mhurhangee/ep-ind-claims huggingface dataset:
An interlayer film for laminated glass comprising: a first layer; a second layer laminated on a first surface of the first layer, wherein the first layer comprises a polyvinyl acetate resin and a plasticizer; and a third layer laminated on a second surface opposite to the first surface of the first layer, wherein the third layer comprises a polyvinyl acetal resin; and the polyvinyl acetal resin in the third layer has an acetylation degree of 15 mol% or less and a hydroxyl group content of 20 mol% or more. a first layer; a second layer laminated on a first surface of the first layer, wherein the first layer comprises a polyvinyl acetate resin and a plasticizer; and a third layer laminated on a second surface opposite to the first surface of the first layer, wherein the third layer comprises a polyvinyl acetal resin; and the polyvinyl acetal resin in the third layer has an acetylation degree of 15 mol% or less and a hydroxyl group content of 20 mol% or more.
A planet carrier for an epicyclic speed reduction gear, comprising an annular cage comprising two sides (9, 10) extending radially and linked by bridges, seats extending axially between the sides (9, 10) and being intended to support planet gears mounted rotating about the seats, characterized in that one of the sides (9, 10) of the cage is irremovably fixed to a torque output member in such a way as to form a single structural assembly, and in that the torque output member comprises an axially extending tubular portion, one end of which is extended by an annular linking portion extending radially and linked to the matching side of the cage, for example by welding or brazing, both sides (9, 10) having the same radial stiffness and the same torsional stiffness.
A polyethylene composition for the manufacture of an article, comprising the following components: - from 35 to 69.5 wt.% of linear low-density polyethylene (LLDPE); - from 30 to 50 wt.% of high-density polyethylene (HDPE); - from 0.5 to 10 wt.% of a nucleating agent selected from talc or soot (carbon black); and - from 0 to 5 wt.% an optional other additive or a mixture of additives, wherein the nucleating agent is introduced into the composition as a masterbatch in the LLDPE when soot (carbon black) is used, or as a masterbatch in the HDPE when talc is used, and polyethylene composition characterized by tear strength to 39.7 MPa and the relative elongation at break at 23°C to 790%. - from 35 to 69.5 wt.% of linear low-density polyethylene (LLDPE); - from 30 to 50 wt.% of high-density polyethylene (HDPE); - from 0.5 to 10 wt.% of a nucleating agent selected from talc or soot (carbon black); and - from 0 to 5 wt.% an optional other additive or a mixture of additives, wherein the nucleating agent is introduced into the composition as a masterbatch in the LLDPE when soot (carbon black) is used, or as a masterbatch in the HDPE when talc is used, and polyethylene composition characterized by tear strength to 39.7 MPa and the relative elongation at break at 23°C to 790%.
A method of automatically generating a background measurement in a spectrometer comprising the steps of: collecting a plurality of candidate scans in the spectrometer; determining for each of the plurality of candidate scans if the candidate scan correlates to an orthonormal basis set that is associated with a recent background description to determine whether the candidate scan matches the recent background description, wherein the orthonormal basis is calculated from a subset of the data collected for a recent background measurement; saving each candidate scan that correlates to the orthonormal basis set as a background scan in a scan cache; and generating a new background measurement from a plurality of the background scans stored in the scan cache if a current background measurement is older than a preselected time interval. collecting a plurality of candidate scans in the spectrometer; determining for each of the plurality of candidate scans if the candidate scan correlates to an orthonormal basis set that is associated with a recent background description to determine whether the candidate scan matches the recent background description, wherein the orthonormal basis is calculated from a subset of the data collected for a recent background measurement; saving each candidate scan that correlates to the orthonormal basis set as a background scan in a scan cache; and generating a new background measurement from a plurality of the background scans stored in the scan cache if a current background measurement is older than a preselected time interval.
A method for sealing a flexible package of collapsible type comprising providing a first seal extending transverse a filling channel of the flexible package, and providing a second seal extending transverse the filling channel of the flexible package, said second seal overlapping said first seal such that a combined seal is provided comprising a top portion formed solely by a first sealing unit, an intermediate portion formed by the first and a second sealing unit, and a bottom portion formed solely by the second sealing unit, characterized by setting operating parameters comprising a time parameter, a temperature parameter and a pressure parameter for providing said first seal and for providing said second seal such that a sealing characteristic below a threshold value is obtained in said top portion and said bottom portion and such that a sealing characteristic equal to or above the threshold value is obtained in said intermediate portion. providing a first seal extending transverse a filling channel of the flexible package, and providing a second seal extending transverse the filling channel of the flexible package, said second seal overlapping said first seal such that a combined seal is provided comprising a top portion formed solely by a first sealing unit, an intermediate portion formed by the first and a second sealing unit, and a bottom portion formed solely by the second sealing unit, characterized by setting operating parameters comprising a time parameter, a temperature parameter and a pressure parameter for providing said first seal and for providing said second seal such that a sealing characteristic below a threshold value is obtained in said top portion and said bottom portion and such that a sealing characteristic equal to or above the threshold value is obtained in said intermediate portion.
