mhurhangee/ep-ind-claims huggingface dataset:
An installation configured for crystallizing and drying granular polymer material with a low level of crystallinity, that is a level of crystallinity less than a threshold value below which the granular polymer material can involve the formation of blocks of granules during the drying process, wherein the level of crystallinity is defined as the weight fraction of polymer in the crystalline state with respect to the total polymer mass, comprising: - at least one crystallization hopper which is connected to a crystallization line, via which there is introduced into the crystallization hopper a first gas flow which is heated to a first temperature which is suitable for increasing the level of crystallinity of the granular polymer material; - an agitation member which is associated with the crystallization hopper and which is provided to maintain the granular material in an agitated state inside the crystallization hopper; - at least one heating hopper which is arranged downstream of the crystallization hopper and which is provided with a heating unit which is provided to heat the crystallized granular polymer material to a second temperature which is greater than the first temperature, - at least one drying hopper which is arranged downstream of the heating hopper and which is connected to a depressurization circuit which is provided to obtain in the drying hopper a predefined level of pressure reduction and to dry the granular polymer material, - at least one supply hopper which is arranged downstream of the drying hopper and upstream of a transformation machine for the granular polymer material. - at least one crystallization hopper which is connected to a crystallization line, via which there is introduced into the crystallization hopper a first gas flow which is heated to a first temperature which is suitable for increasing the level of crystallinity of the granular polymer material; - an agitation member which is associated with the crystallization hopper and which is provided to maintain the granular material in an agitated state inside the crystallization hopper; - at least one heating hopper which is arranged downstream of the crystallization hopper and which is provided with a heating unit which is provided to heat the crystallized granular polymer material to a second temperature which is greater than the first temperature, - at least one drying hopper which is arranged downstream of the heating hopper and which is connected to a depressurization circuit which is provided to obtain in the drying hopper a predefined level of pressure reduction and to dry the granular polymer material, - at least one supply hopper which is arranged downstream of the drying hopper and upstream of a transformation machine for the granular polymer material.
An alpha 1 adrenergic receptor agonist for use in the treatment or prevention of traction alopecia comprising applying a composition comprising a pilomotor effective amount of an alpha 1 adrenergic receptor agonist topically to a portion of skin on the head that includes at least one hair follicle, wherein the composition comprises an alpha 1 adrenergic receptor agonist that is synephrine, or a pharmaceutically acceptable salt or hydrate thereof.
An influenza vaccine for use in immunizing a subject against influenza virus infection, wherein the vaccine comprises: (a) an adjuvant and a standard dose influenza virus antigen from an H1N1 strain, an H3N2 strain and a B strain; or (b) a high-dose influenza virus antigen from an H1N1 strain, an H3N2 strain and a B strain, having between 30 μg and 150 μg of antigen per influenza strain; or (c) an adjuvant and a high-dose influenza virus antigen from an H1N1 strain, an H3N2 strain and a B strain, having between 30 μg and 150 μg of antigen per influenza strain; and wherein the subject is under 65, but 18 years or older and on a statin therapy. (a) an adjuvant and a standard dose influenza virus antigen from an H1N1 strain, an H3N2 strain and a B strain; or (b) a high-dose influenza virus antigen from an H1N1 strain, an H3N2 strain and a B strain, having between 30 μg and 150 μg of antigen per influenza strain; or (c) an adjuvant and a high-dose influenza virus antigen from an H1N1 strain, an H3N2 strain and a B strain, having between 30 μg and 150 μg of antigen per influenza strain;
