mhurhangee/ep-ind-claims huggingface dataset:
A rolling stand, defining a rolling axis, comprising a support structure, a roll holder cartridge configured to go from a working position inside the support structure, at said rolling axis, to an extracted position outside the support structure with a transverse movement with respect to the rolling axis, three rolling rolls (2, 2', 2"), each of which having a respective yoke support (6, 6', 6"), arranged in the roll holder cartridge with axes thereof arranged at 120o with respect to one another, a first roll of said three rolling rolls having rotation axis thereof arranged vertically, at least one hydraulic capsule (4, 4', 4") for each rolling roll (2, 2', 2") fixed to the support structure, for adjusting the radial position of the respective rolling roll, the hydraulic capsule having a respective thrust cylinder and being configured to allow the respective thrust cylinder to cover a distancing stroke from the rolling axis sufficient to allow to clear the path of the roll holder cartridge between the working position and the extracted position, characterized in that the roll holder cartridge has a longitudinal open slot, the central axis of which coincides with the longitudinal central axis of the yoke support of the first roll, and a width in vertical direction greater than the diameter of the tube being rolled, said open slot being closed at a first end near the rolling axis and open at a second end opposite to the first end and coinciding with a side of the roll holder cartridge, considering the position assumed by the roll holder cartridge when it is inserted in the rolling stand.
A pharmaceutical composition, comprising: (a) a glucokinase activator, wherein the glucokinase activator is a compound represented by the following formulae, or a pharmaceutically acceptable salt, an isotope labeled compound, a crystalline form, a hydrate, or a solvate thereof, and (b) a DPP-IV inhibitor. (a) a glucokinase activator, wherein the glucokinase activator is a compound represented by the following formulae, or a pharmaceutically acceptable salt, an isotope labeled compound, a crystalline form, a hydrate, or a solvate thereof, and (b) a DPP-IV inhibitor.
A landing gear for an aircraft comprising: a main strut arranged to be coupled to the aircraft and movable between a deployed condition and a retracted condition, a stay arranged to support the main strut, the stay comprising a first stay arm coupled to the main strut and a second stay arm pivotally coupled to the first stay arm and arranged to be coupled to the aircraft, a lock assembly arranged to prevent movement of the stay when the lock assembly is in a locked position, the lock assembly comprising a first lock link pivotally coupled to the stay and a second lock link pivotally coupled to the first lock link and arranged to be coupled to the aircraft or another component of the landing gear assembly; and a spring coupled to a first member and to a second member, the spring being arranged to generate a biasing force between the first member and the second member to bias the first member toward a predetermined orientation relative to the second member, wherein the first member is the first lock link or the second lock link characterised in that the spring comprises a plurality of elastically deformable washers; and further characterised in that when the main strut is in the retracted condition, the elastically deformable washers are substantially unstressed. a main strut arranged to be coupled to the aircraft and movable between a deployed condition and a retracted condition, a stay arranged to support the main strut, the stay comprising a first stay arm coupled to the main strut and a second stay arm pivotally coupled to the first stay arm and arranged to be coupled to the aircraft, a lock assembly arranged to prevent movement of the stay when the lock assembly is in a locked position, the lock assembly comprising a first lock link pivotally coupled to the stay and a second lock link pivotally coupled to the first lock link and arranged to be coupled to the aircraft or another component of the landing gear assembly; and a spring coupled to a first member and to a second member, the spring being arranged to generate a biasing force between the first member and the second member to bias the first member toward a predetermined orientation relative to the second member, wherein the first member is the first lock link or the second lock link characterised in that the spring comprises a plurality of elastically deformable washers; and further characterised in that when the main strut is in the retracted condition, the elastically deformable washers are substantially unstressed.
