mhurhangee/ep-ind-claims huggingface dataset:
A process for preparing a compound of Formula: wherein: R 1, R 2, R 5 and R 8 are hydrogen; R 3 and R 7 are methoxy; R 4 is OH; R 6 is hydrocarbyl or substituted hydrocarbyl, wherein substituted hydrocarbyl means a hydrocarbyl moiety in which: a carbon chain atom is substituted with a nitrogen atom, an oxygen atom, a silicon atom, a phosphorous atom, a boron atom, or a halogen atom; and/or the carbon chain comprises additional substituents selected from alkyl, alkoxy, acyl, acyloxy, alkenyl, alkenoxy, aryl, aryloxy, amino, amido, acetal, carbamyl, carbocyclo, cyano, ester, ether, halogen, heterocyclo, hydroxy, keto, ketal, phospho, nitro, and thio; R 14 is hydrogen; and R 17 is methyl, the process comprising mixing dihydrosinomenine of Formula: with an amine source of the formula R 6 NH 2, wherein R 6 is hydrocarbyl or substituted hydrocarbyl as defined above, a hydrogen donor comprising a formate ion, a transition metal catalyst, and a proton acceptor chosen from ammonia, ammonium hydroxide, or sodium hydroxide; to produce the compound of Formula, wherein at least one intermediate compound comprising a 6-imine moiety is produced during the process. R 1, R 2, R 5 and R 8 are hydrogen; R 3 and R 7 are methoxy; R 4 is OH; R 6 is hydrocarbyl or substituted hydrocarbyl, wherein substituted hydrocarbyl means a hydrocarbyl moiety in which: a carbon chain atom is substituted with a nitrogen atom, an oxygen atom, a silicon atom, a phosphorous atom, a boron atom, or a halogen atom; and/or the carbon chain comprises additional substituents selected from alkyl, alkoxy, acyl, acyloxy, alkenyl, alkenoxy, aryl, aryloxy, amino, amido, acetal, carbamyl, carbocyclo, cyano, ester, ether, halogen, heterocyclo, hydroxy, keto, ketal, phospho, nitro, and thio; R 14 is hydrogen; and R 17 is methyl, the process comprising mixing dihydrosinomenine of Formula:
Torsion beam axle for a motor vehicle, having a torque tube and longitudinal rocker coupled at the ends of the torsion tube, wherein the torsion tube is formed in its cross-section at least in some portions as a semi-open profile and in the torsion tube a reinforcement plate is set in and coupled, characterised in that the reinforcement plate is form-fittingly coupled with the torsion tube via a collar passage, wherein the collar passage is formed on the torsion tube and engages through the reinforcement plate.
An inspection method for a photovoltaic power generation system including a solar cell string having a plurality of solar cell modules (PV1 - PV10) connected in series between a positive terminal and a negative terminal, the method comprising:sequentially applying an AC inspection signal to the positive terminal and to the negative terminal;measuring, when the AC inspection signal is applied, an inspection signal current and voltage;computing from the measured inspection signal current and voltage:an impedance Zp, when the AC inspection signal is applied to the positive terminal, and an impedance Zn, when the AC inspection signal is applied to the negative terminal, characterized in computing, from the computed impedances Zp and Zn, a combined impedance Zpn, and obtaining a deviation of the combined impedance Zpn from a reference impedance ZO, the reference impedance ZO being the impedance of the solar cell string without defects,comparing the obtained deviation from a predetermined first threshold, and determining that there are at least two defects in the solar cell string if the deviation is greater than or equal to the first threshold.
A flight control system (100, 200) for a flight control surface, said flight control system (100, 200) comprising: a first actuator control electronics, ACE, configured to generate a first control signal for the flight control surface; a second ACE configured to generate a second control signal for the flight control surface; a third ACE configured to generate a third control signal for the flight control surface; a first remote electronics unit, REU, coupled to said first ACE and said second ACE, and configured to operate, based on the first control signal and the second control signal, an actuator (216, 220) coupled to the flight control surface; and a second REU coupled to said second ACE and said third ACE, and configured to operate, based on the second control signal and the third control signal, the actuator (216, 220); wherein said first REU and said second REU are each further configured to operate the actuator (216, 220) only upon receipt of respective control signals originating from at least two of said first ACE, said second ACE, and said third ACE; and wherein said first REU and said second REU are each further configured to operate the actuator (216, 220) independent of each other. a first actuator control electronics, ACE, configured to generate a first control signal for the flight control surface; a second ACE configured to generate a second control signal for the flight control surface; a third ACE configured to generate a third control signal for the flight control surface; a first remote electronics unit, REU, coupled to said first ACE and said second ACE, and configured to operate, based on the first control signal and the second control signal, an actuator (216, 220) coupled to the flight control surface; and a second REU coupled to said second ACE and said third ACE, and configured to operate, based on the second control signal and the third control signal, the actuator (216, 220); wherein said first REU and said second REU are each further configured to operate the actuator (216, 220) only upon receipt of respective control signals originating from at least two of said first ACE, said second ACE, and said third ACE; and wherein said first REU and said second REU are each further configured to operate the actuator (216, 220) independent of each other.