A Ni-base heat resistant alloy, which comprises by mass percent, C: less than 0.08%, Si: 1% or less, Mn: 1% or less, Cr: not less than 15% to less than 28%, Fe: 15% or less, W: more than 5% to not more than 20%, Al: more than 0.5% to not more than 2%, Ti: more than 0.5% to not more than 1.7%, Nd: 0.001 to 0.1% and B: 0.0005 to 0.01%, optionally containing Mo: 15% or less, Co: 20% or less, Nb: 1.0% or less, V: 1.5% or less, Zr: 0.2% or less, Hf: 1% or less, Mg: 0.05% or less, Ca: 0.05% or less, Y: 0.5% or less, La: 0.5% or less and Ce: 0.5% or less, Ta: 8% or less and Re: 8% or less, with the balance being Ni and impurities, in which the contents of P, S, Sn, Pb, Sb, Zn and As among the impurities are P: 0.03% or less, S: 0.01% or less, Sn: 0.020% or less, Pb: 0.010% or less, Sb: 0.005% or less, Zn: 0.005% or less and As: 0.005% or less, and further satisfies the following formulas to: 0.015 ≤ Nd + 13.4 × B ≤ 0.13 Sn + Pb ≤ 0.025 Sb + Zn + As ≤ 0.010 wherein each element symbol in the formulas to represents the content by mass percent of the element concerned, wherein the Ni-base heat resistant alloy contains, by mass percent, one or more elements of one or more groups selected from the following groups <1> to <3>: <1> V: not less than 0.02% to 1.5% or less, Zr: not less than 0.005% to 0.2% or less and Hf: not less than 0.005% to 1% or less, <2> Mg: not less than 0.0005% to 0.05% or less, Ca: not less than 0.0005% to 0.05% or less, Y: not less than 0.0005% to 0.5% or less, La: not less than 0.0005% to 0.5% or less and Ce: not less than 0.0005% to 0.5% or less, <3> Ta: not less than 0.01% to 8% or less and Re: not less than 0.01% to 8% or less. <1> V: not less than 0.02% to 1.5% or less, Zr: not less than 0.005% to 0.2% or less and Hf: not less than 0.005% to 1% or less, <2> Mg: not less than 0.0005% to 0.05% or less, Ca: not less than 0.0005% to 0.05% or less, Y: not less than 0.0005% to 0.5% or less, La: not less than 0.0005% to 0.5% or less and Ce: not less than 0.0005% to 0.5% or less, <3> Ta: not less than 0.01% to 8% or less and Re: not less than 0.01% to 8% or less.
A method for preparing compound of formula III: reacting a compound of formula II' with methylamine or the salt thereof to provide the compound of formula III; wherein R 1, R 2, R 3 and R 4 are each independently selected from the group consisting of substituted or unsubstituted C 1 -C 4 alkyl, substituted or unsubstituted C 1 -C 4 ester group; or R 1, R 2 and the adjacent -N- together form a substituted or unsubstituted 3-10 membered heterocycle, and the heterocycle may contain 1-3 heteroatoms selected from the group consisting of N, O or S; the 3-10 membered heterocycle is monocycle, bicycle, spirocycle or bridged ring; or R 3, R 4 and the adjacent -N- together constitute a substituted or unsubstituted 3-10 membered heterocycle, and the heterocycle may contain 1-3 heteroatoms selected from the group consisting of N, O or S; the 3-10 membered heterocycle is monocycle, bicycle, spirocycle or bridged ring; R 5 is selected from the group consisting of C1-C4 alkoxy, chlorine atom, bromine atom, hydroxyl, or active ester group the substitution is that one or more hydrogen atoms on a group are replaced by substituents selected from the group consisting of halogens, C 1 -C 4 alkyl; wherein the methylamine or the salt thereof is selected from the group consisting of methylamine methanol solution, methylamine ethanol solution, methylamine aqueous solution, methylamine hydrochloride, or methylamine sulfate. wherein R 1, R 2, R 3 and R 4 are each independently selected from the group consisting of substituted or unsubstituted C 1 -C 4 alkyl, substituted or unsubstituted C 1 -C 4 ester group; or R 1, R 2 and the adjacent -N- together form a substituted or unsubstituted 3-10 membered heterocycle, and the heterocycle may contain 1-3 heteroatoms selected from the group consisting of N, O or S; the 3-10 membered heterocycle is monocycle, bicycle, spirocycle or bridged ring; or R 3, R 4 and the adjacent -N- together constitute a substituted or unsubstituted 3-10 membered heterocycle, and the heterocycle may contain 1-3 heteroatoms selected from the group consisting of N, O or S; the 3-10 membered heterocycle is monocycle, bicycle, spirocycle or bridged ring; R 5 is selected from the group consisting of C1-C4 alkoxy, chlorine atom, bromine atom, hydroxyl, or active ester group the substitution is that one or more hydrogen atoms on a group are replaced by substituents selected from the group consisting of halogens, C 1 -C 4 alkyl; wherein the methylamine or the salt thereof is selected from the group consisting of methylamine methanol solution, methylamine ethanol solution, methylamine aqueous solution, methylamine hydrochloride, or methylamine sulfate.
