mhurhangee/ep-ind-claims huggingface dataset:
A process for producing cumene comprising: (a) supplying benzene and a C 3 alkylating agent comprising isopropanol to an alkylation zone comprising a molecular sieve alkylation catalyst under alkylation conditions such that the isopropanol reacts with the benzene to produce a reaction product comprising cumene; (b) ceasing the supply of benzene and C 3 alkylating agent to the alkylation zone; (c) supplying a gaseous stripping agent comprising at least one of N 2, H 2, alkane, He, Ar, CO, and CO 2 to the molecular sieve alkylation catalyst under conditions to remove nitrogenous impurities deposited on the catalyst during (a); and (d) reinitiating the supply of benzene and C 3 alkylating agent to the alkylation zone; wherein said conditions in (c) comprise a temperature in the range from 100 to 600°C and a pressure in the range from 120 kPa-a to 2170 kPa-a, and wherein the alkylation catalyst comprises at least one molecular sieve of the MCM-22 family. (a) supplying benzene and a C 3 alkylating agent comprising isopropanol to an alkylation zone comprising a molecular sieve alkylation catalyst under alkylation conditions such that the isopropanol reacts with the benzene to produce a reaction product comprising cumene; (b) ceasing the supply of benzene and C 3 alkylating agent to the alkylation zone; (c) supplying a gaseous stripping agent comprising at least one of N 2, H 2, alkane, He, Ar, CO, and CO 2 to the molecular sieve alkylation catalyst under conditions to remove nitrogenous impurities deposited on the catalyst during (a); and (d) reinitiating the supply of benzene and C 3 alkylating agent to the alkylation zone;
A method for automatically decelerating an aircraft on a runway, the method comprising: determining whether the aircraft can decelerate to a selected velocity prior to reaching a target location along the runway; and in response to determining that the aircraft can decelerate to the selected velocity prior to reaching the target location, automatically decelerating the aircraft such that the aircraft reaches the selected velocity at the target location; the method further comprising: continuously adjusting a target deceleration required to decelerate the aircraft to meet the selected velocity at the target location, wherein the target deceleration is calculated from the selected velocity, a current distance between the current location of the aircraft and the target location, and a current velocity of the aircraft; passively decelerating the aircraft while the target deceleration is below a minimum deceleration threshold of the aircraft; and responsive to the target deceleration meeting or exceeding the minimum deceleration threshold of the aircraft, applying a brake system command to decelerate the aircraft at the target deceleration such that the aircraft decelerates to meet the selected velocity at the target location. determining whether the aircraft can decelerate to a selected velocity prior to reaching a target location along the runway; and in response to determining that the aircraft can decelerate to the selected velocity prior to reaching the target location, automatically decelerating the aircraft such that the aircraft reaches the selected velocity at the target location; the method further comprising: continuously adjusting a target deceleration required to decelerate the aircraft to meet the selected velocity at the target location, wherein the target deceleration is calculated from the selected velocity, a current distance between the current location of the aircraft and the target location, and a current velocity of the aircraft; passively decelerating the aircraft while the target deceleration is below a minimum deceleration threshold of the aircraft; and responsive to the target deceleration meeting or exceeding the minimum deceleration threshold of the aircraft, applying a brake system command to decelerate the aircraft at the target deceleration such that the aircraft decelerates to meet the selected velocity at the target location. continuously adjusting a target deceleration required to decelerate the aircraft to meet the selected velocity at the target location, wherein the target deceleration is calculated from the selected velocity, a current distance between the current location of the aircraft and the target location, and a current velocity of the aircraft; passively decelerating the aircraft while the target deceleration is below a minimum deceleration threshold of the aircraft; and responsive to the target deceleration meeting or exceeding the minimum deceleration threshold of the aircraft, applying a brake system command to decelerate the aircraft at the target deceleration such that the aircraft decelerates to meet the selected velocity at the target location.
