mhurhangee/ep-ind-claims huggingface dataset:
A receiving device, comprising: a detection module, configured to detect a power parameter of a pilot in a received orthogonal frequency division multiplexing OFDM signal; a determining module, configured to determine a frequency offset value according to the power parameter of the pilot, wherein the frequency offset value is used to indicate a degree and a direction that are of a difference that is between a center frequency of a filter and a center frequency of a laser configured to transmit the OFDM signal in a transmitter and that deviates from a first threshold, the filter comprises a multiplexer configured to filter the OFDM signal in the transmitter, and the first threshold is a difference between a center frequency of the laser and a center frequency of the filter when a bit error rate of the OFDM signal is lowest; and a sending module, configured to send the frequency offset value. a detection module, configured to detect a power parameter of a pilot in a received orthogonal frequency division multiplexing OFDM signal; a determining module, configured to determine a frequency offset value according to the power parameter of the pilot, wherein the frequency offset value is used to indicate a degree and a direction that are of a difference that is between a center frequency of a filter and a center frequency of a laser configured to transmit the OFDM signal in a transmitter and that deviates from a first threshold, the filter comprises a multiplexer configured to filter the OFDM signal in the transmitter, and the first threshold is a difference between a center frequency of the laser and a center frequency of the filter when a bit error rate of the OFDM signal is lowest; and a sending module, configured to send the frequency offset value.
A heat generation system, comprising: - a combustion chamber, said combustion chamber being defined by a water or vapour boiler, and/or a furnace, and/or an incinerator; - a burner for producing a flame in the heat generation system comprising: - a combustion head provided to generate a continuous flame at least when the burner is active and connected to the combustion chamber of the heat generation system; - a fuel supply line and a comburent intake system operatively connected to said combustion head for supplying a flow rate of fuel and a flow rate of comburent, respectively, to said burner; - an auxiliary combustion chamber separate from said combustion head and configured for the combustion of a fuel and for the generation of a flow of flue gases; and - a turbine activated by the flue gases produced by the auxiliary combustion chamber, wherein said turbine is operatively active for contributing at least partially to the movement of the comburent in said comburent intake system; wherein said combustion head is inserted at least in part inside said combustion chamber so that the flame generated extends into said combustion chamber. - a combustion chamber, said combustion chamber being defined by a water or vapour boiler, and/or a furnace, and/or an incinerator; - a burner for producing a flame in the heat generation system comprising: - a combustion head provided to generate a continuous flame at least when the burner is active and connected to the combustion chamber of the heat generation system; - a fuel supply line and a comburent intake system operatively connected to said combustion head for supplying a flow rate of fuel and a flow rate of comburent, respectively, to said burner; - an auxiliary combustion chamber separate from said combustion head and configured for the combustion of a fuel and for the generation of a flow of flue gases; and - a turbine activated by the flue gases produced by the auxiliary combustion chamber, wherein said turbine is operatively active for contributing at least partially to the movement of the comburent in said comburent intake system; wherein said combustion head is inserted at least in part inside said combustion chamber so that the flame generated extends into said combustion chamber. - a combustion head provided to generate a continuous flame at least when the burner is active and connected to the combustion chamber of the heat generation system; - a fuel supply line and a comburent intake system operatively connected to said combustion head for supplying a flow rate of fuel and a flow rate of comburent, respectively, to said burner; - an auxiliary combustion chamber separate from said combustion head and configured for the combustion of a fuel and for the generation of a flow of flue gases; and - a turbine activated by the flue gases produced by the auxiliary combustion chamber, wherein said turbine is operatively active for contributing at least partially to the movement of the comburent in said comburent intake system;
Artificial heart (1, 1', 1"), in particular for imitating a human heart, comprising an energy storage device, an actuator device and two supply chambers (4, 5) each having one inlet opening (9, 10) and one outlet opening (11, 12), wherein each supply chamber (4, 5) is a least defined by one flexible wall (8, 8") and one rigid wall (7, 7") and a volume of each supply chamber (4, 5) can be varied by deforming the flexible wall (8, 8') by means of the actuator device, in that the flexible wall (8, 8'), starting from a suction position in which the volume of the supply chamber (4, 5) is at a maximum can be transferred by means of the actuator device into a pressure position, in which the volume of the supply chamber (4, 5) is at a minimum, wherein the inlet opening (9, 10) and the outlet opening (11, 12) of each supply chamber (4, 5) each have a non-return valve and the non-return valves can be alternately brought into an open and close position, through which a directed flow of blood from the relevant inlet opening (9, 10) to the relevant outlet opening (11, 12) can be generated, wherein the actuator device is arranged between the supply chambers (4, 5), characterised in that the supply chambers (4, 5) are elongated and in the shape of a banana, wherein a midline of each supply chamber (4, 5) is curved with a curvature radius of between 10 cm and 40 cm, and a cross-section taken though the supply chamber (4, 5) perpendicularly to the midline of the relevant supply chamber (4, 5) is in the form of an ellipse in the suction position, wherein the ratio of the semi-major axis to the semi-minor axis of the ellipse is between 1.0 and 2.0.
