mhurhangee/ep-ind-claims huggingface dataset:
A lid for a beverage container comprising a container body having a container cavity, said lid comprising: a lid body arranged for detachably attaching on said container body to selectively enclose said container cavity, said lid body having a receiving slot and an access opening communicating said container cavity and said receiving slot; and a handle actuation arrangement, which comprises: a locking latch movably mounted in said receiving slot; a mouth piece having a liquid discharge opening and a drinking channel communicating between said access opening and said liquid discharge opening, said mouth piece being pivotally connected to said lid body in said receiving slot to move in a locked position and an extended position, wherein in said locked position, said mouth piece is pivotally moved to be received in said receiving slot and engaged with said locking latch, wherein in said extended position, said mouth piece is pivotally moved to extend from said receiving slot; and an actuating handle, which comprises: an engaging member pivotally received in said receiving slot to engage with said mouth piece; and a handle member extended from said engaging member in such a manner that when said handle member is pivotally moved with respect to said lid body, said engaging member is also driven to pivotally move to drive said mouth piece to disengage from said locking latch so as to allow said mouth piece to move from said locked position to said extended position. a lid body arranged for detachably attaching on said container body to selectively enclose said container cavity, said lid body having a receiving slot and an access opening communicating said container cavity and said receiving slot; and a handle actuation arrangement, which comprises: a locking latch movably mounted in said receiving slot; a mouth piece having a liquid discharge opening and a drinking channel communicating between said access opening and said liquid discharge opening, said mouth piece being pivotally connected to said lid body in said receiving slot to move in a locked position and an extended position, wherein in said locked position, said mouth piece is pivotally moved to be received in said receiving slot and engaged with said locking latch, wherein in said extended position, said mouth piece is pivotally moved to extend from said receiving slot; and an actuating handle, which comprises: an engaging member pivotally received in said receiving slot to engage with said mouth piece; and a handle member extended from said engaging member in such a manner that when said handle member is pivotally moved with respect to said lid body, said engaging member is also driven to pivotally move to drive said mouth piece to disengage from said locking latch so as to allow said mouth piece to move from said locked position to said extended position.
A method for handling equipment service flags, comprising the steps of: receiving a request for service of one or more equipment components (312, 316, 320); determining type of the request, wherein the type of the request comprises equipment service for one or more variables; setting (206, 208) one or more flags associated with the one or more variables to indicate that said one or more variables are in equipment service mode such that value changes in said one or more variables do not propagate for prediction update; adjusting the one or more variables; adjusting a model structure, comprising: setting modeling coefficients to zero to remove process relationships and/or adjusting coefficients for more complex modeled process relationships, wherein the adjustment of the model structure is made, at least in part, for at least one of prediction purposes, calibration of associated process output variable process measurements, process POV estimation and future prediction, determination of a manipulated variable control adjustments, determination of feasible manipulated variable and control variable target values, and optimization of a process; determining if the equipment service is completed; resetting the one or more flags if it is determined that the equipment service is completed; readjusting the model structure to propagate the one or more variables; and adjusting one or more internal model predictions to reconnect the one or more variable values. receiving a request for service of one or more equipment components (312, 316, 320); determining type of the request, wherein the type of the request comprises equipment service for one or more variables; setting (206, 208) one or more flags associated with the one or more variables to indicate that said one or more variables are in equipment service mode such that value changes in said one or more variables do not propagate for prediction update; adjusting the one or more variables; adjusting a model structure, comprising: setting modeling coefficients to zero to remove process relationships and/or adjusting coefficients for more complex modeled process relationships, wherein the adjustment of the model structure is made, at least in part, for at least one of prediction purposes, calibration of associated process output variable process measurements, process POV estimation and future prediction, determination of a manipulated variable control adjustments, determination of feasible manipulated variable and control variable target values, and optimization of a process; determining if the equipment service is completed; resetting the one or more flags if it is determined that the equipment service is completed; readjusting the model structure to propagate the one or more variables; and adjusting one or more internal model predictions to reconnect the one or more variable values.
