mhurhangee/patent-ind-claim-en huggingface dataset:
A method for producing a fixed carbon fiber bundle, comprising: causing a fixing agent to adhere to a carbon fiber bundle after opening of the carbon fiber bundle; and fixing a width and a thickness of the carbon fiber bundle by melting and solidifying the fixing agent after setting an average thickness to 180 μm or less, wherein the fixing agent adheres to at least one side of the carbon fiber bundle, and a dividing tear load of the fixed carbon fiber bundle is 0.02 N or more and 1.00 N or less, wherein the average thickness of the carbon fiber bundle just before the fixing agent is supplied is adjusted in the opening step to be 140 μm or less, wherein the average thickness is an average value of the thickness of the fixed carbon fiber bundle measured at 20 points at intervals of 5 m by using a micrometer, wherein the dividing tear load is an average value of ten measured values of maximum sample load, each maximum sample load measured by: cutting the fixed carbon fiber bundle so as to have a carbon fiber length of 100 mm; forming a slit having 30 mm length in a fiber axis direction from one end of the cut sample at a center in a sample width direction to form a first end (a) and a second end (b); fixing the first end (a) to a force gauge; moving the second end (b) in a state in which an angle between the first end (a) and the second end (b) is 180 degrees until the sample is completely torn, and measuring the maximum load at that time. causing a fixing agent to adhere to a carbon fiber bundle after opening of the carbon fiber bundle; and fixing a width and a thickness of the carbon fiber bundle by melting and solidifying the fixing agent after setting an average thickness to 180 μm or less, wherein the fixing agent adheres to at least one side of the carbon fiber bundle, and a dividing tear load of the fixed carbon fiber bundle is 0.02 N or more and 1.00 N or less, wherein the average thickness of the carbon fiber bundle just before the fixing agent is supplied is adjusted in the opening step to be 140 μm or less, wherein the average thickness is an average value of the thickness of the fixed carbon fiber bundle measured at 20 points at intervals of 5 m by using a micrometer, wherein the dividing tear load is an average value of ten measured values of maximum sample load, each maximum sample load measured by: cutting the fixed carbon fiber bundle so as to have a carbon fiber length of 100 mm; forming a slit having 30 mm length in a fiber axis direction from one end of the cut sample at a center in a sample width direction to form a first end (a) and a second end (b); fixing the first end (a) to a force gauge; moving the second end (b) in a state in which an angle between the first end (a) and the second end (b) is 180 degrees until the sample is completely torn, and measuring the maximum load at that time.
A method of supporting a network locating a target node by a Mobility Management Entity, MME , the method comprising: receiving a switching requirement message from a source evolved Node B, eNB, the switching requirement message including a target identifier, ID, and a type of the target eNB; obtaining the closed subscription group identifier, CSG ID, of the target eNB from the target cell global identifier, CGI, included in the packets transparently transferred from the source eNB to the target eNB included in the switching requirement message if the type of the target eNB indicates that the target eNB is an home eNB, HNB, and the target ID is the HNB gateway ID, controlling the access of a User Equipment, UE, to the HNB by determining if the obtained CSG ID is in a CSG white list of the UE. receiving a switching requirement message from a source evolved Node B, eNB, the switching requirement message including a target identifier, ID, and a type of the target eNB; obtaining the closed subscription group identifier, CSG ID, of the target eNB from the target cell global identifier, CGI, included in the packets transparently transferred from the source eNB to the target eNB included in the switching requirement message if the type of the target eNB indicates that the target eNB is an home eNB, HNB, and the target ID is the HNB gateway ID, controlling the access of a User Equipment, UE, to the HNB by determining if the obtained CSG ID is in a CSG white list of the UE.
