mhurhangee/patent-ind-claim-en huggingface dataset:
Aircraft fuselage portion (F) comprising a fuselage structure comprising annular frames perpendicular to a longitudinal direction of extent of said fuselage portion, a flat floor , and vertical struts perpendicular to the floor that extend from the floor to a frame , forming a space, termed triangle region , which is delimited by an underside of the floor , said vertical struts and said frames , characterized in that it comprises a slideway element, termed second slideway element , which is connected to or formed by the fuselage structure and which is designed to form, in said triangle region, a longitudinal slideway by cooperation with a first corresponding slideway element, and in that it additionally comprises, in said triangle region, an aircraft duct assembly comprising at least two ducts extending along a general direction of rectilinear extent, each duct being able to be an electrical, hydraulic or aeraulic duct, and in that it also comprises a duct support , each duct being connected to said duct support , said duct support comprising the first slideway element designed to cooperate with the second slideway element so as to form a slideway in the general direction of extent of said ducts, in which the first slideway element of the duct support cooperates with the second slideway element to form a slideway via which said duct assembly is connected to said fuselage structure.
A non-aqueous inkjet ink composition containing an acrylic resin, a ketone resin, a pigment, and a pigment dispersant, and containing propylene carbonate in an amount of 5 to 25 percent by mass and diethylene glycol dialkyl ether as an organic solvent, wherein the ratio by mass of the diethylene glycol dialkyl ether to the propylene carbonate is between 3.0 and 8.0.
A speaker comprising a frame comprising a magnetic circuit having on the one hand an external metal casing that is toroidal about an axis (A-A) and on the other hand a stack comprising a metallic central core placed between a first magnet and a second magnet , with polarities of opposite directions along the axis (A-A), aligned along this same axis and themselves placed between a first metal disc and a second metal disc , the central core and at least one disc delimiting an air gap with the casing, the speaker comprising mobile equipment that is movable relative to the magnetic circuit along the axis (A-A), the mobile equipment including a spool holder bearing a spool and a membrane , the spool holder being mounted movably through the air gaps , the speaker including a first guide element of the mobile equipment arranged between the mobile equipment and the frame on the side of the membrane relative to the magnetic circuit ; wherein each metal disc delimits, with the casing , an end air gap , the mobile equipment passes all the way through the magnetic circuit through the end air gaps and the speaker includes an additional guide element , arranged between the mobile equipment and the frame , on the side opposite the membrane relative to the magnetic circuit ; wherein the spool comprises a central winding section and two end winding sections , the end winding sections extending at rest each at least partially through an end air gap ; characterized in that , when the central winding section is aligned with the central air gap , the end winding sections are offset from the end air gaps at a distance from the central core . wherein each metal disc delimits, with the casing , an end air gap , the mobile equipment passes all the way through the magnetic circuit through the end air gaps and the speaker includes an additional guide element , arranged between the mobile equipment and the frame , on the side opposite the membrane relative to the magnetic circuit ; wherein the spool comprises a central winding section and two end winding sections , the end winding sections extending at rest each at least partially through an end air gap ; characterized in that , when the central winding section is aligned with the central air gap , the end winding sections are offset from the end air gaps at a distance from the central core .
An architecture of a hybrid propulsive system for an aircraft, comprising an engine comprising at least two shafts rotating independently of one another, two reversible electric machines connected to a distribution network , and a system for controlling the electric machines, wherein : - a rotor of each electric machine is connected to each of the engine shafts by a respective transmission , the shafts having either reversed directions of rotation, or identical directions of rotation, one of the transmissions then including a direction of rotation reversed, - each of the transmissions comprises a disengaging coupling , the disengaging couplings are passive one-way clutches, and the one-way clutches of each electric machine couple the rotor of the electric machine with the shafts for opposite rotational directions of the rotor of the electric machine, wherein - the system for controlling the electric machines enables: - the electric machines to be controlled in a motor mode and in a generator mode in both rotational directions of their rotor, - at least one of the shafts to be driven by both electric machines , and also electricity to be generated from one of both shafts by the first electric machine, simultaneously to the second of both shafts being driven by the second electric machine. - a rotor of each electric machine is connected to each of the engine shafts by a respective transmission , the shafts having either reversed directions of rotation, or identical directions of rotation, one of the transmissions then including a direction of rotation reversed, - each of the transmissions comprises a disengaging coupling , the disengaging couplings are passive one-way clutches, and the one-way clutches of each electric machine couple the rotor of the electric machine with the shafts for opposite rotational directions of the rotor of the electric machine, wherein - the system for controlling the electric machines enables: - the electric machines to be controlled in a motor mode and in a generator mode in both rotational directions of their rotor, - at least one of the shafts to be driven by both electric machines , and also electricity to be generated from one of both shafts by the first electric machine, simultaneously to the second of both shafts being driven by the second electric machine. - the electric machines to be controlled in a motor mode and in a generator mode in both rotational directions of their rotor, - at least one of the shafts to be driven by both electric machines , and also electricity to be generated from one of both shafts by the first electric machine, simultaneously to the second of both shafts being driven by the second electric machine.