A surgical drape comprising: a first drape section including: an exterior surface adjacent to a sterile field for performing a surgical procedure; an interior surface forming a cavity for receiving a non-sterile portion of a robotic surgical system; a first vent through the interior and exterior surfaces in communication with the sterile field; and a second vent through the interior and exterior surfaces in communication with the sterile field and spaced apart from the first vent, wherein the interior and exterior surfaces include a window configured to be positioned adjacent to a monitor screen, the window including a static charge; and a second drape section connected to the first drape section and including an instrument sterile adaptor for engaging a surgical tool and another non-sterile portion of the robotic surgical system, the sterile adaptor configured to transfer signals between the surgical tool and the other non-sterile portion of the robotic surgical system. a first drape section including: an exterior surface adjacent to a sterile field for performing a surgical procedure; an interior surface forming a cavity for receiving a non-sterile portion of a robotic surgical system; a first vent through the interior and exterior surfaces in communication with the sterile field; and a second vent through the interior and exterior surfaces in communication with the sterile field and spaced apart from the first vent, wherein the interior and exterior surfaces include a window configured to be positioned adjacent to a monitor screen, the window including a static charge; and an exterior surface adjacent to a sterile field for performing a surgical procedure; an interior surface forming a cavity for receiving a non-sterile portion of a robotic surgical system; a first vent through the interior and exterior surfaces in communication with the sterile field; and a second vent through the interior and exterior surfaces in communication with the sterile field and spaced apart from the first vent, wherein the interior and exterior surfaces include a window configured to be positioned adjacent to a monitor screen, the window including a static charge; and a second drape section connected to the first drape section and including an instrument sterile adaptor for engaging a surgical tool and another non-sterile portion of the robotic surgical system, the sterile adaptor configured to transfer signals between the surgical tool and the other non-sterile portion of the robotic surgical system.
Furnace, in particular a continuous furnace, for controlling the temperature of at least one substrate, the furnace comprising a housing which comprises an intake opening and an outtake opening, wherein a temperature controlled section is formed between the intake opening and the outtake opening, a carrier element arrangement comprising at least one carrier element for carrying the at least one substrate, wherein the carrier element arrangement comprises a first end and a second end, wherein the carrier element arrangement is formed and arrangable within the housing such that the first end is located within the intake opening and the second end is located within the outtake opening (104, wherein the at least one carrier element comprises a first edge section, a second edge section and a recess within the substrate is carriable, wherein the recess is formed along the transport direction between the first edge section and the second edge section, wherein the first edge section forms the first end of the carrier element arrangement, wherein the second edge section forms the second end of the carrier element arrangement, wherein the recess of the at least one carrier element of the carrier element arrangement is located within the temperature-controlled section, wherein the first end and the second end of the carrier element arrangement are located at the respective intake opening and the respective outtake opening, wherein the first end is dimensioned in such a way that the first end may form a loose fit connection with the intake opening of the housing, so that no or only a small gap between the first end and the intake opening exists and wherein the second end is dimensioned in such a way that the second end may form a loose fit connection with the outtake opening of the housing, so that no or only a small gap between the second end and the intake opening exists.
A computer-implemented method comprising, by an on-board vehicle computer system (100; 300; 400) of a vehicle: obtaining a first vehicle speed limiter, VSL, distance value for the vehicle; storing the first VSL distance value in a memory (112; 312) of a first electronic control unit, ECU, (110; 310) of the on-board vehicle computer system; storing a backup value of the first VSL distance value in a memory (122; 322) of a distinct second ECU (120; 320) of the on-board vehicle computer system, the second ECU being communicatively coupled to the first ECU; reading, by the second ECU, data obtained from the first ECU (110; 310), wherein the data includes a new VSL distance value and diagnostic information; characterised by processing, by the second ECU, the diagnostic information to determine whether the first ECU (110; 310) is operating normally; and determining, by the second ECU, whether to update the stored backup value based at least in part on whether the first ECU (110; 310) is operating normally. obtaining a first vehicle speed limiter, VSL, distance value for the vehicle; storing the first VSL distance value in a memory (112; 312) of a first electronic control unit, ECU, (110; 310) of the on-board vehicle computer system; storing a backup value of the first VSL distance value in a memory (122; 322) of a distinct second ECU (120; 320) of the on-board vehicle computer system, the second ECU being communicatively coupled to the first ECU; reading, by the second ECU, data obtained from the first ECU (110; 310), wherein the data includes a new VSL distance value and diagnostic information; characterised by processing, by the second ECU, the diagnostic information to determine whether the first ECU (110; 310) is operating normally; and determining, by the second ECU, whether to update the stored backup value based at least in part on whether the first ECU (110; 310) is operating normally.