Air supply module for an internal combustion engine of a motor vehicle, comprising an air filter device having a filter housing which has an air inlet and an air outlet ; a filter insert which is received in the filter housing and subdivides the interior of the filter housing into an unfiltered-air portion and a clean-air portion , wherein a bypass line for feeding heated air into the unfiltered-air portion is present, which bypass line extends from a connection opening in the filter housing, and the filter housing between the connection opening and the filter insert has a housing channel , wherein the filter insert has a bypass portion which is directly adjacent to the housing channel , characterized by an air-cooled charge-air cooler for cooling combustion air which is to be fed to the internal combustion engine, the charge-air cooler having an air-inlet side and an air-outlet side for cooling air , and it being possible for cooling air to flow through said cooler in an air-flow direction ; wherein one end of the bypass line , which is assigned to the charge-air cooler , is adjacent to the air-outlet side of the charge-air cooler ; and wherein a fan is provided adjacent to the air-outlet side of the charge-air cooler , said fan forcing the cooling air in the air-flow direction and having a fan wheel and a fan frame , wherein that end of the bypass line that is assigned to the charge-air cooler is fastened to the fan frame and is fluidically connected to the air-outlet side of the charge-air cooler via an opening in the fan frame . an air filter device having a filter housing which has an air inlet and an air outlet ; a filter insert which is received in the filter housing and subdivides the interior of the filter housing into an unfiltered-air portion and a clean-air portion , wherein a bypass line for feeding heated air into the unfiltered-air portion is present, which bypass line extends from a connection opening in the filter housing, and the filter housing between the connection opening and the filter insert has a housing channel , wherein the filter insert has a bypass portion which is directly adjacent to the housing channel , characterized by an air-cooled charge-air cooler for cooling combustion air which is to be fed to the internal combustion engine, the charge-air cooler having an air-inlet side and an air-outlet side for cooling air , and it being possible for cooling air to flow through said cooler in an air-flow direction ; wherein one end of the bypass line , which is assigned to the charge-air cooler , is adjacent to the air-outlet side of the charge-air cooler ; and wherein a fan is provided adjacent to the air-outlet side of the charge-air cooler , said fan forcing the cooling air in the air-flow direction and having a fan wheel and a fan frame , wherein that end of the bypass line that is assigned to the charge-air cooler is fastened to the fan frame and is fluidically connected to the air-outlet side of the charge-air cooler via an opening in the fan frame .
A dispenser for storing and launching countermeasures , comprising an elongate body provided with at least one launch opening adapted for storing the countermeasures in cartridges , where the dispenser comprises a plurality of cartridges , where the dispenser is adapted to be mounted on an aircraft with the longitudinal direction of the elongate body essentially coinciding with the direction of motion of the aircraft , wherein the dispenser comprises a manoeuvrable spoiler arranged in front of the launch opening, where the spoiler is adapted to be fully retracted before a countermeasure has been launched, and that the spoiler is adapted to extend outwards in a predefined manner when a countermeasure has been launched from a cartridge , where the spoiler is adapted to create a turbulent air flow over the cartridge when the countermeasure has been launched, the spoiler is adapted to be extended outwards from the elongated body in dependency of the number of launched countermeasures .
Sealing device for the edge region of a movable leaf of a door or a window, with a sealing strip movable relative to the leaf for the optional sealing a gap between the leaf and another body, wherein movement of the sealing strip can be driven from the open to the sealing position by a guided sliding movement of a release element relative to the leaf , wherein movement of the release element is transferable via an elastic transmission component to the driving side of a lockable transmission mechanism, through the driven side of which movement of the sealing strip can be driven into the sealing position, and wherein the lock of the lockable transmission mechanism against moving the sealing strip into the sealing position, can be disengaged through the sliding movement of the release element over a predetermined minimum distance, characterised in that the lock is formed by a flexible spring which is resilient to buckling through movement of the release element , wherein the lock is engaged as long as the flexible spring is not buckled, and wherein the lock is thus released when the flexible spring is buckled.
A turbomachine casing extending about an axis (X), said casing comprising: - a hub comprising an outer wall and an inner wall , between which an annular flange extends; - an outer shell ; - a plurality of arms each extending between the hub and the outer shell ; the casing further comprising a plurality of main stiffeners , each arranged in the extension of an arm between the outer wall and the inner wall protruding from the flange , each main stiffener comprising two ribs arranged opposite each other and diverging from each other away from the outer wall towards the inner wall . - a hub comprising an outer wall and an inner wall , between which an annular flange extends; - an outer shell ; - a plurality of arms each extending between the hub and the outer shell ;
A protective case for an electronic device comprising: a main housing ; a lid ; the main housing and lid removably joined to define an air and water tight volume for receiving the electronic device and wherein air is not transferred into or out of the volume; and wherein the main housing includes at least one secondary sound port comprising at least one membrane and operable to transmit sound to and from the electronic device positioned in the volume; and wherein air trapped within the air and water tight volume transfers acoustic energy from a sound source within the case to the at least one membrane wherein the at least one membrane is impermeable to air, and wherein the membrane vibrates in response to an air pressure differential so that sound is operable to be transmitted to an exterior of the case , and wherein the main housing joined with the lid defines an air piston wherein the lid includes a microphone port having a membrane assembly attached thereon, the membrane assembly being non permeable to air and water, and the membrane assembly being compliantly mounted with respect to the microphone port allowing the membrane assembly to freely vibrate. a main housing ; a lid ; the main housing and lid removably joined to define an air and water tight volume for receiving the electronic device and wherein air is not transferred into or out of the volume; and wherein the main housing includes at least one secondary sound port comprising at least one membrane and operable to transmit sound to and from the electronic device positioned in the volume; and wherein air trapped within the air and water tight volume transfers acoustic energy from a sound source within the case to the at least one membrane wherein the at least one membrane is impermeable to air, and wherein the membrane vibrates in response to an air pressure differential so that sound is operable to be transmitted to an exterior of the case , and wherein the main housing joined with the lid defines an air piston wherein the lid includes a microphone port having a membrane assembly attached thereon, the membrane assembly being non permeable to air and water, and the membrane assembly being compliantly mounted with respect to the microphone port allowing the membrane assembly to freely vibrate.
