mhurhangee/ep-ind-claims huggingface dataset:
A composition comprising milk-based protein hydrolysate obtainable by treatment of a solution of a milk-based proteinaceous material with a) at least one trypsin-like endopeptidase derived from a microorganism, and b) at least one chymotrypsin-like endopeptidase derived from a microorganism for the induction of oral tolerance in infants or patients in need thereof, or for reducing the risk of allergies in infants or patients in need thereof, or for reducing the severity or frequency of allergies during infancy or later in life, especially in infants or patients in need thereof, wherein the at least one trypsin-like endopeptidase is derived from a strain of Kutzneria albida and has at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, at least 96%, at least 97%, at least 98%, at least 99% or 100% sequence identity to the mature polypeptide SEQ ID NO:1; and wherein the at least one chymotrypsin-like endopeptidase is derived from a strain of Nocardiopsis Sp. or Metarhizium anisopliae and wherein the at least one chymotrypsin-like endopeptidase has at least 75%, at least 80%, at least 85%, at least 90%, at least 95%, at least 96%, at least 97%, at least 98%, at least 99% or 100% sequence identity to polypeptide sequences of EMBL CDS CAI94179 or TREMBL:Q9Y843. a) at least one trypsin-like endopeptidase derived from a microorganism, and b) at least one chymotrypsin-like endopeptidase derived from a microorganism
An electrically-heated catalytic converter comprising: a substrate made of ceramic, the substrate including a catalyst coated layer; electrode films made of ceramic, the electrode films being disposed on a surface of the substrate; electrode terminals made of ceramic, each of the electrode terminals being secured to a corresponding one of the electrode films; and external electrodes each attached to a corresponding one of the electrode terminals via a brazing filler metal, the electrically-heated catalytic converter being characterised in that a thermal expansion coefficient of the brazing filler metal is equal to or higher than a thermal expansion coefficient of the electrode terminals, and is equal to or lower than a thermal expansion coefficient of the external electrodes, and the thermal expansion coefficient of each of the electrode terminals decreases from a portion at which the electrode terminal is joined to the brazing filler metal toward a portion at which the electrode terminal is joined to the corresponding electrode film. a substrate made of ceramic, the substrate including a catalyst coated layer; electrode films made of ceramic, the electrode films being disposed on a surface of the substrate; electrode terminals made of ceramic, each of the electrode terminals being secured to a corresponding one of the electrode films; and external electrodes each attached to a corresponding one of the electrode terminals via a brazing filler metal, the electrically-heated catalytic converter being characterised in that a thermal expansion coefficient of the brazing filler metal is equal to or higher than a thermal expansion coefficient of the electrode terminals, and is equal to or lower than a thermal expansion coefficient of the external electrodes, and the thermal expansion coefficient of each of the electrode terminals decreases from a portion at which the electrode terminal is joined to the brazing filler metal toward a portion at which the electrode terminal is joined to the corresponding electrode film.
Generator comprising winding arrangements, each winding arrangement comprising at least an inner coil and an outer coil constituting a concentric structure of coils, wherein the inner coil is constituted by an inner conductor and the outer coil is constituted by an outer conductor, wherein the inner conductor is wound around a tooth, wherein the inner and outer conductors are connected in series, and wherein the inner conductor has a smaller electrical resistance per unit length than the outer conductor.
A method for transferring data between a movable unit and a stationary unit of a linear transport system, wherein the linear transport system comprises a guide rail for guiding the movable unit, a plurality of stationary units, a controller, and a linear motor for driving the movable unit along the guide rail, wherein the linear motor comprises a stator and a rotor, wherein the stator comprises the stationary units, each comprising one or a plurality of drive coils, wherein the rotor is arranged at the movable unit and comprises one or a plurality of magnets, wherein the stationary units each comprise at least a stationary antenna, wherein the movable unit comprises a movable antenna, wherein the following steps are carried out by the controller: - determining position data of the movable antenna of the movable unit; - selecting that stationary antenna within the linear transport system that is closest to the movable antenna based on the position data of the movable antenna; - outputting a data packet of the selected stationary antenna to the stationary unit, wherein the data packet comprises a control signal, the control signal including identification information by which the selected stationary antenna may be identified, wherein the data packet comprises a data signal to be transmitted via the selected stationary antenna, wherein the data signal comprises a start sequence, the start sequence being configured to trigger a data receipt of the movable unit, wherein the data signal comprises a first communication frame following the start sequence, the first communication frame comprising a start bit and user data to be transmitted, wherein the first communication frame comprises a time stamp. - determining position data of the movable antenna of the movable unit; - selecting that stationary antenna within the linear transport system that is closest to the movable antenna based on the position data of the movable antenna; - outputting a data packet of the selected stationary antenna to the stationary unit, wherein the data packet comprises a control signal, the control signal including identification information by which the selected stationary antenna may be identified, wherein the data packet comprises a data signal to be transmitted via the selected stationary antenna, wherein the data signal comprises a start sequence, the start sequence being configured to trigger a data receipt of the movable unit, wherein the data signal comprises a first communication frame following the start sequence, the first communication frame comprising a start bit and user data to be transmitted, wherein the first communication frame comprises a time stamp.
