mhurhangee/ep-ind-claims huggingface dataset:
A measurement method, of using a measurement system in a photolithography process to measure a plurality of first marks (Mxi) and a plurality of second marks (Myi) different from the first marks as measurement objects formed on a prescribed substrate, comprising: a first process of setting a measurement condition for the measurement system to a first condition when measuring the first marks among the marks which are the measurement objects on the prescribed substrate; a second process, after measuring all of the first marks on the prescribed substrate under the first condition, of switching the measurement condition from the first condition and setting a second condition; and a third process of measuring the second marks among the marks which are the measurement objects on the prescribed substrate, under the second condition, wherein the measurement condition comprises at least one among an illumination condition for an illumination beam which illuminates the marks, and a light-receiving condition when receiving a beam arising from the marks illuminated by the illumination beam, and wherein the first marks are marks formed to measure positions on the prescribed substrate in a prescribed direction in a two-dimensional plane, and the second marks are marks formed to measure positions on the prescribed substrate in the direction perpendicular to the prescribed direction in the two-dimensional plane. a first process of setting a measurement condition for the measurement system to a first condition when measuring the first marks among the marks which are the measurement objects on the prescribed substrate; a second process, after measuring all of the first marks on the prescribed substrate under the first condition, of switching the measurement condition from the first condition and setting a second condition; and a third process of measuring the second marks among the marks which are the measurement objects on the prescribed substrate, under the second condition, wherein the measurement condition comprises at least one among an illumination condition for an illumination beam which illuminates the marks, and a light-receiving condition when receiving a beam arising from the marks illuminated by the illumination beam, and wherein the first marks are marks formed to measure positions on the prescribed substrate in a prescribed direction in a two-dimensional plane, and the second marks are marks formed to measure positions on the prescribed substrate in the direction perpendicular to the prescribed direction in the two-dimensional plane.
An airship comprising: a hull configured to contain a gas; and at least one propulsion assembly coupled to the hull and including a propulsion device; characterised by a longitudinally-oriented aerodynamic component disposed at a central portion of a top surface of the hull, the longitudinally-oriented aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one longitudinally-oriented aerodynamic component is configured to direct airflow around the airship; and two transversely-oriented aerodynamic components disposed fore and aft, respectively, of the longitudinally-oriented aerodynamic component, the transversely-oriented aerodynamic components including a plurality of fairing structures including one or more slats configured to direct airflow. a hull configured to contain a gas; and at least one propulsion assembly coupled to the hull and including a propulsion device; characterised by a longitudinally-oriented aerodynamic component disposed at a central portion of a top surface of the hull, the longitudinally-oriented aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one longitudinally-oriented aerodynamic component is configured to direct airflow around the airship; and two transversely-oriented aerodynamic components disposed fore and aft, respectively, of the longitudinally-oriented aerodynamic component, the transversely-oriented aerodynamic components including a plurality of fairing structures including one or more slats configured to direct airflow.
A magnetic sensor arrangement for determining an operating state of a magnetic sensor, the magnetic sensor arrangement comprising a magnetic sensor being adapted to provide an output voltage being modulated by a movement of an encoder component, the encoder component providing a periodic changing magnetic field being generated due to a relative movement of the encoder component in relation to the magnetic sensor arrangement, and a sensor control unit being coupled to the magnetic sensor and comprising a comparator for sensing the encoder period based on the sensor output voltage and a counter for counting the duration of the encoder period, the sensor control unit being adapted to receive the output voltage signal of the magnetic sensor, wherein the output voltage signal is a function of time, to determine a momentary value of the duration of the encoder period based on an output signal of the counter and based on the output voltage signal; to determine at least one point of sampling based on the determined momentary value of the duration of the encoder period and to sample the output voltage signal to the at least one determined point of sampling, to change the reference quantity from time to rotational angle by mapping the output voltage signal to a converted signal being a function of rotational angle such that spectral signal power portions of the converted signal are associated with orders of the encoder rotational speed, to determine a first signal power being indicative for a first portion of orders of the encoder rotational speed, to determine a second signal power being indicative for a second portion of orders of the encoder rotational speed, wherein determining the first signal power and the second signal power comprises multiplying the sampling values with complex harmonic coefficients, and accumulating the multiplied values for a selected time period, to determine a ratio of the first signal power and the second signal power, the ratio being indicative for a signal distortion of the output voltage signal, and to determine the operating state of the magnetic sensor based on the determined ratio, wherein determining the ratio of the first signal power and the second signal power corresponds to determining a ratio of subtotals of the results of the accumulation.
