mhurhangee/patent-ind-claim-en huggingface dataset:
A two-way signal positioning method, used by a two-way signal positioning system to identify a device location of a locating device to be measured in a specific space, the specific space including a plurality of known locating devices , and the method including the following steps: controlling the locating device to be measured to transmit a plurality of positioning signals of a plurality of transmission powers; causing the plurality of known locating devices to receive the plurality of positioning signals and return a plurality of response signals to the device to be measured; recording the strengths of the plurality of positioning signals, the strengths of the plurality of response signals, and the coordinates of the plurality of known locating devices to a database ; identifying the known locating devices corresponding to the stronger signals among the plurality of positioning signals received and the plurality of response signals; obtaining a signal strength-distance function and a signal strength-distance standard deviation function from the database ; using coordinates of the known locating devices corresponding to the stronger signals as circle centers; obtaining a basic radius under the strengths of the plurality of positioning signals and the strengths of the plurality of response signals according to the signal strength-distance function; obtaining a basis for radius adjustment according to the signal strength-distance standard deviation function; and identifying the device location of the locating device to be measured based on the signal strength-distance function and the signal strength-distance standard deviation function. controlling the locating device to be measured to transmit a plurality of positioning signals of a plurality of transmission powers; causing the plurality of known locating devices to receive the plurality of positioning signals and return a plurality of response signals to the device to be measured; recording the strengths of the plurality of positioning signals, the strengths of the plurality of response signals, and the coordinates of the plurality of known locating devices to a database ; identifying the known locating devices corresponding to the stronger signals among the plurality of positioning signals received and the plurality of response signals; obtaining a signal strength-distance function and a signal strength-distance standard deviation function from the database ; using coordinates of the known locating devices corresponding to the stronger signals as circle centers; obtaining a basic radius under the strengths of the plurality of positioning signals and the strengths of the plurality of response signals according to the signal strength-distance function; obtaining a basis for radius adjustment according to the signal strength-distance standard deviation function; and identifying the device location of the locating device to be measured based on the signal strength-distance function and the signal strength-distance standard deviation function.
Cooking appliance with a housing , in which a cooking chamber is configured, and with a door for closing the cooking chamber, wherein the door is arranged on the housing in a pivotable manner and is able to be lowered into a storage space in the housing , and with a drive unit with a motor , by means of which the movement of the door can be brought about automatically, characterised in that the drive unit has a cable pull device , which is coupled to the motor and the door , wherein it is possible for the movement of the door to be brought about as a function of a motorised actuation of the cable pull device , wherein the movement path of the door , which is brought about automatically by means of the drive unit , is only part of the complete movement path between a closed position of the door and a fully opened position of the door , and wherein a movement path of the door , which is not brought about by the drive unit , extends between the closed position of the door and the start of the partial path.
A catalyst comprising nanostructured elements comprising microstructured support whiskers bearing a thin film of nanoscopic catalyst particles comprising a catalyst material according to the formula Pt x Ni (1-x) where x is between 0.21 and 0.39, wherein nanoscopic catalyst particles means particles of catalyst material having at least one dimension equal to or smaller than about 15 nm or having a crystallite size of about 15 nm or less, as measure from diffraction peak half widths of standard 2-theta x-ray diffraction scans.
Method for limiting a driving speed ( v ) of a vehicle when driving around a corner (K), wherein a course of a curvature ( κ ) in a road portion ahead of the vehicle is determined, wherein, on the basis of the course of the curvature ( κ ) and physical load limits of the vehicle, a course of a permissible cornering speed ( v ) is determined, and the vehicle is controlled in such a way that the determined permissible cornering speeds (v) are not exceeded when driving around the corner (K), wherein - by evaluating the course of the curvature ( κ ), a road portion on which the curvature ( κ ) is greater than a predetermined curvature limit value ( κ lim ) is identified as a corner portion, characterized in that - local curvature maxima are identified on the identified corner portion, and wherein - if a plurality of local curvature maxima are identified on the corner portion, a permissible cornering speed ( v ) is determined for each local curvature maximum on the basis of the curvature ( κ ) and a permissible lateral acceleration ( α quer zul ) . - by evaluating the course of the curvature ( κ ), a road portion on which the curvature ( κ ) is greater than a predetermined curvature limit value ( κ lim ) is identified as a corner portion, characterized in that - local curvature maxima are identified on the identified corner portion, and wherein - if a plurality of local curvature maxima are identified on the corner portion, a permissible cornering speed ( v ) is determined for each local curvature maximum on the basis of the curvature ( κ ) and a permissible lateral acceleration ( α quer zul ) .
