mhurhangee/patent-ind-claim-en huggingface dataset:
A method of selectively enabling one of a first and a second operating mode in a repeater , the repeater providing access to a network, the repeater having a wireless receiver and a wireless transmitter for providing bidirectional communication with a mobile station through a first wireless link, wherein, in the first operating mode, the wireless transmitter is not continuously enabled, and wherein, in the second operating mode, the wireless transmitter is continuously enabled, the method including, at the repeater and in the first operating mode: - receiving, from an access point , status information about a second wireless link between the access point and the mobile station; - receiving, a probe message from the mobile station; - determining, from the received status information and information provided by the probe message from the mobile station, a spatial distance of the mobile station to the repeater and to the access point; and - switching to the second operating mode, allowing association of the mobile station with the repeater via the first wireless link, based on the spatial distance of the mobile station to the repeater and to the access point determined from the received status information and information provided by the probe message from the mobile station. - receiving, from an access point , status information about a second wireless link between the access point and the mobile station; - receiving, a probe message from the mobile station; - determining, from the received status information and information provided by the probe message from the mobile station, a spatial distance of the mobile station to the repeater and to the access point; and - switching to the second operating mode, allowing association of the mobile station with the repeater via the first wireless link, based on the spatial distance of the mobile station to the repeater and to the access point determined from the received status information and information provided by the probe message from the mobile station.
A remote electrical tilt antenna management apparatus, comprising: an obtaining module , configured to obtain a first permission configuration file, wherein the first permission configuration file comprises information about a first permission of a first base station to perform an operation on a first remote electrical tilt, RET, unit; and a configuration module , configured to configure , according to the first permission configuration file, the first permission of the first base station to perform an operation on the first RET; characterized in that the configuration module is further configured to configure, according to the first permission configuration file, a second permission of a second base station to perform an operation on the first RET; and wherein the first permission is a control permission and the second permission is a query permission or the first permission is a query permission and the second permission is a control permission. an obtaining module , configured to obtain a first permission configuration file, wherein the first permission configuration file comprises information about a first permission of a first base station to perform an operation on a first remote electrical tilt, RET, unit; and a configuration module , configured to configure , according to the first permission configuration file, the first permission of the first base station to perform an operation on the first RET; characterized in that the configuration module is further configured to configure, according to the first permission configuration file, a second permission of a second base station to perform an operation on the first RET; and wherein the first permission is a control permission and the second permission is a query permission or the first permission is a query permission and the second permission is a control permission.
An environmental control system (ECS, 12) for an aircraft , the environmental control system comprising: an ECS refrigeration unit configured to receive ambient air and a first portion and a second portion of hot bleed air, wherein the ECS refrigeration unit is operable to: indirectly exchange heat between the first portion of the hot bleed air and the ambient air to form a partially cooled, hot air stream ; and compress, further indirect heat exchange, and expand the partially cooled, hot air stream to form a cooled and expanded air stream having a temperature of less than -3.33°C (26°F), the ECS refrigeration unit comprising a low limit valve configured to introduce the second portion of the hot bleed air to the cooled and expanded air stream ; and characterized in that the ECS comprises a low limit valve control configured to regulate the low limit valve to control the rate of introduction of the second portion of the hot bleed air to the cooled and expanded air stream to form a combined air stream that when exiting the ECS refrigeration unit is a sub-freezing air stream having a temperature of less than 0°C (32°F) but greater than the cooled and expanded air stream , and a duct that is disposed downstream from the ECS refrigeration unit and that is configured to receive the sub-freezing air stream , and wherein the duct has an inner surface that comprises an ice-phobic treatment . indirectly exchange heat between the first portion of the hot bleed air and the ambient air to form a partially cooled, hot air stream ; and compress, further indirect heat exchange, and expand the partially cooled, hot air stream to form a cooled and expanded air stream having a temperature of less than -3.33°C (26°F), the ECS refrigeration unit comprising a low limit valve configured to introduce the second portion of the hot bleed air to the cooled and expanded air stream ; and characterized in that the ECS comprises a low limit valve control configured to regulate the low limit valve to control the rate of introduction of the second portion of the hot bleed air to the cooled and expanded air stream to form a combined air stream that when exiting the ECS refrigeration unit is a sub-freezing air stream having a temperature of less than 0°C (32°F) but greater than the cooled and expanded air stream , and a duct that is disposed downstream from the ECS refrigeration unit and that is configured to receive the sub-freezing air stream , and wherein the duct has an inner surface that comprises an ice-phobic treatment .
