mhurhangee/ep-ind-claims huggingface dataset:
Method for selecting a gear ratio of a gearbox in a drivetrain of a motor vehicle, comprising: receiving (30, 40, 50) a variable dependent on an accelerator pedal position; calculating (31, 41, 51) a drivetrain parameter for at least two gear ratios of the gearbox; ascertaining (32, 53), out of the at least two gear ratios of the gearbox, gear ratios that satisfy a predefined condition; calculating at least one further drivetrain parameter on the basis of the variable, which is dependent on an accelerator pedal position, for the gear ratios of the at least two gear ratios of the gearbox that satisfy the predefined condition; and selecting (33, 44, 54) a setpoint gear ratio on the basis of the calculated drivetrain parameter for the at least two gear ratios and on the basis of the calculated at least one further drivetrain parameter for the gear ratios of the at least two gear ratios of the gearbox that satisfy the predefined condition, taking into consideration the variable that is dependent on the accelerator pedal position. receiving (30, 40, 50) a variable dependent on an accelerator pedal position; calculating (31, 41, 51) a drivetrain parameter for at least two gear ratios of the gearbox; ascertaining (32, 53), out of the at least two gear ratios of the gearbox, gear ratios that satisfy a predefined condition; calculating at least one further drivetrain parameter on the basis of the variable, which is dependent on an accelerator pedal position, for the gear ratios of the at least two gear ratios of the gearbox that satisfy the predefined condition; and selecting (33, 44, 54) a setpoint gear ratio on the basis of the calculated drivetrain parameter for the at least two gear ratios and on the basis of the calculated at least one further drivetrain parameter for the gear ratios of the at least two gear ratios of the gearbox that satisfy the predefined condition, taking into consideration the variable that is dependent on the accelerator pedal position.
A polyaxial bone anchoring device comprising a bone anchoring element (1, 1', 1") having a head (3, 3', 3") and a shaft (2, 2', 2") for anchoring in the bone, a receiving part (4, 4', 4") for coupling the bone anchoring element (1, 1', 1") to a rod, the receiving part (4, 4', 4") comprising an accommodation space (8, 8', 8") for accommodating the head (3, 3', 3") and a coaxial bore (41, 41', 41") being in communication with the accommodation space (8, 8', 8"), the coaxial bore (41, 41', 41") having a bore axis, a pressure member (6, 6', 6") configured to move in the bore (41, 41', 41") and comprising a first surface for engaging the head (3, 3', 3") and a second surface on which the rod acts, wherein the pressure member (6, 6', 6") is configured to assume a first position in which it exerts a preload onto the head (3, 3', 3") that results from friction between the first surface and the head (3, 3', 3") to enable the shaft (2, 2', 2") to be maintained in a desired angular position before locking the head (3, 3', 3") in the receiving part (4, 4', 4"), and a second position in which the head (3, 3', 3") is locked with respect to the receiving part (4, 4', 4"), and wherein the first position is obtained by moving the pressure member (6, 6', 6") by the action of a predefined force acting onto the pressure member (6, 6', 6") in an axial direction and wherein the pressure member (6, 6', 6") is maintained in the first position by interaction with the receiving part (4, 4', 4") and can be released from the first position through action of an axial force, characterized in that the pressure member (6, 6', 6") is a single piece substantially cylindrical member and an outer diameter of the pressure member (6, 6', 6") is slightly larger than an inner diameter of the coaxial bore (41, 41', 41") to achieve an interference fit connection between an inner surface of the coaxial bore and the outer cylindrical surface (65, 65', 65b") of the pressure member, or between parts of the inner surface of the coaxial bore and of the outer cylindrical surface of the pressure member.
