mhurhangee/patent-ind-claim-en huggingface dataset:
Reactive adhesive composition comprising • a polymer obtainable by free-radical polymerization of at least one monomer, namely one or more (meth)acrylate monomers and optionally additionally vinylic comonomers, - where the polymer has a molar mass Mw (GPC) of at least 5000 g/mol and at most 200 000 g/mol - and at least one of the monomers has been functionalized with at least one epoxy group, • and at least one initiator for a curing reaction involving the polymer, characterized in that the proportion of the epoxy-functionalized monomer(s) (a) is more than 30% by weight, based on the entirety of the parent monomers of the epoxy-functionalized (co)polymer. • a polymer obtainable by free-radical polymerization of at least one monomer, namely one or more (meth)acrylate monomers and optionally additionally vinylic comonomers, - where the polymer has a molar mass Mw (GPC) of at least 5000 g/mol and at most 200 000 g/mol - and at least one of the monomers has been functionalized with at least one epoxy group, - where the polymer has a molar mass Mw (GPC) of at least 5000 g/mol and at most 200 000 g/mol - and at least one of the monomers has been functionalized with at least one epoxy group, • and at least one initiator for a curing reaction involving the polymer,
Gas pressure spring , having a first hollow chamber which has a first axial end section and a second axial end section , the first hollow chamber having an opening on the second axial end section ; having an axially displaceable, first piston rod which extends through the opening ; having a second hollow chamber which is arranged in or outside the first hollow chamber ; having a first piston which is connected to the first piston rod on an axial end section of the first piston rod , which axial end section is arranged in the first hollow chamber or the second hollow chamber , and which first piston is arranged movably in the first hollow chamber or the second hollow chamber ; having a second piston which is arranged movably between the first axial end section and the first piston in the first hollow chamber or the second hollow chamber ; and having means for fixing and releasing the second piston in order to adjust a stroke of the first piston rod , characterized in that the first piston and the second piston are arranged in the first chamber volume (V1), the first piston rod being of substantially hollow configuration, a second piston rod which is of substantially hollow configuration being arranged at least in sections in a cavity of the first piston rod , the second piston being connected to an axial end section of the second piston rod , which axial end section faces the first axial end section of the first hollow chamber .
A method for ensuring parallel data random access, comprising: transmitting, by a user equipment, a random access sequence through a physical random access channel, PRACH, with other uplink transmission in a same subframe of different carriers, wherein the other uplink transmission comprises physical uplink control channel, PUCCH, and a physical uplink shared channel, PUSCH, and wherein when power is limited, a priority of transmission power of the PRACH and a priority of transmission power of an uplink channel over which the other uplink transmission is performed are controlled by the user equipment, wherein a priority of transmission power of the PRACH and a priority of transmission power of an uplink channel over which the other uplink transmission is performed are controlled by the user equipment as follows: a priority of transmission power of a PUSCH that does not include uplink control information, UCI, is controlled to be lower than a priority of transmission power of a PUSCH that includes UCI, the priority of transmission power of the PUSCH that includes the UCI is controlled to be lower than a priority of transmission power of the PUCCH, and the priority of transmission power of the PUCCH is controlled to be lower than a priority of transmission power of the PRACH. transmitting, by a user equipment, a random access sequence through a physical random access channel, PRACH, with other uplink transmission in a same subframe of different carriers, wherein the other uplink transmission comprises physical uplink control channel, PUCCH, and a physical uplink shared channel, PUSCH, and wherein when power is limited, a priority of transmission power of the PRACH and a priority of transmission power of an uplink channel over which the other uplink transmission is performed are controlled by the user equipment, wherein a priority of transmission power of the PRACH and a priority of transmission power of an uplink channel over which the other uplink transmission is performed are controlled by the user equipment as follows: a priority of transmission power of a PUSCH that does not include uplink control information, UCI, is controlled to be lower than a priority of transmission power of a PUSCH that includes UCI, the priority of transmission power of the PUSCH that includes the UCI is controlled to be lower than a priority of transmission power of the PUCCH, and the priority of transmission power of the PUCCH is controlled to be lower than a priority of transmission power of the PRACH.
A vehicle body front structure for an electric vehicle, comprising a battery pack mounted beneath a vehicle body floor , a bracket having a rear part and a front part thereof, the rear part being fixed to the battery pack and the front part being fixed to the vehicle body floor , and a vehicle body frame disposed in a fore-and-aft direction in front of the vehicle body floor , wherein a rear end part of the vehicle body frame is inclined downward from an upper front to a rear, the bracket is inclined downward from the upper front to the rear, and when viewed in the fore-and-aft direction, at least part of the bracket overlaps the rear end part of the vehicle body frame .
