mhurhangee/ep-ind-claims huggingface dataset:
An olefin polymer comprising a higher molecular weight component and a lower molecular weight component, wherein the olefin polymer has: a density in a range from 0.895 to 0.930 g/cm 3 (ASTM D1505 & ASTM D4703); a ratio of Mw/Mn in a range from 8 to 35; a HLMI in a range from 4 to 50 g/10 min (ASTM D1238); less than 0.008 LCB per 1000 total carbon atoms; and a reverse comonomer distribution. a density in a range from 0.895 to 0.930 g/cm 3 (ASTM D1505 & ASTM D4703); a ratio of Mw/Mn in a range from 8 to 35; a HLMI in a range from 4 to 50 g/10 min (ASTM D1238); less than 0.008 LCB per 1000 total carbon atoms; and a reverse comonomer distribution.
Simulation and test system, characterized in that it comprises a first level comprising a communication layer in the form of a ring computer network provided with communication nodes consisting of routing means (R0, R1, R2,..., Rn) linked together, a second level around the first level, the said second level comprising calculation nodes grouping together heterogeneous calculation means, the calculation nodes being associated with the communication nodes of the communication layer, and a third level consisting of the actual systems under test, the said heterogeneous calculation means comprising: - at least one work station based on one or more processors suitable for carrying out a sequential or parallel execution of software avionics models; - at least one first reconfigurable calculation circuit suitable for carrying out a parallel execution of hardware avionics models; - one or more input/output interface boards which integrate at least one second reconfigurable circuit hosting one or more input/output resources suitable for simulating various avionics buses such as AFDX, MIL-STD-1553, ARINC 429, etc. so as to replace specialized input/output boards, the said routing means (R0, R1, R2,..., Rn) being embodied on the basis of routers provided with a switch ensuring inter and intra node(s) communication, of an arbitrator suitable for ensuring an arbitration strategy at the level of the switch and a synchronization between the calculation elements and the inputs/outputs, of a reconfigurable component hosting a clock resource for defining a time base common to the whole set of elements of the node, a memory component or a memory resource on the reconfigurable component, designed to store routing tables so as to route the inter and intra node(s) communication frames. - at least one work station based on one or more processors suitable for carrying out a sequential or parallel execution of software avionics models; - at least one first reconfigurable calculation circuit suitable for carrying out a parallel execution of hardware avionics models; - one or more input/output interface boards which integrate at least one second reconfigurable circuit hosting one or more input/output resources suitable for simulating various avionics buses such as AFDX, MIL-STD-1553, ARINC 429, etc. so as to replace specialized input/output boards,
A drive system for a brushless DC motor having a rotor including at least one permanent magnet and a stator including at least one phase winding, the drive system comprising a drive circuit including switch means adapted to be connected with the phase winding and to vary the current passing through the phase winding; rotor position sensing means arranged to sense the position of the rotor; and control means arranged to provide drive signals to control the switch means; the drive system including means to receive a temperature signal that has a value dependent upon the temperature of the at least one magnet of the rotor, the control means being arranged to vary the phase of the current passing through the winding relative to the rotor position dependent upon the temperature of the rotor magnet, characterised in that the control means is adapted to control the motor in a normal control mode, whereby the control means is arranged to advance the phase of the current passing through the winding as a function of the motor rotor speed, when the rotor magnet temperature is below a predetermined temperature and in an abnormal control mode, whereby the amount of phase advance is less than that applied if the motor were operating in the normal control mode, when the rotor magnet temperature is above said predetermined temperature.
