mhurhangee/ep-ind-claims huggingface dataset:
A data transmission method, comprising: receiving, by a communications node, N spatial reuse parameters, SRPs; determining, by the communications node based on the received N SRPs, that the communications node is capable of performing spatial reuse link transmission; and transmitting, by the communications node, data by using a spatial reuse link, wherein the determining, by the communications node based on the received N SRPs, that the communications node is capable of performing spatial reuse link transmission is specifically: determining, by the communications node based on a current moment T, Q effective SRPs of the N SRPs, wherein Q is a positive integer less than or equal to N, and the effective SRPs are SRPs whose corresponding TXOP transmission times comprise the current moment T; adjusting, by the communications node, a transmit parameter to meet the Q effective SRPs, wherein the transmit parameter of the communications node is a function of the Q effective SRPs: TX = f SRP 1, SRP 2,..., SRPQ; and if the transmit parameter meets a transmission requirement of the spatial reuse link, determining that the communications node is capable of performing spatial reuse link transmission. receiving, by a communications node, N spatial reuse parameters, SRPs; determining, by the communications node based on the received N SRPs, that the communications node is capable of performing spatial reuse link transmission; and transmitting, by the communications node, data by using a spatial reuse link, wherein the determining, by the communications node based on the received N SRPs, that the communications node is capable of performing spatial reuse link transmission is specifically: determining, by the communications node based on a current moment T, Q effective SRPs of the N SRPs, wherein Q is a positive integer less than or equal to N, and the effective SRPs are SRPs whose corresponding TXOP transmission times comprise the current moment T; adjusting, by the communications node, a transmit parameter to meet the Q effective SRPs, wherein the transmit parameter of the communications node is a function of the Q effective SRPs: TX = f SRP 1, SRP 2,..., SRPQ; and if the transmit parameter meets a transmission requirement of the spatial reuse link, determining that the communications node is capable of performing spatial reuse link transmission. determining, by the communications node based on a current moment T, Q effective SRPs of the N SRPs, wherein Q is a positive integer less than or equal to N, and the effective SRPs are SRPs whose corresponding TXOP transmission times comprise the current moment T; adjusting, by the communications node, a transmit parameter to meet the Q effective SRPs, wherein the transmit parameter of the communications node is a function of the Q effective SRPs: TX = f SRP 1, SRP 2,..., SRPQ; and if the transmit parameter meets a transmission requirement of the spatial reuse link, determining that the communications node is capable of performing spatial reuse link transmission.
An aircraft, comprising: a fuselage; a wing; and a decoupled joint, interconnecting the fuselage and the wing, wherein: the joint is decoupled using an active suspension system, which comprises a plurality of actuators, connected between the wing and the fuselage, configured to selectively adjust a relative position of the wing and fuselage in response to dynamic loads upon the wing and/or the fuselage; the active suspension system comprises at least four actuators connected between the wing and the fuselage; and the active suspension system comprises four actuator groups, each positioned at one of four corners of a wing main spar assembly, each actuator group comprising three actuators oriented at substantially orthogonal angles. a fuselage; a wing; and a decoupled joint, interconnecting the fuselage and the wing, the joint is decoupled using an active suspension system, which comprises a plurality of actuators, connected between the wing and the fuselage, configured to selectively adjust a relative position of the wing and fuselage in response to dynamic loads upon the wing and/or the fuselage; the active suspension system comprises at least four actuators connected between the wing and the fuselage; and the active suspension system comprises four actuator groups, each positioned at one of four corners of a wing main spar assembly, each actuator group comprising three actuators oriented at substantially orthogonal angles.
A three-dimensional display device comprising: a plurality of transmissive display units (101, 102) arranged in different depth positions in view from an observer; and a moire vanishing element that diffuses a light, characterized in that the moiré vanishing element has a spatial frequency characteristic to cut off a spatial frequency more than a spatial frequency having a cycle being twice as large as an interval of boundaries of pixels forming a first transmissive display unit arranged behind the moiré vanishing element in the view from the observer. a plurality of transmissive display units (101, 102) arranged in different depth positions in view from an observer; and a moire vanishing element that diffuses a light, characterized in that the moiré vanishing element has a spatial frequency characteristic to cut off a spatial frequency more than a spatial frequency having a cycle being twice as large as an interval of boundaries of pixels forming a first transmissive display unit arranged behind the moiré vanishing element in the view from the observer.