A swirler for a combustor of a gas turbine engine comprising: an inner injector; an outer annular injector which at least partially surrounds said inner injector; and an air-assist atomizer upstream of said inner injector; wherein said air-assist atomizer includes a cascade of porous walls (112A, 112B); wherein said cascade of porous walls (112A, 112B) is a cascade of screens, each with decreasing porosity, wherein the inner injector includes a central passage, an annular central passage, and an inner annular passage, wherein the central passage includes a convergent-divergent exit, wherein the outer annular injector includes an outer annular passage radially outboard of the inner annular passage, wherein an outer wall bounds the outer annular passage, wherein the outer annular passage includes an annular recess tube to stabilize the airflow and facilitate a desired velocity profile and rotation to settle the flame at a desired location beyond a divergent exit defined by an outer wall distal end of the outer wall and the distal end of the inner annular wall. an inner injector; an outer annular injector which at least partially surrounds said inner injector; and an air-assist atomizer upstream of said inner injector; wherein said air-assist atomizer includes a cascade of porous walls (112A, 112B); wherein said cascade of porous walls (112A, 112B) is a cascade of screens, each with decreasing porosity, wherein the inner injector includes a central passage, an annular central passage, and an inner annular passage, wherein the central passage includes a convergent-divergent exit, wherein the outer annular injector includes an outer annular passage radially outboard of the inner annular passage, wherein an outer wall bounds the outer annular passage, wherein the outer annular passage includes an annular recess tube to stabilize the airflow and facilitate a desired velocity profile and rotation to settle the flame at a desired location beyond a divergent exit defined by an outer wall distal end of the outer wall and the distal end of the inner annular wall.
Cleaning device for cleaning items to be cleaned, wherein the cleaning device is selected from the group consisting of a dishwasher and cleaning and disinfecting equipment, wherein the cleaning device includes at least one nozzle system for acting upon the items to be cleaned with at least one cleaning fluid, wherein the cleaning device additionally includes at least one pump for conveying the cleaning fluid to the nozzle system, wherein the nozzle system comprises at least one high pressure nozzle and at least one low pressure nozzle, wherein the high pressure nozzle and the low pressure nozzle are connected fluidically to the pump, wherein at least one fluidic switching element for adjusting an inflow of the cleaning fluid to the low pressure nozzle is connected upstream of the low pressure nozzle, wherein the pump is developed in multiple stages, wherein the pump comprises at least one low pressure stage and at least one high pressure stage which is mounted downstream of the low pressure stage in a direction of flow of the cleaning fluid, wherein an outlet of the low pressure stage is connected to an inlet of the high pressure stage, wherein an outlet of the high pressure stage is connected fluidically to the nozzle system, wherein the outlet of the low pressure stage is additionally connected fluidically to the nozzle system by means of a bypass by bypassing the high pressure stage.
Torque transmission assembly for a drive system of a vehicle, comprising a housing, on which a pump impeller is provided, and in the interior of which housing a turbine impeller is provided, a drive-side friction face arrangement which is coupled to the housing for joint rotation about a rotational axis, an output-side friction face arrangement which is coupled to an output member for joint rotation about the rotational axis and can be brought into frictional engagement with the drive-side friction face arrangement, and a deflection mass arrangement with a deflection mass carrier and at least one deflection mass which is supported on the deflection mass carrier and can be deflected out of a basic relative position with regard to the deflection mass carrier, the deflection mass carrier being connected fixedly to the housing for conjoint rotation about the rotational axis, characterized in that the deflection mass arrangement is arranged in the interior of the housing.
A VPN communication controlling device, which is an edge device in a network, characterized by comprising: a common database (common DB), disposed in a VPN for setting a path between edge devices in a network when a path setting request is issued by a customer so as to supply a different network information for each customer so as to be used for setting a path, the common DB being used for exchanging information between the edge devices in the network and core devices in the network; a link information setting section for setting a link information in the common DB; a link information exchanging section for exchanging the link information among the other edge devices, the core devices, customer edge devices, and the device itself; a route calculating section which determines a transferring route for a control information which is used for exchanging the link information; a VPNDB generating section for generating a VPNDB which is a DB which is different for each VPN and which is used for exchanging information between customer edge devices and edge devices which belong to the VPN corresponding to the VPNDB; a VPNID setting device for adding VPNID as an information for identifying each VPN to each link information, categorized for each VPN related to the link information, by categorizing the link information in the common DB; and a filtering section for extracting the link information for the same VPNID from the link information to which the VPNID. for the common DB is added so as to contain the link information in a corresponding VPNDB. a common database (common DB), disposed in a VPN for setting a path between edge devices in a network when a path setting request is issued by a customer so as to supply a different network information for each customer so as to be used for setting a path, the common DB being used for exchanging information between the edge devices in the network and core devices in the network; a link information setting section for setting a link information in the common DB; a link information exchanging section for exchanging the link information among the other edge devices, the core devices, customer edge devices, and the device itself; a route calculating section which determines a transferring route for a control information which is used for exchanging the link information; a VPNDB generating section for generating a VPNDB which is a DB which is different for each VPN and which is used for exchanging information between customer edge devices and edge devices which belong to the VPN corresponding to the VPNDB; a VPNID setting device for adding VPNID as an information for identifying each VPN to each link information, categorized for each VPN related to the link information, by categorizing the link information in the common DB; and a filtering section for extracting the link information for the same VPNID from the link information to which the VPNID. for the common DB is added so as to contain the link information in a corresponding VPNDB.
