mhurhangee/patent-ind-claim-en huggingface dataset:
A method for transmitting a service stream in a flexible Ethernet, comprising: obtaining a to-be-transmitted service stream, wherein the service stream is to be transmitted by using a target virtual connection supported by a physical connection group between a transmit end and a receive end, the physical connection group comprises multiple physical connections and supports at least one virtual connection, and the target virtual connection is any one of the at least one virtual connection; determining , from total bandwidth resources of the multiple physical connections and according to timeslot configuration tables used by the multiple physical connections, a timeslot bandwidth resource that belongs to the target virtual connection, wherein a timeslot configuration table used by each physical connection is used to indicate a virtual connection to which each timeslot bandwidth resource obtained by dividing a bandwidth resource of each physical connection belongs; and transmitting the service stream to the receive end by using the timeslot bandwidth resource that belongs to the target virtual connection, wherein an overhead code block transmitted over each physical connection comprises a first field, the first field indicates an identifier of the timeslot configuration table used by each physical connection, the overhead code block transmitted over each physical connection further comprises fields used for a management channel, and the management channel is used to: when the timeslot configuration table used by each physical connection changes, transmit content of a changed timeslot configuration table. obtaining a to-be-transmitted service stream, wherein the service stream is to be transmitted by using a target virtual connection supported by a physical connection group between a transmit end and a receive end, the physical connection group comprises multiple physical connections and supports at least one virtual connection, and the target virtual connection is any one of the at least one virtual connection; determining , from total bandwidth resources of the multiple physical connections and according to timeslot configuration tables used by the multiple physical connections, a timeslot bandwidth resource that belongs to the target virtual connection, wherein a timeslot configuration table used by each physical connection is used to indicate a virtual connection to which each timeslot bandwidth resource obtained by dividing a bandwidth resource of each physical connection belongs; and transmitting the service stream to the receive end by using the timeslot bandwidth resource that belongs to the target virtual connection, wherein an overhead code block transmitted over each physical connection comprises a first field, the first field indicates an identifier of the timeslot configuration table used by each physical connection, the overhead code block transmitted over each physical connection further comprises fields used for a management channel, and the management channel is used to: when the timeslot configuration table used by each physical connection changes, transmit content of a changed timeslot configuration table.
Method for determining a wear state of components of a suspension means arrangement of an elevator system , the method comprising: - monitoring an actual time curve of a first parameter which correlates with the wear state of at least one first monitored component of the components; - comparing the actual time curve of the monitored first parameter with a predetermined expected time curve of the first parameter; - determining the wear state of the monitored component based on a result of the comparison, characterized in that the wear state is determined based on an incipient decrease in a modulus of elasticity of a cable-like suspension means of the suspension means arrangement after a preceding successive increase in the modulus of elasticity of the cable-like suspension means . - monitoring an actual time curve of a first parameter which correlates with the wear state of at least one first monitored component of the components; - comparing the actual time curve of the monitored first parameter with a predetermined expected time curve of the first parameter; - determining the wear state of the monitored component based on a result of the comparison, characterized in that the wear state is determined based on an incipient decrease in a modulus of elasticity of a cable-like suspension means of the suspension means arrangement after a preceding successive increase in the modulus of elasticity of the cable-like suspension means .