A brake caliper (1, 1') for a disc brake comprising a caliper body, a brake pad and at least one retraction device of the brake pad from a braking disc, said device being configured to retract said brake pad from at least one of opposite braking surfaces (6, 7) delimited by the braking disc; wherein the brake pad comprises a friction material delimiting a pad plane adapted to lean against the braking surface (6, 7) to exert a braking action on the braking disc, said brake pad being adapted to receive a thrust along an axial direction (X-X) by at least one thrust device hosted in the caliper body; wherein the caliper body delimits a first pad abutment surface, inclined in a non-orthogonal direction with respect to the pad plane and with respect to said axial direction (X-X), to delimit a tapered space with the braking surface (6, 7) of the braking disc, the first pad abutment surface being oriented so that, during the braking action, said surface guides the brake pad wedging in the tapered space; wherein the brake pad delimits a retraction surface, inclined in a non-orthogonal direction with respect to the pad plane and oriented so that, during the retraction action, the brake pad is guided partially outside of the tapered space, characterized in that the retraction device of the brake pad comprises a working portion (16, 17), movable in a transverse direction (Y-Y), incident or substantially orthogonal with respect to the axial direction (X-X), said portion (16, 17) being pressed in abutment of the retraction surface, slidably along the latter, to retract the brake pad.
Orientable rocket motor system for an airborne vehicle, said rocket motor comprising a combustion chamber and a nozzle connected by a neck of said nozzle, and said system making it possible to orient said rocket motor with respect to a reference position (P o) defining a reference axis (m o - m o) which, when said rocket motor is in said reference position (P o), is orthogonal to the orifice for ejecting gases from the nozzle and passes through the centre of said gas-ejection orifice, characterised in that it comprises tilting means: • by which said rocket motor is rigidly connected to said nozzle neck by the adjacent part of said nozzle, and • which are adapted to tilt said nozzle and said combustion chamber in opposite directions so that said rocket motor adopts, with respect to said reference position (P o), tilted positions (P 1, P 2, P 3) in which the centre of said orifice for ejecting gases from the nozzle is situated on said reference axis (m o - m o), said tilting means comprising a hollow base structure, having a truncated pyramid shape: • that is deformable in both directions (12,1, 12.2) of a first deformation direction, under the action of first actuation means, • which carries said rocket motor by the small base thereof, and • inside which said combustion chamber is housed. • by which said rocket motor is rigidly connected to said nozzle neck by the adjacent part of said nozzle, and • which are adapted to tilt said nozzle and said combustion chamber in opposite directions so that said rocket motor adopts, with respect to said reference position (P o), tilted positions (P 1, P 2, P 3) in which the centre of said orifice for ejecting gases from the nozzle is situated on said reference axis (m o - m o), • that is deformable in both directions (12,1, 12.2) of a first deformation direction, under the action of first actuation means, • which carries said rocket motor by the small base thereof, and • inside which said combustion chamber is housed.
A compliance unit comprising a body portion, a slide portion, and a table portion, wherein a retainer that holds a plurality of first balls is arranged between a slide body constituting the slide portion and a base plate constituting the table portion, the plurality of first balls are arranged around an axis of the slide portion that coincides with a Z-axis, a single second ball is arranged on the axis of the slide portion between a first ball receiving plate constituting the slide portion and a second ball receiving plate constituting the table portion, the table portion is movable in a XY plane with respect to the slide portion, and the table portion is tiltable with respect to the slide portion. a retainer that holds a plurality of first balls is arranged between a slide body constituting the slide portion and a base plate constituting the table portion, the plurality of first balls are arranged around an axis of the slide portion that coincides with a Z-axis, a single second ball is arranged on the axis of the slide portion between a first ball receiving plate constituting the slide portion and a second ball receiving plate constituting the table portion, the table portion is movable in a XY plane with respect to the slide portion, and the table portion is tiltable with respect to the slide portion.