Sowing unit for a single-grain seed drill comprising: - a first storage container for storing seed, - soil cultivation tools for opening and closing a sowing furrow, - at least one separating device designed for the individual dispensing of seed from the storage container into the sowing furrow by means of a pressure difference generated by a fan, - at least one second storage container for storing granular material, - at least one metering device for the metered dispensing of granular material from the second storage container into a delivery line , characterized in that the delivery line is connected to the metering device via an injector device , and an air flow can be supplied to the injector device via an air inlet , wherein the granular material is accelerated in the delivery line by the air flow directed through the injector device , wherein an exhaust air flow, in particular mixed with dust particles and/or dressing agents, exits the separating device due to the application of the pressure difference, in that the sowing unit comprises an exhaust air system , which is designed to capture the exiting exhaust air flow and to supply it to the injector device by means of an exhaust air line , so that the air flow is at least partially provided by the captured exhaust air flow. - a first storage container for storing seed, - soil cultivation tools for opening and closing a sowing furrow, - at least one separating device designed for the individual dispensing of seed from the storage container into the sowing furrow by means of a pressure difference generated by a fan, - at least one second storage container for storing granular material, - at least one metering device for the metered dispensing of granular material from the second storage container into a delivery line ,
A drapable electronic component, comprising: • an electronic layer formed by printing ink, and • a protective layer characterized in that : • the protective layer forms a complex which comprises a fabric and a protective polymer layer coating one side of the fabric • the electronic layer is deposited on the fabric, on the side of the fabric opposite the deposition side of the protective polymer layer • the fabric is obtained by weaving continuous yarns and is characterized by a cover factor CF25 higher than or equal to 0.5, typically of 0.5 to 3, in particular between 0.6 and 2.5, more particularly between 0.7 and 2, for example between 0.7 and 1.5, CF25 being calculated as follows: CF25 = [(number of filaments/cm × diameter of 1 filament in cm) warp + (number of filaments/cm × diameter of 1 filament in cm) weft ] × 25 / thickness of said fabric in μm. • an electronic layer formed by printing ink, and • a protective layer • the protective layer forms a complex which comprises a fabric and a protective polymer layer coating one side of the fabric • the electronic layer is deposited on the fabric, on the side of the fabric opposite the deposition side of the protective polymer layer • the fabric is obtained by weaving continuous yarns and is characterized by a cover factor CF25 higher than or equal to 0.5, typically of 0.5 to 3, in particular between 0.6 and 2.5, more particularly between 0.7 and 2, for example between 0.7 and 1.5, CF25 being calculated as follows: CF25 = [(number of filaments/cm × diameter of 1 filament in cm) warp + (number of filaments/cm × diameter of 1 filament in cm) weft ] × 25 / thickness of said fabric in μm.
Drinking vessel with a teat and a fastening ring in particular for infants and small children, the teat comprising - a hollow suction part with at least one through-hole for liquid nutrition, - which is connected at the bottom to a substantially annular disc-shaped nipple flange which serves to be fastened to the mouth of the vessel by means of the fastening ring with an annular disc-shaped ring flange overlapping the nipple flange for pressing the bottom side of the nipple flange flat against the front-side edge of the mouth , and - at least one recess (14.1, 14.2) extending in the radial direction of the nipple flange on the top side of the nipple flange , wherein the at least one recess (14.1, 14.2) is designed in such a way that the ring flange pressing against the top side of the nipple flange has a gap from the upper side of the floor (15.1, 15.2) of the recess (14.1, 14.2) during the fastening of the teat on the mouth of the vessel , and the nipple flange has sufficient flexibility at least in the area of the recess (14.1, 14.2) so that the floor (15.1, 15.2) arches up and air from outside flows back into the vessel under the arched floor (15.1, 15.2) of the recess (14.1, 14.2) in the radial direction when the teat is fastened on the mouth of the vessel and a negative pressure is created in the vessel when the suction part is sucked on. characterized in that the floor (15.1, 15.2) of the recess (14.1, 14.2) has a downwards curvature, which is pressed flat when the suction part is mounted on the vessel by means of the fastening ring , so that the floor (15.1, 15.2) of the recess (14.1, 14.2) rests against the edge of the mouth under elastic initial tension. - a hollow suction part with at least one through-hole for liquid nutrition, - which is connected at the bottom to a substantially annular disc-shaped nipple flange which serves to be fastened to the mouth of the vessel by means of the fastening ring with an annular disc-shaped ring flange overlapping the nipple flange for pressing the bottom side of the nipple flange flat against the front-side edge of the mouth , and - at least one recess (14.1, 14.2) extending in the radial direction of the nipple flange on the top side of the nipple flange , wherein the at least one recess (14.1, 14.2) is designed in such a way that the ring flange pressing against the top side of the nipple flange has a gap from the upper side of the floor (15.1, 15.2) of the recess (14.1, 14.2) during the fastening of the teat on the mouth of the vessel , and the nipple flange has sufficient flexibility at least in the area of the recess (14.1, 14.2) so that the floor (15.1, 15.2) arches up and air from outside flows back into the vessel under the arched floor (15.1, 15.2) of the recess (14.1, 14.2) in the radial direction when the teat is fastened on the mouth of the vessel and a negative pressure is created in the vessel when the suction part is sucked on.