A method for performing a random access procedure by a mobile terminal in a wireless communication system, the method comprising: transmitting (S710) a preamble for random access in uplink; receiving (S720) a Medium Access Control, MAC, random access response, RAR, message including only one MAC sub-header that includes a back-off parameter; and performing back-off according to the back-off parameter, wherein the MAC RAR message does not include any MAC RAR payload. transmitting (S710) a preamble for random access in uplink; receiving (S720) a Medium Access Control, MAC, random access response, RAR, message including only one MAC sub-header that includes a back-off parameter; and performing back-off according to the back-off parameter, wherein the MAC RAR message does not include any MAC RAR payload.
A tubular connecting system , comprising: a tong configured to apply a torque on an upper tubular , to torque a connection of the upper tubular to a lower tubular ; a torque linkage extending at least partially vertically from the tong, the torque linkage being configured to transmit a force or force-pair, or pure torque, generated by the tong applying the torque to the upper tubular; characterized in that the tubular connecting system further comprises: a transmission plate removably coupled to the torque linkage so as to transmit linear forces thereto, therefrom, or both, wherein the transmission plate is configured to receive the lower tubular therethrough; and a landing plate removably coupled to the transmission plate and configured to engage the lower tubular, wherein the landing plate is configured to counteract the torque as it is applied to the lower tubular by the tong. a tong configured to apply a torque on an upper tubular , to torque a connection of the upper tubular to a lower tubular ; a torque linkage extending at least partially vertically from the tong, the torque linkage being configured to transmit a force or force-pair, or pure torque, generated by the tong applying the torque to the upper tubular; characterized in that the tubular connecting system further comprises: a transmission plate removably coupled to the torque linkage so as to transmit linear forces thereto, therefrom, or both, wherein the transmission plate is configured to receive the lower tubular therethrough; and a landing plate removably coupled to the transmission plate and configured to engage the lower tubular, wherein the landing plate is configured to counteract the torque as it is applied to the lower tubular by the tong. a transmission plate removably coupled to the torque linkage so as to transmit linear forces thereto, therefrom, or both, wherein the transmission plate is configured to receive the lower tubular therethrough; and a landing plate removably coupled to the transmission plate and configured to engage the lower tubular, wherein the landing plate is configured to counteract the torque as it is applied to the lower tubular by the tong.
An optical system for imaging an object onto an image plane (IP) of a microscope , comprising in total four lens groups (L1, L2, L3, L4), wherein: a first lens group (L1) having negative power, a second lens group (L2) having positive power, a third lens group (L3) having positive power and a fourth lens group (L4) having negative power are arranged in this order from an object side, the first lens group (L1) and the fourth lens group (L4) are stationary, and the second lens group (L2) and the third lens group (L3) are independently movable along an optical axis (O) of the optical system for focusing the object onto the image plane (IP) while zooming between a short focal length extremity and a long focal length extremity. a first lens group (L1) having negative power, a second lens group (L2) having positive power, a third lens group (L3) having positive power and a fourth lens group (L4) having negative power are arranged in this order from an object side, the first lens group (L1) and the fourth lens group (L4) are stationary, and the second lens group (L2) and the third lens group (L3) are independently movable along an optical axis (O) of the optical system for focusing the object onto the image plane (IP) while zooming between a short focal length extremity and a long focal length extremity.
A motor vehicle , preferably a commercial vehicle, particularly preferably a truck, comprising a vehicle frame ; a driver's cab ; a working platform , which is arranged at the rear of the cab above the vehicle frame ; and a tank , preferably a reducing agent tank, which is arranged between the working platform and the vehicle frame , characterized in that the tank is elastically supported or rests on the vehicle frame , and that the tank comprises at least one recess, preferably a through hole or a dome section, through which the working platform is supported on the vehicle frame . a vehicle frame ; a driver's cab ; a working platform , which is arranged at the rear of the cab above the vehicle frame ; and a tank , preferably a reducing agent tank, which is arranged between the working platform and the vehicle frame , that the tank is elastically supported or rests on the vehicle frame , and that the tank comprises at least one recess, preferably a through hole or a dome section, through which the working platform is supported on the vehicle frame .