A rotor for an electric machine comprising a shaft, a spider supported by the shaft, and a laminated drum radially enclosing the spider, wherein the spider has a plurality of apart elements defining ducts between each other, the ducts extend parallel to a longitudinal rotor axis, wherein the laminated drum has a plurality of cooling channels connected to the ducts, the cooling channels extend radially and perpendicular to the rotor axis, such as that during operation a cooling gas circulates through the ducts and cooling channels, the rotor further comprises a multitude of throttle elements each throttle element includes a wall which is an elongated plate housed in one of the ducts and is provided with apertures, characterized in that the wall is configured to slide longitudinally along the inner surface of the laminated drum, the apertures having sizes and spacing corresponding to the cooling channels, and it further comprises an activation system configured to adjust the position of the wall such that the apertures are aligned with the cooling channels or partially or completely close them in order to adjust the cooling gas flow while in operation.
A control system for controlling an operation of a spacecraft, comprising: a model predictive controller to produce a solution for controlling thrusters of the spacecraft by optimizing a cost function over a finite receding horizon using a model of dynamics of the spacecraft effecting a pose of the spacecraft and a model of dynamics of momentum exchange devices of the spacecraft effecting an orientation of the spacecraft, wherein the optimization is subject to hard constraints on angles of thrusts generated by thrusters of the spacecraft, wherein the hard constraints requires the angles of thrusts in the solution to fall within a predetermined range defined by the hard constraints; and a thruster controller to operate the thrusters according to the solution of the MPC, characterized in that the optimization is subject to soft constraints on angles of thrusts generated by thrusters of the spacecraft and wherein the soft constraints penalize the solution for deviation of the angles of thrusts from nominal angles corresponding to a torque-free thrust passing through the center of the mass of the spacecraft. a model predictive controller to produce a solution for controlling thrusters of the spacecraft by optimizing a cost function over a finite receding horizon using a model of dynamics of the spacecraft effecting a pose of the spacecraft and a model of dynamics of momentum exchange devices of the spacecraft effecting an orientation of the spacecraft, wherein the optimization is subject to hard constraints on angles of thrusts generated by thrusters of the spacecraft, wherein the hard constraints requires the angles of thrusts in the solution to fall within a predetermined range defined by the hard constraints; and a thruster controller to operate the thrusters according to the solution of the MPC, characterized in that the optimization is subject to soft constraints on angles of thrusts generated by thrusters of the spacecraft and wherein the soft constraints penalize the solution for deviation of the angles of thrusts from nominal angles corresponding to a torque-free thrust passing through the center of the mass of the spacecraft.
Steering system for motor vehicles, in particular for agricultural machines, comprising: - a first steering assembly of the front wheels (W3, W4) comprises a front axle, two front hubs (103, 104) and first actuating means to directly steer the hubs (103, 104) to rotate only each of said front wheels (W3, W4) by a respective angle (α1), (α2); characterized in that it further comprises: - a second steering assembly comprises a pivoting support, hinged to a fixed axle support, and second actuating means to rotate the pivoting support around a pin with regard to the fixed axle support; the second steering assembly being also able to support the axle rotating together with the pivoting support to independently steer the front axle and the front wheels (W3, W4) of an angle (β); said second steering assembly being activated only after that each angle (α1), (α2) has reached a respective pre-determined value (α1*), (α2*) during the steering performed by said first steering assembly. - a first steering assembly of the front wheels (W3, W4) comprises a front axle, two front hubs (103, 104) and first actuating means to directly steer the hubs (103, 104) to rotate only each of said front wheels (W3, W4) by a respective angle (α1), (α2); characterized in that it further comprises: - a second steering assembly comprises a pivoting support, hinged to a fixed axle support, and second actuating means to rotate the pivoting support around a pin with regard to the fixed axle support; the second steering assembly being also able to support the axle rotating together with the pivoting support to independently steer the front axle and the front wheels (W3, W4) of an angle (β);
A windowpane for a combustion apparatus in which a light-blocking layer containing an inorganic pigment powder and a glass powder is formed on at least part of a peripheral portion of a surface of a transparent crystallized glass plate, wherein the light-blocking layer contains 30 to 50% by mass of the inorganic pigment powder and 50 to 70% by mass of the glass powder and has a thickness of 1 to 10 μm and the inorganic pigment powder has an average particle size of 0.8 μm or less.
