mhurhangee/ep-ind-claims huggingface dataset:
Metal azo pigments, characterized in that they comprise the following components: a) at least three metal azo compounds which differ at least in the type of metal and which each contain • structural units of the formula, or the tautomeric forms thereof, in which R1 and R2 are each independently OH, NH2 or NHR5, R3 and R4 are each independently =O or =NR5, R5 is hydrogen or alkyl, preferably C1-C4-alkyl, and • Ni2+ and/or Zn2+ ions and at least one further metal ion Me, where Me is a di- or trivalent metal ion selected from the group of Cu2+, A13+, Fe2+, Fe3+, Co2+ and Co3+, with the proviso that the amount of Zn2+ and Ni2+ ions together is 70 mol% to less than 95 mol% and the amount of metal ions Me is more than 5 mol% to 30 mol%, based in each case on one mole of all metal ions in the metal azo pigment, and where the molar ratio of Zn2+ to Ni2+ ions in the metal azo pigment is 92:5 to 5:92, preferably 70:10 to 10:70 and more preferably 60:25 to 25:60, and, b) at least one compound of the formula in which R6 is hydrogen or alkyl, preferably C1-C4-alkyl optionally mono- or polysubstituted by OH. a) at least three metal azo compounds which differ at least in the type of metal and which each contain • structural units of the formula, or the tautomeric forms thereof, in which R1 and R2 are each independently OH, NH2 or NHR5, R3 and R4 are each independently =O or =NR5, R5 is hydrogen or alkyl, preferably C1-C4-alkyl, and • Ni2+ and/or Zn2+ ions and at least one further metal ion Me, where Me is a di- or trivalent metal ion selected from the group of Cu2+, A13+, Fe2+, Fe3+, Co2+ and Co3+, with the proviso that the amount of Zn2+ and Ni2+ ions together is 70 mol% to less than 95 mol% and the amount of metal ions Me is more than 5 mol% to 30 mol%, based in each case on one mole of all metal ions in the metal azo pigment, and where the molar ratio of Zn2+ to Ni2+ ions in the metal azo pigment is 92:5 to 5:92, preferably 70:10 to 10:70 and more preferably 60:25 to 25:60, and, • structural units of the formula, or the tautomeric forms thereof, in which R1 and R2 are each independently OH, NH2 or NHR5, R3 and R4 are each independently =O or =NR5, R5 is hydrogen or alkyl, preferably C1-C4-alkyl, and • Ni2+ and/or Zn2+ ions and at least one further metal ion Me, where Me is a di- or trivalent metal ion selected from the group of Cu2+, A13+, Fe2+, Fe3+, Co2+ and Co3+, b) at least one compound of the formula in which R6 is hydrogen or alkyl, preferably C1-C4-alkyl optionally mono- or polysubstituted by OH.
A stabilizer composition comprising: a. a microcrystalline cellulose; and b. a water-soluble carboxymethylcellulose selected from: i) a low viscosity water-soluble carboxymethylcellulose having a Brookfield viscosity of from 10 to 200 cps measured at a 2.6% dispersion in deionized water using an RVT viscometer at 20 rpm at 20°C-23°C, wherein the weight ratio of the microcrystalline cellulose and the carboxymethylcellulose is from 95:5 to 70:30; and ii) a medium viscosity water-soluble carboxymethylcellulose having a Brookfield viscosity of from 200 to 4000 cps measured at a 2.6% dispersion in deionized water using an RVT viscometer at 20 rpm at 20°C-23°C wherein the weight ratio of the microcrystalline cellulose and the carboxymethyl cellulose is from 95:5 to 70:30; characterized in that said water-soluble carboxymethylcellulose has a degree of substitution of from 0.45 to 0.85, the stabilizer composition is produced by co-attriting an admixture of said microcrystalline cellulose in the form of a wetcake having at least 42% solids with said water-soluble carboxymethylcellulose, and when the stabilizer composition includes the low viscosity water soluble carboxymethylcellulose, upon dispersion in water at 2.6% solids, the stabilizer composition has an initial viscosity of at least 750 cps, a set-up viscosity of at least 2900 cps, and a set-up gel strength G' of at least 20 Pa, and when the stabilizer composition includes the medium viscosity water soluble carboxymethylcellulose, upon dispersion in water at 2.6% solids, the stabilizer composition has an initial viscosity of at least 1000 cps, a set-up viscosity of at least 3500 cps, and a set-up gel strength G' of at least 40 Pa. a. a microcrystalline cellulose; and b. a water-soluble carboxymethylcellulose selected from: i) a low viscosity water-soluble carboxymethylcellulose having a Brookfield viscosity of from 10 to 200 cps measured at a 2.6% dispersion in deionized water using an RVT viscometer at 20 rpm at 20°C-23°C, wherein the weight ratio of the microcrystalline cellulose and the carboxymethylcellulose is from 95:5 to 70:30; and ii) a medium viscosity water-soluble carboxymethylcellulose having a Brookfield viscosity of from 200 to 4000 cps measured at a 2.6% dispersion in deionized water using an RVT viscometer at 20 rpm at 20°C-23°C wherein the weight ratio of the microcrystalline cellulose and the carboxymethyl cellulose is from 95:5 to 70:30; i) a low viscosity water-soluble carboxymethylcellulose having a Brookfield viscosity of from 10 to 200 cps measured at a 2.6% dispersion in deionized water using an RVT viscometer at 20 rpm at 20°C-23°C, wherein the weight ratio of the microcrystalline cellulose and the carboxymethylcellulose is from 95:5 to 70:30; and ii) a medium viscosity water-soluble carboxymethylcellulose having a Brookfield viscosity of from 200 to 4000 cps measured at a 2.6% dispersion in deionized water using an RVT viscometer at 20 rpm at 20°C-23°C wherein the weight ratio of the microcrystalline cellulose and the carboxymethyl cellulose is from 95:5 to 70:30;