A magnetic bearing , adapted to equip a rotary apparatus, wherein the magnetic bearing comprises: - an actuator sub-assembly provided with a magnetic base and at least three actuator bobbins mounted on the magnetic base , and - a sensor sub-assembly provided with at least three magnetic sensor bobbins associated with the actuator bobbins ; at least one sub-assembly (2 ; 4) amidst the actuator sub-assembly and the sensor sub-assembly comprising at least three sectors mounted together; and each sector including: - at least one actuator bobbin when the sector belongs to the actuator sub-assembly , or - at least one magnetic sensor bobbin when the sector belongs to the sensor sub-assembly wherein the sensor sub-assembly comprises a base and an intermediate magnetic support which is provided with sensor horns and is fastened between the base and each magnetic sensor bobbin received on one of the sensor horns . - an actuator sub-assembly provided with a magnetic base and at least three actuator bobbins mounted on the magnetic base , and - a sensor sub-assembly provided with at least three magnetic sensor bobbins associated with the actuator bobbins ; - at least one actuator bobbin when the sector belongs to the actuator sub-assembly , or - at least one magnetic sensor bobbin when the sector belongs to the sensor sub-assembly
A variable pressure system for both the compression and expansion of gases comprising: a hydraulic cylinder having a first stroke and a second stroke; a gas tank ; and a variable pressure vessel having a volume and being operably connected to the hydraulic cylinder and operably connected to the tank; wherein the variable pressure vessel includes: a liquid chamber having a variable volume that changes responsive to the first stroke and the second stroke; a gas chamber having a variable volume that changes responsive to the first stroke and the second stroke, characterized in that the gas chamber has an outer wall wherein at least a portion of the outer wall is thermally conductive and allows heat to transfer therethrough; and the variable pressure system has a moveable flexible barrier between the liquid chamber and the gas chamber , and wherein movement of the moveable barrier causes the volume in the liquid chamber and the volume in the gas chamber to displace each other and the volume in the gas chamber plus the volume in the liquid chamber is generally constant and generally equals the volume in the variable pressure vessel . a hydraulic cylinder having a first stroke and a second stroke; a gas tank ; and a variable pressure vessel having a volume and being operably connected to the hydraulic cylinder and operably connected to the tank; wherein the variable pressure vessel includes: a liquid chamber having a variable volume that changes responsive to the first stroke and the second stroke; a gas chamber having a variable volume that changes responsive to the first stroke and the second stroke, characterized in that the gas chamber has an outer wall wherein at least a portion of the outer wall is thermally conductive and allows heat to transfer therethrough; and the variable pressure system has a moveable flexible barrier between the liquid chamber and the gas chamber , and wherein movement of the moveable barrier causes the volume in the liquid chamber and the volume in the gas chamber to displace each other and the volume in the gas chamber plus the volume in the liquid chamber is generally constant and generally equals the volume in the variable pressure vessel . a liquid chamber having a variable volume that changes responsive to the first stroke and the second stroke; a gas chamber having a variable volume that changes responsive to the first stroke and the second stroke, characterized in that the gas chamber has an outer wall wherein at least a portion of the outer wall is thermally conductive and allows heat to transfer therethrough; and the variable pressure system has a moveable flexible barrier between the liquid chamber and the gas chamber , and wherein movement of the moveable barrier causes the volume in the liquid chamber and the volume in the gas chamber to displace each other and the volume in the gas chamber plus the volume in the liquid chamber is generally constant and generally equals the volume in the variable pressure vessel .
Method for preparing a reconditioning of a damaged portion of a component , particularly of an aircraft, by adding an insert , which fills and/or bridges the damaged portion , comprising the steps of: a. Producing a 3D CAD repair model of the damaged portion by scanning; b. Analysing the repair model and thus evaluating complexity of the damage and/or its reconditioning; c. As a function of the complexity, deciding between at least two alternative means to perform at least a following step d: d. Analysing the repair model and thus dimensioning the reconditioning including the insert ; e. Producing the insert having at least one fastening structure integrated; and working the damaged portion and thus creating a complementary structure adapted to cooperate with the fastening structure , wherein the fastening structure is a pin or a rivet. a. Producing a 3D CAD repair model of the damaged portion by scanning; b. Analysing the repair model and thus evaluating complexity of the damage and/or its reconditioning; c. As a function of the complexity, deciding between at least two alternative means to perform at least a following step d: d. Analysing the repair model and thus dimensioning the reconditioning including the insert ; e. Producing the insert having at least one fastening structure integrated; and working the damaged portion and thus creating a complementary structure adapted to cooperate with the fastening structure , wherein the fastening structure is a pin or a rivet.