A histologic tissue sample support device for orienting and retaining tissue samples during processing, embedding and sectioning in a microtome, comprising: a tissue cassette, the tissue cassette including a perforated bottom wall and at least one perforated side wall for defining a tissue sample receiving space, the cassette formed of material which is sectioned in a microtome and is resistant to degradation from solvents and chemicals used to fix, process and stain tissue, the tissue cassette including an elongate channel for receiving at least one tissue sample, the channel including resilient fingers (140, 142) on opposite sides along the length of the channel for resiliently engaging and holding the tissue sample during processing and embedding, wherein the resilient fingers (140, 142) face each other; and tissue sample biasing structure configured to extend into the channel to retain the tissue sample or samples against the bottom wall during processing and embedding, the tissue sample biasing structure further being capable of successful sectioning in the microtome.
A method of operating an Uninterruptible Power Supply, in short UPS, system, comprising: activating an idle state for a UPS module included in the UPS system; providing a UPS module test input to the UPS module in the idle state by applying an ac input to a rectifier circuit included in the UPS module, while power is provided to a load by another UPS module in the UPS system; providing, from the UPS module in the idle state, a UPS module test response to the UPS module test input; and identifying the UPS module as a potentially faulty UPS module responsive to determining that the UPS module test response varies from the predetermined UPS module test response by more than a threshold value. activating an idle state for a UPS module included in the UPS system; providing a UPS module test input to the UPS module in the idle state by applying an ac input to a rectifier circuit included in the UPS module, while power is provided to a load by another UPS module in the UPS system; providing, from the UPS module in the idle state, a UPS module test response to the UPS module test input; and identifying the UPS module as a potentially faulty UPS module responsive to determining that the UPS module test response varies from the predetermined UPS module test response by more than a threshold value.
A method for providing a user interface, in which at least one application program is carried out and graphic data of an operating interface are generated and output; wherein for the application program a tile-mode or full-image mode can be activated, wherein the operating interface has a sub-region (10.1; 11.1, 11.2, 11.3, 11.4, 11.5) to which the application program is assigned and which comprises graphic elements (12, 13, 14, 15, 16; 22, 23, 24, 25, 26,; 22.1, 22.2, 22.3, 22.4; 31 to 38) assigned to the application program, wherein, if the tile-mode is activated, the sub-region (11.1, 11.2, 11.3, 11.4, 11.5) has a first surface extent and the graphic elements (12, 13, 14, 15, 16; 31 to 34) are arranged relative to one another in a first arrangement; and, if the full-image mode is activated, the sub-region (10.1) has a second surface extent, which is different from the first surface extent, and the graphic elements (20 to 26; 22.1, 22.2, 22.3, 22.4; 31 to 38) are arranged relative to one another in a second arrangement, which is different from the first arrangement; wherein in the event of the switch between the tile-mode and the full-image mode a transition animation is generated and displayed; wherein the transition animation for at least one subset of the graphic elements (12, 13, 14, 15, 16; 31 to 34) comprises a translation and the translation is output as continuous movement, characterized in that a vehicle speed is detected; and the transition animation is formed in dependence on the vehicle speed.