A free fall simulator comprising: - a wind tunnel system ; - a flight chamber connected to the wind tunnel system such that the wind tunnel system and the flight chamber allow for a continuous flow of circulating air, and - a cooling system for cooling of the air circulating in the wind tunnel system, wherein the cooling system comprises: - an air inlet sucking in a part of the air circulating in the wind tunnel system; and - at least one heat exchanger comprising a coolant; and - at least one air outlet adapted such that the cooled air leaves the cooling system through the at least one air outlet; characterized in that the cooling system further comprises: - a closed pressure chamber comprising a cooling area , wherein pressure in said cooling area is higher than atmospheric pressure, and - at least one auxiliary fan configured to maintain pressure within the cooling area of the pressure chamber higher than the atmospheric pressure, and in that the at least one heat exchanger is located inside of the closed pressure chamber so that the cooling of the circulating air takes place in the cooling area . - a wind tunnel system ; - a flight chamber connected to the wind tunnel system such that the wind tunnel system and the flight chamber allow for a continuous flow of circulating air, and - a cooling system for cooling of the air circulating in the wind tunnel system, wherein the cooling system comprises: - an air inlet sucking in a part of the air circulating in the wind tunnel system; and - at least one heat exchanger comprising a coolant; and - at least one air outlet adapted such that the cooled air leaves the cooling system through the at least one air outlet; - a closed pressure chamber comprising a cooling area , wherein pressure in said cooling area is higher than atmospheric pressure, and - at least one auxiliary fan configured to maintain pressure within the cooling area of the pressure chamber higher than the atmospheric pressure,
A laser system comprising: a) a laser source configured to generate a laser light beam; b) an ion trap ; c) a first beamsplitter configured to split the laser light beam into a first front side laser light beam and a back side laser light beam for a back side of the ion trap; d) a multi-channel acousto-optic modulator , i.e. AOM, comprising: a. a second beamsplitter to split the first front side laser light beam into a plurality of second front side laser light beams from the second beamsplitter , b, a common acousto-optic medium configured to receive the plurality of front side laser light beams, and c. a respective plurality of electrodes coupled to the common acousto-optic medium for each of the second front side laser light beams; e) a plurality of radio frequency (RF) drivers each configured to generate respective RF drive signals for each of the plurality of electrodes ; f) an input telescope configured to direct the front side laser light beam to the second beamsplitter ; and g) an output telescope configured to direct the plurality of second front side laser light beams to a front side of the ion trap ; h) wherein the electrodes comprise phased array transducer electrodes; and wherein each RF driver is configured to drive alternating electrodes of the respective phased array transducer electrodes out of phase. a) a laser source configured to generate a laser light beam; b) an ion trap ; c) a first beamsplitter configured to split the laser light beam into a first front side laser light beam and a back side laser light beam for a back side of the ion trap; d) a multi-channel acousto-optic modulator , i.e. AOM, comprising: a. a second beamsplitter to split the first front side laser light beam into a plurality of second front side laser light beams from the second beamsplitter , b, a common acousto-optic medium configured to receive the plurality of front side laser light beams, and c. a respective plurality of electrodes coupled to the common acousto-optic medium for each of the second front side laser light beams; a. a second beamsplitter to split the first front side laser light beam into a plurality of second front side laser light beams from the second beamsplitter , b, a common acousto-optic medium configured to receive the plurality of front side laser light beams, and c. a respective plurality of electrodes coupled to the common acousto-optic medium for each of the second front side laser light beams; e) a plurality of radio frequency (RF) drivers each configured to generate respective RF drive signals for each of the plurality of electrodes ; f) an input telescope configured to direct the front side laser light beam to the second beamsplitter ; and g) an output telescope configured to direct the plurality of second front side laser light beams to a front side of the ion trap ; h) wherein the electrodes comprise phased array transducer electrodes; and wherein each RF driver is configured to drive alternating electrodes of the respective phased array transducer electrodes out of phase.