An electronic device, comprising: an inverted-F antenna resonating element; an antenna ground that is separated from the inverted-F antenna resonating element by an opening; an antenna feed path that is coupled to the inverted-F antenna resonating element; and non-near-field communications circuitry coupled to the antenna feed path that transmits and receives signals in a non-near-field communications signal band using the inverted-F antenna resonating element and the antenna ground; near field communications circuitry coupled to the antenna feed path that transmits and receives signals in a near field communications band using a loop antenna that includes a segment of the inverted-F antenna resonating element and a portion of the antenna ground, wherein the non-near-field communications circuitry comprises cellular telephone transceiver circuitry and the non-near-field communications signal band comprises a cellular telephone band above 700 MHz. an inverted-F antenna resonating element; an antenna ground that is separated from the inverted-F antenna resonating element by an opening; an antenna feed path that is coupled to the inverted-F antenna resonating element; and non-near-field communications circuitry coupled to the antenna feed path that transmits and receives signals in a non-near-field communications signal band using the inverted-F antenna resonating element and the antenna ground; near field communications circuitry coupled to the antenna feed path that transmits and receives signals in a near field communications band using a loop antenna that includes a segment of the inverted-F antenna resonating element and a portion of the antenna ground, wherein the non-near-field communications circuitry comprises cellular telephone transceiver circuitry and the non-near-field communications signal band comprises a cellular telephone band above 700 MHz.
A test system for testing a device under test, the test system comprising at least one feed antenna, a shielded chamber, and at least a first reflector and a second reflector, wherein the test system is a compact antenna test range, wherein the first reflector and the second reflector are arranged inside the shielded chamber, wherein the first reflector is configured and arranged such that it redirects outgoing test signals emitted by the at least one feed antenna towards the second reflector and incoming test signals coming from the second reflector towards the at least one feed antenna, wherein the device under test is arranged outside the shielded chamber encompassing the first reflector and the second reflector, wherein the shielded chamber comprises at least a first interface associated with the device under test, wherein the first interface and the feed antenna are located at different sides of the shielded chamber, which are perpendicular to each other, the test system being characterized in that a phase center of the at least one feed antenna is located on top of the shielded chamber or below the shielded chamber. wherein the test system is a compact antenna test range, wherein the first reflector and the second reflector are arranged inside the shielded chamber, wherein the first reflector is configured and arranged such that it redirects outgoing test signals emitted by the at least one feed antenna towards the second reflector and incoming test signals coming from the second reflector towards the at least one feed antenna, wherein the device under test is arranged outside the shielded chamber encompassing the first reflector and the second reflector, wherein the shielded chamber comprises at least a first interface associated with the device under test, wherein the first interface and the feed antenna are located at different sides of the shielded chamber, which are perpendicular to each other, the test system being characterized in that a phase center of the at least one feed antenna is located on top of the shielded chamber or below the shielded chamber.
A resin composition comprising: a cyanate ester resin represented by formula; an epoxy resin; an inorganic filler; and a maleimide compound; the content of the inorganic filler being 301 to 700 parts by weight based on 100 parts by weight in total of the cyanate ester resin and the epoxy resin; the content of the maleimide compound being 5 to 75 parts by weight based on 100 parts by weight in total of the cyanate ester resin and the maleimide compound; and wherein the inorganic filler is selected from the group consisting of aluminum hydroxide, heat treated products of aluminum hydroxide, boehmite, metal hydrates of magnesium hydroxide, zinc borate, aluminum oxide, boron nitride, magnesium oxide, aluminum nitride, and silicon nitride; wherein Rs each independently represent a hydrogen atom or a methyl group; and n is an integer of 1 to 50. a cyanate ester resin represented by formula; an epoxy resin; an inorganic filler; and a maleimide compound; the content of the inorganic filler being 301 to 700 parts by weight based on 100 parts by weight in total of the cyanate ester resin and the epoxy resin; the content of the maleimide compound being 5 to 75 parts by weight based on 100 parts by weight in total of the cyanate ester resin and the maleimide compound; and wherein the inorganic filler is selected from the group consisting of aluminum hydroxide, heat treated products of aluminum hydroxide, boehmite, metal hydrates of magnesium hydroxide, zinc borate, aluminum oxide, boron nitride, magnesium oxide, aluminum nitride, and silicon nitride; wherein Rs each independently represent a hydrogen atom or a methyl group; and n is an integer of 1 to 50.