Folding propeller for a watercraft, comprising a hub drivable about an axis of rotation via a drive shaft, and a propeller blade having a propeller blade tip portion, a propeller blade shaft portion and a propeller blade root portion, wherein the propeller blade is arranged on the hub so as to be pivotable about a pivot axis between a maximum closed position and a maximum open position, wherein the pivot axis defines, together with a normal (N D) to the axis of rotation that intersects the pivot axis, a maximum opening plane (E Max), wherein, in the driven state and in a pivoted position of the propeller blade in the region of the maximum open position, an opening force acts on the propeller blade, which force results from the rotation of the folding propeller and is directed substantially radially outwards with respect to the axis of rotation, wherein an effective force application point of the opening force is arranged spaced apart from the maximum opening plane (E Max) and is substantially arranged in the closing direction of the propeller blade, characterised in that the effective force application point of the opening force corresponds to the centre of mass of the propeller blade and the opening force is a centrifugal force, that the centre of mass of the propeller blade is arranged distally with respect to the centroid of the propeller blade, and that the centre of mass of the propeller blade is arranged either in the propeller blade tip portion or in the propeller blade shaft portion. a hub drivable about an axis of rotation via a drive shaft, and a propeller blade having a propeller blade tip portion, a propeller blade shaft portion and a propeller blade root portion, wherein the propeller blade is arranged on the hub so as to be pivotable about a pivot axis between a maximum closed position and a maximum open position, wherein the pivot axis defines, together with a normal (N D) to the axis of rotation that intersects the pivot axis, a maximum opening plane (E Max), wherein, in the driven state and in a pivoted position of the propeller blade in the region of the maximum open position, an opening force acts on the propeller blade, which force results from the rotation of the folding propeller and is directed substantially radially outwards with respect to the axis of rotation, wherein an effective force application point of the opening force is arranged spaced apart from the maximum opening plane (E Max) and is substantially arranged in the closing direction of the propeller blade, characterised in that the effective force application point of the opening force corresponds to the centre of mass of the propeller blade and the opening force is a centrifugal force, that the centre of mass of the propeller blade is arranged distally with respect to the centroid of the propeller blade, and that the centre of mass of the propeller blade is arranged either in the propeller blade tip portion or in the propeller blade shaft portion.
A mobile power plant having an engine together with a main gearbox and a free wheel assembly suitable for driving a rotary wing by means of the main gearbox and further having an electric motor-generator, wherein supplemental to the main gearbox there is provided an accessory gear box, an additional freewheel assembly and a pump, said electric motor-generator being on a first side mechanically connected in series via said additional freewheel assembly and said accessory gear box to said main gear box in order to be capable of being driven by said main gear box and said electric motor-generator being mechanically connected on a second side to said pump.
A liner tube for a core barrel assembly, comprising: a sleeve having an inner surface configured to be coupled to a layer of material configured to absorb or adsorb formation fluids or parts of formation fluids, the sleeve being substantially cylindrical, wherein, at every longitudinal location of the sleeve with respect to a longitudinal axis of the sleeve, a transverse cross-section of a wall of the sleeve includes at least one gap extending radially through the entire wall of the sleeve, the at least one gap separating a portion of the sleeve wall on one circumferential side of the at least one gap from another portion of the sleeve wall on an opposite circumferential side of the at least one gap, and the sleeve having a flexibility in a circumferential direction greater than that of a sleeve without a gap extending radially through an entire wall of the sleeve at a transverse cross-section of the sleeve at every longitudinal location of the sleeve; wherein the at least one gap comprises at least one slot formed in an outer surface of the sleeve, each slot extending completely radially through a wall of the sleeve from an outer surface of the sleeve to the inner surface of the sleeve, at least a portion of the slot extending longitudinally discontinuously along at least a portion of an entire length of the sleeve, wherein the slot comprises a plurality of segments, and one or more formations of material of the wall of the sleeve separate the segments of the slot.
