mhurhangee/patent-ind-claim-en huggingface dataset:
An apparatus of a user equipment UE, the apparatus comprising one or more processors and memory configured to: identify configuration information received via a higher layer for a plurality of receive, Rx, beams for the UE from a cellular base station, the configuration information including a plurality of Rx beam indices for the plurality of Rx beams; identify a physical-layer communication received from the cellular base station indicating a selected Rx beam index; identify a selected Rx beam from the plurality of Rx beams using the selected Rx beam index; and signal transceiver circuitry at the UE to receive a downlink, DL, transmission using the selected Rx beam, wherein the DL transmission is received in a physical downlink shared channel, PDSCH, wherein the selected Rx beam index is indicated in a received enhanced physical downlink control channel, ePDCCH. identify configuration information received via a higher layer for a plurality of receive, Rx, beams for the UE from a cellular base station, the configuration information including a plurality of Rx beam indices for the plurality of Rx beams; identify a physical-layer communication received from the cellular base station indicating a selected Rx beam index; identify a selected Rx beam from the plurality of Rx beams using the selected Rx beam index; and signal transceiver circuitry at the UE to receive a downlink, DL, transmission using the selected Rx beam, wherein the DL transmission is received in a physical downlink shared channel, PDSCH, wherein the selected Rx beam index is indicated in a received enhanced physical downlink control channel, ePDCCH.
Hydraulic mount having - a supporting spring , - a working chamber which is at least partially encompassed by the supporting spring and which is filled with a hydraulic liquid, - a compensation chamber , and - a throttle channel which is formed between the working chamber and the compensation chamber and which serves for the exchange of hydraulic liquid, - an intermediate chamber , - a first, movable control unit which is arranged between the working chamber and the intermediate chamber and which separates said two chambers from one another, and - a second movable control unit which forms a wall portion of the intermediate chamber , characterized in that the second control unit has at least one control diaphragm , wherein at least one control diaphragm of the first control unit and at least one control diaphragm of the second control unit are formed by one common diaphragm. - a supporting spring , - a working chamber which is at least partially encompassed by the supporting spring and which is filled with a hydraulic liquid, - a compensation chamber , and - a throttle channel which is formed between the working chamber and the compensation chamber and which serves for the exchange of hydraulic liquid, - an intermediate chamber , - a first, movable control unit which is arranged between the working chamber and the intermediate chamber and which separates said two chambers from one another, and - a second movable control unit which forms a wall portion of the intermediate chamber ,
An ophthalmic surgical system for treating eye tissue during a cataract surgical procedure, comprising: a light source (10, LS) for generating a beam of light; an imaging device configured to be used to determine a size and a location of the lens of the eye tissue, the imaging device being an Optical Coherence Tomography (OCT) device; a delivery system (16, L1, G1, G2) for focusing the beam onto the eye tissue in the lens; and a controller (12, CPU) operatively coupled to the light source, the imaging device and the delivery system, and configured to: determine parameters of a cutting pattern based on the size and the location of the lens; and control the light source and the delivery system such that the light beam is focused at multiple focal points in the eye tissue and at multiple depths within the eye tissue and to scan the light beam in the cutting pattern at the eye tissue at the determined location in the lens, so as to cut the eye tissue. a light source (10, LS) for generating a beam of light; an imaging device configured to be used to determine a size and a location of the lens of the eye tissue, the imaging device being an Optical Coherence Tomography (OCT) device; a delivery system (16, L1, G1, G2) for focusing the beam onto the eye tissue in the lens; and a controller (12, CPU) operatively coupled to the light source, the imaging device and the delivery system, and configured to: determine parameters of a cutting pattern based on the size and the location of the lens; and control the light source and the delivery system such that the light beam is focused at multiple focal points in the eye tissue and at multiple depths within the eye tissue and to scan the light beam in the cutting pattern at the eye tissue at the determined location in the lens, so as to cut the eye tissue. determine parameters of a cutting pattern based on the size and the location of the lens; and control the light source and the delivery system such that the light beam is focused at multiple focal points in the eye tissue and at multiple depths within the eye tissue and to scan the light beam in the cutting pattern at the eye tissue at the determined location in the lens, so as to cut the eye tissue.