Method for controlling the electronic ignition of an internal combustion chamber of a gas-powered fixing tool, characterized in that it comprises the following steps: • detection (E 1) of a first mechanical event at a first instant (t 1); • detection of a second mechanical event at a second instant; • generation of a control signal for triggering the ignition of the combustion chamber following the detection of the second mechanical event, if the time (Δt) between the first and second mechanical events is greater than a first predetermined threshold (Δt R1), characterized in that it further comprises: • a step of generation (E 2) of a medium ignition voltage (V z) initiated as soon as the first mechanical event is detected at the first instant (t 1); • a step of voltage comparison (E 5) to compare said medium ignition voltage relative to a reference trigger voltage (V d), and in that said trigger control is generated on the additional condition that the medium ignition voltage (V 2) has an amplitude greater than the reference trigger voltage (V d). • detection (E 1) of a first mechanical event at a first instant (t 1); • detection of a second mechanical event at a second instant; • generation of a control signal for triggering the ignition of the combustion chamber following the detection of the second mechanical event, if the time (Δt) between the first and second mechanical events is greater than a first predetermined threshold (Δt R1), • a step of generation (E 2) of a medium ignition voltage (V z) initiated as soon as the first mechanical event is detected at the first instant (t 1); • a step of voltage comparison (E 5) to compare said medium ignition voltage relative to a reference trigger voltage (V d),
An apparatus comprising: a plurality of mixing circuits (1610, 1700) configured to generate a plurality of frequency converted signals; at least one mixing circuit of the plurality of mixing circuits is configured with a plurality of paths(1710, 1720, 1730), each path representing one linearity mode, the plurality of paths comprising: a first path of a high-linearity mode configured with a first metal oxide semiconductor resistor; and a second path of a low-linearity mode configured with a second metal oxide semiconductor resistor and a first mode switch, the first and second metal oxide semiconductor resistors are controlled by a local oscillating signal; and a plurality of combining circuits configured to combine the plurality of frequency converted signals to generate a differential baseband output signal (1630, 1632). a plurality of mixing circuits (1610, 1700) configured to generate a plurality of frequency converted signals; at least one mixing circuit of the plurality of mixing circuits is configured with a plurality of paths(1710, 1720, 1730), each path representing one linearity mode, the plurality of paths comprising: a first path of a high-linearity mode configured with a first metal oxide semiconductor resistor; and a second path of a low-linearity mode configured with a second metal oxide semiconductor resistor and a first mode switch, the first and second metal oxide semiconductor resistors are controlled by a local oscillating signal; and a plurality of combining circuits configured to combine the plurality of frequency converted signals to generate a differential baseband output signal (1630, 1632). a first path of a high-linearity mode configured with a first metal oxide semiconductor resistor; and a second path of a low-linearity mode configured with a second metal oxide semiconductor resistor and a first mode switch, the first and second metal oxide semiconductor resistors are controlled by a local oscillating signal; and a plurality of combining circuits configured to combine the plurality of frequency converted signals to generate a differential baseband output signal (1630, 1632).