An apparatus for conveying an electrical signal, comprising: hinge means, a first member; a second member, hinged to the first member via 1 the hinge means; and at least one first bridge component arranged to provide an electromagnetic coupling between the first and second members, whereby a portion of the at least one first bridge component spans a gap between the first and second members; wherein the at least one first bridge component comprises at least one free end that is configured to be free to slide relative to at least one of the first member or second member while maintaining the electromagnetic coupling between the first and second members, such that the length of said portion of the at least one first bridge component that spans the gap between the first and second members is variable so as to allow the first and second members to move between a folded state and an unfolded state. hinge means, a first member; a second member, hinged to the first member via 1 the hinge means; and at least one first bridge component arranged to provide an electromagnetic coupling between the first and second members, whereby a portion of the at least one first bridge component spans a gap between the first and second members; wherein the at least one first bridge component comprises at least one free end that is configured to be free to slide relative to at least one of the first member or second member while maintaining the electromagnetic coupling between the first and second members, such that the length of said portion of the at least one first bridge component that spans the gap between the first and second members is variable so as to allow the first and second members to move between a folded state and an unfolded state.
A system for enabling delivery of electrosurgical energy to a medical device, comprising: an electrosurgical generator configured to selectively deliver an electrosurgical energy signal; an electrosurgical delivery device configured to connect to the electrosurgical generator and receive an electrosurgical energy signal therefrom; packaging material that houses the electrosurgical delivery device; a packaging readable module connected to the packaging material and configured to uniquely identify the electrosurgical delivery device housed in the packaging material; and a read module in communication with the electrosurgical generator, the read module configured to identify the packaging readable module and further configured to determine the viability of the electrosurgical delivery device; wherein delivery of the electrosurgical energy to the electrosurgical delivery device is enabled by the read module if the electrosurgical delivery device is a viable device, characterised in that the packaging readable module is incorporated into the packaging material such that prior to opening the packaging material, the packaging readable module is accessible by the read module through one or more layers of the packaging material and wherein the packaging readable module is positioned on the packaging material such that the packaging readable module is destroyed or rendered unreadable upon opening of the packaging material, wherein the packaging material is configured so that opening the packaging material exposes the packaging readable module to ambient conditions thereby rendering the packaging readable module unreadable. an electrosurgical generator configured to selectively deliver an electrosurgical energy signal; an electrosurgical delivery device configured to connect to the electrosurgical generator and receive an electrosurgical energy signal therefrom; packaging material that houses the electrosurgical delivery device; a packaging readable module connected to the packaging material and configured to uniquely identify the electrosurgical delivery device housed in the packaging material; and a read module in communication with the electrosurgical generator, the read module configured to identify the packaging readable module and further configured to determine the viability of the electrosurgical delivery device; wherein delivery of the electrosurgical energy to the electrosurgical delivery device is enabled by the read module if the electrosurgical delivery device is a viable device, characterised in that the packaging readable module is incorporated into the packaging material such that prior to opening the packaging material, the packaging readable module is accessible by the read module through one or more layers of the packaging material and wherein the packaging readable module is positioned on the packaging material such that the packaging readable module is destroyed or rendered unreadable upon opening of the packaging material, wherein the packaging material is configured so that opening the packaging material exposes the packaging readable module to ambient conditions thereby rendering the packaging readable module unreadable.