A process for urea production, comprising: a synthesis step of synthesizing urea from ammonia and carbon dioxide to generate a urea synthesis solution; a decomposition step of, by heating the urea synthesis solution generated in the synthesis step, decomposing ammonium carbamate and separating a gaseous mixture containing ammonia and carbon dioxide from the urea synthesis solution to obtain a urea synthesis solution which is higher in urea concentration than the urea synthesis solution obtained in the synthesis step; a condensation step of, with use of a submerged condenser including a shell and tube heat exchange structure including a U-tube, absorbing and condensing at least a part of the gaseous mixture obtained in the decomposition step in an absorption medium on a shell side, and generating steam on a tube side with use of heat generated during the condensation; a recycling step of recycling at least a part of a liquid, said liquid being obtained from the shell side in the condensation step, to the synthesis step; and a water supply step of supplying water to the tube side of the submerged condenser at a mass flow rate that is three times or more of a generation rate of the steam generated in the submerged condenser. a synthesis step of synthesizing urea from ammonia and carbon dioxide to generate a urea synthesis solution; a decomposition step of, by heating the urea synthesis solution generated in the synthesis step, decomposing ammonium carbamate and separating a gaseous mixture containing ammonia and carbon dioxide from the urea synthesis solution to obtain a urea synthesis solution which is higher in urea concentration than the urea synthesis solution obtained in the synthesis step; a condensation step of, with use of a submerged condenser including a shell and tube heat exchange structure including a U-tube, absorbing and condensing at least a part of the gaseous mixture obtained in the decomposition step in an absorption medium on a shell side, and generating steam on a tube side with use of heat generated during the condensation; a recycling step of recycling at least a part of a liquid, said liquid being obtained from the shell side in the condensation step, to the synthesis step; and a water supply step of supplying water to the tube side of the submerged condenser at a mass flow rate that is three times or more of a generation rate of the steam generated in the submerged condenser.
A method for transmitting a configuration file in a Passive Optical Network, comprising: sending, at the OLT, a type of an optical network termination, ONT, and an identifier, ID, of a user to an Element Management System, EMS; receiving, at the OLT, a configuration file in a format of extensible Markup Language, XML, or text file, TXT, sent by the EMS, the configuration file is determined by the EMS in accordance with the type of the ONT and the ID of the user; sending, at the OLT, the configuration file through an ONU Management Control Interface, OMCI file loading channel to the ONT. sending, at the OLT, a type of an optical network termination, ONT, and an identifier, ID, of a user to an Element Management System, EMS; receiving, at the OLT, a configuration file in a format of extensible Markup Language, XML, or text file, TXT, sent by the EMS, the configuration file is determined by the EMS in accordance with the type of the ONT and the ID of the user; sending, at the OLT, the configuration file through an ONU Management Control Interface, OMCI file loading channel to the ONT.
An amorphous polymer (P) comprising segments (S1) of formula segments (S2) of formula and segments (S3) of formula wherein the amorphous polymer (P) comprises 80.1 to 89% by mol of segments (S1) and 11 to 19.9% by mol of segments (S2), based on the total number of mols of segments (S1) and segments (S2) comprised in the amorphous polymer (P). segments (S1) of formula segments (S2) of formula and segments (S3) of formula wherein the amorphous polymer (P) comprises 80.1 to 89% by mol of segments (S1) and 11 to 19.9% by mol of segments (S2), based on the total number of mols of segments (S1) and segments (S2) comprised in the amorphous polymer (P). 80.1 to 89% by mol of segments (S1) and 11 to 19.9% by mol of segments (S2), based on the total number of mols of segments (S1) and segments (S2) comprised in the amorphous polymer (P).