Epitaxial deposition reactor comprising at least one susceptor; wherein the susceptor comprises a disc-shaped portion with an upper zone and a lower zone and a cylindrical or conical portion with an upper zone and a lower zone, said disc-shaped portion being adapted to directly or indirectly support one or more substrates on said upper zone; wherein said disc-shaped portion and said cylindrical or conical portion are coaxial; wherein the lower zone of said disc-shaped portion and the upper zone of said cylindrical or conical portion are joined together directly or through a possible intermediate portion so that heat can flow by conduction from said cylindrical or conical portion to said disc-shaped portion; wherein said disc-shaped portion and said cylindrical or conical portion and said possible intermediate portion are made entirely of a material that is a heat conductor, preferably graphite; wherein the epitaxial deposition reactor comprises further a first inductor adapted to directly heat said disc-shaped portion by electromagnetic induction, a second inductor adapted to directly heat said cylindrical or conical portion by electromagnetic induction and indirectly heat said disc-shaped portion, and means for supplying power to said first and second inductors (4, 5); wherein said first inductor is flat; wherein said second inductor is cylindrical or conical; wherein said first and second inductors (4, 5) are adapted to be power-supplied by said means independently at different frequencies. wherein the susceptor comprises a disc-shaped portion with an upper zone and a lower zone and a cylindrical or conical portion with an upper zone and a lower zone, said disc-shaped portion being adapted to directly or indirectly support one or more substrates on said upper zone; wherein said disc-shaped portion and said cylindrical or conical portion are coaxial; wherein the lower zone of said disc-shaped portion and the upper zone of said cylindrical or conical portion are joined together directly or through a possible intermediate portion so that heat can flow by conduction from said cylindrical or conical portion to said disc-shaped portion; wherein said disc-shaped portion and said cylindrical or conical portion and said possible intermediate portion are made entirely of a material that is a heat conductor, preferably graphite; wherein the epitaxial deposition reactor comprises further a first inductor adapted to directly heat said disc-shaped portion by electromagnetic induction, a second inductor adapted to directly heat said cylindrical or conical portion by electromagnetic induction and indirectly heat said disc-shaped portion, and means for supplying power to said first and second inductors (4, 5); wherein said first inductor is flat; wherein said second inductor is cylindrical or conical; wherein said first and second inductors (4, 5) are adapted to be power-supplied by said means independently at different frequencies.
A process for purifying methyl methacrylate; said process comprising: (a) feeding a reaction product mixture comprising methanol, methyl methacrylate and alkali metal methacrylates, methacrolein, water and heavy byproducts to a first distillation column having at least 15 trays; wherein said reaction product mixture and a C 6 -C 7 hydrocarbon enter the first distillation column above the middle of the distillation column; (b) removing a first overhead stream comprising C 6 -C 7 hydrocarbon, methacrolein, methanol, water and methyl methacrylate; (c) removing a first bottoms stream comprising water, methyl methacrylate and alkali metal methacrylates and heavy byproducts; (d) feeding the first overhead stream to a first water separator to produce (i) a first organic phase which is returned to the first distillation column and (ii) a first aqueous phase which enters a methanol drying distillation column which produces a second overhead stream rich in methanol and a second bottoms stream which is rich in water, and at least a portion of said second bottoms stream is fed to the first water separator; (e) feeding the first bottoms stream to a second water separator to produce (i) a second aqueous phase which is fed to an MMA stripper distillation column which produces a third overhead stream rich in water and a third bottoms stream comprising water and alkali metal methacrylates and (ii) a second organic phase; (f) combining the second organic phase and the second bottoms stream into a third water separator which produces (i) a third organic phase which enters an MMA drying distillation column which produces a fourth overhead stream and a fourth bottoms stream, and (ii) a third aqueous phase; and (g) feeding the fourth bottoms stream to an MMA product distillation column which produces an MMA product stream and a bottoms stream.
A microchannel plate comprising: a. a substrate comprising a plate of glass fibers defining a plurality of pores (104; 180) extending from a top surface of the substrate to a bottom surface of the substrate, the plurality of pores (104; 180) having reduced lead-glass on an outer surface that forms a first emissive layer; b. a top electrode positioned on the top surface of the substrate; c. a bottom electrode positioned on the bottom surface of the substrate; d. a barrier layer formed on top of the first emissive layer; and e. a second emissive layer formed over the barrier layer, the second emissive layer having a different material composition than the first emissive layer and being configured to achieve at least one of an increase in secondary electron emission efficiency and a decrease in gain degradation as a function of time compared to the microchannel plate without the second emissive layer; wherein: the second emissive layer is formed with atomic layer deposition; and the barrier layer forms a barrier between the first emissive layer and the second emissive layer. a. a substrate comprising a plate of glass fibers defining a plurality of pores (104; 180) extending from a top surface of the substrate to a bottom surface of the substrate, the plurality of pores (104; 180) having reduced lead-glass on an outer surface that forms a first emissive layer; b. a top electrode positioned on the top surface of the substrate; c. a bottom electrode positioned on the bottom surface of the substrate; d. a barrier layer formed on top of the first emissive layer; and e. a second emissive layer formed over the barrier layer, the second emissive layer having a different material composition than the first emissive layer and being configured to achieve at least one of an increase in secondary electron emission efficiency and a decrease in gain degradation as a function of time compared to the microchannel plate without the second emissive layer;
A high power output transformer, comprising a primary and a secondary in galvanic isolation forming a flyback converter, wherein: - the primary comprises at least one primary winding having at least two primary turns and a primary rectifier comprising a junction diode circuit; - the secondary comprises at least one secondary winding having at least one secondary turn; and - the flyback converter comprises at the primary at least one metal-oxide-semiconductor field-effect transistor, MOSFET,, notably a Silicon Carbide MOSFET, and at the secondary at least one Silicon Carbide diode. - the primary comprises at least one primary winding having at least two primary turns and a primary rectifier comprising a junction diode circuit; - the secondary comprises at least one secondary winding having at least one secondary turn; and - the flyback converter comprises at the primary at least one metal-oxide-semiconductor field-effect transistor, MOSFET,, notably a Silicon Carbide MOSFET, and at the secondary at least one Silicon Carbide diode.