Stator assembly for a gas turbine comprising: • a stator ring, which extends about a longitudinal axis and comprises an inner edge and an outer edge; the outer edge being provided with an annular groove; the annular groove defining a leading wall and a trailing wall; the trailing wall being provided with an annular trailing radial face and with an annular trailing axial face; • a plurality of stator vanes radially arranged and coupled alongside one another to the outer edge of the stator ring so as to close the annular grove and define an annular cooling channel; • the stator ring being provided with at least one trailing cooling hole having an inlet facing the annular cooling channel and an outlet arranged on the annular trailing radial face; wherein the trailing cooling hole extends along an extension axis; on a tangential plane defined by the longitudinal axis and a circumferential direction, which is orthogonal to the longitudinal axis and orthogonal to a radial direction in turn orthogonal to the longitudinal axis, a first angle (β) is defined by the projection of the extension axis on the tangential plane and the axial direction characterized in that the first angle is comprised between 20° and 70°. • a stator ring, which extends about a longitudinal axis and comprises an inner edge and an outer edge; the outer edge being provided with an annular groove; the annular groove defining a leading wall and a trailing wall; the trailing wall being provided with an annular trailing radial face and with an annular trailing axial face; • a plurality of stator vanes radially arranged and coupled alongside one another to the outer edge of the stator ring so as to close the annular grove and define an annular cooling channel; • the stator ring being provided with at least one trailing cooling hole having an inlet facing the annular cooling channel and an outlet arranged on the annular trailing radial face; wherein the trailing cooling hole extends along an extension axis; on a tangential plane defined by the longitudinal axis and a circumferential direction, which is orthogonal to the longitudinal axis and orthogonal to a radial direction in turn orthogonal to the longitudinal axis, a first angle (β) is defined by the projection of the extension axis on the tangential plane and the axial direction characterized in that the first angle is comprised between 20° and 70°.
A method executed by a terminal device in a wireless telecommunications system configured to support communications between network infrastructure equipment and terminal devices using a primary component carrier operating on radio resources within a first frequency band and a secondary component carrier operating on radio resources within a second frequency band, wherein the second frequency band comprises radio resources which are shared with wireless communication devices that are not part of the wireless telecommunications system, and wherein the wireless telecommunications system supports a connected mode of operation in which terminal devices receive user-plane data from the network infrastructure equipment using the primary and / or secondary component carrier and an idle mode of operation in which terminal devices do not receive user-plane data from the network infrastructure equipment, wherein the method comprises: establishing a measurement configuration for making measurements of radio channel conditions for radio resources within the second frequency band; making a measurement of radio channel conditions for radio resources within the second frequency band in accordance with the measurement configuration while the terminal device is operating in the idle mode; determining if the measurement of radio channel conditions meets a trigger criterion, and if so, switching from the idle mode of operation to the connected mode of operation and transmitting a measurement report to the network infrastructure equipment to indicate the trigger criterion has been met, and returning to the idle mode of operation after transmitting the measurement report to the network infrastructure equipment. establishing a measurement configuration for making measurements of radio channel conditions for radio resources within the second frequency band; making a measurement of radio channel conditions for radio resources within the second frequency band in accordance with the measurement configuration while the terminal device is operating in the idle mode; determining if the measurement of radio channel conditions meets a trigger criterion, and if so, switching from the idle mode of operation to the connected mode of operation and transmitting a measurement report to the network infrastructure equipment to indicate the trigger criterion has been met, and returning to the idle mode of operation after transmitting the measurement report to the network infrastructure equipment.
A method of automating an autorotation in an aircraft, the method comprising: recognizing a failure of an engine; analyzing a flight condition of the aircraft; actuating a swashplate mechanism with a command from a flight control computer to an actuator associated with the swashplate mechanism so as to change a pitch of a plurality of main rotor blades to predictively achieve a target rotor speed value of rotor blades; and temporarily halting the step of actuating the swashplate mechanism for a period of time after a pilot has made an overriding input. recognizing a failure of an engine; analyzing a flight condition of the aircraft; actuating a swashplate mechanism with a command from a flight control computer to an actuator associated with the swashplate mechanism so as to change a pitch of a plurality of main rotor blades to predictively achieve a target rotor speed value of rotor blades; and temporarily halting the step of actuating the swashplate mechanism for a period of time after a pilot has made an overriding input.