A multiple layer polymer interlayer comprising: a first layer comprising poly(vinyl butyral) resin and a first plasticizer; a second layer comprising poly(vinyl butyral) resin and a second plasticizer; and a third layer comprising poly(vinyl butyral) resin and a third plasticizer disposed between the first layer and the second layer; and wherein at least one of the first, second and third plasticizers is a high refractive index plasticizer having a refractive index of at least 1.460; wherein at least one layer is a soft layer and at least one layer is a stiff layer, wherein the soft layer comprises a poly(vinyl butyral) resin having a residual hydroxyl content from 8 to 21 wt.%, wherein the stiff layer comprises a poly(vinyl butyral) resin having a residual hydroxyl content from 16 to 35 wt.%, wherein the glass transition temperature of the soft layer is at least 2°C lower than that of the stiff layer, and the residual hydroxyl content between the adjacent soft and stiff layers differs by at least 2 wt.%, and wherein the difference between the refractive index of the soft layer and the stiff layer (Delta RI) is less than 0.010; the refractive index, the hydroxyl content and the glass transition temperature being measured according to the methods in the description. a first layer comprising poly(vinyl butyral) resin and a first plasticizer; a second layer comprising poly(vinyl butyral) resin and a second plasticizer; and a third layer comprising poly(vinyl butyral) resin and a third plasticizer disposed between the first layer and the second layer; and wherein at least one of the first, second and third plasticizers is a high refractive index plasticizer having a refractive index of at least 1.460; wherein at least one layer is a soft layer and at least one layer is a stiff layer, wherein the soft layer comprises a poly(vinyl butyral) resin having a residual hydroxyl content from 8 to 21 wt.%, wherein the stiff layer comprises a poly(vinyl butyral) resin having a residual hydroxyl content from 16 to 35 wt.%, wherein the glass transition temperature of the soft layer is at least 2°C lower than that of the stiff layer, and the residual hydroxyl content between the adjacent soft and stiff layers differs by at least 2 wt.%, and wherein the difference between the refractive index of the soft layer and the stiff layer (Delta RI) is less than 0.010; the refractive index, the hydroxyl content and the glass transition temperature being measured according to the methods in the description.
A liquid blow molding method for molding a bottomed tubular-shaped preform into a liquid-containing container in which a content liquid (L) is held, the liquid blow molding method comprising: a first supply step of supplying, through a first supply path , a first liquid (L1) at a predetermined pressure into the preform that has been heated to a predetermined temperature to liquid blow mold the preform ; and a second supply step of supplying, through a second supply path that is different from the first supply path , a second liquid (L2) into the preform after or simultaneously with the supply of the first liquid (L1), characterized by that the method further comprises a suck-back step, performed after the preform is liquid blow molded into the container having a predetermined shape in the first supply step, of sucking out a predetermined amount of the first liquid (L1) from the container that has been molded in the predetermined shape in the first supply step, wherein in the second supply step, the second liquid (L2) is supplied into the container from which the predetermined amount of the first liquid (L1) has been sucked out in the suck-back step. a first supply step of supplying, through a first supply path , a first liquid (L1) at a predetermined pressure into the preform that has been heated to a predetermined temperature to liquid blow mold the preform ; and a second supply step of supplying, through a second supply path that is different from the first supply path , a second liquid (L2) into the preform after or simultaneously with the supply of the first liquid (L1), a suck-back step, performed after the preform is liquid blow molded into the container having a predetermined shape in the first supply step, of sucking out a predetermined amount of the first liquid (L1) from the container that has been molded in the predetermined shape in the first supply step, wherein in the second supply step, the second liquid (L2) is supplied into the container from which the predetermined amount of the first liquid (L1) has been sucked out in the suck-back step.
Device for nuclear magnetic resonance therapy, comprising a device for generating an alternating magnetic field, a device for generating a magnetic field running transversely to the sweep field, as well as device for stretching a user, wherein a periodically alternating force can be generated during a treatment with magnetic resonances.
A formed film comprising: a first surface generally located in a first plane; a second surface generally located in a second plane parallel to and spaced from the first plane; a third surface generally located in a third plane parallel to and spaced from the first plane and the second plane, in between the first plane and the second plane; a porous structure extending between the second surface and the third surface; and a plurality of raised areas having sidewalls extending between the first surface and the third surface, and top portions defining the first surface, the plurality of sidewalls, the porous structure and the first plane defining a plurality of gathering volumes, wherein the plurality of raised areas comprise a plurality of micro-apertures, and wherein the porous structure comprises a fibrillated structure. a first surface generally located in a first plane; a second surface generally located in a second plane parallel to and spaced from the first plane; a third surface generally located in a third plane parallel to and spaced from the first plane and the second plane, in between the first plane and the second plane; a porous structure extending between the second surface and the third surface; and a plurality of raised areas having sidewalls extending between the first surface and the third surface, and top portions defining the first surface, the plurality of sidewalls, the porous structure and the first plane defining a plurality of gathering volumes, wherein the plurality of raised areas comprise a plurality of micro-apertures, and wherein the porous structure comprises a fibrillated structure.