A lift truck carriage comprising one or more rails (120, 122), each rail comprising a fixture mount to support one or more load handling fixtures and characterised in that a base portion to house a sensor configured to measure forces on the one or more rails (120 122) from the one or more load handling fixtures.
A method of reporting power headroom for a user equipment, UE, to a base station, the method comprising: generating power headroom information by subtracting a first value associated with physical uplink shared channel, PUSCH, and physical uplink control channel, PUCCH transmit power from a second value associated with a maximum UE transmit power in a subframe if a simultaneous PUCCH and PUSCH transmission is allowed; and transmitting (405, 409, 705, 709, 1005, 1009) the power headroom information to the base station. generating power headroom information by subtracting a first value associated with physical uplink shared channel, PUSCH, and physical uplink control channel, PUCCH transmit power from a second value associated with a maximum UE transmit power in a subframe if a simultaneous PUCCH and PUSCH transmission is allowed; and transmitting (405, 409, 705, 709, 1005, 1009) the power headroom information to the base station.
A hydraulic steering system comprising: a steering valve defining a first fluid connection; and a steering cylinder defining a second fluid connection, wherein hydraulic steering fluid moves between the first and second fluid connections (304, 306); characterized by: a piston (308, 350, 370) disposed in a fluid channel between the first and second fluid connections (304, 306), the piston (308, 350, 370) bi-directionally movable along a linear path when the hydraulic steering fluid flows between the first and second fluid connections (304, 306); a detector to detect the bi-directional movement of the piston (308, 350, 370) away from a default position of the piston (308, 350, 370); and a processor communicatively coupled to the detector, the processor to interpret the movement of the piston (308, 350, 370). a steering valve defining a first fluid connection; and a steering cylinder defining a second fluid connection, wherein hydraulic steering fluid moves between the first and second fluid connections (304, 306); characterized by: a piston (308, 350, 370) disposed in a fluid channel between the first and second fluid connections (304, 306), the piston (308, 350, 370) bi-directionally movable along a linear path when the hydraulic steering fluid flows between the first and second fluid connections (304, 306); a detector to detect the bi-directional movement of the piston (308, 350, 370) away from a default position of the piston (308, 350, 370); and a processor communicatively coupled to the detector, the processor to interpret the movement of the piston (308, 350, 370).
Test method for measuring partial discharges at a splice of single-core submarine cables for medium and high voltage having the following method steps that are to be undertaken on both cable ends joined in the splice: - producing an insulating clearance, which is secure against breakthrough for the magnitude of the test voltage and that has no screens, at the cable ends, wherein an outer screen is present on the cable insulation in the region of the splice (8, 20), - providing transitions between the insulating clearance and the outer screen at the cable end with a conductive field control funnel as individual body and transitions between the insulating clearance and the cable splice provided with the outer screen with a field control element having an integrated field control funnel, - bringing the field control funnel present at the cable end and the cable conductor into contact with earth potential; - applying a high-voltage potential to the outer screen of the cable splice; - performing partial discharge measurement. - producing an insulating clearance, which is secure against breakthrough for the magnitude of the test voltage and that has no screens, at the cable ends, wherein an outer screen is present on the cable insulation in the region of the splice (8, 20), - providing transitions between the insulating clearance and the outer screen at the cable end with a conductive field control funnel as individual body and transitions between the insulating clearance and the cable splice provided with the outer screen with a field control element having an integrated field control funnel, - bringing the field control funnel present at the cable end and the cable conductor into contact with earth potential; - applying a high-voltage potential to the outer screen of the cable splice; - performing partial discharge measurement.