A wind generator , comprising a wind wheel which is mounted so that it is rotatable about a horizontal or approximately horizontal rotational axis, and which has one or more blades or other wind-guiding surfaces for converting flow energy of the wind into rotational energy, and at least one generator , coupled to the hub or shaft of the wind wheel or to the output shaft of a gear connected thereto, for converting the rotational energy into electrical energy, wherein the center of gravity of the wind wheel , together with the hub and rotor shaft and rotatable parts coupled thereto which rotate about the same rotational axis, is translationally movable in a direction completely or predominantly in parallel to the rotational axis of the wind turbine , wherein the wind wheel is neither arranged within a wind tunnel nor surrounded by wind deflector blades, so that the wind wheel is always able to catch a maximum of the inflowing air, characterized in that a) the wind generator is designed as a road vehicle with bottom-side wheels, b) wherein the road vehicle is designed for a translational propulsion in a direction parallel to the rotational axis of the wind wheel in order to virtually increase or reduce the inflow velocity of the wind, c) and wherein a freewheel is situated between the wind wheel and the electric generator associated therewith, so that in the event of a countergust, the electric generator , despite the decelerated wind wheel , can continue to rotate freely in a practically undecelerated manner. a) the wind generator is designed as a road vehicle with bottom-side wheels, b) wherein the road vehicle is designed for a translational propulsion in a direction parallel to the rotational axis of the wind wheel in order to virtually increase or reduce the inflow velocity of the wind, c) and wherein a freewheel is situated between the wind wheel and the electric generator associated therewith, so that in the event of a countergust, the electric generator , despite the decelerated wind wheel , can continue to rotate freely in a practically undecelerated manner.
A refractometer apparatus for optically measuring a refractive index difference, comprising a light source unit for providing a light beam, a measurement cell arrangement having a reference cell and a sample cell , a position sensitive device which comprises a lateral-effect photodiode having an active layer and a first and a second electric contact point for receiving a current each on opposing sides of the active layer an optical focusing module for focusing the light beam to a spot on the active layer a concave lens element arranged between the measurement cell arrangement and the position sensitive device , and a reflector which is arranged to reflect light of the light beam at an angle, which light has traversed the measurement cell arrangement having the reference cell and the sample cell , back to the measurement cell arrangement to traverse the measurement cell arrangement a second time before traversing the concave lens element and being incident on the active layer of the lateral-effect photodiode of the position sensitive device , and wherein the position sensitive device is adapted to provide an indication of the position of the spot on the active layer , wherein the reflector is arranged to reflect the light of a first beam path between the light source unit and the reflector at an angle of less than 15 degrees to a second beam path between the reflector and the active layer of the lateral-effect photodiode, and wherein the concave lens element is trimmed at one side so as to reduce its size in one direction substantially perpendicular to the light beam propagation direction, wherein the trimmed side of the concave lens element is arranged close to the first beam path and the first beam path is unobstructed by the concave lens element , and wherein the concave lens element is arranged in the second beam path between the measurement cell arrangement and the position sensitive device so as to change the focal length of the light which traversed the measurement cell arrangement twice.
A fiber optic sensor comprising: a light source , a polarizing element , a detector , a polarization maintaining, PM, fiber , and a sensing element , wherein the sensor further comprises a cross-coupling element in an optical path between the polarizing element and the sensing element , with the cross-coupling element generating a defined cross-coupling between the two orthogonal polarizations of the fundamental mode in the PM fiber , and wherein the cross-coupling element and the sensing element are separated along the optical path, characterised in that the cross-coupling element and the sensing element are separated by at least one element selected from the group consisting of: at least a section of PM fiber , a retarder , a Faraday rotator , and combinations thereof. a light source , a polarizing element , a detector , a polarization maintaining, PM, fiber , and a sensing element , wherein the sensor further comprises a cross-coupling element in an optical path between the polarizing element and the sensing element , with the cross-coupling element generating a defined cross-coupling between the two orthogonal polarizations of the fundamental mode in the PM fiber , and wherein the cross-coupling element and the sensing element are separated along the optical path, characterised in that the cross-coupling element and the sensing element are separated by at least one element selected from the group consisting of: at least a section of PM fiber , a retarder , a Faraday rotator , and combinations thereof.
An air nozzle cleaning tool suitable for cleaning an air nozzle , comprising a housing , at least one air knife element in said housing, each air knife element having an air knife discharge slot suitable for discharging air and at least one tab extending from said air knife discharge slot, wherein the air knife discharge slot and the at least one tab are configured to be alignable with a slot in the air nozzle to be cleaned.
Single-axle vehicle (E) with a drive , a cooler and a first spiked roller and a second spiked roller , wherein a cross member is arranged between the first spiked roller and the second spiked roller , wherein the drive and the cooler are arranged on the cross member , wherein the drive is connected in a force-transmitting manner to the two spiked rollers and is operatively connected to the cooler , wherein the cooler is arranged facing the first spiked roller and/or the second spiked roller so as to receive air, wherein the first spiked roller and/or the second spiked roller is/are designed to be air-permeable, wherein the first spiked roller and/or the second spiked roller each consist of a roller tube , characterized in that in an inner section of the roller tube an outer shell and an inner shell are arranged, wherein the outer shell and the inner shell have a funnel shape , wherein the first funnel shape of the outer shell forms a first base and the second funnel shape forms a second base .