A method for carrier scheduling, comprising: determining, by a base station, an uplink carrier and a downlink carrier for a mobile terminal, wherein the uplink carrier is adapted to transmit uplink information and the downlink carrier is adapted to transmit downlink information; characterized in that the method further comprises: scheduling, by the base station, the uplink carrier and/or the downlink carrier for the mobile terminal in different time domains based on a predetermined anti-interference scheduling strategy after judging that the mobile terminal does not support simultaneous information transmissions in opposite directions on the uplink carrier and the downlink carrier according to capability information about whether the mobile terminal supports simultaneous information transmissions in opposite directions on at least two frequency bands included in each frequency band combination for non-contiguous carrier aggregation supported by the mobile terminal itself. determining, by a base station, an uplink carrier and a downlink carrier for a mobile terminal, wherein the uplink carrier is adapted to transmit uplink information and the downlink carrier is adapted to transmit downlink information; characterized in that the method further comprises: scheduling, by the base station, the uplink carrier and/or the downlink carrier for the mobile terminal in different time domains based on a predetermined anti-interference scheduling strategy after judging that the mobile terminal does not support simultaneous information transmissions in opposite directions on the uplink carrier and the downlink carrier according to capability information about whether the mobile terminal supports simultaneous information transmissions in opposite directions on at least two frequency bands included in each frequency band combination for non-contiguous carrier aggregation supported by the mobile terminal itself.
Method for determining the position of a multiplicity of measurement locations in a measurement system, the measurement system comprising a. a circular apparatus for receiving reaction vessels, which has a multiplicity of measurement locations arranged on a circular trajectory and a physical reference location, wherein each measurement location is arranged at a known distance from the physical reference location, and b. a measurement apparatus, wherein either the apparatus for receiving reaction vessels is rotatable about the vertical axis thereof or the measurement apparatus is moveable on a horizontal circular trajectory about the vertical axis of the apparatus for receiving reaction vessels, the method comprising the following steps: i. rotating the apparatus for receiving reaction vessels about the vertical axis thereof or moving the measurement apparatus on a horizontal circular trajectory about the vertical axis of the apparatus for receiving reaction vessels with a constant rotational speed in each case; ii. measuring a physical reference signal at the physical reference location during each revolution; characterized by the further steps of iii. determining a virtual reference location by means of a phase locked loop which outputs an output pulse sequence, wherein each pulse of the output pulse sequence corresponds to the virtual reference location of the associated revolution, and iv. calculating the position of the measurement locations on the basis of predetermined time intervals from the virtual reference location. a. a circular apparatus for receiving reaction vessels, which has a multiplicity of measurement locations arranged on a circular trajectory and a physical reference location, wherein each measurement location is arranged at a known distance from the physical reference location, and b. a measurement apparatus, wherein either the apparatus for receiving reaction vessels is rotatable about the vertical axis thereof or the measurement apparatus is moveable on a horizontal circular trajectory about the vertical axis of the apparatus for receiving reaction vessels, i. rotating the apparatus for receiving reaction vessels about the vertical axis thereof or moving the measurement apparatus on a horizontal circular trajectory about the vertical axis of the apparatus for receiving reaction vessels with a constant rotational speed in each case; ii. measuring a physical reference signal at the physical reference location during each revolution; characterized by the further steps of iii. determining a virtual reference location by means of a phase locked loop which outputs an output pulse sequence, wherein each pulse of the output pulse sequence corresponds to the virtual reference location of the associated revolution, and iv. calculating the position of the measurement locations on the basis of predetermined time intervals from the virtual reference location.