A direct injection diesel engine including a cylinder block defining at least one cylinder which is closed by a cylinder head and reciprocably receives a respective piston, the piston defining a combustion chamber comprising a recess (8, 10) formed in the piston crown, the recess being defined by a base and a side wall (13, 14), a substantially conical or frusto-conical projection upstanding from the base, the recess including a lower toroidal portion furthest from the piston crown and an upper portion closest to the piston crown whose diameter increases towards the piston crown, the upper and lower portions being separated by an annular lip of arcuate shape in axial cross-section extending into the recess, the maximum depth of the recess from the base to the plane of the piston crown being between 13 and 22% of the diameter of the piston, the cylinder head carrying a fuel injector which is situated substantially on the cylinder axis and includes a plurality of fuel injection orifices, the recess in the piston crown being rotationally symmetrical about the axis of the piston in axial cross section, the cylinder communicating with two inlet valves and two exhaust valves in the cylinder head, the inlet valves being of the type arranged to induce swirl of the inflowing air in the cylinder substantially about the cylinder axis, characterised in that the diameter of the upper portion closest to the piston crown increases progressively towards the piston crown, that the included angle of the conical or frusto-conical projection is between 104° and 108°, that the diameter of the lip is between 54 and 59% of the diameter of the piston, the diameter of the upper portion of the recess increasing from 54 to 59% of the diameter of the piston at the line of minimum diameter of the lip to between 72 and 76% of the diameter of the piston at the line where the side wall of the recess intersects the plane of the piston crown, that the conical or frusto-conical projection merges with the base along a circular line whose diameter is between 38 and 44% of the diameter of the piston, that the line (h) of minimum diameter of the lip is situated at a distance of between 5 and 10% of the diameter of the piston from the plane of the piston crown and that the fuel injection orifices are so arranged that the fuel jets through them extend at an angle which diverges from the surface of the projection by 15 to 19°, whereby the fuel jets impinge firstly on the arcuate side wall of the lower portion of the recess.
A pharmaceutical product comprising a) as a first component a pharmaceutical composition comprising as an active ingredient a therapeutically effective amount of 4-{[(2R,3S,4R,5S)-4-(4-Chloro-2-fluoro-phenyl)-3-(3-chloro-2-fluoro-phenyl)-4-cyano-5-(2,2-dimethyl-propyl)-pyrrolidine-2-carbonyl]-amino}-3-methoxy-benzoic acid (Compound A) or a pharmaceutically acceptable salt, ester of said compound; b) a second component comprising a pharmaceutical composition comprising a therapeutically effective amount of capecitabine; and c) a third component comprising a pharmaceutical composition comprising a therapeutically effective amount of oxaliplatin for use in the combined, sequential or simultaneous, treatment of cancer, in particular solid tumors such as colon, colorectal, breast and lung cancer.
A mobility management method, applied to a scenario in which a first terminal device moves, and comprising: determining, by a control plane network element (1300, 1600), a changed media access control address, MAC, address of the first terminal device (1400, 1700) after the first terminal device moves; determining, by the control plane network element (1300, 1600), at least one second terminal device (1500, 1800) that belongs to a same terminal device group as the first terminal device (1400, 1700), wherein the first terminal device (1400, 1700) is a terminal device whose address changes after the movement, and the at least one second terminal device (1500, 1800) is a terminal device other than the first terminal device (1400, 1700) in the terminal device group; and notifying, by the control plane network element (1300, 1600), the first terminal device (1400, 1700) and the at least one second terminal device (1500, 1800) to update to the changed MAC address of the first terminal device (1400, 1700). determining, by a control plane network element (1300, 1600), a changed media access control address, MAC, address of the first terminal device (1400, 1700) after the first terminal device moves; determining, by the control plane network element (1300, 1600), at least one second terminal device (1500, 1800) that belongs to a same terminal device group as the first terminal device (1400, 1700), wherein the first terminal device (1400, 1700) is a terminal device whose address changes after the movement, and the at least one second terminal device (1500, 1800) is a terminal device other than the first terminal device (1400, 1700) in the terminal device group; and notifying, by the control plane network element (1300, 1600), the first terminal device (1400, 1700) and the at least one second terminal device (1500, 1800) to update to the changed MAC address of the first terminal device (1400, 1700).