A method for adjusting powers of at least two generator sets, characterized in that the method comprises steps of: measuring rotational feature of each engine, calculating at least the lowest harmonic wave of said rotational feature of each engine, obtaining crank angle information of each engine, determining a phase of each engine with respect to a global phase coordinate, determining a phase of each harmonic wave in the global phase coordinate, calculating phase differences between the corresponding phases of the engines, calculating a global crank angle reference of each harmonic wave, adjusting actuator means of each engine to obtain global crank angle reference of the respective order. measuring rotational feature of each engine, calculating at least the lowest harmonic wave of said rotational feature of each engine, obtaining crank angle information of each engine, determining a phase of each engine with respect to a global phase coordinate, determining a phase of each harmonic wave in the global phase coordinate, calculating phase differences between the corresponding phases of the engines, calculating a global crank angle reference of each harmonic wave, adjusting actuator means of each engine to obtain global crank angle reference of the respective order.
A method for moving User Equipment, UE, comprising: receiving, by a Radio Network Controller, RNC, a first message sent by the UE; according to a decision rule, deciding, by the RNC, whether a target RNC Cluster corresponding to the first message is a RNC Cluster where the RNC is located, wherein the RNC Cluster is composed of one or more RNCs; based on that the decision result is yes, then sending, by the RNC, a second message to perform internal processing of the first message in the RNC Cluster; or, based on that the decision result is no, then sending, by the RNC, the second message to the target RNC Cluster; wherein the RNC Cluster has an RNC Cluster Identity, ID, and the value of the RNC Cluster ID is same as the first n bits of an RNC ID of the RNC in the RNC Cluster. receiving, by a Radio Network Controller, RNC, a first message sent by the UE; according to a decision rule, deciding, by the RNC, whether a target RNC Cluster corresponding to the first message is a RNC Cluster where the RNC is located, wherein the RNC Cluster is composed of one or more RNCs; based on that the decision result is yes, then sending, by the RNC, a second message to perform internal processing of the first message in the RNC Cluster; or, based on that the decision result is no, then sending, by the RNC, the second message to the target RNC Cluster; wherein the RNC Cluster has an RNC Cluster Identity, ID, and the value of the RNC Cluster ID is same as the first n bits of an RNC ID of the RNC in the RNC Cluster.
A blood component collection cassette which includes a cassette main body, where a flow path is formed, and is configured to be mountable to a blood component separation device, wherein a sheet-shaped filter member configured to trap a blood coagulated clot is arranged on the flow path in the cassette main body, the cassette main body has a filter housing unit that houses the filter member, a first tube having an inner cavity communicating with an inner space of the filter housing unit and a second tube having an inner cavity communicating with the inner space at a position different from a position where the first tube communicates with the inner space are arranged in the cassette main body, and the inner space is separated by the filter member into a first space on the side of the first tube and a second space on the side of the second tube, wherein the cassette main body has a first sheet and a second sheet which are formed of a soft material, the first sheet and the second sheet are superposed in a thickness direction and bonded to each other, and the flow path is formed between the first sheet and the second sheet. a sheet-shaped filter member configured to trap a blood coagulated clot is arranged on the flow path in the cassette main body, the cassette main body has a filter housing unit that houses the filter member, a first tube having an inner cavity communicating with an inner space of the filter housing unit and a second tube having an inner cavity communicating with the inner space at a position different from a position where the first tube communicates with the inner space are arranged in the cassette main body, and the inner space is separated by the filter member into a first space on the side of the first tube and a second space on the side of the second tube, wherein the cassette main body has a first sheet and a second sheet which are formed of a soft material, the first sheet and the second sheet are superposed in a thickness direction and bonded to each other, and the flow path is formed between the first sheet and the second sheet.
A peripheral catheter, comprising: a catheter body comprising a proximal end, a distal end, a lumen extending between the proximal end and the distal end, and a distal lumen opening, wherein the catheter body has a truncated length sufficient to access a peripheral vein of a patient; and a plurality of holes (508, 510) positioned on the distal end of the catheter body, wherein each of the plurality of holes is formed through a wall thickness of the catheter body and in communication with the lumen, wherein each of the plurality of holes has a generally tear-drop shape. a catheter body comprising a proximal end, a distal end, a lumen extending between the proximal end and the distal end, and a distal lumen opening, wherein the catheter body has a truncated length sufficient to access a peripheral vein of a patient; and a plurality of holes (508, 510) positioned on the distal end of the catheter body, wherein each of the plurality of holes is formed through a wall thickness of the catheter body and in communication with the lumen, wherein each of the plurality of holes has a generally tear-drop shape.
