mhurhangee/patent-ind-claim-en huggingface dataset:
A station, STA, comprising: a processor; and a transceiver, the processor and the transceiver configured to: receive, from an access point, AP, a solicitation for basic service set, BSS, color information of an overlapping BSS, OBSS; transmit, in response to the solicitation, a high efficiency, HE, operation element that includes the BSS color information of the OBSS; receive, from the AP in a BSS that the STA is associated with, a BSS color change announcement element that includes a BSS color information field and a color switching time field, wherein the BSS color information field indicates a new BSS color determined based on the transmitted BSS color information of the OBSS, and the color switching time field indicates when the AP will switch to the new BSS color; and use the new BSS color for communication with the AP after the AP switches to the new BSS color. a processor; and a transceiver, the processor and the transceiver configured to: receive, from an access point, AP, a solicitation for basic service set, BSS, color information of an overlapping BSS, OBSS; transmit, in response to the solicitation, a high efficiency, HE, operation element that includes the BSS color information of the OBSS; receive, from the AP in a BSS that the STA is associated with, a BSS color change announcement element that includes a BSS color information field and a color switching time field, wherein the BSS color information field indicates a new BSS color determined based on the transmitted BSS color information of the OBSS, and the color switching time field indicates when the AP will switch to the new BSS color; and use the new BSS color for communication with the AP after the AP switches to the new BSS color. receive, from an access point, AP, a solicitation for basic service set, BSS, color information of an overlapping BSS, OBSS; transmit, in response to the solicitation, a high efficiency, HE, operation element that includes the BSS color information of the OBSS; receive, from the AP in a BSS that the STA is associated with, a BSS color change announcement element that includes a BSS color information field and a color switching time field, wherein the BSS color information field indicates a new BSS color determined based on the transmitted BSS color information of the OBSS, and the color switching time field indicates when the AP will switch to the new BSS color; and use the new BSS color for communication with the AP after the AP switches to the new BSS color.
Sensor system comprising a frame supporting a force-sensing tip arranged to generate a signal based upon a force applied by said force-sensing tip to a material to be tested, characterised in that said system further comprises: - an input drum mounted in said frame such that it can rotate about an input axis of rotation (A); - an output lever supported by said frame by means of an output revolute joint defining an output axis of rotation (C); wherein said force-sensing tip is mounted on said output lever such that said force-sensing tip is arranged to be brought into contact with a material to be tested; and wherein said sensor system comprises a mechanical transmission (302, 303, 304, 305, 307; 301a, 312) arranged to kinematically link said input drum to said output lever such that a rotation of said input drum about said input axis of rotation (A) causes said output lever to pivot in an oscillatory manner about said output axis of rotation (C). - an input drum mounted in said frame such that it can rotate about an input axis of rotation (A); - an output lever supported by said frame by means of an output revolute joint defining an output axis of rotation (C);
An aerosol generating device , comprising: a liquid source of a liquid aerosol formulation comprising a high volatility carrier and a second component; a flow passage in fluid communication with the liquid source ; a heater disposed to heat liquid aerosol formulation in a heated portion of the flow passage to produce a vapor which admixes with air to produce an aerosol; a mouthpiece through which the aerosol is inhaled by a user of the aerosol generating device ; a power supply; a controller operable to deliver power from the power supply to the heater so as to maintain the heater at a temperature range effective to vaporize the liquid aerosol formulation in the flow passage ; a pressure sensor ; an air passage through which air is supplied into the mouthpiece ; and a valve which opens and closes the air passage ; wherein the controller is operable to actuate the valve within a predetermined time period after the pressure sensor detects a pressure drop in the mouthpiece as the user inhales on the mouthpiece to allow air to be supplied into the mouthpiece. a liquid source of a liquid aerosol formulation comprising a high volatility carrier and a second component; a flow passage in fluid communication with the liquid source ; a heater disposed to heat liquid aerosol formulation in a heated portion of the flow passage to produce a vapor which admixes with air to produce an aerosol; a mouthpiece through which the aerosol is inhaled by a user of the aerosol generating device ; a power supply; a controller operable to deliver power from the power supply to the heater so as to maintain the heater at a temperature range effective to vaporize the liquid aerosol formulation in the flow passage ; a pressure sensor ; an air passage through which air is supplied into the mouthpiece ; and a valve which opens and closes the air passage ; wherein the controller is operable to actuate the valve within a predetermined time period after the pressure sensor detects a pressure drop in the mouthpiece as the user inhales on the mouthpiece to allow air to be supplied into the mouthpiece.