Method for automatically removing a cable foil from a cable portion to be processed of an electrical cable, wherein the cable foil is at least partially exposed in the cable portion to be processed, after which, in the region of the cable portion to be processed, at least one crack encircling the cable foil in the shape of a ring is introduced into the cable foil, after which the cable foil is removed from the cable portion to be processed, and wherein at least the following steps are provided for introducing the encircling crack in the shape of a ring: - pre-processing at least one outer layer of the cable foil facing away from the cable centre axis at least in the region of an intended crack position (R P) running around at least partially annularly, wherein the mechanical load-bearing capacity of the outer layer in the region of the intended crack position (R P) is at least reduced by the pre-processing; - eccentrical twisting of the cable portion to be processed and/or bending of the cable portion to be processed in such a way that an inner layer of the cable foil located underneath the pre-processed outer layer cracks in a partially annular or annularly circumferential manner. - pre-processing at least one outer layer of the cable foil facing away from the cable centre axis at least in the region of an intended crack position (R P) running around at least partially annularly, wherein the mechanical load-bearing capacity of the outer layer in the region of the intended crack position (R P) is at least reduced by the pre-processing; - eccentrical twisting of the cable portion to be processed and/or bending of the cable portion to be processed in such a way that an inner layer of the cable foil located underneath the pre-processed outer layer cracks in a partially annular or annularly circumferential manner.
Tyre comprising a carcass reinforcement comprising at least one wire of diameter d expressed in mm, d being less than or equal to 0,25 mm, the steel being a made of ferritic-pearlitic or pearlitic carbon steel comprising: - between 0,3% and 0.7% by weight of manganese, - between 0,1% and 0.3% by weight of silicon, - at most 0,045% by weight of phosphorus, - at most 0,045% by weight of sulphur, and - at most 0,008% by weight of nitrogen characterized in that the wire has a carbon content by weight C, expressed in %, such that 0,42% ≤ C ≤ 0,48%, at most 0,05% by weight of chromium and a maximum tensile strength R, expressed in MPa, such that R ≥ A.(920.C + 500)/d 1/2 with A=0,87 and R ≤ 3,7.(920.C+500), the maximum tensile strength R being measured according to the ISO 6892 standard of 1984. - between 0,3% and 0.7% by weight of manganese, - between 0,1% and 0.3% by weight of silicon, - at most 0,045% by weight of phosphorus, - at most 0,045% by weight of sulphur, and - at most 0,008% by weight of nitrogen
A shut-off valve, particularly a quick-closing valve, for a liquid and/or gaseous fluid, having a substantially cylindrical plug, which can be moved relatively to a valve seat in a fluid chamber of a housing central part along a vertical axis of a housing by means of a drive unit and a valve spindle coupled to the same on the drive side, a drive-side first plug surface and a second plug surface opposite the same being at least approximately the same size, the drive-side valve spindle being coupled to the plug and a compensating valve spindle, which can be displaced in a dependent and passive manner, being connected to the plug on the opposite side thereof, the drive-side valve spindle and the compensating valve spindle being guided out of the fluid chamber, so that the end faces facing away from the plug cannot be loaded with a fluid pressure and have an at least approximately equal outer diameter (D 1,2), characterized in that the drive-side valve spindle is sealed with respect to a housing upper part by means of first metal bellows and a first metal membrane, and the compensating valve spindle is sealed with respect to a housing lower part by means of second metal bellows and a second metal membrane.
Arrangement comprising a first unit having a plug arrangement which has at least one plug and a second unit having a socket arrangement which has at least one corresponding socket, the at least one plug and the at least one socket forming a plug connection when connected to one another wherein, the plug connection is surrounded by a shielding device, which provides good electromagnetic shielding and is formed by the at least one plug and the at least one socket independently, wherein a) the electromagnetic shielding device can be assembled from a first shielding element, which surrounds the plug arrangement, and a second shielding element which surrounds the socket arrangement, wherein b) the at least one plug and/or the at least one socket are arranged in a floating or flexible form to compensate for any tolerances in the mating of the plug connection, the shielding device being connected to the housings (3a,6a) of the units (3,6), which are connected by the plug connection, independently from the floating or flexible arrangement, wherein c) the at least one plug is connected to a first mount element, which is provided with the first shielding element, and the at least one socket is connected to a second mount element which is provided with the second shielding element, wherein d) the first mount element and the second mount element are each provided with mutually corresponding guide elements (18,19) for defined connection to one another, wherein e) the second unit is in the form of a portable flight data recorder in which data obtained from a digital camera can be stored during a photographic flight of an aircraft, and wherein the first unit is in the form of an adaptor which is suitable for holding the flight data recorder, with the adaptor being electrically and/or mechanically connected to the aircraft. a) the electromagnetic shielding device can be assembled from a first shielding element, which surrounds the plug arrangement, and a second shielding element which surrounds the socket arrangement, wherein b) the at least one plug and/or the at least one socket are arranged in a floating or flexible form to compensate for any tolerances in the mating of the plug connection, the shielding device being connected to the housings (3a,6a) of the units (3,6), which are connected by the plug connection, independently from the floating or flexible arrangement, wherein c) the at least one plug is connected to a first mount element, which is provided with the first shielding element, and the at least one socket is connected to a second mount element which is provided with the second shielding element, wherein d) the first mount element and the second mount element are each provided with mutually corresponding guide elements (18,19) for defined connection to one another, wherein e) the second unit is in the form of a portable flight data recorder in which data obtained from a digital camera can be stored during a photographic flight of an aircraft, and wherein the first unit is in the form of an adaptor which is suitable for holding the flight data recorder, with the adaptor being electrically and/or mechanically connected to the aircraft.