A label printer for printing labels applied to a carrier tape, in particular wound onto a roll, comprising a printhead and a counter-element to the printhead, which is configured to hold the carrier tape with the labels in contact with the printhead, in particular a driven print roller, wherein the carrier tape can be led between the printhead and the counter-element; a drive mechanism for the carrier tape having a driven carrier tape drawing roller which is rotatable about an axis of rotation; and at least one non-driven carrier tape pressure roller which is associated with the carrier tape drawing roller, which has two axial ends, which is rotatable about a rotational axis and which extends in parallel with the axis of rotation of the carrier tape drawing roller, wherein the carrier tape can be led between the carrier tape drawing roller and the respective carrier tape pressure roller and can in particular be transported along a predefined carrier tape transport path, characterized in that the respective carrier tape pressure roller is displaceably supported perpendicular to its rotational axis and in a displacement direction toward the carrier tape drawing roller, with a spring device being provided to exert a pressing force onto the carrier tape, said spring device preloading the respective carrier tape pressure roller in the displacement direction. a printhead and a counter-element to the printhead, which is configured to hold the carrier tape with the labels in contact with the printhead, in particular a driven print roller, wherein the carrier tape can be led between the printhead and the counter-element; a drive mechanism for the carrier tape having a driven carrier tape drawing roller which is rotatable about an axis of rotation; and at least one non-driven carrier tape pressure roller which is associated with the carrier tape drawing roller, which has two axial ends, which is rotatable about a rotational axis and which extends in parallel with the axis of rotation of the carrier tape drawing roller, wherein the carrier tape can be led between the carrier tape drawing roller and the respective carrier tape pressure roller and can in particular be transported along a predefined carrier tape transport path,
A method for transmitting uplink data in an unlicensed band by a user equipment, UE, the method comprising: receiving configuration information for one or more subbands for a system bandwidth of a cell configured in the unlicensed band or a bandwidth part configured in the unlicensed band; receiving downlink control information including uplink frequency domain resource allocation information for transmitting uplink data in the bandwidth part or the system bandwidth; performing a listen before talk, LBT, operation on each of subbands where a frequency resource allocated for uplink data transmission belongs, based on the resource allocation information and determining whether the LBT operation is identified to succeed on all of the subbands where the frequency resource allocated for the uplink data transmission belongs; and transmitting the uplink data in all of the subbands where the frequency resource allocated for the uplink data transmission belongs only when the LBT operation is identified to succeed on all of the subbands where the frequency resource allocated for the uplink data transmission belongs. receiving configuration information for one or more subbands for a system bandwidth of a cell configured in the unlicensed band or a bandwidth part configured in the unlicensed band; receiving downlink control information including uplink frequency domain resource allocation information for transmitting uplink data in the bandwidth part or the system bandwidth; performing a listen before talk, LBT, operation on each of subbands where a frequency resource allocated for uplink data transmission belongs, based on the resource allocation information and determining whether the LBT operation is identified to succeed on all of the subbands where the frequency resource allocated for the uplink data transmission belongs; and transmitting the uplink data in all of the subbands where the frequency resource allocated for the uplink data transmission belongs only when the LBT operation is identified to succeed on all of the subbands where the frequency resource allocated for the uplink data transmission belongs.
A method for the measurement of angles at a workpiece during the bending of the workpiece to a predetermined angle in a press brake, where the bending operation takes place between a moveable die and a pressure table, comprising at least one measurement arrangement that can be displaced along a guide parallel to the workpiece with a measurement head intended for the measurement of the angle at the workpiece after the bending operation, and adjustment means for adjusting the curvature of the pressure table towards or away from the movable die, wherein the process stages of the operation: - that the moveable die is displaced in the direction towards the workpiece, - that the workpiece is bent, - that the moveable die is displaced in the direction away from the workpiece, characterised in that the at least one measurement arrangement is caused to move along the guide, whereby - several present values of the angle are measured continuously along the complete length of the workpiece, in that - a target value of the angle at the workpiece is measured at one position along the workpiece, in that - the pressure table is adjusted in those positions at which the present values of the angle at the workpiece deviate from the target value of the angle at the workpiece, in that - the moveable die is displaced in the direction towards the workpiece, in that, - the workpiece is bent to its final form, and in that - the moveable die is displaced away from the workpiece. - that the moveable die is displaced in the direction towards the workpiece, - that the workpiece is bent, - that the moveable die is displaced in the direction away from the workpiece, - several present values of the angle are measured continuously along the complete length of the workpiece, in that - a target value of the angle at the workpiece is measured at one position along the workpiece, in that - the pressure table is adjusted in those positions at which the present values of the angle at the workpiece deviate from the target value of the angle at the workpiece, in that - the moveable die is displaced in the direction towards the workpiece, in that, - the workpiece is bent to its final form, and in that - the moveable die is displaced away from the workpiece.
Measuring instrument (10, 110, 210) for the gravimetric determination of moisture content, with a housing (20, 120, 220) and a weighing device arranged inside the housing (20, 120, 220), wherein the weighing device comprises a load receiver (60, 160, 260) onto which a sample can be placed, wherein the housing (20, 120, 220) comprises a stationary housing part (21, 121, 221) and a movable housing part (22, 122, 222), wherein the movable housing part (22, 122, 222) can alternately occupy a measuring position and a loading position, wherein in said loading position the stationary housing part (21, 121, 221) and the movable housing part (22, 122, 222) are spaced apart from each other in such a way that a sample can be put on the load receiver (60, 160, 260), wherein in said measuring position, the stationary housing part (21, 121, 221) and the movable housing part (22, 122, 222) form an essentially enclosed testing compartment surrounding the load receiver (60, 160, 260), and wherein a sample-heating means (70, 170, 270) is arranged in the testing compartment to perform the function of heating a sample that is placed on the load receiver (60, 160, 260), characterized in that the movable housing part (22, 122, 222) can be brought from the measuring position into the loading position by means of a position-changing device (24, 224) and that said movement from the measuring position into the loading position takes place simultaneously in a horizontal and a vertical direction.