A supply item for an imaging device comprising: a body ; a magnetic key located on the body having a plurality of magnetic plates in the shape of a circle wherein a portion of the circle arc is a straight edge , and wherein the longest dimension is greater than 0.3 mm and less than 1.0 mm, each having a flat top surface and a flat bottom surface parallel to its top surface, arranged in a first layer and a second layer with the bottom surfaces of magnetic plates in the first layer located above and parallel to the top surfaces of magnetic plates in the second layer, the magnetic key has an outer surface , the plurality of magnetic plates generate a magnetic field above the outer surface having an intensity that varies along the outer surface; and a non-volatile memory located on the body containing an array of numbers corresponding to the intensity of the magnetic field above the outer surface at a plurality of locations and also containing a digital signature generated from the array of numbers; wherein each magnetic plate has a north pole and a south pole and a magnetic pole line running from the south pole to the north pole, and the plurality of magnetic plates contains at least three magnetic pole lines that are not parallel to each other. a body ; a magnetic key located on the body having a plurality of magnetic plates in the shape of a circle wherein a portion of the circle arc is a straight edge , and wherein the longest dimension is greater than 0.3 mm and less than 1.0 mm, each having a flat top surface and a flat bottom surface parallel to its top surface, arranged in a first layer and a second layer with the bottom surfaces of magnetic plates in the first layer located above and parallel to the top surfaces of magnetic plates in the second layer, the magnetic key has an outer surface , the plurality of magnetic plates generate a magnetic field above the outer surface having an intensity that varies along the outer surface; and a non-volatile memory located on the body containing an array of numbers corresponding to the intensity of the magnetic field above the outer surface at a plurality of locations and also containing a digital signature generated from the array of numbers; wherein each magnetic plate has a north pole and a south pole and a magnetic pole line running from the south pole to the north pole, and the plurality of magnetic plates contains at least three magnetic pole lines that are not parallel to each other.
A system for heating an exterior of an aircraft , the system comprising: an aircraft skin having a bulk conductive medium, and two or more coupling strips spaced apart from one another and attached to the aircraft skin , each of the coupling strips comprising a multi-layer structure extending along a surface of the aircraft skin that forms, in combination with the aircraft skin, an electrical transmission line, the multi-layer structure comprising: a first dielectric layer over the aircraft skin, a conductive layer over the first dielectric layer, a second dielectric layer over the conductive layer, and a conductive shielding layer over the second dielectric layer; and a power control system coupled to the conductive layer of each of the coupling strips and to the aircraft skin, the power control system configured to heat the surface of the aircraft skin by providing high frequency electrical current to the coupling strips, thereby, generating skin effect electrical currents within the bulk medium of the aircraft skin. an aircraft skin having a bulk conductive medium, and two or more coupling strips spaced apart from one another and attached to the aircraft skin , each of the coupling strips comprising a multi-layer structure extending along a surface of the aircraft skin that forms, in combination with the aircraft skin, an electrical transmission line, the multi-layer structure comprising: a first dielectric layer over the aircraft skin, a conductive layer over the first dielectric layer, a second dielectric layer over the conductive layer, and a conductive shielding layer over the second dielectric layer; and a power control system coupled to the conductive layer of each of the coupling strips and to the aircraft skin, the power control system configured to heat the surface of the aircraft skin by providing high frequency electrical current to the coupling strips, thereby, generating skin effect electrical currents within the bulk medium of the aircraft skin.
A system for automatic harmonization of data and/or data models which exist in different formats and which originate from different heterogeneous data sources or data pools using a semantic middleware for the technical data integration on system level and for content-related data analysis, wherein data from connected data sources will be actively synchronized by the middleware by means of push principle or passively by means of pull principle, wherein these data will at first be adjusted to one another with respect to the format thereof or will be transformed for interoperability into content objects with semantic typification and attributes with attribute names and attribute values, and afterwards, these data will be semantically analysed with respect to the content thereof, wherein the system will search for content objects having a similar content and if similar content objects are found, the respective attribute names of the accordances and the respective content type will be adopted for the analysed content object, such that the uniform information model of the integrated data will be extended and harmonised in an incremental manner, i.e. step by step. at first be adjusted to one another with respect to the format thereof or will be transformed for interoperability into content objects with semantic typification and attributes with attribute names and attribute values, and afterwards, these data will be semantically analysed with respect to the content thereof, wherein the system will search for content objects having a similar content and if similar content objects are found, the respective attribute names of the accordances and the respective content type will be adopted for the analysed content object, such that the uniform information model of the integrated data will be extended and harmonised in an incremental manner, i.e. step by step.