A system for analysing radioactive waste packages comprising a neutron source, the analysis system including a plurality of detection devices and a calculator, the analysis system being characterised in that at least one detection device is configured to detect fast neutrons, and at least one detection device is configured to detect thermal neutrons, each detection device being configured to deliver an electrical detection signal comprising pulses each being representative of the detection of a respective neutron coming from the source, the calculator being configured to receive the detection signal delivered by each detection device and to identify, in each detection signal received, pulses corresponding to thermal neutrons and/or pulses corresponding to fast neutrons, the calculator being also configured to calculate, for each detection device, from the detection signal received from the detection device, a first number of coincidences, depending on the number of real coincidences of fission fast neutrons detected by the detection device, and a second number of coincidences, depending on the number of real coincidences of fission thermal neutrons detected by the detection device, the calculator being further configured to determine a position of the source relative to a predetermined point of the analysis system from the first number of coincidences and the second number of coincidences calculated for at least one part of the detection devices. at least one detection device is configured to detect fast neutrons, and at least one detection device is configured to detect thermal neutrons, each detection device being configured to deliver an electrical detection signal comprising pulses each being representative of the detection of a respective neutron coming from the source, the calculator being configured to receive the detection signal delivered by each detection device and to identify, in each detection signal received, pulses corresponding to thermal neutrons and/or pulses corresponding to fast neutrons, the calculator being also configured to calculate, for each detection device, from the detection signal received from the detection device, a first number of coincidences, depending on the number of real coincidences of fission fast neutrons detected by the detection device, and a second number of coincidences, depending on the number of real coincidences of fission thermal neutrons detected by the detection device, the calculator being further configured to determine a position of the source relative to a predetermined point of the analysis system from the first number of coincidences and the second number of coincidences calculated for at least one part of the detection devices.
Method for incorporating photographic facial images and/or films of a person into the planning of odontological and/or cosmetic dental treatments and/or the preparation of restorations for said person, characterized in that the photographic facial images and/or films are produced using the camera function of a smart device, wherein the user of the method is guided through the production of the facial images and/or films with the aid of an application for the smart device, and the produced images and/or films are incorporated into software for a computer-assisted design of the treatments and/or restorations, characterized in that a template for the positioning of the mouth region is provided in the display of the smart device for the guidance through the production of the facial images and/or films.
A method comprising: providing a plurality of processes, each of said plurality of processes being configured to hold a block of data (130, 180, 220) destined for others of said plurality of processes; providing at least one instance of data repacking circuitry comprising: receiving circuitry configured to receive at least one block of data from each of at least two different source processes of the plurality of processes; repacking circuitry configured to repack blocks of data received from the two different source processes and destined for the same destination process of the plurality of processes into a single message to the destination process; and sending circuitry configured to send the repacked data to said at least one destination process of the plurality of processes; receiving a set of data for all-to-all data exchange, the set of data being configured as a matrix, the matrix being distributed among the plurality of processes; and transposing the data by: each of the plurality of processes sending matrix data from said process to said data repacking circuitry; and said data repacking circuitry receiving, repacking, and sending the resulting matrix data to destination processes. providing a plurality of processes, each of said plurality of processes being configured to hold a block of data (130, 180, 220) destined for others of said plurality of processes; providing at least one instance of data repacking circuitry comprising: receiving circuitry configured to receive at least one block of data from each of at least two different source processes of the plurality of processes; repacking circuitry configured to repack blocks of data received from the two different source processes and destined for the same destination process of the plurality of processes into a single message to the destination process; and sending circuitry configured to send the repacked data to said at least one destination process of the plurality of processes; receiving circuitry configured to receive at least one block of data from each of at least two different source processes of the plurality of processes; repacking circuitry configured to repack blocks of data received from the two different source processes and destined for the same destination process of the plurality of processes into a single message to the destination process; and sending circuitry configured to send the repacked data to said at least one destination process of the plurality of processes; receiving a set of data for all-to-all data exchange, the set of data being configured as a matrix, the matrix being distributed among the plurality of processes; and transposing the data by: each of the plurality of processes sending matrix data from said process to said data repacking circuitry; and said data repacking circuitry receiving, repacking, and sending the resulting matrix data to destination processes.