A ring laser gyroscope comprising: a cavity containing a gain medium; a first plurality of reflective surfaces (104, 106, 108) coupled to the cavity, the first plurality of reflective surfaces including at least a first reflective surface, a second reflective surface, and a third reflective surface, wherein the first reflective surface, the second reflective surface, and the third reflective surface of the plurality of reflective surfaces are positioned to reflect light along a path defined in the cavity between the plurality of reflective surfaces; at least one medium exciter (112, 114, 116) operable to excite the gain medium, wherein the excited gain medium induces first and second laser fields within the cavity; and characterized by further comprising a saturation beam source, the saturation beam source emitting a saturation beam that intersects the first and second laser fields at a first interaction region of the cavity, wherein the saturation beam interacts with the gain medium to reduce the gain of the first and second laser fields at a first range of frequencies. a cavity containing a gain medium; a first plurality of reflective surfaces (104, 106, 108) coupled to the cavity, the first plurality of reflective surfaces including at least a first reflective surface, a second reflective surface, and a third reflective surface, wherein the first reflective surface, the second reflective surface, and the third reflective surface of the plurality of reflective surfaces are positioned to reflect light along a path defined in the cavity between the plurality of reflective surfaces; at least one medium exciter (112, 114, 116) operable to excite the gain medium, wherein the excited gain medium induces first and second laser fields within the cavity; and characterized by further comprising a saturation beam source, the saturation beam source emitting a saturation beam that intersects the first and second laser fields at a first interaction region of the cavity, wherein the saturation beam interacts with the gain medium to reduce the gain of the first and second laser fields at a first range of frequencies.
A stent-graft system comprising a first hollow cylindrical stent-graft body and at least one second hollow cylindrical stent-graft body, wherein the first and the second stent-graft bodies (30; 50) are two structurally separate stent-graft bodies, and wherein the first and the second stent-graft bodies each have a first end (32; 52), a second end (33; 53), and a longitudinal axis (37; 57), wherein the first and the second stent-graft bodies (30; 50) each comprise a stent-graft portion (34; 54) which is formed from a stent-graft scaffold (20; 60) and a prosthesis material (35; 55) applied thereon, wherein the first and the second stent-graft bodies (30; 50) each further comprise a stent portion (38; 58) which is formed from a stent scaffold (22; 62) which is free from prosthesis material and comprises a first (23; 63) and a second (24; 64) stent-portion end, wherein the stent portion (38; 58) is fixedly connected via its first stent-portion end (23; 63) to the stent-graft portion (34; 54) in each case, and wherein the stent portion of the first stent-graft body and the stent portion of the second stent-graft body are designed in such a way that they can be at least partially inserted into one another via their respective second stent-portion ends (24; 64) in order to form one shared stent portion which is free from prosthesis material.
Method for steering a steerable interceptor missile powered by an engine for intercepting a moving target during a midcourse phase of the interception, wherein the interceptor missile is steered by means of real steering commands, which are generated at respective steering times on the basis of free control parameters, which are available in the form of a current parameter vector, wherein the free control parameters are constantly and/or repetitively optimized in the course of the midcourse phase by means of an optimization procedure for optimizing the control parameters, wherein the optimization procedure takes place in parallel with the actual steering, wherein optimized control parameters are taken into the current parameter vector once they are available from the optimization procedure, characterized in that newly detected information about the movement of the target and/or information about the flight of the interceptor missile are included in the optimization procedure as soon as they are available. wherein the interceptor missile is steered by means of real steering commands, which are generated at respective steering times on the basis of free control parameters, which are available in the form of a current parameter vector, wherein the free control parameters are constantly and/or repetitively optimized in the course of the midcourse phase by means of an optimization procedure for optimizing the control parameters, wherein the optimization procedure takes place in parallel with the actual steering, wherein optimized control parameters are taken into the current parameter vector once they are available from the optimization procedure, characterized in that newly detected information about the movement of the target and/or information about the flight of the interceptor missile are included in the optimization procedure as soon as they are available.
A sintered body from a powder containing at least Co and/or Fe and B, and containing B in an amount of 10 to 50 at%, wherein an oxygen content is 100 wtppm or less and a total content of Al and Si is 100 wtppm or less.