A reconfigurable floorboard system for use in an aircraft, the reconfigurable floorboard system comprising: a floor grid structure (100; 202) comprising: a plurality of floor beams configured to extend laterally between opposite sides of a fuselage of the aircraft; and a plurality of floor tracks configured to extend substantially orthogonally to the floor beams; and a plurality of floorboards (112; 300) configured to be disposed on the grid structure, each floorboard comprising: a substantially trapezoid shaped plate; characterized in that each floorboard further comprises: an interlocking feature formed proximate an edge of at least three sides of the plate for interlocking with adjacent floorboards, each interlocking feature being formed to interlock with a mating interlocking feature formed at an edge of a side of at least one adjacent floorboard; and a notch formed on an underside of the plate proximate each corner of the plate to contact a member of the floor grid structure to prevent lateral movement of the floorboard. a floor grid structure (100; 202) comprising: a plurality of floor beams configured to extend laterally between opposite sides of a fuselage of the aircraft; and a plurality of floor tracks configured to extend substantially orthogonally to the floor beams; and a plurality of floor beams configured to extend laterally between opposite sides of a fuselage of the aircraft; and a plurality of floor tracks configured to extend substantially orthogonally to the floor beams; and a plurality of floorboards (112; 300) configured to be disposed on the grid structure, each floorboard comprising: a substantially trapezoid shaped plate; characterized in that each floorboard further comprises: an interlocking feature formed proximate an edge of at least three sides of the plate for interlocking with adjacent floorboards, each interlocking feature being formed to interlock with a mating interlocking feature formed at an edge of a side of at least one adjacent floorboard; and a notch formed on an underside of the plate proximate each corner of the plate to contact a member of the floor grid structure to prevent lateral movement of the floorboard. an interlocking feature formed proximate an edge of at least three sides of the plate for interlocking with adjacent floorboards, each interlocking feature being formed to interlock with a mating interlocking feature formed at an edge of a side of at least one adjacent floorboard; and a notch formed on an underside of the plate proximate each corner of the plate to contact a member of the floor grid structure to prevent lateral movement of the floorboard.
A hydrocracking catalyst synthesis method using a synthesis system comprising at least one high-pressure container to receive the support material and the metal precursor and having at least one body resistant to high pressure; at least one carbon dioxide source for supplying carbon dioxide gas into the high-pressure container; at least one pump for delivering the carbon dioxide supplied into the high-pressure container under a pressure allowing it to transform into the supercritical phase; at least one temperature regulation unit to regulate the temperature of the high-pressure container so as to bring the carbon dioxide supplied to the high-pressure container to a temperature allowing it to transform into the supercritical phase; at least one heating furnace to heat and to subject to calcination said support material after the said metal precursor is dissolved in the carbon dioxide in the supercritical phase and adsorbed into the support material the synthesis method comprising the steps of - introducing (a) the metal precursor comprising nickel and/or tungsten, and support material which is in the form of a zeolite pellet into the high-pressure container; - supplying the carbon dioxide received from the carbon dioxide source by means of the pump into the high-pressure container at a pressure allowing the carbon dioxide to transform into the supercritical phase; - bringing the carbon dioxide in the high-pressure container to a temperature allowing it to transform into the supercritical phase by means of the temperature regulation unit so that the metal precursor in the high-pressure container is dissolved in carbon dioxide and adsorbed (b) by the support material; - heating the support material inside the said furnace and subjecting it to a calcination (c) process so as to allow the metal precursor adsorbed by the support material to oxidize. - introducing (a) the metal precursor comprising nickel and/or tungsten, and support material which is in the form of a zeolite pellet into the high-pressure container; - supplying the carbon dioxide received from the carbon dioxide source by means of the pump into the high-pressure container at a pressure allowing the carbon dioxide to transform into the supercritical phase; - bringing the carbon dioxide in the high-pressure container to a temperature allowing it to transform into the supercritical phase by means of the temperature regulation unit so that the metal precursor in the high-pressure container is dissolved in carbon dioxide and adsorbed (b) by the support material; - heating the support material inside the said furnace and subjecting it to a calcination (c) process so as to allow the metal precursor adsorbed by the support material to oxidize.