An association method for a synchronization block and a paging-scheduling signaling message, comprising: receiving, by a terminal, a multiplexing mode indication information, wherein the multiplexing mode indication information is used for indicating the multiplexing mode of the synchronization block and the paging-scheduling signaling message; performing, by the terminal, beam scanning on a received synchronization block to obtain a target synchronization block; and determining, by the terminal, a paging-scheduling signaling message corresponding to the target synchronization block according to a correspondence between the synchronization block and the paging-scheduling signaling message; wherein the correspondence between the synchronization block and the paging-scheduling signaling message is indicated by a correspondence indication information received from a base station, the correspondence indication information is determined in response to the multiplexing mode being determined as time division multiplexing. receiving, by a terminal, a multiplexing mode indication information, wherein the multiplexing mode indication information is used for indicating the multiplexing mode of the synchronization block and the paging-scheduling signaling message; performing, by the terminal, beam scanning on a received synchronization block to obtain a target synchronization block; and determining, by the terminal, a paging-scheduling signaling message corresponding to the target synchronization block according to a correspondence between the synchronization block and the paging-scheduling signaling message; wherein the correspondence between the synchronization block and the paging-scheduling signaling message is indicated by a correspondence indication information received from a base station, the correspondence indication information is determined in response to the multiplexing mode being determined as time division multiplexing.
A method for operating a flight control system of an aircraft, comprising: determining first and second values, wherein the first and second values comprise a first input force value from a first sensor associated with a pilot control column of the flight control system of the aircraft and a second input force value from a second sensor associated with a first officer control column of the flight control system of the aircraft; based on the values, determining a location of a jam in the flight control system of the aircraft, and wherein the location of the jam is determined based on a first summation of the first and second values. determining first and second values, wherein the first and second values comprise a first input force value from a first sensor associated with a pilot control column of the flight control system of the aircraft and a second input force value from a second sensor associated with a first officer control column of the flight control system of the aircraft; based on the values, determining a location of a jam in the flight control system of the aircraft, and wherein the location of the jam is determined based on a first summation of the first and second values.
Insufflation device, comprising an insufflator, at least one gas supply line and at least one insufflation cannula, which is connected to the insufflator for the purposes of insufflating an insufflation gas by way of the gas supply line, said insufflator having a housing with an inlet and at least one first outlet for the insufflation gas, to which the at least one gas supply line is connected, wherein there is a fluid path in the housing between the inlet and the first outlet, interposed on which there is a measurement, control and regulation device for release of the gas under control and regulation, said device being electronically connected to operating means, the insufflation device has a switchover device embodied to provide a switchover of the gas flow under control and regulation for the purposes of releasing gas either from the tissue dissection probe or from the at least one insufflation cannula, characterized in that - the insufflator, by way of a gas supply line, furthermore has an additional fluid connection to a pneumatic tissue dissection probe, the latter being connected electronically to the measurement, control and regulation device. - the insufflator, by way of a gas supply line, furthermore has an additional fluid connection to a pneumatic tissue dissection probe, the latter being connected electronically to the measurement, control and regulation device.
An inter-Node B handover method in a carrier aggregation scenario, the method comprising: sending a Handover Request Acknowledge message including handover reference frequency point information by a target evolved Node B (eNB) through a source eNB to a user equipment, wherein the handover reference frequency point information comprises center frequency point information of an uplink component carrier designated for the user equipment to initiate a random access request, and center frequency point information of a downlink component carrier for the target cell of the target eNB to send a random access response; and requesting a random access by the user equipment according to the center frequency point information of the uplink component carrier; wherein, the method further comprises: sending the Handover Request Acknowledge message by the target eNB either through an interface S1 or through an interface X2 before receiving the Handover Request Acknowledge message by the user equipment; and wherein, the processing of sending the Handover Request Acknowledge message by the target eNB through the interface S1 comprises: sending a transparent container of the Handover Request Acknowledge message by the target eNB through the interface S1 to a mobility management entity; and transparently transmitting the transparent container by the mobility management entity to the source eNB through a Handover Command message; the processing of sending the Handover Request Acknowledge message by the target eNB through the interface X2 comprises: sending the transparent container of the Handover Request Acknowledge message by the target eNB through the interface X2 to the source eNB. sending a Handover Request Acknowledge message including handover reference frequency point information by a target evolved Node B (eNB) through a source eNB to a user equipment, wherein the handover reference frequency point information comprises center frequency point information of an uplink component carrier designated for the user equipment to initiate a random access request, and center frequency point information of a downlink component carrier for the target cell of the target eNB to send a random access response; and requesting a random access by the user equipment according to the center frequency point information of the uplink component carrier; sending the Handover Request Acknowledge message by the target eNB either through an interface S1 or through an interface X2 before receiving the Handover Request Acknowledge message by the user equipment; and sending a transparent container of the Handover Request Acknowledge message by the target eNB through the interface S1 to a mobility management entity; and transparently transmitting the transparent container by the mobility management entity to the source eNB through a Handover Command message; sending the transparent container of the Handover Request Acknowledge message by the target eNB through the interface X2 to the source eNB.