A propulsion bay intended to be transported, at least temporarily, in a space launcher, including: - an adapter (3, 4, 5) for cooperation with at least one on-board system (6, 7, 8), temporarily, on the bay, the adapter including a carrier structure including an inner space for receiving a first on-board system in the inner space, the carrier structure including an end for cooperation with a second on-board system, the first system and the second system forming artificial satellites, the adapter being adapted for cooperation with a third on-board system forming an additional system of liquid or solid space propulsion, the first system, the second system and the third system including a power supply, characterized in that the propulsion bay includes: - at least one electric motor for space propulsion configured to be powered by the power supply of the first or second or third system (6, 7, 8). - an adapter (3, 4, 5) for cooperation with at least one on-board system (6, 7, 8), temporarily, on the bay, the adapter including a carrier structure including an inner space for receiving a first on-board system in the inner space, the carrier structure including an end for cooperation with a second on-board system, the first system and the second system forming artificial satellites, the adapter being adapted for cooperation with a third on-board system forming an additional system of liquid or solid space propulsion, the first system, the second system and the third system including a power supply, characterized in that the propulsion bay includes: - at least one electric motor for space propulsion configured to be powered by the power supply of the first or second or third system (6, 7, 8).
An accessory for a subsea pipeline, the accessory comprising: a rigid pipe support frame defining a pipe course; and at least one carriage arranged to support a pipe or a fitting attached to a pipe, the carriage being movable with respect to the frame in a direction generally parallel to the pipe course; characterised in that at least one angularly movable connection acting between the pipe or fitting and the frame allows a pipe or fitting supported by the carriage to tilt locally with respect to the frame as the pipe bends during laying. a rigid pipe support frame defining a pipe course; and at least one carriage arranged to support a pipe or a fitting attached to a pipe, the carriage being movable with respect to the frame in a direction generally parallel to the pipe course;
A gas turbine engine component (18, 20) comprising: an airfoil having a pressure side and a suction side; and a sacrificial squealer tip located at one end of the airfoil to engage with an adjacent surface and thereby form a seal, the squealer tip terminating in a squealer tip apex; characterised in that the squealer tip apex follows a continuously curved circular or elliptical cross-sectional profile from the pressure side to the suction side of the airfoil, in a plane extending from the pressure side to the suction side of the airfoil. an airfoil having a pressure side and a suction side; and a sacrificial squealer tip located at one end of the airfoil to engage with an adjacent surface and thereby form a seal, the squealer tip terminating in a squealer tip apex; characterised in that the squealer tip apex follows a continuously curved circular or elliptical cross-sectional profile from the pressure side to the suction side of the airfoil, in a plane extending from the pressure side to the suction side of the airfoil.
A method for transmitting a pilot signal, comprising: determining, by a transmit end device based on prestored N pilot patterns, a target pilot pattern corresponding to a total quantity of transport layers to transmit data, so as to determine a target time-frequency resource for transmitting a pilot signal based on the target pilot pattern, wherein the target pilot pattern corresponds to an index number, the N pilot patterns are different from each other, N is determined based on a maximum transport layer quantity L and a code length C of an orthogonal cover code, OCC, used between transport layers, N= ┌ L/ C ┐, wherein ┌ ┐ represents roundup, a value of C is 2 n, and n is a natural number greater than or equal to 1; and sending, by the transmit end device, indication information to a receive end device, wherein the indication information is used to indicate the index number of the target pilot pattern, for instructing the receive end device to receive the pilot signal from the transmit end device based on the target time-frequency resource. determining, by a transmit end device based on prestored N pilot patterns, a target pilot pattern corresponding to a total quantity of transport layers to transmit data, so as to determine a target time-frequency resource for transmitting a pilot signal based on the target pilot pattern, wherein the target pilot pattern corresponds to an index number, the N pilot patterns are different from each other, N is determined based on a maximum transport layer quantity L and a code length C of an orthogonal cover code, OCC, used between transport layers, N= ┌ L/ C ┐, wherein ┌ ┐ represents roundup, a value of C is 2 n, and n is a natural number greater than or equal to 1; and sending, by the transmit end device, indication information to a receive end device, wherein the indication information is used to indicate the index number of the target pilot pattern, for instructing the receive end device to receive the pilot signal from the transmit end device based on the target time-frequency resource.
Method for constructing a trafficway tunnel, a conduit shaft or a pressurized-water shaft in tubbing construction mode, wherein tubbing components are assembled in a machine-generated bore in the rock, to form a continuous lining in the form of a tubbing tube, and the annular gap between the bore and the outer wall of the tubbing tube is filled by a polymerization-curing reactive resin and filler, characterized in that the filler is a cement-containing composition and in that the filler, before or while it is conveyed into the annular gap, is supplied with the polymerization-curing reactive resin, which is mixed with the filler and is dispersed therein. tubbing components are assembled in a machine-generated bore in the rock, to form a continuous lining in the form of a tubbing tube, and the annular gap between the bore and the outer wall of the tubbing tube is filled by a polymerization-curing reactive resin and filler, characterized in that the filler is a cement-containing composition and in that the filler, before or while it is conveyed into the annular gap, is supplied with the polymerization-curing reactive resin, which is mixed with the filler and is dispersed therein.