Use of a vulcanisable composition for production of a vulcanisate in contact with coolant, characterized in that the vulcanisable composition comprises (i) at least one HNBR-PEG acrylate copolymer and (ii) at least one peroxide compound, where the HNBR-PEG acrylate copolymer contains 10% to 35% by weight of α,β-ethylenically unsaturated nitrile units, 15% to 80% by weight of conjugated diene units and 10% to 50% by weight of PEG acrylate units derived from a PEG acrylate of the general Formula where R is hydrogen or branched or unbranched C 1 -C 20 -alkyl, n is 1 to 8, and R 1 is hydrogen or CH 3 -. wherein the coolant is a composition comprising water, a freezing point depressant, and a corrosion inhibitor. (i) at least one HNBR-PEG acrylate copolymer and (ii) at least one peroxide compound, where the HNBR-PEG acrylate copolymer contains 10% to 35% by weight of α,β-ethylenically unsaturated nitrile units, 15% to 80% by weight of conjugated diene units and 10% to 50% by weight of PEG acrylate units derived from a PEG acrylate of the general Formula where R is hydrogen or branched or unbranched C 1 -C 20 -alkyl, n is 1 to 8, and R 1 is hydrogen or CH 3 -. wherein the coolant is a composition comprising water, a freezing point depressant, and a corrosion inhibitor. where the HNBR-PEG acrylate copolymer contains 10% to 35% by weight of α,β-ethylenically unsaturated nitrile units, 15% to 80% by weight of conjugated diene units and 10% to 50% by weight of PEG acrylate units derived from a PEG acrylate of the general Formula where R is hydrogen or branched or unbranched C 1 -C 20 -alkyl, n is 1 to 8, and R 1 is hydrogen or CH 3 -. wherein the coolant is a composition comprising water, a freezing point depressant, and a corrosion inhibitor.
A method for manufacturing a biodegradable and industrially compostable flexible foam moulded product, the method comprising: introducing a thermoplastic biopolymer blended masterbatch for foaming into a barrel of a moulding apparatus; introducing a fluid into the barrel under temperature and pressure conditions to produce a super critical fluid, which upon contact with the thermoplastic biopolymer blended masterbatch produces a thermoplastic foamed melt; injecting the thermoplastic foamed melt into a cavity of a suitable mould shape; applying a gas counterpressure to the cavity, wherein a control unit is configured to dynamically apply varying GCP pressures at the melt-injection stage; and cooling the cavity to produce the biodegradable and industrially compostable flexible foam moulded product. introducing a thermoplastic biopolymer blended masterbatch for foaming into a barrel of a moulding apparatus; introducing a fluid into the barrel under temperature and pressure conditions to produce a super critical fluid, which upon contact with the thermoplastic biopolymer blended masterbatch produces a thermoplastic foamed melt; injecting the thermoplastic foamed melt into a cavity of a suitable mould shape; applying a gas counterpressure to the cavity, wherein a control unit is configured to dynamically apply varying GCP pressures at the melt-injection stage; and cooling the cavity to produce the biodegradable and industrially compostable flexible foam moulded product.
A vehicle interior component comprising: (a) a base; (b) a cover configured to move relative to the base between a closed position and an open position; and (c) a latch mechanism configured to provide an unlatched state for the cover and a latched state for the cover; wherein the latch mechanism comprises a counterweight coupled via a pivot to a latch configured to move the latch between a retracted position and an extended position through an intermediate position; and wherein the latch mechanism is configured to provide the latched state when actuated by an inertia force on the counterweight; characterized in that the latch mechanism comprises a magnet arrangement, wherein the magnet arrangement comprises a magnet in the base and a magnet coupled to the latch, wherein the magnet in the base is configured to retain the latch in the intermediate position by magnetic repulsion when the cover is in the closed position relative to the base. (a) a base; (b) a cover configured to move relative to the base between a closed position and an open position; and (c) a latch mechanism configured to provide an unlatched state for the cover and a latched state for the cover; wherein the latch mechanism comprises a counterweight coupled via a pivot to a latch configured to move the latch between a retracted position and an extended position through an intermediate position; and wherein the latch mechanism is configured to provide the latched state when actuated by an inertia force on the counterweight; characterized in that the latch mechanism comprises a magnet arrangement, wherein the magnet arrangement comprises a magnet in the base and a magnet coupled to the latch, wherein the magnet in the base is configured to retain the latch in the intermediate position by magnetic repulsion when the cover is in the closed position relative to the base.