A rotary connector (10, 30, 50), comprising: a case including a housing space and fixed to a vehicle body that includes a steering wheel including a steering-side electric component; a rotor (110, 210, 310) that is rotatable around a rotational axis relative to the case and includes a disc-shaped flat plate part that constitutes the rotor (110, 210, 310) and faces the housing space; a first connector (10D, 10E) provided on the rotor (110, 210, 310) and electrically connected to the steering-side electric component; a second connector provided on the case and electrically connected to a vehicle-side electric component in the vehicle body; a flexible cable that is provided in a wound state in the housing space of the case and electrically connects the first connector (10D, 10E) to the second connector; and a controller(120, 220, 320) that includes a circuit board (122A, 222A, 322A) that faces the housing space, and is disposed between the first connector (10D, 10E) and the flexible cable and performs a predetermined process on an electric signal transmitted between the first connector (10D, 10E) and the flexible cable, wherein the controller (120, 220, 320) is configured to rotate together with the rotor (110, 210, 310); and wherein the circuit board (122A, 222A, 322A) includes a circuit board extension part that protrudes outward in a radial direction from an outer periphery of the flat plate part in plan view seen in the direction of the rotational axis. a case including a housing space and fixed to a vehicle body that includes a steering wheel including a steering-side electric component; a rotor (110, 210, 310) that is rotatable around a rotational axis relative to the case and includes a disc-shaped flat plate part that constitutes the rotor (110, 210, 310) and faces the housing space; a first connector (10D, 10E) provided on the rotor (110, 210, 310) and electrically connected to the steering-side electric component; a second connector provided on the case and electrically connected to a vehicle-side electric component in the vehicle body; a flexible cable that is provided in a wound state in the housing space of the case and electrically connects the first connector (10D, 10E) to the second connector; and a controller(120, 220, 320) that includes a circuit board (122A, 222A, 322A) that faces the housing space, and is disposed between the first connector (10D, 10E) and the flexible cable and performs a predetermined process on an electric signal transmitted between the first connector (10D, 10E) and the flexible cable, wherein the controller (120, 220, 320) is configured to rotate together with the rotor (110, 210, 310); and wherein the circuit board (122A, 222A, 322A) includes a circuit board extension part that protrudes outward in a radial direction from an outer periphery of the flat plate part in plan view seen in the direction of the rotational axis.
A self-assembled microparticle comprising an acid of general formula HOOC-(CH 2) n -COOH wherein n is at least 5 and not more than 40 and an organic base in which the molar ratio of acid groups to basic groups in the acid and base is from 0.6 to 1.4:1, the microparticle being obtainable by a process comprising contacting the said acid and organic base in aqueous solution, wherein the acid is insoluble in the aqueous solution and the organic base is soluble in the aqueous solution wherein the microparticle comprises a multi-lamellar structure.