Use of a composition containing 1,8-para-menthenethiol and 3-mercaptohexyl acetate as an odor-masking agent.
A solid-state image pickup element , comprising: a plurality of effective pixels arranged in a matrix form and not shielded from light, wherein each of the plurality of effective pixels includes: a photodiode configured to convert incident light into a photocurrent; an amplification transistor configured to amplify a voltage between a gate of the amplification transistor having a potential depending on the photocurrent and a source of the amplification transistor having a reference potential (GND) and output the amplified voltage from a drain of the amplification transistor ; characterized in that the solid-state image pickup element further includes a potential supply section configured to, in each of the plurality of effective pixels, supply the anode of the photodiode and the bulk of the amplification transistor with a predetermined potential lower than the reference potential (GND). a photodiode configured to convert incident light into a photocurrent; an amplification transistor configured to amplify a voltage between a gate of the amplification transistor having a potential depending on the photocurrent and a source of the amplification transistor having a reference potential (GND) and output the amplified voltage from a drain of the amplification transistor ; characterized in that the solid-state image pickup element further includes a potential supply section configured to, in each of the plurality of effective pixels, supply the anode of the photodiode and the bulk of the amplification transistor with a predetermined potential lower than the reference potential (GND).
A head tube for a bicycle for providing a coupling between a bicycle frame and a wheel of the bicycle , where the head tube comprises a central axis (D), where the head tube comprises - a tubular member comprising a terminal first edge and a terminal second edge - a first bearing having a first diameter (A), - a second bearing having a second diameter (A), - where the first bearing and the second bearing are adapted to provide a rotation around the central axis (D) of the head tube , - where the first bearing is arranged in a first position in a direction along the central axis (D) where the first position is closer to the terminal first edge than the terminal second edge and the second bearing is arranged in a second position in a direction along the central axis (D) where the second position is closer to the terminal second edge than the terminal first edge, - characterised in that the size of the first and/or second diameter (A) is larger than the distance from the first position of the first bearing to the second position of the second bearing . - a tubular member comprising a terminal first edge and a terminal second edge - a first bearing having a first diameter (A), - a second bearing having a second diameter (A), - where the first bearing and the second bearing are adapted to provide a rotation around the central axis (D) of the head tube , - where the first bearing is arranged in a first position in a direction along the central axis (D) where the first position is closer to the terminal first edge than the terminal second edge and the second bearing is arranged in a second position in a direction along the central axis (D) where the second position is closer to the terminal second edge than the terminal first edge, - characterised in that the size of the first and/or second diameter (A) is larger than the distance from the first position of the first bearing to the second position of the second bearing .
System for Content Distribution Internetworking, comprising: - a plurality of Content Delivery Networks, CDN, each defining an operating business (OB i ) having its respective local origin server (OS i ), said defined operating business (OB i ) being an arbitrary geographic area; and - computing means for performing the interconnection of said plurality of CDNs, wherein: - said computing means comprises of a global origin server, (OS G ), configured to coordinate. the formation of a global network by connecting to some or all of the said local origin servers (OS i ) in each of the said operating business (OB i )s; and - said global origin server (OS G ), is configured to maintain meta-data of the buckets that are in each of said local origin server (OS i ) in the plurality of CDNs, said buckets being logical containers holding CDN content, so in case a requested content is not in said local origin server (OS i ) the location of said requested content is determined from said global origin server (OS G ), and wherein the system is adapted and configured to implement the method of claim 15. - a plurality of Content Delivery Networks, CDN, each defining an operating business (OB i ) having its respective local origin server (OS i ), said defined operating business (OB i ) being an arbitrary geographic area; and - computing means for performing the interconnection of said plurality of CDNs, wherein: - said computing means comprises of a global origin server, (OS G ), configured to coordinate. the formation of a global network by connecting to some or all of the said local origin servers (OS i ) in each of the said operating business (OB i )s; and - said global origin server (OS G ), is configured to maintain meta-data of the buckets that are in each of said local origin server (OS i ) in the plurality of CDNs, said buckets being logical containers holding CDN content,
