mhurhangee/ep-ind-claims huggingface dataset:
A gas turbine engine comprising: a compressor section; a combustor in fluid communication with the compressor section; a turbine section in fluid communication with the combustor, the turbine section including a fan drive turbine and a second turbine, the fan drive turbine including a plurality of turbine stages; a fan including a plurality of blades rotatable about an axis; and a speed change system driven by the fan drive turbine for rotating the fan about the axis, wherein the fan drive turbine includes a first aft rotor attached to a first shaft and the second turbine includes a second aft rotor attached to a second shaft, characterised in that: a ratio between the number of fan blades and the number of fan drive turbine stages is between 2.5 and 8.5; and a first bearing assembly is disposed axially forward of a first connection between the first aft rotor and the first shaft, and a second bearing assembly is disposed axially aft of a second connection between the second aft rotor and the second shaft; and the engine includes a power density greater than 1.5 lbf/in 3 (407.17 kN/m 3) and less than or equal to about 5.5 lbf/in 3 (1,493.96 kN/m 3), wherein the power density is the sea level take-off flat-rated static thrust divided by the volume of the turbine section. a compressor section; a combustor in fluid communication with the compressor section; a turbine section in fluid communication with the combustor, the turbine section including a fan drive turbine and a second turbine, the fan drive turbine including a plurality of turbine stages; a fan including a plurality of blades rotatable about an axis; and a speed change system driven by the fan drive turbine for rotating the fan about the axis, wherein the fan drive turbine includes a first aft rotor attached to a first shaft and the second turbine includes a second aft rotor attached to a second shaft, a ratio between the number of fan blades and the number of fan drive turbine stages is between 2.5 and 8.5; and a first bearing assembly is disposed axially forward of a first connection between the first aft rotor and the first shaft, and a second bearing assembly is disposed axially aft of a second connection between the second aft rotor and the second shaft; and the engine includes a power density greater than 1.5 lbf/in 3 (407.17 kN/m 3) and less than or equal to about 5.5 lbf/in 3 (1,493.96 kN/m 3), wherein the power density is the sea level take-off flat-rated static thrust divided by the volume of the turbine section.
A method of obtaining a part made of low-silicon aluminum alloy, containing: - silicon at a content lying in the range of 0.5% to 3%; - magnesium at a content lying in the range of 0.65% to 1%; - copper at a content lying in the range of 0.20% to 0.40%; - manganese at a content lying in the range of 0.15% to 0.25%; - titanium at a content lying in the range of 0.10% to 0.20%; and - strontium at a content lying in the range of 0 ppm to 120 ppm; the remainder of the alloy consisting of aluminium and possible impurities, wherein the method comprises the steps of: - casting said alloy in a mold so as to obtain the part; - after the casting, demolding the part constituting a preform that is still hot; - cooling said preform and then subjecting said preform to an operation adapted for reheating sais preform to a temperature lying in the range of 470°C to 550°C; - positioning said part between two shells of a die that defines a cavity of dimensions substantially equal to but less than those of the mold; and - strongly pressing the two shells together to exert on the part disposed between said shells a combined effect of pressing and surface kneading. - silicon at a content lying in the range of 0.5% to 3%; - magnesium at a content lying in the range of 0.65% to 1%; - copper at a content lying in the range of 0.20% to 0.40%; - manganese at a content lying in the range of 0.15% to 0.25%; - titanium at a content lying in the range of 0.10% to 0.20%; and - strontium at a content lying in the range of 0 ppm to 120 ppm; - casting said alloy in a mold so as to obtain the part; - after the casting, demolding the part constituting a preform that is still hot; - cooling said preform and then subjecting said preform to an operation adapted for reheating sais preform to a temperature lying in the range of 470°C to 550°C; - positioning said part between two shells of a die that defines a cavity of dimensions substantially equal to but less than those of the mold; and - strongly pressing the two shells together to exert on the part disposed between said shells a combined effect of pressing and surface kneading.