Method performed by a network node for allocating resources to a User Equipment, UE, which network node operates in a wireless communication network and serves the UE, the method comprises: - determining a system load of the network node for the UE, wherein when the UE is capable of receiving control information on EPDCCH, the system load is determined based on: • a first system load metrics on a physical resource shared by a Physical Downlink Shared CHannel, PDSCH, and EPDCCH, which first load metrics comprises a load due to EPDCCH and a load due to multiplexed PDSCH, and • a second system load metrics on the physical resource shared by the PDSCH and the EPDCCH, which second load metrics comprises a load due to multiplexed EPDCCH and a load due to PDSCH, when the UE is not capable of receiving control information on EPDCCH, the system load is determined based on: • the first system load metrics on the physical resource shared by the PDSCH and EPDCCH, which first load metrics comprises a load due to EPDCCH and a load due to multiplexed PDSCH, • a third system load metrics on a physical resource for carrying Physical Downlink Control CHannel, PDCCH; - determining whether or not to allocate resources to the UE based on the determined system load metrics. - determining a system load of the network node for the UE, wherein when the UE is capable of receiving control information on EPDCCH, the system load is determined based on: • a first system load metrics on a physical resource shared by a Physical Downlink Shared CHannel, PDSCH, and EPDCCH, which first load metrics comprises a load due to EPDCCH and a load due to multiplexed PDSCH, and • a second system load metrics on the physical resource shared by the PDSCH and the EPDCCH, which second load metrics comprises a load due to multiplexed EPDCCH and a load due to PDSCH, when the UE is not capable of receiving control information on EPDCCH, the system load is determined based on: • the first system load metrics on the physical resource shared by the PDSCH and EPDCCH, which first load metrics comprises a load due to EPDCCH and a load due to multiplexed PDSCH, • a third system load metrics on a physical resource for carrying Physical Downlink Control CHannel, PDCCH; • a first system load metrics on a physical resource shared by a Physical Downlink Shared CHannel, PDSCH, and EPDCCH, which first load metrics comprises a load due to EPDCCH and a load due to multiplexed PDSCH, and • a second system load metrics on the physical resource shared by the PDSCH and the EPDCCH, which second load metrics comprises a load due to multiplexed EPDCCH and a load due to PDSCH, • the first system load metrics on the physical resource shared by the PDSCH and EPDCCH, which first load metrics comprises a load due to EPDCCH and a load due to multiplexed PDSCH, • a third system load metrics on a physical resource for carrying Physical Downlink Control CHannel, PDCCH; - determining whether or not to allocate resources to the UE based on the determined system load metrics.
A method for processing calcinated carbon bodies for anodes or cathodes for use in connection with electrolytic production of aluminium, in which the carbon bodies are processed by means of a rotating processing tool, the tool consists of a mainly circular disc with cutting edges arranged at its outer periphery, wherein the processing tool or the carbon body is moved along a linear path thus making slot (s) in the carbon body, wherein the processing is done without the presence of cutting/cooling liquid, wherein, the cutting edges are made of polycrystalline diamond and have a speed greater than 100 m/min. and less than 300 m/min. relative to the carbon body.
A spunbond bicomponent fiber comprising: a first polymer component, a second polymer component, and the first polymer component and the second polymer component form the spunbond bicomponent fiber, the spunbond bicomponent fiber having a ribbon shape with a side-by-side cross-section, wherein a self-crimped spunbond bicomponent fiber is produced upon subjecting the spunbond bicomponent fiber to at least one of a thermal energy and a mechanical force, wherein an aspect ratio of the spunbond bicomponent fiber is greater than 2:1, wherein the aspect ratio is defined as a unitless ratio of a dimension d1 and a dimension d2, the dimension d1 being a first maximum dimension of a cross-section of the fiber measured along a first axis of the cross-section and the dimension d2 being a second maximum dimension of the cross-section measured along a second axis of the cross-section that is perpendicular to the first axis, wherein the first polymer component and the second polymer component have an interface that is substantially parallel to a major bisector defining the ribbon shape of the spunbond bicomponent fiber. a first polymer component, a second polymer component, and the first polymer component and the second polymer component form the spunbond bicomponent fiber, the spunbond bicomponent fiber having a ribbon shape with a side-by-side cross-section, wherein an aspect ratio of the spunbond bicomponent fiber is greater than 2:1, wherein the aspect ratio is defined as a unitless ratio of a dimension d1 and a dimension d2, the dimension d1 being a first maximum dimension of a cross-section of the fiber measured along a first axis of the cross-section and the dimension d2 being a second maximum dimension of the cross-section measured along a second axis of the cross-section that is perpendicular to the first axis, wherein the first polymer component and the second polymer component have an interface that is substantially parallel to a major bisector defining the ribbon shape of the spunbond bicomponent fiber.