A voltage supply unit of a vehicle, provided with a first output adapted to supply a first voltage to a first load and provided with a second output adapted to supply a second voltage to a second load , where the voltage supply unit comprises a battery comprising a first battery stack and a second battery stack connected in series, the first battery stack providing the first voltage which is a low voltage output, and the first battery stack and the second battery stack providing the second voltage which is a high voltage output, and an electronic control unit , the electronic control unit being adapted to regulate the energy state of the first battery stack of the battery to a first energy state, and to regulate the energy state of the second battery stack of the battery to a second energy state, where the first energy state differs from the second energy state, wherein the electronic control unit is adapted to control the first energy state of the first battery stack to be within a predefined SoC-window, characterized in that the second energy state of the second battery stack is allowed to exceed this predefined SoC-window, such that more energy can be stored in the second battery stack to make sure that the voltage of the first battery stack will be within the predefined SoC-window during a charge event, regardless of the voltage level of the second battery stack
An image display apparatus comprising: a synthesizing device that is configured to synthesize a rear image and rear side images to generate a synthesized image , wherein the rear image is captured by a rear imaging device that is configured to image a rear area located at the rear of a first vehicle and the rear side images are captured by rear side imaging devices that are configured to image a rear side area located at the rear and the side of the first vehicle; and a displaying device that is configured to display the synthesized image, the synthesizing device being configured to vary an imaging range included in each of a rear image area and rear side image areas in the synthesized image on the basis of a distance between the first vehicle and a second vehicle that exists at the rear of the first vehicle, wherein the rear image area is an area in which the rear image is displayed in the synthesized image and the rear side image areas are areas in which the rear side images are displayed in the synthesized image, when the synthesizing device generates the synthesized image; wherein the synthesizing device is configured to vary the imaging range included in the rear image area in the synthesized image when said distance is shorter than a predetermined first threshold value (TH1) to be larger than the imaging range included in the rear image area in the synthesized image when said distance is longer than the first threshold value. a synthesizing device that is configured to synthesize a rear image and rear side images to generate a synthesized image , wherein the rear image is captured by a rear imaging device that is configured to image a rear area located at the rear of a first vehicle and the rear side images are captured by rear side imaging devices that are configured to image a rear side area located at the rear and the side of the first vehicle; and a displaying device that is configured to display the synthesized image, the synthesizing device being configured to vary an imaging range included in each of a rear image area and rear side image areas in the synthesized image on the basis of a distance between the first vehicle and a second vehicle that exists at the rear of the first vehicle, wherein the rear image area is an area in which the rear image is displayed in the synthesized image and the rear side image areas are areas in which the rear side images are displayed in the synthesized image, when the synthesizing device generates the synthesized image; wherein the synthesizing device is configured to vary the imaging range included in the rear image area in the synthesized image when said distance is shorter than a predetermined first threshold value (TH1) to be larger than the imaging range included in the rear image area in the synthesized image when said distance is longer than the first threshold value.
A method of applying turmeric on hierarchical zeolites, characterized in that to hierarchical zeolite possessing secondary porosity, pores in the range 2-50 nm, synthesised on the basis of faujasite and either non-ionic structure forming agents selected from the group of polyethylene glycol octadecyl ether or Pluronic F127 or the ionic structure-forming agent hexadecyltrimethylammonium bromide in the presence or absence of piperine, the following is added: - a solvent, advantageously acetone in an amount of 2.5-12.5% w/w, advantageously 12.5% w/w in relation to hierarchical zeolite, - 20-60% w/w of turmeric, advantageously 20% w/w of turmeric in relation to hierarchical zeolite, and - 0.1-0.4% w/w of piperine, advantageously 0.1% w/w of piperine in relation to hierarchical zeolite, whereas the entire process of mixing is conducted for 24-30 h advantageously 24 h in a temperature of 20-40°C advantageously in 23°C, and - washing the obtained product with a water-ethanol solution in a volumetric ration of 1:1 and - drying afterwards. - a solvent, advantageously acetone in an amount of 2.5-12.5% w/w, advantageously 12.5% w/w in relation to hierarchical zeolite, - 20-60% w/w of turmeric, advantageously 20% w/w of turmeric in relation to hierarchical zeolite, and - 0.1-0.4% w/w of piperine, advantageously 0.1% w/w of piperine in relation to hierarchical zeolite, whereas the entire process of mixing is conducted for 24-30 h advantageously 24 h in a temperature of 20-40°C advantageously in 23°C, and - washing the obtained product with a water-ethanol solution in a volumetric ration of 1:1 and - drying afterwards.