A container holder comprising: an inner liner, an outer shell, and an intermediate layer in between the inner liner and the outer shell, the inner liner providing an inner wall, where the inner wall defines a cavity for receiving a container; the container holder defining a first portion and a second portion and the first portion follows a curved profile and the second portion follows a flat profile such that a cross-section of the container holder follows a D-shape; a pocket located on the outer shell and on the first portion; the second portion having a series of openings extending through the outer shell to vent the cavity to an outside; characterized in that a series of loops covers the series of openings on the second portion and in that the container holder comprises a pair of clips mounted to the series of loops. an inner liner, an outer shell, and an intermediate layer in between the inner liner and the outer shell, the inner liner providing an inner wall, where the inner wall defines a cavity for receiving a container; the container holder defining a first portion and a second portion and the first portion follows a curved profile and the second portion follows a flat profile such that a cross-section of the container holder follows a D-shape; a pocket located on the outer shell and on the first portion; the second portion having a series of openings extending through the outer shell to vent the cavity to an outside; characterized in that a series of loops covers the series of openings on the second portion and in that the container holder comprises a pair of clips mounted to the series of loops.
An injection device fixed to the wall of the lower part of a container intended to contain a product to be cooled in bulk, said injection device comprising a hollow cylindrical body in which a valve forced by a spring is inserted, said injection device comprising a through channel substantially parallel to said valve intended to be fed with pressurised cryogenic fluid, one end of said through channel being connected to the cryogenic fluid supply system and the opposite end opening out at the seat of the valve, characterised in that the spring is weighted such that the valve cannot slide without being subjected to a cryogenic fluid pressure at least equal to a threshold pressure and thus allow the fact that, as soon as the cryogenic fluid pressure is less than a determined threshold, the pressure required to make the valve slide is no longer reached and the seat of the valve is repositioned in an impervious manner against said wall.
A non-contact bearing comprising: a housing including a plurality of gas channels; 1 at least one impeller (1702, 1802) contained in the housing; a first plurality of externally pressurized gas bearings (1803, 2203) configured to support the at least one impeller radially; and a second plurality of externally pressurized gas bearings (1807, 2007, 2207) configured to support the impeller axially; characterized in that each externally pressurized gas bearings of the first and second pluralities of externally pressurized gas bearings includes a porous media element positioned over multiple plenums and the plurality of gas channels are configured to supply pressurized gas to the plenums of the first and second pluralities of externally pressurized gas bearings. 2 a housing including a plurality of gas channels; 1 at least one impeller (1702, 1802) contained in the housing; a first plurality of externally pressurized gas bearings (1803, 2203) configured to support the at least one impeller radially; and a second plurality of externally pressurized gas bearings (1807, 2007, 2207) configured to support the impeller axially; characterized in that each externally pressurized gas bearings of the first and second pluralities of externally pressurized gas bearings includes a porous media element positioned over multiple plenums and the plurality of gas channels are configured to supply pressurized gas to the plenums of the first and second pluralities of externally pressurized gas bearings. 2
An ostomy bag including in an accessible wall a closable exit aperture and means for selectively releasing accumulated gas through the aperture, the bag comprising a closure which covers the aperture and attaches to the bag by means of a reusable seal, wherein closure is provided in the form of a sealing flap which folds down from a seam around the edge of the bag and which is hinged to a body of the ostomy bag along the line of the seam and the hinge is formed by a section of the seam which is straight.
A communication apparatus comprising: a circuitry configured to receive first information related to channel quality measurement about a directional beam from a terminal device via another communication apparatus serving the terminal device; decide restriction on resources used for transmission of a reference signal over the directional beam on the basis of the the first information as an operation of the communication apparatus; characterized in that the circuitry is configured to decide, as the restriction, lengthening a period of transmission of the reference signal; lengthen said period; and notify the operation of the communication apparatus to the other communication apparatus. receive first information related to channel quality measurement about a directional beam from a terminal device via another communication apparatus serving the terminal device; decide restriction on resources used for transmission of a reference signal over the directional beam on the basis of the the first information as an operation of the communication apparatus; characterized in that the circuitry is configured to decide, as the restriction, lengthening a period of transmission of the reference signal; lengthen said period; and notify the operation of the communication apparatus to the other communication apparatus.