A reclaiming device comprising: a reclaimer configured to introduce and store a part of a regenerated absorbent; a first alkaline agent supply section configured to supply an alkaline agent to the reclaimer; a heating section configured to heat the absorbent stored in the reclaimer and to which the alkaline agent has been mixed to obtain recovered vapor; a vapor cooler configured to cool the recovered vapor discharged from the reclaimer through a vapor line (L 12); a first gas-liquid separator configured to separate a coexisting substance entrained in the cooled recovered vapor into recovered absorption agent vapor and a liquid coexisting substance by gas-liquid separation; a cooler configured to cool the separated recovered absorption agent vapor; a second gas-liquid separator configured to separate the recovered absorption agent vapor after cooling into a low-boiling point substance flue gas and a recovered absorbent by gas-liquid separation; a heat exchanger configured to perform heat exchange of the liquid coexisting substance separated in the first gas-liquid separator with vapor condensed water from vapor supplied to the reclaimer to increase a temperature; a CO 2 absorber configured to bring the liquid coexisting substance after increase in the temperature and a CO 2 gas in contact; a second alkaline agent supply section configured to supply the alkaline agent to the liquid coexisting substance after absorption of CO 2; and a distiller configured to distill the liquid coexisting substance to which the alkaline agent has been supplied while introducing the CO 2 gas thereinto. a reclaimer configured to introduce and store a part of a regenerated absorbent; a first alkaline agent supply section configured to supply an alkaline agent to the reclaimer; a heating section configured to heat the absorbent stored in the reclaimer and to which the alkaline agent has been mixed to obtain recovered vapor; a vapor cooler configured to cool the recovered vapor discharged from the reclaimer through a vapor line (L 12); a first gas-liquid separator configured to separate a coexisting substance entrained in the cooled recovered vapor into recovered absorption agent vapor and a liquid coexisting substance by gas-liquid separation; a cooler configured to cool the separated recovered absorption agent vapor; a second gas-liquid separator configured to separate the recovered absorption agent vapor after cooling into a low-boiling point substance flue gas and a recovered absorbent by gas-liquid separation; a heat exchanger configured to perform heat exchange of the liquid coexisting substance separated in the first gas-liquid separator with vapor condensed water from vapor supplied to the reclaimer to increase a temperature; a CO 2 absorber configured to bring the liquid coexisting substance after increase in the temperature and a CO 2 gas in contact; a second alkaline agent supply section configured to supply the alkaline agent to the liquid coexisting substance after absorption of CO 2; and a distiller configured to distill the liquid coexisting substance to which the alkaline agent has been supplied while introducing the CO 2 gas thereinto.