An embolus deflector for protecting against cerebral embolization comprising a blood flow permeable covering configured to extend over either (a) the ostia of the right common carotid and left common carotid arteries, or (b) the ostia of the brachiocephalic and the left common carotid arteries; characterized in that the deflector comprises an expandable support frame, wherein the support frame comprises multiple petals, wherein each petal is formed from wire, wherein porous material extends between the wire of the petals to form the blood flow permeable covering; wherein the support frame has a closed configuration wherein the petals are restrained and an open configuration wherein the petals are opened, wherein in the closed configuration the support frame is sized and configured to be introduced into the aorta, and the support frame is sized and configured to be converted from the closed configuration to the open configuration within the aorta, wherein in the open configuration the support frame is sized and configured to support the blood flow permeable covering within the aorta in a position within the aortic arch and against the aortic wall such that the blood flow permeable covering extends over and covers the left common carotid artery ostium while simultaneously extending over and covering at least one of the ostia of the brachiocephalic artery or of the right common carotid artery, wherein the blood flow permeable covering simultaneously presents a low profile against the aortic wall and within the lumen of the aortic arch to thereby cause minimal resistance to blood flow in the aortic arch by permitting blood to flow through the aortic arch past the blood flow permeable covering without passing therethrough and also to allow sheaths, catheters, or wires to pass through the aortic arch and past the blood flow permeable covering without passing therethrough..
An actuating device, in particular for a thermostat valve, with an expansion substance element including a housing and at least one expansion substance received in the housing, and with a heating pin, which can be supplied with electrical energy for heating the expansion substance, wherein the heating pin passes through a closure device of the expansion substance element, and wherein the expansion substance element is movable relative to the heating pin by heating the expansion substance, characterized in that the heating pin comprises a base body with an outer side facing the expansion substance, wherein at least one heating element (40, 70) is arranged on the outer side, which can be supplied with the electrical energy, and wherein at least a partial area of an outer surface of the heating pin is formed by the at least one heating element (40, 70), which is in contact with the expansion substance in radial direction of the heating pin.
A composition for the removal of biofilm formed by Staphylococcus aureus containing bacteriophage capable of killing Staphylococcus aureus specifically and effective in destroying biofilm formed by Staphylococcus oureus as an active ingredient, wherein the bacteriophage is the Myoviridae family T4-like phage genus bacteriophage designated bacteriophage SAP-1 and deposited at the Korean Collection for Type Cultures on July 10, 2007 under the Accession No: KCTC 11153BP or the Podoviridoe family φ29-like virus genus bacteriophage designated bacteriophage SAP-2 and deposited at the Korean Collection for Type Cultures on July 10, 2007 under the Accession No: KCTC 11154BP.
An ice protection system suitable for being connected to an associated aerodynamic structure, the system comprising: a heating device (400, 858, 948) having a plurality of carbon nanotube resistive heating elements; and a controller comprising: a power circuit topology having at least one buck converter; and a processor configured to: determine an ideal setpoint temperature of one or more of the plurality of CNT resistive heating elements; determine a progressively adjusted setpoint temperature by comparing the ideal setpoint temperature to a current measured temperature of one or more of the plurality of CNT resistive heating elements; and produce a drive signal output based on at least the measured current temperature and the instantaneous progressively adjusted setpoint temperature. a heating device (400, 858, 948) having a plurality of carbon nanotube resistive heating elements; and a controller comprising: a power circuit topology having at least one buck converter; and a processor configured to: determine an ideal setpoint temperature of one or more of the plurality of CNT resistive heating elements; determine a progressively adjusted setpoint temperature by comparing the ideal setpoint temperature to a current measured temperature of one or more of the plurality of CNT resistive heating elements; and produce a drive signal output based on at least the measured current temperature and the instantaneous progressively adjusted setpoint temperature. a power circuit topology having at least one buck converter; and a processor configured to: determine an ideal setpoint temperature of one or more of the plurality of CNT resistive heating elements; determine a progressively adjusted setpoint temperature by comparing the ideal setpoint temperature to a current measured temperature of one or more of the plurality of CNT resistive heating elements; and produce a drive signal output based on at least the measured current temperature and the instantaneous progressively adjusted setpoint temperature. determine an ideal setpoint temperature of one or more of the plurality of CNT resistive heating elements; determine a progressively adjusted setpoint temperature by comparing the ideal setpoint temperature to a current measured temperature of one or more of the plurality of CNT resistive heating elements; and produce a drive signal output based on at least the measured current temperature and the instantaneous progressively adjusted setpoint temperature.