An electronic control unit connected to a network in an in-vehicle network system, the in-vehicle network system including a plurality of apparatuses that perform communication of frames via the network, the electronic control unit comprising: a first control circuit; and a second control circuit, wherein the first control circuit is connected to the in-vehicle network bus via the second control circuit, wherein the second control circuit is configured to perform a first determination process (S1300, S4300, S5300) on a received frame that is received from the network, to which the second control circuit is connected, to determine a conformity of the received frame with a first rule, wherein, upon determining that the received frame conforms to the first rule, the second control circuit is configured to transmit the received frame to the first control circuit, wherein, upon determining that the received frame does not conform to the first rule, the second control circuit is configured not to transmit the received frame to the first control circuit, and wherein the first control circuit is configured to perform a second determination process (S1600, S4600, S5600) on the received frame, received via the second control circuit, to determine a conformity of the received frame with a second rule that is different from the first rule. a first control circuit; and a second control circuit, wherein the first control circuit is connected to the in-vehicle network bus via the second control circuit, wherein the second control circuit is configured to perform a first determination process (S1300, S4300, S5300) on a received frame that is received from the network, to which the second control circuit is connected, to determine a conformity of the received frame with a first rule, wherein, upon determining that the received frame conforms to the first rule, the second control circuit is configured to transmit the received frame to the first control circuit, wherein, upon determining that the received frame does not conform to the first rule, the second control circuit is configured not to transmit the received frame to the first control circuit, and wherein the first control circuit is configured to perform a second determination process (S1600, S4600, S5600) on the received frame, received via the second control circuit, to determine a conformity of the received frame with a second rule that is different from the first rule.
A composition comprising an isolated human truncated cystathionine beta synthase (htCBS) mutant polypeptide conjugated to a PEG moiety, wherein the isolated htCBS mutant polypeptide comprises the amino acid sequence of SEQ ID NO:3 with a change of a cysteine at the amino acid position corresponding to 15 of SEQ ID NO:3 to a serine and lacking the N-terminal first methionine residue corresponding to SEQ ID NO:3, and is PEGylated with ME-200GS; for use in a method of treating homocystinuria in a human subject, wherein the PEGylated htCBS mutant polypeptide is administered at least once a week for at least six weeks in a dose between 0.33 and 10 mg/kg.
A system comprising: a starter air valve in fluid communication with an air turbine starter to drive motoring of a gas turbine engine responsive to a compressed air flow from a compressed air source; a manual override operably connected to the starter air valve, the manual override is operable to open the starter air valve a select percentage by moving the manual override to a detent engaged position, wherein the select percentage is operable to allow enough airflow to achieve the maximum allowed motoring speed of the gas turbine engine; a controller operable to detect when the manual override is in the detent engaged position; and a pressure regulating bleed valve in fluid communication with the starter air valve, the pressure regulating bleed valve operable to bleed a portion of the compressed air flow to regulate a motoring speed of the gas turbine engine in response to detection of the manual override in a detent engaged position. a starter air valve in fluid communication with an air turbine starter to drive motoring of a gas turbine engine responsive to a compressed air flow from a compressed air source; a manual override operably connected to the starter air valve, the manual override is operable to open the starter air valve a select percentage by moving the manual override to a detent engaged position, wherein the select percentage is operable to allow enough airflow to achieve the maximum allowed motoring speed of the gas turbine engine; a controller operable to detect when the manual override is in the detent engaged position; and a pressure regulating bleed valve in fluid communication with the starter air valve, the pressure regulating bleed valve operable to bleed a portion of the compressed air flow to regulate a motoring speed of the gas turbine engine in response to detection of the manual override in a detent engaged position.
A device for controlling an air flow in a motor vehicle compartment, the device comprising: - at least one frame defining an opening, the frame extending in a transverse plane, the opening extending along a flow axis of the air (X-X') substantially perpendicular to the transverse plane; - a plurality of slats extending across the frame, the slats being arranged above one another; and - an actuator connected to each of the slats by a respective fastener; each slat extending in a respective air deflection plane, and each slat being movable relative to the frame around a respective slat axis, using the actuator, between: - a closed position, in which the slats cooperate with one another to block the passage of the air through the opening, and - an open position, in which the slats allow the air to flow through the opening, and in which the deflection planes of the slats intersect one another upstream from the frame relative to the flow axis (X-X') of the air flow, characterized in that each fastener is mounted rotatably only on the actuator, around a respective actuating axis. - at least one frame defining an opening, the frame extending in a transverse plane, the opening extending along a flow axis of the air (X-X') substantially perpendicular to the transverse plane; - a plurality of slats extending across the frame, the slats being arranged above one another; and - an actuator connected to each of the slats by a respective fastener; - a closed position, in which the slats cooperate with one another to block the passage of the air through the opening, and - an open position, in which the slats allow the air to flow through the opening, and in which the deflection planes of the slats intersect one another upstream from the frame relative to the flow axis (X-X') of the air flow,