Optical module for an independent line of sight, in relation to a second line, wherein the optical module is capable of being arranged on a sight unit and wherein the optical module contains at least a first mirror and at least a movably arranged second mirror , characterised in that it is possible to select, by moving the first mirror; i) that the optical module provides an independent line of sight, when the optical path passes via a second entry point arranged on the optical module, via at least the movably arranged second mirror and the first mirror, to an exit point arranged on the optical module, or ii) that the optical module does not influence the optical path through the optical module, when the optical path passes freely through the optical module through a first entry point arranged on the optical module to the exit point arranged on the optical module. i) that the optical module provides an independent line of sight, when the optical path passes via a second entry point arranged on the optical module, via at least the movably arranged second mirror and the first mirror, to an exit point arranged on the optical module, or ii) that the optical module does not influence the optical path through the optical module, when the optical path passes freely through the optical module through a first entry point arranged on the optical module to the exit point arranged on the optical module.
A bearing monitoring apparatus comprising: a rolling bearing including an outer ring , an inner ring disposed coaxially with the outer ring, the inner ring being on an inner peripheral side of the outer ring, multiple rolling elements disposed between the outer ring and the inner ring, and a strain gauge configured to detect strain of the outer ring or the inner ring, the strain gauge including at least two resistors and the resistors being arranged in a same direction as an arrangement direction of the rolling elements so as to correspond to spacing between rolling elements that are next to each other, characterised in that the bearing monitoring apparatus further comprises a waveform generator configured to generate a first distorted waveform based on an output of one resistor and to generate a second distorted waveform based on an output of another resistor; a subtracting unit configured to subtract the second distorted waveform from the first distorted waveform to generate a differential waveform; and a comparator configured to compare the differential waveform against a reference value to detect a wear state of the rolling bearing. a rolling bearing including an outer ring , an inner ring disposed coaxially with the outer ring, the inner ring being on an inner peripheral side of the outer ring, multiple rolling elements disposed between the outer ring and the inner ring, and a strain gauge configured to detect strain of the outer ring or the inner ring, the strain gauge including at least two resistors and the resistors being arranged in a same direction as an arrangement direction of the rolling elements so as to correspond to spacing between rolling elements that are next to each other, an outer ring , an inner ring disposed coaxially with the outer ring, the inner ring being on an inner peripheral side of the outer ring, multiple rolling elements disposed between the outer ring and the inner ring, and a strain gauge configured to detect strain of the outer ring or the inner ring, the strain gauge including at least two resistors and the resistors being arranged in a same direction as an arrangement direction of the rolling elements so as to correspond to spacing between rolling elements that are next to each other, characterised in that the bearing monitoring apparatus further comprises a waveform generator configured to generate a first distorted waveform based on an output of one resistor and to generate a second distorted waveform based on an output of another resistor; a subtracting unit configured to subtract the second distorted waveform from the first distorted waveform to generate a differential waveform; and a comparator configured to compare the differential waveform against a reference value to detect a wear state of the rolling bearing.
A patient turning apparatus comprising: a reconfigurable support platform comprising: a plurality of laterally extending support slats configured for pivotal movement about a longitudinally extending central region of the platform; at least one support slat being configured to follow a pivotal movement of a longitudinally adjacent support slat about the central region , through at least a portion of a pivotal range of movement of the longitudinally adjacent support slat; the apparatus further comprising means operable to control pivotal movement of at least one support slat of the platform about the central region; wherein the means operable to control pivotal movement of at least one support slat of the platform comprises an inflatable bladder and wherein the support platform further comprises a support sheet comprising a plurality of laterally extending pockets formed therein for separately receiving a support slat. a reconfigurable support platform comprising: a plurality of laterally extending support slats configured for pivotal movement about a longitudinally extending central region of the platform; at least one support slat being configured to follow a pivotal movement of a longitudinally adjacent support slat about the central region , through at least a portion of a pivotal range of movement of the longitudinally adjacent support slat; a plurality of laterally extending support slats configured for pivotal movement about a longitudinally extending central region of the platform; at least one support slat being configured to follow a pivotal movement of a longitudinally adjacent support slat about the central region , through at least a portion of a pivotal range of movement of the longitudinally adjacent support slat; the apparatus further comprising means operable to control pivotal movement of at least one support slat of the platform about the central region; wherein the means operable to control pivotal movement of at least one support slat of the platform comprises an inflatable bladder and wherein the support platform further comprises a support sheet comprising a plurality of laterally extending pockets formed therein for separately receiving a support slat.