A lighter comprising: a housing having a supply of fuel; a valve operable to release the fuel; an ignition mechanism (26, 426, 526, 626) operable to create a spark; an actuating member (25, 225, 325, 425, 525) extending from the housing, the actuating member (25, 225, 325, 425, 525) being movable to selectively perform at least one step in igniting the fuel; and an inhibiting member (205, 305, 405, 505, 605) extending from the housing, characterized in that the inhibiting member (205, 305, 405, 505, 605) is biased to a first position permitting the actuating member (25, 225, 325, 425, 525) to perform the at least one step in igniting the fuel; in that the actuating member (25, 225, 325, 425, 525) is movable along a first axis and the inhibiting member is movable along a second axis that is substantially parallel to the first axis, and in that moving the inhibiting member (205, 305, 405, 505, 605) a predetermined distance to a second position along the second axis resists the actuating member from performing the at least one step in igniting the fuel. a housing having a supply of fuel; a valve operable to release the fuel; an ignition mechanism (26, 426, 526, 626) operable to create a spark; an actuating member (25, 225, 325, 425, 525) extending from the housing, the actuating member (25, 225, 325, 425, 525) being movable to selectively perform at least one step in igniting the fuel; and an inhibiting member (205, 305, 405, 505, 605) extending from the housing, characterized in that the inhibiting member (205, 305, 405, 505, 605) is biased to a first position permitting the actuating member (25, 225, 325, 425, 525) to perform the at least one step in igniting the fuel; in that the actuating member (25, 225, 325, 425, 525) is movable along a first axis and the inhibiting member is movable along a second axis that is substantially parallel to the first axis, and in that moving the inhibiting member (205, 305, 405, 505, 605) a predetermined distance to a second position along the second axis resists the actuating member from performing the at least one step in igniting the fuel.
Process for coating thermally and chemically stressed components of a fluidized-bed reactor for producing high-purity granular polysilicon, wherein the fluidized-bed reactor which is free of bulk material is flushed with a reactive gas mixture at an average tube wall temperature of from 600 to 1400°C for a period of from 1 hour to 8 days and at a pressure of from 1 to 15 bar (bar abs) and the surfaces of the reactor which have a temperature of more than 600°C are thereby provided with an in-situ coating of Si and/or Si 3 N 4 by means of a CVD process.
An anvil assembly comprising: an anvil center rod assembly; a head assembly pivotally secured to the anvil center rod assembly; and a sleeve member slidably disposed about the anvil center rod assembly and configured to slide relative to the anvil center rod assembly as the head assembly pivots relative to the anvil center rod assembly, wherein the sleeve member includes a sleeve body disposed about the anvil center rod assembly, the sleeve body including a plurality of teeth for engaging the head assembly, wherein the head assembly includes a housing and a post extending proximally from the housing, the post includes a plurality of teeth configured to engage the plurality of teeth formed on the sleeve body while the head assembly pivots relative to the anvil center rod assembly. an anvil center rod assembly; a head assembly pivotally secured to the anvil center rod assembly; and a sleeve member slidably disposed about the anvil center rod assembly and configured to slide relative to the anvil center rod assembly as the head assembly pivots relative to the anvil center rod assembly, wherein the sleeve member includes a sleeve body disposed about the anvil center rod assembly, the sleeve body including a plurality of teeth for engaging the head assembly, wherein the head assembly includes a housing and a post extending proximally from the housing, the post includes a plurality of teeth configured to engage the plurality of teeth formed on the sleeve body while the head assembly pivots relative to the anvil center rod assembly.
Housing for accommodating electronic components, wherein the housing has a first and a second housing part (10, 20), which first and second housing parts form a housing upper part and a housing lower part with a respective coupling region (11, 21) and which first and second housing parts can be coupled to one another by means of their respective coupling region, wherein the housing parts each have a housing base area and, in an assembled state, form an interior which is designed for bordering the components in a space-saving manner, wherein the housing has accommodation means (14a, 24a) for defined arrangement of the component, wherein each housing part is provided for accommodating at least one component, wherein the accommodation means (14a, 24a) are provided in each housing part, characterized in that each housing part has, in the coupling region, a cutout (13, 23) in the vertical outer wall of the housing part, which cutout, together with the coupling region of an adjacent housing part, forms a respective bushing from the inside to the outside for a plug in an assembled state of the housing, and the cutout (13, 23) is provided for a plug of the component in the second housing part, which component is to be provided in the first housing part.