An aerosol provision system for generating an aerosol for inhalation by a user comprising: a housing enclosing at least partially an air channel and an aerosol generating element; a detector configured to detect an instantaneous strength of inhalation by detecting an amount of air flow or a pressure difference in the air channel during an inhalation by the user; a first indicator configured to provide a first indication to the user; and a controller connected to the detector and the first indicator, characterised in that the controller is configured to control the first indicator to generate the first indication to the user during the inhalation, the indication varying during the inhalation based on the instantaneous strength of inhalation detected by the detector. a housing enclosing at least partially an air channel and an aerosol generating element; a detector configured to detect an instantaneous strength of inhalation by detecting an amount of air flow or a pressure difference in the air channel during an inhalation by the user; a first indicator configured to provide a first indication to the user; and a controller connected to the detector and the first indicator, characterised in that the controller is configured to control the first indicator to generate the first indication to the user during the inhalation, the indication varying during the inhalation based on the instantaneous strength of inhalation detected by the detector.
A fluorochrome material for use in therapeutic treatment by administering the fluorochrome material to an individual, externally applying a magnetic field to the individual to guide the fluorochrome material to a target area, and then applying external light to the target area, thereby allowing the fluorochrome material in the target area to become phosphorescent, wherein the fluorochrome material contains a metal-salen complex represented by the following Chemical Formula: N,N'-Bis(salicylidene)ethylenediamine metal, wherein M in the Chemical Formula is Fe and the fluorochrome material has a peak of intensity of phosphorescence at a wavelength around 380 nm.
A drawing process for an arc corner connecting rib of a metal box shell, the drawing process comprising the following steps: preparing a rectangular metal shell whose vertex corner portions are arc corner transition portions; drawing by means of a first metal drawing mould a top face plate of the rectangular metal shell for the first time, so that a plurality of first convex strips are formed in a first area between the two arc corner transition portions of the top face plate; and drawing by means of a second metal drawing mould a side face plate and the arc corner transition portions of the rectangular metal shell obtained after the first-time drawing moulding for the second time, so that a plurality of second convex strips are formed in a second area between the two arc corner transition portions of the side face plate. preparing a rectangular metal shell whose vertex corner portions are arc corner transition portions; drawing by means of a first metal drawing mould a top face plate of the rectangular metal shell for the first time, so that a plurality of first convex strips are formed in a first area between the two arc corner transition portions of the top face plate; and drawing by means of a second metal drawing mould a side face plate and the arc corner transition portions of the rectangular metal shell obtained after the first-time drawing moulding for the second time, so that a plurality of second convex strips are formed in a second area between the two arc corner transition portions of the side face plate.
A data management system comprising: a data acquiring unit configured to acquire measurement data generated by measuring a measurement target from each of a plurality of sensors; a data storage unit configured to store the acquired measurement data; and a data-amount reducing unit configured to delete part of the measurement data acquired from a target sensor based on the measurement data acquired from another sensor among the plurality of sensors to reduce an amount of data to be stored, characterized in that the data management system further comprises: a data predicting unit configured to generate prediction data obtained by predicting measurement data for each of the plurality of sensors by using the measurement data acquired from the another sensor; and a sensor selecting unit configured to select the target sensor for which part of the measurement data is to be deleted based on a difference between the acquired measurement data and the generated prediction data. a data acquiring unit configured to acquire measurement data generated by measuring a measurement target from each of a plurality of sensors; a data storage unit configured to store the acquired measurement data; and a data-amount reducing unit configured to delete part of the measurement data acquired from a target sensor based on the measurement data acquired from another sensor among the plurality of sensors to reduce an amount of data to be stored, characterized in that the data management system further comprises: a data predicting unit configured to generate prediction data obtained by predicting measurement data for each of the plurality of sensors by using the measurement data acquired from the another sensor; and a sensor selecting unit configured to select the target sensor for which part of the measurement data is to be deleted based on a difference between the acquired measurement data and the generated prediction data. a data predicting unit configured to generate prediction data obtained by predicting measurement data for each of the plurality of sensors by using the measurement data acquired from the another sensor; and a sensor selecting unit configured to select the target sensor for which part of the measurement data is to be deleted based on a difference between the acquired measurement data and the generated prediction data.
