) a fusion protein of the recombinant protein with the Fc fragment of an immunoglobulin; or (c) a fusion protein of a concatemer of the recombinant protein with the Fc fragment of an immunoglobulin.
A method for locating idle-state user equipment, UE, comprising: sending, by an access network device, a paging message to UE in a cell, wherein the paging message comprises read instruction information, and the read instruction information is used to instruct the UE in the cell to read a system message; and sending, by the access network device, the system message to the UE in the cell,; and locating, by the access network device, the idle-state UE in the cell according to a location update process initiated by the idle-state UE in the cell characterized in that a cell location identifier in the system message is a preset location identifier, and the preset location identifier is used to trigger the UE in the cell to initiate the location update process. sending, by an access network device, a paging message to UE in a cell, wherein the paging message comprises read instruction information, and the read instruction information is used to instruct the UE in the cell to read a system message; and sending, by the access network device, the system message to the UE in the cell,; and locating, by the access network device, the idle-state UE in the cell according to a location update process initiated by the idle-state UE in the cell characterized in that a cell location identifier in the system message is a preset location identifier, and the preset location identifier is used to trigger the UE in the cell to initiate the location update process.
A solar cell module provided with a back sheet having, on a water-impermeable sheet at the opposite side of a sealant layer of the solar cell module, a cured coating film of a coating material comprising a fluorine-containing polymer, characterized in that the fluorine-containing polymer has a curable functional group, wherein the cured coating film is adhered directly to the water-impermeable sheet, and a white pigment or a black pigment is dispersed in the cured coating film. wherein the cured coating film is adhered directly to the water-impermeable sheet, and a white pigment or a black pigment is dispersed in the cured coating film.
A printing sleeve comprising: a compressible layer; a first polymeric cord reinforcing layer wound around said compressible layer; wherein at least a portion of adjacent windings of said cord reinforcing layer have flowed together and bonded to form a reinforcing layer having reduced thickness; and a printing surface layer on said cord reinforcing layer. a compressible layer; a first polymeric cord reinforcing layer wound around said compressible layer; wherein at least a portion of adjacent windings of said cord reinforcing layer have flowed together and bonded to form a reinforcing layer having reduced thickness; and a printing surface layer on said cord reinforcing layer.