Aircraft comprising an air intake , the air intake comprising: an air duct arranged inside the aircraft , an inlet in one end of the air duct , a flap door , and driving means, wherein: the air intake is suitable for providing airflow through the air duct to the inside of the aircraft , the flap door is hinged in at least a first end to the inlet , the driving means are configured for moving the flap door between at least two positions, wherein said positions are: a closed position wherein the flap door closes the inlet , and an opened position wherein the flap door forms an angle (α) with respect to the closed position of the flap door , wherein the angle (α) is different from 0, wherein the flap door comprises a barrier filter configured to filter an incoming airflow into the air duct , and the driving means are configured for moving the flap door from the closed position to an opened position by pivoting the flap door around the first end towards outside the aircraft and towards the rear part of the aircraft , characterized in that the flap door is double hinged in the first end and in a second end to the inlet , and wherein the driving means are configured for moving the flap door from the closed position to a fallback position by pivoting the flap door around the second end towards inside the air duct and towards the front part of the aircraft . an air duct arranged inside the aircraft , an inlet in one end of the air duct , a flap door , and driving means, the air intake is suitable for providing airflow through the air duct to the inside of the aircraft , the flap door is hinged in at least a first end to the inlet , the driving means are configured for moving the flap door between at least two positions, wherein said positions are: a closed position wherein the flap door closes the inlet , and an opened position wherein the flap door forms an angle (α) with respect to the closed position of the flap door , wherein the angle (α) is different from 0, wherein the flap door comprises a barrier filter configured to filter an incoming airflow into the air duct , and the driving means are configured for moving the flap door from the closed position to an opened position by pivoting the flap door around the first end towards outside the aircraft and towards the rear part of the aircraft , a closed position wherein the flap door closes the inlet , and an opened position wherein the flap door forms an angle (α) with respect to the closed position of the flap door , wherein the angle (α) is different from 0, wherein the flap door comprises a barrier filter configured to filter an incoming airflow into the air duct , and the driving means are configured for moving the flap door from the closed position to an opened position by pivoting the flap door around the first end towards outside the aircraft and towards the rear part of the aircraft ,
A component for a gas turbine engine comprising: at least one airfoil (90; 90') having a radially inner end and a radially outer end; a platform (92; 92') including a radially outer surface attached to the radially inner end of the airfoil (90; 90'), and a radially inner side of the platform (92; 92') that includes a forward surface (110; 110') and an aft surface (112; 112'); a pocket (114, 116; 114', 116') recessed into at least one of the forward surface (110; 110') and the aft surface (112; 112'); and a cover plate (118, 120; 118', 120') covering the pocket (114...116'), characterised in that the component further comprises: a first abradable seal (96, 98; 96', 98') attached to a radially inner surface (118B; 120B) of the cover plate (118...120'), wherein the cover plate (118....120') includes a radially outer surface in contact with the at least one of the forward surface (110;110') and the aft surface (112;112'). at least one airfoil (90; 90') having a radially inner end and a radially outer end; a platform (92; 92') including a radially outer surface attached to the radially inner end of the airfoil (90; 90'), and a radially inner side of the platform (92; 92') that includes a forward surface (110; 110') and an aft surface (112; 112'); a pocket (114, 116; 114', 116') recessed into at least one of the forward surface (110; 110') and the aft surface (112; 112'); and a cover plate (118, 120; 118', 120') covering the pocket (114...116'), characterised in that the component further comprises: a first abradable seal (96, 98; 96', 98') attached to a radially inner surface (118B; 120B) of the cover plate (118...120'), wherein the cover plate (118....120') includes a radially outer surface in contact with the at least one of the forward surface (110;110') and the aft surface (112;112').
Machine tool, in particular a semi-stationary or mobile machine tool and/or sawing machine, for machining workpieces (W) using a working tool , in particular a separating tool or a sawing tool, wherein the machine tool comprises a machine base for setting down on a ground surface and a drive assembly arranged thereon with a drive motor and a tool receptacle drivable by the drive motor for the working tool , in particular for a separating tool, wherein the machine base comprises a support surface for supporting the workpiece (W) and comprises at least one side contact body with a side contact surface , which is at an angle to the support surface , in particular perpendicular, and extends along a longitudinal axis (L), wherein the machine tool comprises at least one abutment body with an abutment surface , which can be fixed opposite the support surface by means of a holding device on the machine tool , so that the workpiece (W) for machining by the working tool , in particular for the production of a crown-moulding cut, is supported adjacent to the side contact surface between the support surface and the abutment surface , and the side contact surface of the at least one side contact body comprises a support section and a tool section , wherein the side contact surface protrudes further in front of the support surface in the region of the support section than in the region of the tool section , which is provided for making a larger clearance available for the working tool, characterised in that the abutment body can be releasably fixed on the machine base using the holding device , in at least two different longitudinal positions (L1, L2) with respect to the longitudinal axis (L).