A planet wheel assembly for a planetary gear, the planet wheel assembly comprising: - a planet shaft , - a planet wheel for meshing with a sun shaft and with a gear ring, the planet wheel having first and second radial contact surfaces facing radially towards the planet shaft and first and second axial contact surfaces , - first and second bushings connected to the planet shaft , and - a first radial sliding element between a radial contact surface of the first bushing and the first radial contact surface of the planet wheel, a second radial sliding element between a radial contact surface of the second bushing and the second radial contact surface of the planet wheel, a first axial sliding element between an axial contact surface of the first bushing and the first axial contact surface of the planet wheel, and a second axial sliding element between an axial contact surface of the second bushing and the second axial contact surface of the planet wheel, wherein the planet wheel is shaped to constitute a circumferential projection which protrudes radially towards the planet has axially facing surfaces constituting the first and second axial contact surfaces of the planet wheel, characterized in that the planet wheel is shaped to constitute a circumferential projection which is axially between the first and second radial sliding elements . - a planet shaft , - a planet wheel for meshing with a sun shaft and with a gear ring, the planet wheel having first and second radial contact surfaces facing radially towards the planet shaft and first and second axial contact surfaces , - first and second bushings connected to the planet shaft , and - a first radial sliding element between a radial contact surface of the first bushing and the first radial contact surface of the planet wheel, a second radial sliding element between a radial contact surface of the second bushing and the second radial contact surface of the planet wheel, a first axial sliding element between an axial contact surface of the first bushing and the first axial contact surface of the planet wheel, and a second axial sliding element between an axial contact surface of the second bushing and the second axial contact surface of the planet wheel,
A turbine component comprising: a root ; and an airfoil extending from the root to a tip opposite the root , the airfoil forming a leading edge and a trailing edge portion extending to a trailing edge ; a plurality of radial cooling channels in the trailing edge portion of the airfoil are arranged to permit radial flow of a cooling fluid through the trailing edge portion , each radial cooling channel having a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface ; wherein the plurality of radial cooling channels in the trailing edge portion have a radial geometry selected from the group consisting of wavy, serpentine, irregular, and combinations thereof; characterized in that the airfoil comprises a metal three-dimensionally printed first section and a metal three-dimensionally printed second section , the first section being welded or brazed to the second section to form the airfoil , at least a portion of the plurality of radial cooling channels being formed at a formed surface of the first section or the second section . a root ; and an airfoil extending from the root to a tip opposite the root , the airfoil forming a leading edge and a trailing edge portion extending to a trailing edge ; a plurality of radial cooling channels in the trailing edge portion of the airfoil are arranged to permit radial flow of a cooling fluid through the trailing edge portion , each radial cooling channel having a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface ; wherein the plurality of radial cooling channels in the trailing edge portion have a radial geometry selected from the group consisting of wavy, serpentine, irregular, and combinations thereof; characterized in that the airfoil comprises a metal three-dimensionally printed first section and a metal three-dimensionally printed second section , the first section being welded or brazed to the second section to form the airfoil , at least a portion of the plurality of radial cooling channels being formed at a formed surface of the first section or the second section .