A mobile device for enabling secure authentication between a user and a third party using a one-time-passcode, OTP, authentication mechanism, the mobile device comprising: a display for displaying information to the user; a local one-time-passcode generating module which is configured to: generate at regular intervals a local one-time passcode which is unique to the mobile device, wherein the local one-time-passcode is a regularly changing local one-time-passcode; receive (S300, S400), from a remote authentication module , a third party one-time passcode which is unique to the third party via an SMS message sent from the remote authentication module; and combine (S306, S406) the local one-time passcode with the third party one-time-passcode to generate a combined one-time-passcode for authenticating the user to the third party wherein the combined one-time-passcode is displayed to the user on the display. a display for displaying information to the user; a local one-time-passcode generating module which is configured to: generate at regular intervals a local one-time passcode which is unique to the mobile device, wherein the local one-time-passcode is a regularly changing local one-time-passcode; receive (S300, S400), from a remote authentication module , a third party one-time passcode which is unique to the third party via an SMS message sent from the remote authentication module; and combine (S306, S406) the local one-time passcode with the third party one-time-passcode to generate a combined one-time-passcode for authenticating the user to the third party wherein the combined one-time-passcode is displayed to the user on the display. generate at regular intervals a local one-time passcode which is unique to the mobile device, wherein the local one-time-passcode is a regularly changing local one-time-passcode; receive (S300, S400), from a remote authentication module , a third party one-time passcode which is unique to the third party via an SMS message sent from the remote authentication module; and combine (S306, S406) the local one-time passcode with the third party one-time-passcode to generate a combined one-time-passcode for authenticating the user to the third party wherein the combined one-time-passcode is displayed to the user on the display.
Method of heteroepitaxial growth of III-Nitride semiconductors on a substrate, which substrate may be any of a single-crystal diamond, a polycrystalline diamond, silicon, germanium or an alloy with chemical formula Si x C y Ge 1-(x+y) , whereby 0≤ x,y ≤1, 0≤ x+y ≤1 and x or y less than 0.5, comprising the growing of an AlN nucleation layer on the substrate using active nitrogen species produced by a nitrogen plasma source, whereby the thickness of the AlN nucleation layer is less than 5 nm, and overgrowing the AlN nucleation layer by a layer of a III-nitride compound with orientation and III metal-face polarity.
A thermal sprayed coating for a sliding member, composed of an iron-based alloy containing chromium (Cr), carbon (C ), silicon (Si) and manganese (Mn), wherein a content of chromium is 8 mass % or more and 20 mass % or less, a content of carbon is 0,005 mass % or more and 0,2 mass % or less, a content of silicon is 0,1 mass % or more and 0,5 mass % or less, a content of manganese is 0,3 mass % or more and 4 mass % or less, andthe thermal sprayed coating includes a structure in which the average grain diameter of the crystal grains is 3 μm or less, and Vickers hardness is 300 Hv or more. a content of chromium is 8 mass % or more and 20 mass % or less, a content of carbon is 0,005 mass % or more and 0,2 mass % or less, a content of silicon is 0,1 mass % or more and 0,5 mass % or less, a content of manganese is 0,3 mass % or more and 4 mass % or less, andthe thermal sprayed coating includes a structure in which the average grain diameter of the crystal grains is 3 μm or less, and Vickers hardness is 300 Hv or more.
An aircraft door which can be mounted in a fuselage in a reference frame X, Y, Z and comprising a casing forming a coaming rigidly connected to the fuselage, a door leaf and a door arm , this door arm connecting the door leaf to the casing by means of a hanging system enabling the door leaf to be installed and the position thereof relative to the fuselage to be adjusted, this system comprising a pair of fasteners each comprising a pivot that is rotary about a common axis parallel to the axis Z, a base fastened to the casing , and a trolley that is movable on this base along the axis Y, the base and the trolley of each fastener forming two translational adjustment links in directions parallel to the axes X and Y to adjust the position of the door, said translation adjustment linkages forming adjustments axe, said this aircraft door being characterized in that , for each of the fasteners , the directions of the adjustment axes are secant in a plane parallel to the plane XY