Method for operating a grenade, wherein a two-part firing pin (26, 55, 67) pretensioned by a spring is activated by releasing a rocker arm, in that the firing pin (26, 55, 67) is tensioned when the rocker arm is held, the tensioned firing pin (26, 55, 67) is fixed by the rocker arm being held and is thereby locked in the tensioned state by a closed coupling (43, 56, 71) between the parts of the firing pin (26, 55, 67), the locking of the tensioned firing pin (26, 55, 67) is removed by releasing the rocker arm and the firing pin (26, 55, 67) thereby activates a fuse of at least one charge causing an optical and/or acoustic effect or a detonation, wherein, when the rocker arm is released, the coupling (43, 56) of the firing pin (26, 55) is automatically released and the spring-tensioned firing pin (26, 55) is thereby triggered to activate the charge, either in that the locking of the tensioned firing pin (26, 55) is automatically released after the rocker arm has been released through automatic opening and separation of the coupling (43, 56) as a consequence of the spring pretensioning of the firing pin (26, 55) and the rocker arm is thereby automatically pivoted by the spring force of the pretensioned spring of the firing pin (26, 55) into a position releasing the coupling (43, 56), or in that a locking of a main part to an extension part of the striking pin is maintained by at least one coupling body until the ignition process is initiated by a spring-pretensioned locking sleeve which surrounds the main part at least in part and allows a relative movement between the main part and the locking sleeve and the spring-pretensioned locking sleeve is held by the rocker arm in a longitudinally non-displaceable manner until the rocker arm for initiating the ignition process is released.
Tap changer for uninterrupted changeover between two winding taps (n, n+1) of a tapped transformer, wherein two load branches are provided in such a form that one load branch is electrically connected with the first winding tap (n) and the other load branch with the second winding tap (n+1), wherein the first load branch has at least one first switching element acting as a main contact and parallel thereto a series connection of a switch-over resistance as well as a second switching element acting as a resistance contact, wherein the second load branch has at least one third switching element acting as a main contact and parallel thereto a series connection of a further switch-over resistance as well as a fourth switching element acting as a resistance contact and wherein the first and second load branches are connected each at one side by a common load diverter, characterised in that additionally provided in the first load branch is a first mechanical switch-over contact by which the side, which is not connected with the load diverter, of the parallel connection of the first load branch (MSV1, R1, TTV1) is selectably connectible with the first winding tap (n) or the second winding tap (n+1) and additionally provided in the second load branch is a second mechanical switch-over contact by which the side, which is not connected with the load diverter, of the parallel connection of the second load branch (MSV2, R2, TTV2) is similarly selectably connectible with the first winding tap (n) or the second winding tap (n+1).
A multi-layer sliding bearing element made from a composite material comprising a supporting metal layer and a further layer, in particular a sliding layer, as well as optionally an intermediate layer between the supporting metal layer and the further layer, wherein the further layer is formed of a cast alloy of a lead-free copper base alloy, in which sulfide precipitates are contained, characterized in that the copper base alloy contains between 0.1 wt.% and 3 wt.% sulfur, between 0.01 wt.% and 4 wt.% iron, between 0 wt.%, in particular 0.001 wt.%, and 2 wt.% phosphorus, at least one element from a first group consisting of zinc, tin, aluminum, manganese, nickel, silicon, chromium, indium of in total between 0.1 wt.% and 49 wt.%, wherein the proportion of zinc amounts to between 0 wt.% and 45 wt.%, the proportion of tin amounts to between 0 wt.% and 40 wt.%, the proportion of aluminum amounts to between 0 wt.% and 15 wt.%, the proportion of manganese amounts to between 0 wt.% and 10 wt.%, the proportion of nickel amounts to between 0 wt.% and 10 wt.%, the proportion of silicon amounts to between 0.01 wt.% and 7 wt.%, the proportion of chromium amounts to between 0 wt.% and 2 wt.%, and the proportion of indium amounts to between 0 wt.% and 10 wt.%, and at least one element from a second group consisting of silver, magnesium, cobalt, titanium, zirconium, arsenic, lithium, yttrium, calcium, vanadium, molybdenum, tungsten, antimony, selenium, tellurium, bismuth, niobium, palladium each to a proportion of between 0 wt.% and 1.5 wt.%, wherein the summary proportion of the elements of the second group amounts to between 0 wt.% and 2 wt.%, and the balance adding up to 100 wt.% being constituted by copper and impurities originating from the production of the elements.
A method for producing a fertilizer comprising: decomposing one or more biopolymers in an initial water substratum to produce hydro lyzates thereof, wherein the initial water substratum includes a plurality of raw materials dispersed within a liquid; and performing a polymerization of the hydrolyzates to produce a co-polymer of fulvic acid and poly-metallic humates (CPFAPH), wherein the decomposing stage further comprises: stirring the biopolymers and initial water substratum; and treating the initial water substratum with an oxygen-containing gas. decomposing one or more biopolymers in an initial water substratum to produce hydro lyzates thereof, wherein the initial water substratum includes a plurality of raw materials dispersed within a liquid; and performing a polymerization of the hydrolyzates to produce a co-polymer of fulvic acid and poly-metallic humates (CPFAPH), wherein the decomposing stage further comprises: stirring the biopolymers and initial water substratum; and treating the initial water substratum with an oxygen-containing gas.