A method for laser hardening an essentially cylindrical surface of a workpiece, in particular of the wheel rim of the wheel disk of a track guided railroad wheel, at least with a partial width of its running surface subjected to wear and/or the side of its wheel flange facing the running surface , comprising the following procedural steps: - Projecting a laser spot onto the surface of the wheel disk to be machined by means of a laser source, - Generating a relative motion between the surface and the laser source by rotating the wheel disk around its axis of rotation, - Scanning the laser beam in relation to the surface to be machined during the rotational motion, - Modulating the laser beam according to various criteria, such as with regard to its power and/or its scanning speed and/or its laser spot size and/or its scanning pattern, - wherein the laser spot describes a scanning pattern in the form of narrow lines transverse to the surface to be machined, corresponding to the rotation of the wheel disk , and extends over its entire width, wherein the line form of the scanning pattern runs with its longitudinal axis inclined to the axis of rotation of the wheel disk , and wherein the laser source is operated at a reduced power after at least one first complete revolution of the wheel disk within an overlapping zone that adjoins the beginning and/or end of the surface to be machined. - Projecting a laser spot onto the surface of the wheel disk to be machined by means of a laser source, - Generating a relative motion between the surface and the laser source by rotating the wheel disk around its axis of rotation, - Scanning the laser beam in relation to the surface to be machined during the rotational motion, - Modulating the laser beam according to various criteria, such as with regard to its power and/or its scanning speed and/or its laser spot size and/or its scanning pattern, - wherein the laser spot describes a scanning pattern in the form of narrow lines transverse to the surface to be machined, corresponding to the rotation of the wheel disk , and extends over its entire width, wherein the line form of the scanning pattern runs with its longitudinal axis inclined to the axis of rotation of the wheel disk , and
A method for producing a thin film ferroelectric device , the method comprising: (a) depositing the organic polymeric ferroelectric precursor material onto a first conductive material such that the organic polymeric ferroelectric precursor material has a first surface and an opposing second surface, wherein the first surface of the organic polymeric ferroelectric precursor material is in contact with the first conductive material; (b) depositing a second conductive material on the second surface of the organic polymeric ferroelectric precursor material to form a stack , wherein the organic polymeric ferroelectric precursor material is positioned at least partially between the first and second conductive materials ; (c) subjecting the stack to a first temperature above a melting temperature of the organic polymeric ferroelectric precursor material for 1 to 60 minutes to form an organic polymeric ferroelectric material having ferroelectric hysteresis properties; and (d) subjecting the stack to a second temperature below the melting temperature of the organic polymeric ferroelectric precursor material for 10 to 70 minutes to densify the organic polymeric ferroelectric material and to obtain a thin film ferroelectric device , wherein interfacial cracks present in the organic polymeric ferroelectric material having ferroelectric hysteresis properties obtained in step (c) are substantially removed in step (d), thereby reducing leakage current in the organic polymeric ferroelectric material when compared with the organic polymeric ferroelectric material obtained in step (c). (a) depositing the organic polymeric ferroelectric precursor material onto a first conductive material such that the organic polymeric ferroelectric precursor material has a first surface and an opposing second surface, wherein the first surface of the organic polymeric ferroelectric precursor material is in contact with the first conductive material; (b) depositing a second conductive material on the second surface of the organic polymeric ferroelectric precursor material to form a stack , wherein the organic polymeric ferroelectric precursor material is positioned at least partially between the first and second conductive materials ; (c) subjecting the stack to a first temperature above a melting temperature of the organic polymeric ferroelectric precursor material for 1 to 60 minutes to form an organic polymeric ferroelectric material having ferroelectric hysteresis properties; and (d) subjecting the stack to a second temperature below the melting temperature of the organic polymeric ferroelectric precursor material for 10 to 70 minutes to densify the organic polymeric ferroelectric material and to obtain a thin film ferroelectric device ,
A system for computerized authentication of a laminated object, the system comprising: a digital medium storing a digital image of at least a portion of the laminated object in a computer-implemented memory; a shininess analyzer operative, using a processor, to generate shininess data quantifying shininess of said digital image; and a parameterized computerized authentication sub-system operative to differentially perform at least one laminated object authentication operation based on said shininess data wherein said image is represented by a multiplicity of pixels and said shininess analyzer is operative for quantifying shininess of the image by: generating a 2-dimensional histogram array representing frequency of occurrence of each of a plurality of n-tuplets of color component values, in the image, wherein each said n-tuplet comprises at least a pair of color values from among at least 3 color components representing each of said multiplicity of pixels. a digital medium storing a digital image of at least a portion of the laminated object in a computer-implemented memory; a shininess analyzer operative, using a processor, to generate shininess data quantifying shininess of said digital image; and a parameterized computerized authentication sub-system operative to differentially perform at least one laminated object authentication operation based on said shininess data wherein said image is represented by a multiplicity of pixels and said shininess analyzer is operative for quantifying shininess of the image by: generating a 2-dimensional histogram array representing frequency of occurrence of each of a plurality of n-tuplets of color component values, in the image, wherein each said n-tuplet comprises at least a pair of color values from among at least 3 color components representing each of said multiplicity of pixels. generating a 2-dimensional histogram array representing frequency of occurrence of each of a plurality of n-tuplets of color component values, in the image, wherein each said n-tuplet comprises at least a pair of color values from among at least 3 color components representing each of said multiplicity of pixels.