A lock plates assortment for a blade arrangement of a gas turbine, with a plurality of different lock plates (10, 20, 30), the lock plates having a first flange (11, 21, 31), a second flange (12,22, 32) and a connecting bridge (13, 23, 33) between the first and the second flange, and different lock plates respectively having different geometrical coding, characterized in that the first flange (11, 21, 31) and/or the second flange (12, 22, 32) of the lock plates (10, 20, 30) has a coding area (15, 25, 35), wherein the geometrical coding of the lock plates is arranged in the coding area and wherein the coding area (15, 25, 35) is arranged on a flange surface facing away from the connecting bridge and/or on an edge that connects the surface facing away to the surface facing the connecting bridge.
Coolable gas turbine compressor rotor with a multiplicity of welded-together rotor disks (3a, 3b, 4, 5), wherein each rotor disk (3a, 3b, 4, 5) extends over at least three blade stages and of which at least two rotor disks (3a, 3b) are arranged axially next to each other and at the last and second from last point of the rotor in the flow direction, characterized in that the last rotor disk in the flow direction and the second from last rotor disk in the flow direction have, on the facing side, an annular recess in each case which extends around the rotational axis of the disks, wherein the axially facing recesses form an annulus (H") between the last rotor disk and the second from last rotor disk, and the last rotor disk in the flow direction and the second from last rotor disk in the flow direction have a central region which encompasses the rotational axis of the rotor and extends from the rotational axis radially outward to the annulus (H"), and the last and second from last rotor disks (3a, 3b) have an in each case radially outer region which encompasses the radially outer surface of the rotor and extends radially inward to the annulus (H"), and for discharging heat from the central region of the last two rotor disks (3a, 3b) in the flow direction, the last two rotor disks (3a, 3b) in the flow direction are abutment-joined together in their central region and are welded together in their radially outer region of the rotor disks (3a, 3b) and an annulus (H") extends between the central region and the radially outer region of the last two rotor disks (3a, 3b) in the flow direction.
A method for detecting 5-hydroxymethylcytosine in a nucleic acid, comprising the steps of: oxidizing 5-hydroxymethylcytosine possibly present in a nucleic acid sample by treating the nucleic acid sample with a tungstic acid-based oxidizing agent; and determining the position of the oxidized 5-hydroxymethylcytosine in the nucleic acid sample. oxidizing 5-hydroxymethylcytosine possibly present in a nucleic acid sample by treating the nucleic acid sample with a tungstic acid-based oxidizing agent; and determining the position of the oxidized 5-hydroxymethylcytosine in the nucleic acid sample.
Polymerizable composition characterized in that it comprises: a) acrylates and/or methacrylates, b) 0.05% to 70% by weight of SiO 2 particles having an average particle size of 1 to 30 nm which have polymerizable groups of the methacryloyl, acryloyl, styryl, itaconyl, crotonyl, vinyl, allyl and/or alkenyl type on the surface and are present in dispersion in the acrylates and/or methacrylates, at least 50% of the SiO 2 particles consisting of individual, unaggregated or unagglomerated primary particles, c) not more than 2% by weight of crosslinker molecules. a) acrylates and/or methacrylates, b) 0.05% to 70% by weight of SiO 2 particles having an average particle size of 1 to 30 nm which have polymerizable groups of the methacryloyl, acryloyl, styryl, itaconyl, crotonyl, vinyl, allyl and/or alkenyl type on the surface and are present in dispersion in the acrylates and/or methacrylates, at least 50% of the SiO 2 particles consisting of individual, unaggregated or unagglomerated primary particles, c) not more than 2% by weight of crosslinker molecules.
An in vitro method for identifying neovascular structures in mammalian tissue, wherein said neovascular structures are identified by the detection of at least one surface protein in said tissue, the at least one protein being selected from the group consisting of Periostin including isoforms thereof and new splice variants A, B, D, E, wherein the mammalian tissue is mature mammalian kidney tissue, preferably human mature kidney tissue, and wherein positive identification is determined relative to mature mammalian kidney control tissue.
A receptor molecule or antibody or antibody fragment against an antigenic determinant which comprises the following amino acid sequence SEQ ID NO: 3 RNVVW