A method for manufacturing a blade in composite material having an added metal leading edge for gas turbine aeroengine, the method comprising: - producing a blade body in composite material comprising in longitudinal direction (D L) a blade root part, a shank part and an airfoil body part, the airfoil body part extending in longitudinal direction between the shank part and an airfoil body tip and in transverse direction (D T) between a foremost edge portion and a rear edge portion, - manufacturing, via additive manufacturing, a leading edge extending in the longitudinal direction between a lower end intended to be present at the shank part of the blade body in composite material and an upper end intended to be present at the tip of the airfoil body part, - bonding the manufactured leading edge onto the foremost edge portion of the airfoil body of the blade body in composite material, characterized in that the leading edge comprises a first portion in a first metal material and extending from the lower end of the leading edge as far as an intermediate position located between the lower end and upper end of the leading edge, and a second portion in a second metal material extending from the intermediate position as far as the upper end of said leading edge, the second metal material having greater density than the density of the first metal material. - producing a blade body in composite material comprising in longitudinal direction (D L) a blade root part, a shank part and an airfoil body part, the airfoil body part extending in longitudinal direction between the shank part and an airfoil body tip and in transverse direction (D T) between a foremost edge portion and a rear edge portion, - manufacturing, via additive manufacturing, a leading edge extending in the longitudinal direction between a lower end intended to be present at the shank part of the blade body in composite material and an upper end intended to be present at the tip of the airfoil body part, - bonding the manufactured leading edge onto the foremost edge portion of the airfoil body of the blade body in composite material, characterized in that the leading edge comprises a first portion in a first metal material and extending from the lower end of the leading edge as far as an intermediate position located between the lower end and upper end of the leading edge, and a second portion in a second metal material extending from the intermediate position as far as the upper end of said leading edge, the second metal material having greater density than the density of the first metal material.
Method for managing communication sessions when accessing, from a user appliance, services provided by resource devices (30, 40) of a communication network, the method comprising a step of establishing a first communication session (31, S1) between a first appliance of the network (30, CS1) and the user appliance for the transmission of data relating to a first service, characterized in that it comprises: a step of interception of a message (REQ-DNS) generated when establishing access to a second service by the user appliance in order to control redirection of said user appliance to the first network appliance for the purpose of acquiring data relating to the second service, and a step of assembly, by the first appliance (30, CS1), of data relating to the second service and received from a corresponding resource device, with the data relating to the first service, so as to transmit all of the data to the user appliance via said first communication session (31, S1). a step of interception of a message (REQ-DNS) generated when establishing access to a second service by the user appliance in order to control redirection of said user appliance to the first network appliance for the purpose of acquiring data relating to the second service, and a step of assembly, by the first appliance (30, CS1), of data relating to the second service and received from a corresponding resource device, with the data relating to the first service, so as to transmit all of the data to the user appliance via said first communication session (31, S1).
A spacecraft comprising: a main body that has an accommodation space for accommodating an electronic device therein; an oscillator configured to output a radio wave including a frequency of a predetermined frequency band; at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) that are disposed on an exterior portion of the main body to be exposed to space and configured to amplify electric power of the radio wave output by the oscillator, each of the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) forming a side surface of a rectangular parallelepiped, each of the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) being supported by a frame so as to connect the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d); and an antenna that is disposed on the exterior portion of the main body and is for emitting the radio wave to an outside with the electric power amplified by the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d), wherein the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) and the antenna are fixed on a same surface side of the main body to be arranged along a central axis of the antenna. a main body that has an accommodation space for accommodating an electronic device therein; an oscillator configured to output a radio wave including a frequency of a predetermined frequency band; at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) that are disposed on an exterior portion of the main body to be exposed to space and configured to amplify electric power of the radio wave output by the oscillator, each of the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) forming a side surface of a rectangular parallelepiped, each of the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) being supported by a frame so as to connect the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d); and an antenna that is disposed on the exterior portion of the main body and is for emitting the radio wave to an outside with the electric power amplified by the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d), wherein the at least four amplifiers (112-la, 112-1b, 112-1c, 112-1d) and the antenna are fixed on a same surface side of the main body to be arranged along a central axis of the antenna.