A method for manufacturing a duct for air intake and for attenuating mouth noises and radiated noises intended to be connected to an internal combustion engine, characterized in that it comprises the steps of: - (a): providing a mold comprising two molding cavities, each cavity having at least one groove adapted to mold a rib and having at least two half-bores adapted to mold end sleeves, - (b): providing a core adapted to be positioned between the cavities, for molding an air intake duct, - (c): positioning on the core a tubular sheet made of an air-porous material, - (d): positioning between the molding cavities the core with the tubular sheet, - (e): injecting into the, or each, groove and into each half-bore of each cavity a thermoplastic material, for overmolding ribs and end sleeves on the tubular sheet, in order to form a duct. - (a): providing a mold comprising two molding cavities, each cavity having at least one groove adapted to mold a rib and having at least two half-bores adapted to mold end sleeves, - (b): providing a core adapted to be positioned between the cavities, for molding an air intake duct, - (c): positioning on the core a tubular sheet made of an air-porous material, - (d): positioning between the molding cavities the core with the tubular sheet, - (e): injecting into the, or each, groove and into each half-bore of each cavity a thermoplastic material, for overmolding ribs and end sleeves on the tubular sheet, in order to form a duct.
A terminal apparatus configured for a fifth-generation cellular system standardized by 3GPP and configured to support EN-DC, comprising a receiver configured to receive an RRC connection reconfiguration message from a base station apparatus, wherein the RRC connection reconfiguration message includes a radio bearer identity, the terminal apparatus further comprises a configuration unit configured to establish a PDCP entity for NR in accordance with a PDCP entity configuration for NR in a case that the radio bearer identity is not a part of current configuration of the terminal apparatus and in a case that the RRC connection reconfiguration message includes the PDCP entity configuration for NR, and the PDCP entity, which is established in accordance with the PDCP entity configuration for NR, corresponds to an MCG bearer for the EN-DC. a receiver configured to receive an RRC connection reconfiguration message from a base station apparatus, wherein the RRC connection reconfiguration message includes a radio bearer identity, the terminal apparatus further comprises a configuration unit configured to establish a PDCP entity for NR in accordance with a PDCP entity configuration for NR in a case that the radio bearer identity is not a part of current configuration of the terminal apparatus and in a case that the RRC connection reconfiguration message includes the PDCP entity configuration for NR, and the PDCP entity, which is established in accordance with the PDCP entity configuration for NR, corresponds to an MCG bearer for the EN-DC.
A DNA molecule encoding a bispecific antibody that binds to both human BAFF and to human IL-17, said DNA molecule comprising a polynucleotide sequence encoding a polypeptide having the amino acid sequence of SEQ ID NO: 1 and comprising a polynucleotide sequence encoding a polypeptide having the amino acid sequence of SEQ ID NO: 2.
Method for reducing in-flight noise for a hybrid helicopter, said hybrid helicopter including: - at least one main rotor provided with a plurality of first blades and at least partially providing the lift and/or the forward propulsion of said hybrid helicopter; - at least one propeller provided with a plurality of second blades and at least partially providing the forward propulsion of said hybrid helicopter; - an autopilot device; and - at least one calculator; characterized in that said method includes the following steps: - determining flight conditions of said hybrid helicopter using at least one sensor of said hybrid helicopter, said flight conditions including an air speed of said hybrid helicopter and an aerodynamic slope of a trajectory followed by said hybrid helicopter; - determining a first value of a first feature of said at least one propeller according to a first database as a function of said flight conditions; - determining a second value of a second feature of said at least one main rotor according to a second database as a function of said first value of said first feature so as to limit noise generation due to a vortex wake caused by each rotating first blade of said at least one main rotor; and - implementing a stabilized flight phase of said hybrid helicopter by applying said first value of said first feature to said at least one propeller and said second value of said second determined feature to said at least one main rotor. - at least one main rotor provided with a plurality of first blades and at least partially providing the lift and/or the forward propulsion of said hybrid helicopter; - at least one propeller provided with a plurality of second blades and at least partially providing the forward propulsion of said hybrid helicopter; - an autopilot device; and - at least one calculator; - determining flight conditions of said hybrid helicopter using at least one sensor of said hybrid helicopter, said flight conditions including an air speed of said hybrid helicopter and an aerodynamic slope of a trajectory followed by said hybrid helicopter; - determining a first value of a first feature of said at least one propeller according to a first database as a function of said flight conditions; - determining a second value of a second feature of said at least one main rotor according to a second database as a function of said first value of said first feature so as to limit noise generation due to a vortex wake caused by each rotating first blade of said at least one main rotor; and - implementing a stabilized flight phase of said hybrid helicopter by applying said first value of said first feature to said at least one propeller and said second value of said second determined feature to said at least one main rotor.