A method of adapting autonomous control of an autonomous vehicle based on a determined yaw parameter of an additional vehicle, the method comprising: receiving, from a phase coherent Light Detection and Ranging (LIDAR) component of a vehicle, a group of LIDAR data points of a sensing cycle of the phase coherent LIDAR component, each of the LIDAR data points of the group indicating a corresponding instantaneous range and a corresponding instantaneous velocity for a corresponding point in an environment of the vehicle, and each of the LIDAR data points of the group being generated based on a corresponding sensing event of the phase coherent LIDAR component during the sensing cycle, wherein the corresponding instantaneous range and the corresponding instantaneous velocity for the corresponding point in the environment of the vehicle are based on the corresponding sensing event without reference to a prior or subsequent sensing event; determining that a subgroup (582A-B; 583A-B; 584A-C; 585A-C; 682A-H), of the LIDAR data points of the group, corresponds to an additional vehicle that is in addition to the vehicle; based on determining that the subgroup corresponds to the additional vehicle: determining an instantaneous yaw parameter of the additional vehicle based on a plurality of the LIDAR data points of the subgroup; and adapting autonomous control of the vehicle based on the determined instantaneous yaw parameter of the additional vehicle. receiving, from a phase coherent Light Detection and Ranging (LIDAR) component of a vehicle, a group of LIDAR data points of a sensing cycle of the phase coherent LIDAR component, each of the LIDAR data points of the group indicating a corresponding instantaneous range and a corresponding instantaneous velocity for a corresponding point in an environment of the vehicle, and each of the LIDAR data points of the group being generated based on a corresponding sensing event of the phase coherent LIDAR component during the sensing cycle, wherein the corresponding instantaneous range and the corresponding instantaneous velocity for the corresponding point in the environment of the vehicle are based on the corresponding sensing event without reference to a prior or subsequent sensing event; determining that a subgroup (582A-B; 583A-B; 584A-C; 585A-C; 682A-H), of the LIDAR data points of the group, corresponds to an additional vehicle that is in addition to the vehicle; based on determining that the subgroup corresponds to the additional vehicle: determining an instantaneous yaw parameter of the additional vehicle based on a plurality of the LIDAR data points of the subgroup; and adapting autonomous control of the vehicle based on the determined instantaneous yaw parameter of the additional vehicle. determining an instantaneous yaw parameter of the additional vehicle based on a plurality of the LIDAR data points of the subgroup; and adapting autonomous control of the vehicle based on the determined instantaneous yaw parameter of the additional vehicle.
An image capture apparatus that generates an omnidirectional image using a plurality of imaging lenses (103a, 103b) with different capture directions, comprising: detecting means for detecting an orientation of the image capture apparatus, characterized by identifying means for, when the image capture apparatus is in a crop mode as an operation mode for generating a first image that is a stabilized image with a smaller field of view than an omnidirectional image, identifying an area to be captured required to generate the stabilized first image on a basis of the initial position of the area to be captured within a capturable area (303, 305) of one of the plurality of the imaging lenses when the imaging device is in a reference orientation and a difference between the reference orientation and a current orientation of the image capture apparatus detected by the detecting means; and control means for, when the image capture apparatus is in the operation mode, enabling image capture using one or more imaging lenses, from among the plurality of imaging lenses (103a, 103b) having a capturable area which include at least a portion of the area to be captured and disabling image capture using one or more imaging lenses, from among the plurality of imaging lenses (103a, 103b), having a capturable area which does not include any portion of the area to be captured. detecting means for detecting an orientation of the image capture apparatus, characterized by identifying means for, when the image capture apparatus is in a crop mode as an operation mode for generating a first image that is a stabilized image with a smaller field of view than an omnidirectional image, identifying an area to be captured required to generate the stabilized first image on a basis of the initial position of the area to be captured within a capturable area (303, 305) of one of the plurality of the imaging lenses when the imaging device is in a reference orientation and a difference between the reference orientation and a current orientation of the image capture apparatus detected by the detecting means; and control means for, when the image capture apparatus is in the operation mode, enabling image capture using one or more imaging lenses, from among the plurality of imaging lenses (103a, 103b) having a capturable area which include at least a portion of the area to be captured and disabling image capture using one or more imaging lenses, from among the plurality of imaging lenses (103a, 103b), having a capturable area which does not include any portion of the area to be captured.