An intake structure for an internal combustion engine for use on a saddle-type vehicle , having upper, lower, left, and right ribs for dealing with vibrations and being erected respectively on upper, lower, left, and right surfaces of an intake pipe of the engine , wherein: an injector is disposed between the upper rib and one of the left rib and the right rib , and injector-side installation holes are disposed between the upper rib and the other of the left rib and the right rib , and the injector and the injector-side installation holes are disposed respectively on left and right sides of the upper rib , characterized in that the left and right ribs extend longitudinally along the intake pipe . an injector is disposed between the upper rib and one of the left rib and the right rib , and injector-side installation holes are disposed between the upper rib and the other of the left rib and the right rib , and the injector and the injector-side installation holes are disposed respectively on left and right sides of the upper rib , characterized in that the left and right ribs extend longitudinally along the intake pipe .
An information processing apparatus comprising: a video generation section configured to generate, on a basis of head posture information of a user, a video resulting from control of an angle of view of a virtual camera, the angle of view of the virtual camera corresponding to a field of view of the user within a virtual space, wherein when the user is in a non-acceleration state in the virtual space, the video generation section is configured to generate the video based on a first angle of view of the virtual camera, and wherein when the user is in an acceleration state with acceleration applied in a direction in the virtual space, the video generation section is configured to change the angle of view of the virtual camera from the first angle of view at a time when the user is in the non-acceleration state to a second angle of view based on the acceleration direction of the user in the virtual space and to generate the video based on the second angle of view of the virtual camera in order to induce a visual righting reflex on the user in the real space. a video generation section configured to generate, on a basis of head posture information of a user, a video resulting from control of an angle of view of a virtual camera, the angle of view of the virtual camera corresponding to a field of view of the user within a virtual space, wherein when the user is in a non-acceleration state in the virtual space, the video generation section is configured to generate the video based on a first angle of view of the virtual camera, and wherein when the user is in an acceleration state with acceleration applied in a direction in the virtual space, the video generation section is configured to change the angle of view of the virtual camera from the first angle of view at a time when the user is in the non-acceleration state to a second angle of view based on the acceleration direction of the user in the virtual space and to generate the video based on the second angle of view of the virtual camera in order to induce a visual righting reflex on the user in the real space.
- Tyre having a radial carcass reinforcement comprising a crown reinforcement , itself capped radially with a tread , said tread being joined to two beads via two sidewalls, the crown reinforcement comprising at least one layer of circumferential reinforcing elements , said tread comprising at least one layer of polymer compound forming a tread surface intended to come into contact with a road surface, characterized in that the ratio of the maximum value of tan(δ), denoted tan(δ)max, measured at 60°C on the forward cycle, of said layer of polymer compound forming the tread surface to the complex dynamic shear modulus G ∗ , measured at 25% and 60°C on the forward cycle of said at least one layer of polymer compound forming the tread surface is less than 0.065 and in that the product of the complex dynamic shear modulus G ∗ , measured at 25% and 60°C on the forward cycle of said layer of polymer compound forming the tread surface and the value of deformation at break in elongation of said layer of polymer compound forming the tread surface being greater than or equal to 1280 MPa%.
Process for preparing the complex of formula (II) below: consisting of at least 80% of a diastereoisomeric excess comprising a mixture of the II-RRR and II-SSS isomers of formulae: comprising the following successive steps: a) Complexation of the hexaacid of formula (III) below: with gadolinium to obtain the hexaacid gadolinium complex of formula (I) below: b) Isomerization by heating of the hexaacid gadolinium complex of formula (I) in an aqueous solution with a pH of between 2 and 4, to obtain a diastereoisomerically enriched complex consisting of at least 80% of a diastereoisomeric excess comprising a mixture of the I-RRR and I-SSS isomers of said hexaacid gadolinium complex of formula (I), of formulae: and c) Formation, from the diastereoisomerically enriched complex obtained in step b), of the complex of formula (II), by reaction with 3-amino-1,2-propanediol. a) Complexation of the hexaacid of formula (III) below: with gadolinium to obtain the hexaacid gadolinium complex of formula (I) below: b) Isomerization by heating of the hexaacid gadolinium complex of formula (I) in an aqueous solution with a pH of between 2 and 4, to obtain a diastereoisomerically enriched complex consisting of at least 80% of a diastereoisomeric excess comprising a mixture of the I-RRR and I-SSS isomers of said hexaacid gadolinium complex of formula (I), of formulae: and c) Formation, from the diastereoisomerically enriched complex obtained in step b), of the complex of formula (II), by reaction with 3-amino-1,2-propanediol.