An apparatus for distracting a hip joint having a femoral head and an acetabulum with an acetabular fossa, said apparatus comprising: an elongate flexible member having a proximal end, a distal end, and a shaft extending between the proximal end and the distal end, wherein the shaft is configured for moving from a straight configuration to a curved configuration; a balloon coupled to the elongate flexible member near the distal end, the balloon being fluidly expandable from a collapsed configuration to an expanded configuration, the balloon being configured to engage the acetabulum when the balloon is in the expanded configuration; characterized in that said apparatus comprises an actuation mechanism for moving the elongate flexible member between its straight configuration and its curved configuration; wherein the actuation mechanism is coupled to the distal end of the elongate flexible member so that when the actuation mechanism is activated, the actuation mechanism bends the distal end of the elongate flexible member, and the balloon coupled to the elongate flexible member, into a toroidal shape, with the distal end of the elongate flexible member being releasably coupled to a portion of the shaft of the elongate flexible member proximal to the balloon when in the toroidal shape. an elongate flexible member having a proximal end, a distal end, and a shaft extending between the proximal end and the distal end, wherein the shaft is configured for moving from a straight configuration to a curved configuration; a balloon coupled to the elongate flexible member near the distal end, the balloon being fluidly expandable from a collapsed configuration to an expanded configuration, the balloon being configured to engage the acetabulum when the balloon is in the expanded configuration; characterized in that said apparatus comprises an actuation mechanism for moving the elongate flexible member between its straight configuration and its curved configuration; wherein the actuation mechanism is coupled to the distal end of the elongate flexible member so that when the actuation mechanism is activated, the actuation mechanism bends the distal end of the elongate flexible member, and the balloon coupled to the elongate flexible member, into a toroidal shape, with the distal end of the elongate flexible member being releasably coupled to a portion of the shaft of the elongate flexible member proximal to the balloon when in the toroidal shape.
A method for determining a lateral and vertical path for aircraft guidance from a current aircraft position to a landing runway following a complete loss of engine thrust, the method comprising the steps of: determining, in a processing system , a final approach segment , the final approach segment being a path that the aircraft will traverse to maintain aircraft speed at a controlled landing speed until the aircraft touches down on the landing runway; determining, in the processing system, a deceleration segment , the deceleration segment being a path that the aircraft will traverse, just prior to entering the final approach segment, to reduce the aircraft speed to the controlled landing speed; determining, in the processing system, a driftdown segment , the driftdown segment being a path that the aircraft will traverse, upon the complete loss of engine thrust and just prior to entering the deceleration segment, to reduce aircraft potential energy to a predetermined magnitude; connecting, in the processing system, the driftdown segment to the deceleration segment, and the deceleration segment to the final approach segment, to form a complete lateral and vertical path from the current aircraft position to the landing runway; and rendering, on a display device , a graphical representation of the complete lateral and vertical path from the current aircraft position to the landing runway, wherein the graphical representation of the complete lateral and vertical path updates as the aircraft travels. determining, in a processing system , a final approach segment , the final approach segment being a path that the aircraft will traverse to maintain aircraft speed at a controlled landing speed until the aircraft touches down on the landing runway; determining, in the processing system, a deceleration segment , the deceleration segment being a path that the aircraft will traverse, just prior to entering the final approach segment, to reduce the aircraft speed to the controlled landing speed; determining, in the processing system, a driftdown segment , the driftdown segment being a path that the aircraft will traverse, upon the complete loss of engine thrust and just prior to entering the deceleration segment, to reduce aircraft potential energy to a predetermined magnitude; connecting, in the processing system, the driftdown segment to the deceleration segment, and the deceleration segment to the final approach segment, to form a complete lateral and vertical path from the current aircraft position to the landing runway; and rendering, on a display device , a graphical representation of the complete lateral and vertical path from the current aircraft position to the landing runway, wherein the graphical representation of the complete lateral and vertical path updates as the aircraft travels.
An arrangement for mechanical and electrical contacting of an incandescent wire of a thermal radiation source, comprising an incandescent wire made of refractory metal having at least one flat connection surface to be contacted, a contact surface on which the incandescent wire is contacted and a contacting medium which joins the incandescent wire to the contact surface , characterized in that the flat connection surface of the incandescent wire has at least two perforations and/or a circumferential edge of the connection surface of the incandescent wire has at least two cutouts , wherein the contacting medium is joined to the contact surface with an atomic-level join at the site of the perforations and/or cutouts and through a flange-like configuration of the contacting medium above the connection surface of the incandescent wire at the site of the perforations and/or cutouts forms both an electrical and a mechanical connection with the incandescent wire.