Reciprocating internal combustion engine comprising a cylinder head, a crankcase (7a; 7b) and an assembly, wherein the crankcase (7a; 7b) comprises a recess for accommodating the assembly, wherein the assembly comprises at least two cylinders (2a, 2b; 2a, 2b, 2c; 2a, 2b, 2c, 2d; 2a, 2b, 2c, 2d, 2e, 2f) and a platelike deck plate connecting them, wherein the assembly is of integral design, wherein the platelike deck plate has a clearance (3a; 3b; 3c; 3d; 3e; 3f) for each cylinder (2a; 2b; 2c; 2d; 2e; 2f) and wherein the assembly can be inserted into a crankcase (7a; 7b; 7c) of a reciprocating internal combustion engine or placed upon a crankcase (7a; 7b; 7c) of a reciprocating internal combustion engine and wherein the assembly is arranged between the cylinder head and the crankcase (7a; 7b; 7c) and in the recess for accommodating the assembly and wherein the outer wall areas of the cylinders (2a, 2b, 2c, 2d; 2a, 2b, 2c, 2d, 2e, 2f) of the assembly and the wall areas of the recess in the crankcase (7a; 7b; 7c) for accommodating the assembly form a coolant chamber, characterized in that at least one coolant guideway is arranged between the cylinders (2a, 2b; 2b, 2c; 2c, 2d; 2e, 2f; 2a, 2b, 2c; 2c, 2d, 2e) of the assembly, wherein the coolant guideway of the assembly is realized by drilling through the area between two neighboring cylinders (2a, 2b; 2b, 2c; 2c, 2d; 2d, 2e; 2e, 2f) and/or by a cooling-channel core in the area between two cylinders (2a, 2b; 2b, 2c; 2c, 2d; 2d, 2e; 2e, 2f), and the platelike deck plate of the assembly is configured free of openings except for the clearance (3a; 3b; 3c; 3d) for each cylinder (2a; 2b; 2c; 2d).
A process for producing and purifying 68 Gallium radioisotope, said process comprising the steps of: a) irradiating a target containing a target solution comprising zinc using an accelerated particle beam, b) feeding the irradiated target solution into a strong cation exchanger, c) washing the strong cation exchanger, d) eluting Zinc isotopes from the strong cation exchanger with a Zinc elution solution comprising acetone, e) washing the strong cation exchanger, f) eluting 68 Gallium isotope from the strong cation exchanger with hydrochloric acid solution to obtain an eluted solution, g) feeding said eluted solution into a strong anion exchanger, h) washing the strong anion exchanger, i) eluting 68 Gallium isotope from the strong anion exchanger with hydrochloric acid solution to obtain a final solution, characterized in that a step (α) of diluting the target solution comprising zinc is performed after irradiation of the target solution to obtain a diluted target solution, the dilution step (α) being performed before feeding the irradiated target solution into the strong cation exchanger, the irradiated target solution being diluted at least 5 volume times with water. a) irradiating a target containing a target solution comprising zinc using an accelerated particle beam, b) feeding the irradiated target solution into a strong cation exchanger, c) washing the strong cation exchanger, d) eluting Zinc isotopes from the strong cation exchanger with a Zinc elution solution comprising acetone, e) washing the strong cation exchanger, f) eluting 68 Gallium isotope from the strong cation exchanger with hydrochloric acid solution to obtain an eluted solution, g) feeding said eluted solution into a strong anion exchanger, h) washing the strong anion exchanger, i) eluting 68 Gallium isotope from the strong anion exchanger with hydrochloric acid solution to obtain a final solution,