Electric propulsion architecture for a multi-rotor vertical take-off and landing aircraft, comprising: - N electric generators (G1-G4), N being an integer greater than or equal to 2, - N pairs of rotors (R1_2 - R2_1; R3_4 - R4_3; R5_6 - R6_5; R7_8 - R8_7), characterised in that the architecture further comprises: - for each rotor, a first electric motor (106a-h) and a second electric motor (108a-h), the first electric motor (106a-h) being configured to operate in an active mode and the second electric motor (108a-h) being configured to be in a standby mode and being able to operate in an active mode in a breakdown situation, - for each rotor, a propeller (110a-h) coupled to the first and second electric motors (106a-h, 108a-h) so that, in operation, the first electric motor (106a-h) drives the propeller, wherein, for each pair of rotors (R1_2 - R2_1; R3_4 - R4_3; R5_6 - R6_5; R7_8 - R8_7), one of N electric generators powers the first electric motors (106a-h) of the rotors of a pair of rotors, and another of the N electric generators powers the second electric motors (108a-h) of the rotors of a pair of rotors, and wherein the rotors form counter-rotors (R1_2 - R6_5; R2_1 - R5_6; R3_4 - R8_7; R4_3 - R7_8), and for each counter-rotor, the first and second electric motors (106a-h, 108a-h) of the rotors of each counter-rotor are each powered by one of N electric generators (G1-G4) so that the N electric generators power the first and second electric motors (106a-h, 108a-h) of the rotors of each counter-rotor. - N electric generators (G1-G4), N being an integer greater than or equal to 2, - N pairs of rotors (R1_2 - R2_1; R3_4 - R4_3; R5_6 - R6_5; R7_8 - R8_7), characterised in that the architecture further comprises: - for each rotor, a first electric motor (106a-h) and a second electric motor (108a-h), the first electric motor (106a-h) being configured to operate in an active mode and the second electric motor (108a-h) being configured to be in a standby mode and being able to operate in an active mode in a breakdown situation, - for each rotor, a propeller (110a-h) coupled to the first and second electric motors (106a-h, 108a-h) so that, in operation, the first electric motor (106a-h) drives the propeller, wherein, for each pair of rotors (R1_2 - R2_1; R3_4 - R4_3; R5_6 - R6_5; R7_8 - R8_7), one of N electric generators powers the first electric motors (106a-h) of the rotors of a pair of rotors, and another of the N electric generators powers the second electric motors (108a-h) of the rotors of a pair of rotors, and wherein the rotors form counter-rotors (R1_2 - R6_5; R2_1 - R5_6; R3_4 - R8_7; R4_3 - R7_8), and for each counter-rotor, the first and second electric motors (106a-h, 108a-h) of the rotors of each counter-rotor are each powered by one of N electric generators (G1-G4) so that the N electric generators power the first and second electric motors (106a-h, 108a-h) of the rotors of each counter-rotor.
A method for authenticating a client (1-1, 2-1), the method comprising: - receiving (2-18, 3-18) a parameter value (1-5, 1-6, 1-7) of a device; - receiving (2-20, 3-20) an authentication value of the client; - authenticating (2-21, 3-21) the client based on the authentication value and the parameter value characterized by a step of - determining (2-14, 3-14) the device (1-4, 2-4) to be used for authentication of the client; and in that the device comprises a counter and the parameter value comprises a counter value, and/or the device comprises a level indicator and the parameter value comprises an indicated level, the authentication value comprises a read value of the counter value and/or a read value of the indicated level. - receiving (2-18, 3-18) a parameter value (1-5, 1-6, 1-7) of a device; - receiving (2-20, 3-20) an authentication value of the client; - authenticating (2-21, 3-21) the client based on the authentication value and the parameter value characterized by a step of - determining (2-14, 3-14) the device (1-4, 2-4) to be used for authentication of the client; the device comprises a counter and the parameter value comprises a counter value, and/or the device comprises a level indicator and the parameter value comprises an indicated level, the authentication value comprises a read value of the counter value and/or a read value of the indicated level.
Bearing support for an aircraft engine, manufactured in one piece by powder-bed additive manufacturing from a manufacturing platform (T), comprising a cylindrical element including an annular stiffener with a cross-section that changes along its circumference, this stiffener being formed with alternating portions having a cross-section, as a radial cross-section of the cylindrical element, of a shape corresponding to that of the letter Γ needing to be supported during the additive manufacturing, and of portions having a cross-section, as a radial cross-section of the cylindrical element, of a shape corresponding to that of the letter γ not supported during the additive manufacturing.