Cosmetic cleansing preparation comprising, based on the total weight of the cleansing preparation, a) Sodium Lauroyl Methyl Isethionate, b) Sodium Methyl Cocoyl Taurate, and c) cocamidopropyl betaine, characterized in that cocamidopropyl betaine is present in a proportion from 3.5% by weight to 6% by weight and water is present in a proportion from 60% by weight to 94% by weight. a) Sodium Lauroyl Methyl Isethionate, b) Sodium Methyl Cocoyl Taurate, and c) cocamidopropyl betaine,
An austenitic stainless steel weld metal having a chemical composition consisting of, by mass%, C: 0.05 to 0.11%, Si: 0.10 to 0.50%, Mn: 1.0 to 2.5%, P: 0.035% or less, S: 0.0030% or less, Co: 0.02 to 1.00%, Ni: 9.0 to 11.5%, Cr: 17.0 to 21.0%, Nb: 0.60 to 0.90%, Ta: 0.001 to 0.100%, N: 0.01 to 0.15%, Al: 0.030% or less, O: 0.020% or less, V: 0 to 0.10%, Ti: 0 to 0.10%, W: 0 to 0.50%, Mo: 0 to 0.50%, Cu: 0 to 0.50%, B: 0 to 0.005%, Ca: 0 to 0.010%, Mg: 0 to 0.010%, REM: 0 to 0.10%, and the balance: Fe and impurities, and satisfying formula (i) below: Nb − 7.8 × C ≤ 0.25 where, each symbol of an element in the above formulas represents a content (mass%) of a corresponding element contained in the steel. C: 0.05 to 0.11%, Si: 0.10 to 0.50%, Mn: 1.0 to 2.5%, P: 0.035% or less, S: 0.0030% or less, Co: 0.02 to 1.00%, Ni: 9.0 to 11.5%, Cr: 17.0 to 21.0%, Nb: 0.60 to 0.90%, Ta: 0.001 to 0.100%, N: 0.01 to 0.15%, Al: 0.030% or less, O: 0.020% or less, V: 0 to 0.10%, Ti: 0 to 0.10%, W: 0 to 0.50%, Mo: 0 to 0.50%, Cu: 0 to 0.50%, B: 0 to 0.005%, Ca: 0 to 0.010%, Mg: 0 to 0.010%, REM: 0 to 0.10%, and the balance: Fe and impurities, and satisfying formula (i) below: Nb − 7.8 × C ≤ 0.25 where, each symbol of an element in the above formulas represents a content (mass%) of a corresponding element contained in the steel.
A method of providing an optical filter comprising: forming a layer stack on a substrate to include pairs of two-film dielectric layers and metallic layers, including defining each said pair by: forming an indium-based transparent dielectric film as a first film of said dielectric layers, said transparent dielectric film having a refractive index of at least 1.1; forming a zinc-based film as a second film of said dielectric layers, said zinc-based film having a zinc content of at least 80 percent and having a thickness of at least 15 nm, said zinc-based film being in contact with the indium-based transparent dielectric film; and forming a silver-based film as said metallic layer, said silver-based film being in contact with said zinc-based film. forming a layer stack on a substrate to include pairs of two-film dielectric layers and metallic layers, including defining each said pair by: forming an indium-based transparent dielectric film as a first film of said dielectric layers, said transparent dielectric film having a refractive index of at least 1.1; forming a zinc-based film as a second film of said dielectric layers, said zinc-based film having a zinc content of at least 80 percent and having a thickness of at least 15 nm, said zinc-based film being in contact with the indium-based transparent dielectric film; and forming a silver-based film as said metallic layer, said silver-based film being in contact with said zinc-based film. forming an indium-based transparent dielectric film as a first film of said dielectric layers, said transparent dielectric film having a refractive index of at least 1.1; forming a zinc-based film as a second film of said dielectric layers, said zinc-based film having a zinc content of at least 80 percent and having a thickness of at least 15 nm, said zinc-based film being in contact with the indium-based transparent dielectric film; and forming a silver-based film as said metallic layer, said silver-based film being in contact with said zinc-based film.