Device for remolding a fresh, slipform cast concrete product, said device comprising a stationary digging jaw fixedly attached to a support structure, and a movable digging jaw that is movable with respect to the stationary digging jaw, and means for operating the movable digging jaw, in which remolding said jaws are immersed into the fresh slipform cast concrete product with vertical downwards motion, characterized in that the movable digging jaw is attached to the support structure by intermediation of two or several articulated joints or shafts (6, 7) for shifting the tip of the movable digging jaw towards the stationary digging jaw substantially on the horizontal level.
A combustion control apparatus for a compression self-ignition internal combustion engine in which fuel injected from a fuel injection valve into a cylinder is caused to combust in the cylinder, comprising: oxygen concentration regulating means that is capable of regulating an oxygen concentration in the cylinder before a fuel injection of the fuel injection valve; pressure regulating means that is capable of regulating a pre-ignition pressure in the cylinder; characterized by gas state controlling means that, in the case where a specific region is targeted where the pre-ignition pressure in the cylinder is limited to being no more than a predetermined pressure and where no smoke is generated even when the oxygen concentration is reduced, and where the oxygen concentration in the cylinder and the pre-ignition pressure in the cylinder are put into a state of the specific region from a state in which the oxygen concentration in the cylinder and the pre-ignition pressure in the cylinder are higher than those in the specific region, sets the oxygen concentration in the cylinder and the pre-ignition pressure in the cylinder into a state of the specific region while avoiding a smoke generating region by lowering the pre-ignition pressure in the cylinder by the pressure regulating means and thereafter lowering the oxygen concentration in the cylinder by the oxygen concentration regulating means. oxygen concentration regulating means that is capable of regulating an oxygen concentration in the cylinder before a fuel injection of the fuel injection valve; pressure regulating means that is capable of regulating a pre-ignition pressure in the cylinder; characterized by gas state controlling means that, in the case where a specific region is targeted where the pre-ignition pressure in the cylinder is limited to being no more than a predetermined pressure and where no smoke is generated even when the oxygen concentration is reduced, and where the oxygen concentration in the cylinder and the pre-ignition pressure in the cylinder are put into a state of the specific region from a state in which the oxygen concentration in the cylinder and the pre-ignition pressure in the cylinder are higher than those in the specific region, sets the oxygen concentration in the cylinder and the pre-ignition pressure in the cylinder into a state of the specific region while avoiding a smoke generating region by lowering the pre-ignition pressure in the cylinder by the pressure regulating means and thereafter lowering the oxygen concentration in the cylinder by the oxygen concentration regulating means.
An aircraft landing gear comprising a leg hinged to the aircraft and operable between a deployed position and a retracted position, a folding strut (2; 102) comprising two hinged-together links, a stabilizer member (4; 104) comprising two hinged-together links and a locking member, the leg being stabilized in the deployed position by said folding strut comprising two hinged-together links, the strut being held in the aligned position by said stabilizer member comprising two hinged-together links, themselves held in alignment by said locking member, characterized in that said aircraft landing gear comprises a single operating actuator and that the strut (2; 102) and the stabilizer member (4; 104) are arranged in such a manner that at least one of the links (4a; 104a) of the stabilizer member moves continuously during a movement of the leg from the deployed position to the retracted position, the continuous movement being ensured by a continuous action of said operating actuator, the single operating actuator being of the rotary type, the single operating actuator (10; 110) being attached to said link (4a; 104a) in order to cause the link to pivot against the locking member and exert thereon a force tending simultaneously to bring the links of the stabilizer member out of alignment against the locking member, to bring the links of the strut out of alignment, and to move the leg.
Antenna system, having at least four single radiating elements, wherein the single radiating elements are in the form of horn antennas, and the horn antennas support two mutually orthogonal linear polarizations and are equipped with constrictions (15, 16) in both polarization planes, characterized in that the walls of the horn antennas and the geometric constrictions (15, 16) are at least to some extent of stepped design and the aperture of the horn antennas is at any rate approximately rectangular, the interval between two opposite constrictions (15, 16) and the cross section of the horn antenna opening decreases from the aperture to the horn end of the horn antenna from step to step, at least for some of these steps the steps are designed such that, for the interval d i between the integer i-th steps, wherein i ≥ 0 in two opposite constrictions (15, 16) and the associated edge length a i of the opening of the horn antenna cross section of the integer i-th step, d l ≤ p 1 2 ⁢ π λ F a l 2 − p 2 a l, holds when λ E denotes the free-space wavelength of the lowest useful frequency of the antenna system, p 1 is between 0.3 and 0.4 and p 2 is between 0.25 and 0.35, wherein preferably p 1 = 0.35 and p 2 = 0.29.