A computer-implemented method of predicting thermally induced aberrations of a projection system for projecting a radiation beam, the method comprising: calculating a change in temperature of the projection system from a power of the radiation beam output from the projection system using a dynamic linear function; and calculating the thermally induced aberrations from the calculated change in temperature using a static non-linear function. calculating a change in temperature of the projection system from a power of the radiation beam output from the projection system using a dynamic linear function; and calculating the thermally induced aberrations from the calculated change in temperature using a static non-linear function.
A method of wireless backhaul connection, comprising: determining, by a long-term evolution, LTE, base station when receiving, from a wireless backhaul base station, connection requirement information for donor base stations, a first number of donor base stations required by the wireless backhaul base station for wireless backhaul connection according to the connection requirement information; determining, by the LTE base station, a second number of donor base stations that are capable of providing wireless backhaul service to the wireless backhaul base station; and configuring, by the LTE base station, for the wireless backhaul base station, at least one donor base station for wireless backhaul connection according to the first number and the second number, wherein the wireless backhaul base station and one or more donor base stations are located in a coverage area of the LTE base station. determining, by a long-term evolution, LTE, base station when receiving, from a wireless backhaul base station, connection requirement information for donor base stations, a first number of donor base stations required by the wireless backhaul base station for wireless backhaul connection according to the connection requirement information; determining, by the LTE base station, a second number of donor base stations that are capable of providing wireless backhaul service to the wireless backhaul base station; and configuring, by the LTE base station, for the wireless backhaul base station, at least one donor base station for wireless backhaul connection according to the first number and the second number, wherein the wireless backhaul base station and one or more donor base stations are located in a coverage area of the LTE base station.
A method of manufacturing an antenna structure for a radio frequency identification (RFID) tag, comprising the steps of: providing a conductive layer and a carrier layer supporting the conductive layer; cutting a first antenna pattern through the conductive layer, wherein the cutting of the first antenna pattern through the conductive layer includes a step of performing a partial die cut with one of a rotary die cutter or cold foil process; creating a microprocessor attachment portion by further cutting in the first antenna pattern to create a RFID antenna structure, wherein the cutting of the microprocessor attachment portion in the first antenna pattern includes ablating the conductive layer using a computer controlled cutting laser; and attaching a microprocessor to the microprocessor attachment portion. providing a conductive layer and a carrier layer supporting the conductive layer; cutting a first antenna pattern through the conductive layer, wherein the cutting of the first antenna pattern through the conductive layer includes a step of performing a partial die cut with one of a rotary die cutter or cold foil process; creating a microprocessor attachment portion by further cutting in the first antenna pattern to create a RFID antenna structure, wherein the cutting of the microprocessor attachment portion in the first antenna pattern includes ablating the conductive layer using a computer controlled cutting laser; and attaching a microprocessor to the microprocessor attachment portion.
A method of screening for a Cas9 molecule/guide RNA (gRNA) molecule complex for administration to a subject, the method comprising: (a) generating a plurality of samples, each sample comprising a Cas9 molecule/gRNA molecule complex generated by combining a Cas9 molecule and one of a plurality of gRNA molecules; (b) detecting a melting temperature (T m) value of the Cas9 molecule/gRNA molecule complex in each of the plurality of samples; and (c) selecting at least one sample from the plurality of samples based on one or more of (i) a comparison of the T m values in the plurality of samples to a T m value of a reference Cas9 molecule, a reference Cas9 molecule/gRNA molecule complex or a pre-determined threshold T m value, or (ii) a relative ordering of the T m values of the plurality of samples. (a) generating a plurality of samples, each sample comprising a Cas9 molecule/gRNA molecule complex generated by combining a Cas9 molecule and one of a plurality of gRNA molecules; (b) detecting a melting temperature (T m) value of the Cas9 molecule/gRNA molecule complex in each of the plurality of samples; and (c) selecting at least one sample from the plurality of samples based on one or more of (i) a comparison of the T m values in the plurality of samples to a T m value of a reference Cas9 molecule, a reference Cas9 molecule/gRNA molecule complex or a pre-determined threshold T m value, or (ii) a relative ordering of the T m values of the plurality of samples.