A method for calculating a carrier specific scale factor, CSSF, outside a measurement gap, applied to an evolved universal terrestrial radio access-new radio dual-connectivity, EN-DC, system, comprising: receiving, by a terminal device, first measurement configuration information sent by an evolved universal terrestrial radio access, E-UTRAN, primary cell, wherein the first measurement configuration information comprises M1 first measurement objects, M1≥0, M1 is integer, the first measurement object is a new radio NR measurement object configured on a primary secondary component carrier, PSCC, or a secondary component carrier, SCC, and receiving, by the terminal device, second measurement configuration information sent by a new radio NR primary secondary cell, wherein the second measurement configuration information comprises M3 third measurement objects, and M4 fourth measurement objects, 0≤M3≤1, M4≥0, M3, and M4 are integers, the third measurement object is an NR measurement object configured on the PSCC, the fourth measurement object is an NR measurement object configured on the SCC, and calculating, by the terminal device, a CSSF outside a measurement gap of each measurement object in the M1 first measurement objects, the M3 third measurement objects, and the M4 fourth measurement objects. receiving, by a terminal device, first measurement configuration information sent by an evolved universal terrestrial radio access, E-UTRAN, primary cell, wherein the first measurement configuration information comprises M1 first measurement objects, M1≥0, M1 is integer, the first measurement object is a new radio NR measurement object configured on a primary secondary component carrier, PSCC, or a secondary component carrier, SCC, and receiving, by the terminal device, second measurement configuration information sent by a new radio NR primary secondary cell, wherein the second measurement configuration information comprises M3 third measurement objects, and M4 fourth measurement objects, 0≤M3≤1, M4≥0, M3, and M4 are integers, the third measurement object is an NR measurement object configured on the PSCC, the fourth measurement object is an NR measurement object configured on the SCC, and calculating, by the terminal device, a CSSF outside a measurement gap of each measurement object in the M1 first measurement objects, the M3 third measurement objects, and the M4 fourth measurement objects.
A multi-lumen catheter comprising: a tubular shaft member having a proximal end, a distal end and a longitudinal length therebetween, the tubular shaft member having a first lumen and a second lumen defined therein, the first lumen having a first lumen cross-sectional dimension and a length extending at least along a portion of the length of the tubular shaft member, and the second lumen having a second lumen cross-sectional dimension and a length extending along the length of tubular shaft member, characterized in that the tubular shaft member is a monolithic elongate tubular shaft member having an inner core made of a first material, an outer layer made of a second material, and an intermediate tie layer disposed between the inner core and the outer layer, the first material of the inner core defining the first lumen and the second lumen therein, the first lumen cross-sectional dimension being substantially uniform along the length of the first lumen, the second lumen cross-sectional dimension being substantially uniform along the length of the second lumen, and the tubular shaft member having an outer cross-sectional dimension that varies along the length of the tubular shaft member. the tubular shaft member having a first lumen and a second lumen defined therein, the first lumen having a first lumen cross-sectional dimension and a length extending at least along a portion of the length of the tubular shaft member, and the second lumen having a second lumen cross-sectional dimension and a length extending along the length of tubular shaft member, characterized in that the tubular shaft member is a monolithic elongate tubular shaft member having an inner core made of a first material, an outer layer made of a second material, and an intermediate tie layer disposed between the inner core and the outer layer, the first material of the inner core defining the first lumen and the second lumen therein, the first lumen cross-sectional dimension being substantially uniform along the length of the first lumen, the second lumen cross-sectional dimension being substantially uniform along the length of the second lumen, and the tubular shaft member having an outer cross-sectional dimension that varies along the length of the tubular shaft member.
A mounting structure for a pedal device including a pedal and a bracket that pivotally holds the pedal, the mounting structure being configured to mount the pedal device on a dash panel such that the dash panel is sandwiched by and between the bracket and a master cylinder device, the mounting structure comprising: a plurality of fastening rods that respectively extend through a plurality of holes formed in the dash panel for fastening the bracket and the master cylinder device to each other; and a plurality of collars interposed between the dash panel and the bracket for spacing the dash panel and the bracket apart from each other, the plurality of fastening rods respectively extending through the plurality of collars, wherein the plurality of collars include a pair of collars, and wherein one of the pair of collars has an extending portion (54a; 54b; 54c; 54d; 54e) that extends along the dash panel in a direction away from the other of the pair of collars, the extending portion functioning as a reinforcing member for reducing deformation of the dash panel caused when the pedal is stepped on. a plurality of fastening rods that respectively extend through a plurality of holes formed in the dash panel for fastening the bracket and the master cylinder device to each other; and a plurality of collars interposed between the dash panel and the bracket for spacing the dash panel and the bracket apart from each other, the plurality of fastening rods respectively extending through the plurality of collars, wherein the plurality of collars include a pair of collars, and wherein one of the pair of collars has an extending portion (54a; 54b; 54c; 54d; 54e) that extends along the dash panel in a direction away from the other of the pair of collars, the extending portion functioning as a reinforcing member for reducing deformation of the dash panel caused when the pedal is stepped on.