A method of stabilising a biological sample comprising glutathione (GSH) and glutathione disulfide (GSSG), the method comprising the following steps: a) contacting GSH and GSSG of the provided biological sample with a maleimide under conditions which allow alkylation of the sulfhydryl group of GSH with the maleimide to obtain maleimide-alkylated GSH, b) separating excess maleimide from maleimide-alkylated GSH and GSSG, c) contacting maleimide-alkylated GSH and GSSG with a reducing agent, selected from the group consisting of phosphine-based reducing agents such as tris(2-carboxyethyl)phosphine (TCEP) or tributylphosphine, and thiol-based reducing agents such as dithiothreitol (DTT), dithioerythritol (DTE) or β-mercaptoethanol, under conditions which allow reduction of GSSG by the reducing agent to obtain further GSH, and d) contacting maleimide-alkylated GSH and GSH with a heavy isotopologue of the maleimide under conditions which allow alkylation of the sulfhydryl group of GSH with the heavy isotopologue of the maleimide to obtain a heavy isotopologue of the maleimide-alkylated GSH; whereby a stabilised biological sample, comprising the maleimide-alkylated GSH and the heavy isotopologue thereof, is obtained. a) contacting GSH and GSSG of the provided biological sample with a maleimide under conditions which allow alkylation of the sulfhydryl group of GSH with the maleimide to obtain maleimide-alkylated GSH, b) separating excess maleimide from maleimide-alkylated GSH and GSSG, c) contacting maleimide-alkylated GSH and GSSG with a reducing agent, selected from the group consisting of phosphine-based reducing agents such as tris(2-carboxyethyl)phosphine (TCEP) or tributylphosphine, and thiol-based reducing agents such as dithiothreitol (DTT), dithioerythritol (DTE) or β-mercaptoethanol, under conditions which allow reduction of GSSG by the reducing agent to obtain further GSH, and d) contacting maleimide-alkylated GSH and GSH with a heavy isotopologue of the maleimide under conditions which allow alkylation of the sulfhydryl group of GSH with the heavy isotopologue of the maleimide to obtain a heavy isotopologue of the maleimide-alkylated GSH;
A tightness testing system for a cable gland feed-through of a partition, in particular of an immersible electrical connector, of the type comprising a cable gland body in which sealing means are placed and a cable gland rammer for compressing the sealing means characterized in that it comprises a sealing testing ring inserted in the sealing means and provided with a hole opposite a hole in the gland body opening onto the latter and provided with means for connection to a pressure/vacuum source making it possible to test the sealing of the gland.
A method for robotic machining, comprising: determining a first designed machining path based on a modeled surface for a target surface to be machined; causing a robot to machine the target surface based on the first designed machining path in an adaptive manner to obtain an actual machining path, wherein where the modeled surface is different from the target surface, the robot is caused to follow the target surface; and determining a second designed machining path for the target surface based on the deviation between the actual machining path and the first designed machining path, so as to generate an optimized machining path, wherein the robot is run with controlled force, and causing the robot to machine comprises: causing the robot to apply a controlled force to the target surface via a machining tool; and causing the robot to move with a constant speed. determining a first designed machining path based on a modeled surface for a target surface to be machined; causing a robot to machine the target surface based on the first designed machining path in an adaptive manner to obtain an actual machining path, wherein where the modeled surface is different from the target surface, the robot is caused to follow the target surface; and determining a second designed machining path for the target surface based on the deviation between the actual machining path and the first designed machining path, so as to generate an optimized machining path, wherein the robot is run with controlled force, and causing the robot to machine comprises: causing the robot to apply a controlled force to the target surface via a machining tool; and causing the robot to move with a constant speed. causing the robot to apply a controlled force to the target surface via a machining tool; and causing the robot to move with a constant speed.
An intermediate transfer medium which comprises a substrate, a protective layer and a receiving layer which are layered on a surface of the substrate; wherein the protective layer comprises a binder resin having a number average molecular weight (Mn) of not less than 8,000 and not more than 30,000 and a filler which has a particle diameter of not less than 1 nm and not more than 200 nm, wherein the filler is included in an amount of not less than 5 % by weight and not more than 40 % by weight on a base of total solid content of the protective layer.
A rotating assembly (26-28) for a turbine assembly comprising: an airfoil extending radially outward from, and rotatable about, an axial centerline ; a tip shroud integrally connected proximate a radially outer tip of the airfoil ; a substrate operably coupled to the tip shroud ; and at least one hard face interface member secured to the substrate and configured for interaction with a tip shroud of an adjacent airfoil, wherein the at least one hard face interface member includes a base portion and a plurality of edge portions , wherein a portion of the substrate fully encapsulates the edge portions of the at least one hard face interface member . an airfoil extending radially outward from, and rotatable about, an axial centerline ; a tip shroud integrally connected proximate a radially outer tip of the airfoil ; a substrate operably coupled to the tip shroud ; and at least one hard face interface member secured to the substrate and configured for interaction with a tip shroud of an adjacent airfoil, wherein the at least one hard face interface member includes a base portion and a plurality of edge portions , wherein a portion of the substrate fully encapsulates the edge portions of the at least one hard face interface member .