A coil laying head, defining a longitudinal axis, for forming coils of a substantially rectilinear metal product, comprising - a fixed supporting structure, - a rotor, adapted to rotate about said longitudinal axis and rotatably fixed to said supporting structure, wherein the rotor comprises a bell-shaped member, which expands outwards with respect to said longitudinal axis and has an outer surface thereof provided with at least one spiral-shaped groove, for guiding the metal product, wherein feeding means for feeding the metal product to said at least one groove are provided, characterized in that said bell-shaped member consists of at least three stages mutually arranged in sequence along the longitudinal axis so that the outer surfaces of said stages, provided with spiral-shaped grooves, jointly define the outer surface of the bell-shaped member and can be arranged, by turning at least one stage about said longitudinal axis, in at least one respectively relative angular position so as to define at least one continuous spiral-shaped path for said metal product along the entire outer surface of the bell-shaped member. - a fixed supporting structure, - a rotor, adapted to rotate about said longitudinal axis and rotatably fixed to said supporting structure,
A method for manufacturing a galvanized steel sheet for hot stamping, the method comprising the steps of: annealing a hot-rolled pickled steel sheet or cold-rolled steel sheet under a reducing atmosphere; and galvanizing the steel sheet, the steel sheet consisting of: C in a content of 0.10% to 0.5%; Si in a content of 0.7% to 2.5%; Mn in a content of 1.0% to 3%; and Al in a content of 0.01% to 0.5%, and optionally B in a content of 0.005% or less, Ti in a content of 0.10% or less, Cr and Mo in a content of 1% or less in total, Nb, Zr, and V in a content of 0.1% or less in total, Cu and Ni in a content of 1% or less in total, in percent by mass, the balance being Fe and unavoidable impurities, wherein the annealing is performed at a temperature of 500°C to 700°C for 30 to 270 seconds. C in a content of 0.10% to 0.5%; Si in a content of 0.7% to 2.5%; Mn in a content of 1.0% to 3%; and Al in a content of 0.01% to 0.5%, and optionally B in a content of 0.005% or less, Ti in a content of 0.10% or less, Cr and Mo in a content of 1% or less in total, Nb, Zr, and V in a content of 0.1% or less in total, Cu and Ni in a content of 1% or less in total, in percent by mass, the balance being Fe and unavoidable impurities, wherein the annealing is performed at a temperature of 500°C to 700°C for 30 to 270 seconds.
A method of polishing albumin to remove contaminants comprising passing an albumin enriched solution through a hydrophobic charge-induction chromatographic resin and recovering the albumin solution which passes through the resin.
A system comprising: an aircraft cabin; at least one monitor disposed in a ceiling of the aircraft cabin, oriented to display images downward; at least one environmental camera disposed to produce an image stream of an environment as seen from the aircraft cabin; a recline sensor configured to determine when a passenger seat in the aircaft cabin is in a reclined orientation; and wherein the system comprises: at least one processor in data communication with the at least one environmental camera, the at least one monitor, and a memory storing processor executable code for configuring the at least one processor to: receive the image stream from the at least one environmental camera; render the image stream on the at least one monitor; determine that the passenger seat is in a reclined orientation; and apply a mood affective image routine to the at least one monitor. an aircraft cabin; at least one monitor disposed in a ceiling of the aircraft cabin, oriented to display images downward; at least one environmental camera disposed to produce an image stream of an environment as seen from the aircraft cabin; a recline sensor configured to determine when a passenger seat in the aircaft cabin is in a reclined orientation; and wherein the system comprises: at least one processor in data communication with the at least one environmental camera, the at least one monitor, and a memory storing processor executable code for configuring the at least one processor to: receive the image stream from the at least one environmental camera; render the image stream on the at least one monitor; determine that the passenger seat is in a reclined orientation; and apply a mood affective image routine to the at least one monitor. receive the image stream from the at least one environmental camera; render the image stream on the at least one monitor; determine that the passenger seat is in a reclined orientation; and apply a mood affective image routine to the at least one monitor.
A sustained release pheromone preparation, comprising: a membrane of an ethylene-vinyl acetate copolymer, and at least one C 20-35 aliphatic hydrocarbon compound which is carried in a liquid form by the membrane, is permeable through the membrane, and has such a melting point that the aliphatic hydrocarbon compound is in a solid form at temperature of 5 to 35 °C, wherein the preparation targets an insect pest having the aliphatic hydrocarbon compound as a pheromone substance. a membrane of an ethylene-vinyl acetate copolymer, and at least one C 20-35 aliphatic hydrocarbon compound which is carried in a liquid form by the membrane, is permeable through the membrane, and has such a melting point that the aliphatic hydrocarbon compound is in a solid form at temperature of 5 to 35 °C,