A hydraulic control system of a thrust reverser of a bypass turbojet engine nacelle for an aircraft, comprising actuation and control devices of the thrust reverser including hydraulic cylinders and locks, their hydraulic supply solenoid valves , and sensors , the turbojet engine including a full-authority electronic calculator or the aircraft including an avionics calculator which gives thrust reversal orders, the system including an electronic concentration module distinct from the calculator , carrying out a concentration of all the data related to the operation of the actuation and control devices of the thrust reverser, this module comprising internal contactors for controlling the solenoid valves , means for monitoring the sensors , means for analogically or digitally processing these data carrying out in particular the sequencing of the actuation means, and a communication bus to the calculator , characterized in that some internal contactors piloted by the data processing means , control their solenoid valves in a shared manner with the calculator , with first, upstreams, a control by the calculator , and then, downstreams, a control by the data processing means .
A journal shaft for a journal bearing assembly of an aircraft engine , comprising: a shaft body extending along a longitudinal axis (A), the shaft body having a radially outer surface and a radially inner surface radially spaced apart from the longitudinal axis (A) to define an inner cavity ; and an oil pocket defined in the radially outer surface , one or more passages extending through the shaft body from the radially inner surface to the oil pocket to provide fluid communication between the inner cavity and the oil pocket , the oil pocket including a radially inner base surface and interconnecting transition surfaces extending between the radially inner base surface of the oil pocket and the radially outer surface of the shaft body, wherein the interconnecting transition surfaces form a fluid-dynamically smooth and edgeless transition to the radially outer surface of the journal shaft , characterised in that : the interconnecting transition surfaces define a tangent line relative to the longitudinal axis (A) with a maximum angle (θ) of about six degrees. a shaft body extending along a longitudinal axis (A), the shaft body having a radially outer surface and a radially inner surface radially spaced apart from the longitudinal axis (A) to define an inner cavity ; and an oil pocket defined in the radially outer surface , one or more passages extending through the shaft body from the radially inner surface to the oil pocket to provide fluid communication between the inner cavity and the oil pocket , the oil pocket including a radially inner base surface and interconnecting transition surfaces extending between the radially inner base surface of the oil pocket and the radially outer surface of the shaft body, wherein the interconnecting transition surfaces form a fluid-dynamically smooth and edgeless transition to the radially outer surface of the journal shaft ,
A method for, at a user equipment, UE, performing device-to-device, D2D, communication in a wireless communication system, the method comprising: reporting, using a plurality of radio frequency, RF, circuits implemented in the UE, UE capability information including information about a restricted frequency band among multiple frequency bands aggregated to a base station; and performing a D2D communication with a target UE via a specific frequency band, wherein the D2D communication with the target UE via the specific frequency band and a signal reception from the base station via the restricted frequency band are performed by a same RF circuit among the plurality of RF circuits, wherein the signal reception from the base station via the restricted frequency band is forbidden during the D2D communication with the target UE via the specific frequency band through selecting, among the restricted frequency band and the specific band frequency, the specific frequency band using a switch located prior to the same RF circuit, wherein the UE capability information includes configuration information of the plurality of RF circuits, and wherein the configuration information includes a list of frequency bands which can be used by the plurality of RF circuits for transmission and reception. reporting, using a plurality of radio frequency, RF, circuits implemented in the UE, UE capability information including information about a restricted frequency band among multiple frequency bands aggregated to a base station; and performing a D2D communication with a target UE via a specific frequency band, wherein the D2D communication with the target UE via the specific frequency band and a signal reception from the base station via the restricted frequency band are performed by a same RF circuit among the plurality of RF circuits, wherein the signal reception from the base station via the restricted frequency band is forbidden during the D2D communication with the target UE via the specific frequency band through selecting, among the restricted frequency band and the specific band frequency, the specific frequency band using a switch located prior to the same RF circuit, wherein the UE capability information includes configuration information of the plurality of RF circuits, and wherein the configuration information includes a list of frequency bands which can be used by the plurality of RF circuits for transmission and reception.