A material handling vehicle comprising: a vehicle body; an operator compartment; and a mast including: a mounting platform; a first support member coupled to the mounting platform; a second support member coupled to the mounting platform; and a detection system coupled to the mast, and the mast is coupled to the vehicle body at a frontward location relative to the operator compartment, the position of the mast on the vehicle body prevents the mast from impeding a field of view of an operator positioned in the operator compartment characterized in that the material handling vehicle further comprises a display, and wherein the display includes the highest point of the material handling vehicle. a vehicle body; an operator compartment; and a mast including: a mounting platform; a first support member coupled to the mounting platform; a second support member coupled to the mounting platform; and a detection system coupled to the mast, and the mast is coupled to the vehicle body at a frontward location relative to the operator compartment, the position of the mast on the vehicle body prevents the mast from impeding a field of view of an operator positioned in the operator compartment characterized in that the material handling vehicle further comprises a display, and wherein the display includes the highest point of the material handling vehicle. a mounting platform; a first support member coupled to the mounting platform; a second support member coupled to the mounting platform; and a detection system coupled to the mast, and the mast is coupled to the vehicle body at a frontward location relative to the operator compartment, the position of the mast on the vehicle body prevents the mast from impeding a field of view of an operator positioned in the operator compartment characterized in that the material handling vehicle further comprises a display, and wherein the display includes the highest point of the material handling vehicle.
A ram air turbine, comprising: a turbine assembly comprising blades and a hub to which the blades are connected; a generator or a pump; and a drivetrain mechanically interposed between the turbine assembly and the generator or the pump, each blade comprising: an exterior, airfoil-shaped structure defining an interior; and support structures disposed within the interior which connect with an inner surface of the exterior, airfoil-shaped structure and which define hollow regions within the interior, characterized in that the support structures are provided in a honeycomb pattern, a pitch between proximal support structures varies with increasing radial distance from the hub and widths of the support structures varies with increasing radial distance from the hub such that the support structures are lightest at a tip of the blade. a turbine assembly comprising blades and a hub to which the blades are connected; a generator or a pump; and a drivetrain mechanically interposed between the turbine assembly and the generator or the pump, each blade comprising: an exterior, airfoil-shaped structure defining an interior; and support structures disposed within the interior which connect with an inner surface of the exterior, airfoil-shaped structure and which define hollow regions within the interior, an exterior, airfoil-shaped structure defining an interior; and support structures disposed within the interior which connect with an inner surface of the exterior, airfoil-shaped structure and which define hollow regions within the interior, characterized in that the support structures are provided in a honeycomb pattern, a pitch between proximal support structures varies with increasing radial distance from the hub and widths of the support structures varies with increasing radial distance from the hub such that the support structures are lightest at a tip of the blade.
A method of curing a composite structure, the method comprising: expanding a foam mixture in desired cells of a stock core member, by masking off undesired cells so that the foam mixture does not enter the undesired cells, until the foam mixture becomes an expanded foam; machining the stock core member so that the desired cells of the stock core member form a ramp portion; assembling a first uncured composite skin and a second uncured composite skin with the machined core member therebetween; curing the first uncured composite skin, the second uncured composite skin, and the machined core with heat and pressure. expanding a foam mixture in desired cells of a stock core member, by masking off undesired cells so that the foam mixture does not enter the undesired cells, until the foam mixture becomes an expanded foam; machining the stock core member so that the desired cells of the stock core member form a ramp portion; assembling a first uncured composite skin and a second uncured composite skin with the machined core member therebetween; curing the first uncured composite skin, the second uncured composite skin, and the machined core with heat and pressure.
A method of linear amplification of a least one nucleic acid target in a sample comprising: (a) contacting each target in the sample with a nucleic acid polymerase and a primer comprising - a component preventing copying of the primer by the nucleic acid polymerase; and - at least one exonuclease blocking nucleotide; (b) generating a primer extension product; (c) preventing priming by the 3'-end of the primer extension product (d) repeating steps b) and c) at least once, wherein the component preventing copying of the primer by the nucleic acid polymerase is a precursor of a quadruplex-forming sequence. (a) contacting each target in the sample with a nucleic acid polymerase and a primer comprising - a component preventing copying of the primer by the nucleic acid polymerase; and - at least one exonuclease blocking nucleotide; - a component preventing copying of the primer by the nucleic acid polymerase; and - at least one exonuclease blocking nucleotide; (b) generating a primer extension product; (c) preventing priming by the 3'-end of the primer extension product (d) repeating steps b) and c) at least once,