A robot for cleaning swimming pools, comprising: - a main body having at least one sealed containment space; - a plurality of rotors configured to generate an hydrodynamic thrust designed to move the robot inside an entire volume of a swimming pool; - a control unit inserted in the containment space and configured for modifying at least one respective operating parameter of each rotor in such a way as to direct the hydrodynamic thrust; - swimming pool cleaning means, characterized in that the main body has a substantially parallelepipedal shape; and the plurality of rotors comprises four rotors, each positioned at a respective vertex of the parallelepiped. - a main body having at least one sealed containment space; - a plurality of rotors configured to generate an hydrodynamic thrust designed to move the robot inside an entire volume of a swimming pool; - a control unit inserted in the containment space and configured for modifying at least one respective operating parameter of each rotor in such a way as to direct the hydrodynamic thrust; - swimming pool cleaning means,
A composition for application to a keratin surface, said composition comprising, by weight of the total composition: - from 0.1 to 25% of at least one non-sensitizing pressure sensitive adhesive that is the polycondensate of a silanol endblocked polydimethylsiloxane and a silicate resin; - from 0.01 to 35% of at least one copolymer of vinyl pyrrolidone and a long chain alpha olefin; - from 0.01 to 70% of at least one montmorillonite mineral; and - from 0.1 to 85% of at least one volatile solvent; wherein the ratio of the pressure sensitive adhesive to the vinyl pyrrolidone copolymer in the final composition is at least 2 to 1 and the polycondensate, after formulation into the composition, is not reactive with the copolymer or the montmorillonite mineral. - from 0.1 to 25% of at least one non-sensitizing pressure sensitive adhesive that is the polycondensate of a silanol endblocked polydimethylsiloxane and a silicate resin; - from 0.01 to 35% of at least one copolymer of vinyl pyrrolidone and a long chain alpha olefin; - from 0.01 to 70% of at least one montmorillonite mineral; and - from 0.1 to 85% of at least one volatile solvent;
A method for implementing an intelligent network service, comprising: receiving an intelligent network service request triggered from a visited mobile switching centre, VMSC, of a mobile terminal; after receiving the intelligent network service request triggered from the VMSC, determining whether the intelligent network service request is triggered in the international roaming; and if the intelligent network service request is not triggered in the international roaming, directly triggering the intelligent network service that the mobile terminal subscribes to; if the intelligent network service request is triggered in international roaming, generating a temporary calling number for an international roaming call which is of the mobile terminal and at the VMSC, and saving a corresponding relationship between the temporary calling number and an actual called number in the international roaming call, wherein the temporary calling number comprises a country code of a home country of the mobile terminal; returning the temporary calling number to the VMSC, so that the VMSC routes the international roaming call to a mobile switching centre in a home country of the mobile terminal according to the country code; receiving the intelligent network service request triggered from the mobile switching centre in a home country for the temporary calling number; and acquiring the actual called number according to the temporary calling number, and triggering an intelligent network service that the mobile terminal subscribes to with the actual called number. receiving an intelligent network service request triggered from a visited mobile switching centre, VMSC, of a mobile terminal; after receiving the intelligent network service request triggered from the VMSC, determining whether the intelligent network service request is triggered in the international roaming; and if the intelligent network service request is not triggered in the international roaming, directly triggering the intelligent network service that the mobile terminal subscribes to; if the intelligent network service request is triggered in international roaming, generating a temporary calling number for an international roaming call which is of the mobile terminal and at the VMSC, and saving a corresponding relationship between the temporary calling number and an actual called number in the international roaming call, wherein the temporary calling number comprises a country code of a home country of the mobile terminal; returning the temporary calling number to the VMSC, so that the VMSC routes the international roaming call to a mobile switching centre in a home country of the mobile terminal according to the country code; receiving the intelligent network service request triggered from the mobile switching centre in a home country for the temporary calling number; and acquiring the actual called number according to the temporary calling number, and triggering an intelligent network service that the mobile terminal subscribes to with the actual called number.
Device for packaging a cosmetic product, comprising a having an opening defined by a neck of the container, and a cap for closing the container, the cap comprising: - a cover element, - a closing-off element for the opening, connected to the cover element, - a spring member located between the cover element and the closing-off element, - a mechanism for locking the cap on the container, the locking mechanism comprising a means for retaining the cover element on the container and a means for actuating the retaining means so as to selectively enable the cover element to move with respect to the container from a locked position of the cover element to an unlocked position of the cover element in which the cap can be separated freely from the container, the device comprising a seal able to engage with the closing-off element and the neck of the container, the seal being in contact with the closing-off element and the neck of the container in the unlocked position of the cap, characterized in that the contact between the seal and the neck of the container when the seal is secured to the closing-off element, and/or between the seal and the closing-off element when the seal is secured to the container, takes place radially with respect to the movement axis of the cover element from the locked position to the unlocked position. - a cover element, - a closing-off element for the opening, connected to the cover element, - a spring member located between the cover element and the closing-off element, - a mechanism for locking the cap on the container, the locking mechanism comprising a means for retaining the cover element on the container and a means for actuating the retaining means so as to selectively enable the cover element to move with respect to the container from a locked position of the cover element to an unlocked position of the cover element in which the cap can be separated freely from the container, the device comprising a seal able to engage with the closing-off element and the neck of the container, the seal being in contact with the closing-off element and the neck of the container in the unlocked position of the cap, characterized in that the contact between the seal and the neck of the container when the seal is secured to the closing-off element, and/or between the seal and the closing-off element when the seal is secured to the container, takes place radially with respect to the movement axis of the cover element from the locked position to the unlocked position.