A method for calibrating a system comprising an external eye-tracking device and a computing device (12a; 12b) and for capturing the gaze of a user (P) on the screen of the computing device in real-time, wherein the calibration of the system comprises: capturing with one or more cameras of the eye-tracking device at least of one image of landmarks (f1, f2, f3...fn) of the face of the user (P) to identify the 3D position of each landmark in the coordinate system of said eye tracking device, ECS; capturing with a camera of the computing device (12a; 12b) the same landmarks (f1, f2, f3...fn) of the face of the user (P) in the image coordinate system, ICS of the computing device camera to identify the 2D position of each landmark in the ICS ; computing the 3D pose of the camera of the computing device , defined as the camera coordinate system, CCS as a function of the 3D position and 2D position of each landmark (f1, f2, f3...fn) respectively in the ECS and in the ICS, and computing the 3D pose of the screen of the computing device, defined as the screen coordinate system, SCS , as a function of the CCS and mechanical parameters describing how the screen is positioned with respect to the camera of the computing device, and wherein capturing the gaze of a user (P) on the screen of the computing device in real-time comprises retrieving a gaze ray (d) of the user (P) with the eye-tracking device , and intersecting the gaze ray (d) of the user (P) with the plane of the screen of the computing device, as a function of the ECS and SCS parameters, to capture the gaze-on-screen in real-time. capturing with one or more cameras of the eye-tracking device at least of one image of landmarks (f1, f2, f3...fn) of the face of the user (P) to identify the 3D position of each landmark in the coordinate system of said eye tracking device, ECS; capturing with a camera of the computing device (12a; 12b) the same landmarks (f1, f2, f3...fn) of the face of the user (P) in the image coordinate system, ICS of the computing device camera to identify the 2D position of each landmark in the ICS ; computing the 3D pose of the camera of the computing device , defined as the camera coordinate system, CCS as a function of the 3D position and 2D position of each landmark (f1, f2, f3...fn) respectively in the ECS and in the ICS, and computing the 3D pose of the screen of the computing device, defined as the screen coordinate system, SCS , as a function of the CCS and mechanical parameters describing how the screen is positioned with respect to the camera of the computing device, and wherein capturing the gaze of a user (P) on the screen of the computing device in real-time comprises retrieving a gaze ray (d) of the user (P) with the eye-tracking device , and intersecting the gaze ray (d) of the user (P) with the plane of the screen of the computing device, as a function of the ECS and SCS parameters, to capture the gaze-on-screen in real-time.
A liquid hand dishwashing cleaning composition comprising: a) from 5% to 50% by weight of the total composition of a surfactant system, wherein the surfactant system comprises: at least 40% by weight of the surfactant system of anionic surfactant, wherein the anionic surfactant comprises at least 50% by weight of the anionic surfactant of alkyl sulfate anionic surfactant, wherein the alkyl sulfate anionic surfactant: a. has an alkyl chain comprising an average of from 8 to 18 carbon atoms; b. has an average degree of branching of less than 15%, and c. has an average degree of alkoxylation of less than 0.5; and a co-surfactant selected from the group consisting of an amphoteric surfactant, a zwitterionic surfactant and mixtures thereof; and b) from 0.1% to 10% by weight of the total composition of polypropyleneglycol, wherein the polypropyleneglycol has a weight average molecular weight from 500 g/mol to 1800 g/mol. a) from 5% to 50% by weight of the total composition of a surfactant system, wherein the surfactant system comprises: at least 40% by weight of the surfactant system of anionic surfactant, wherein the anionic surfactant comprises at least 50% by weight of the anionic surfactant of alkyl sulfate anionic surfactant, wherein the alkyl sulfate anionic surfactant: a. has an alkyl chain comprising an average of from 8 to 18 carbon atoms; b. has an average degree of branching of less than 15%, and c. has an average degree of alkoxylation of less than 0.5; and a co-surfactant selected from the group consisting of an amphoteric surfactant, a zwitterionic surfactant and mixtures thereof; and at least 40% by weight of the surfactant system of anionic surfactant, wherein the anionic surfactant comprises at least 50% by weight of the anionic surfactant of alkyl sulfate anionic surfactant, wherein the alkyl sulfate anionic surfactant: a. has an alkyl chain comprising an average of from 8 to 18 carbon atoms; b. has an average degree of branching of less than 15%, and c. has an average degree of alkoxylation of less than 0.5; and a. has an alkyl chain comprising an average of from 8 to 18 carbon atoms; b. has an average degree of branching of less than 15%, and c. has an average degree of alkoxylation of less than 0.5; and a co-surfactant selected from the group consisting of an amphoteric surfactant, a zwitterionic surfactant and mixtures thereof; and b) from 0.1% to 10% by weight of the total composition of polypropyleneglycol, wherein the polypropyleneglycol has a weight average molecular weight from 500 g/mol to 1800 g/mol.
A method for monitoring fuel actuation system health comprising: causing a metering valve (220; 600) to move from a first position to a second position; detecting a first travel distance of the metering valve (220; 600); storing the first travel distance of the metering valve (220; 600) to a memory to generate a first travel distance history; and determining a level of degradation of a fuel actuation system based on at least the first travel distance history; characterised by : detecting at least one of a temperature of a fuel or a pressure of the fuel; and storing the at least one of the temperature of the fuel or the pressure of the fuel to the memory to create at least one of a fuel temperature history or a fuel pressure history, wherein the determining the level of degradation of the fuel actuation system is further based on the at least one of the fuel temperature history or the fuel pressure history. causing a metering valve (220; 600) to move from a first position to a second position; detecting a first travel distance of the metering valve (220; 600); storing the first travel distance of the metering valve (220; 600) to a memory to generate a first travel distance history; and determining a level of degradation of a fuel actuation system based on at least the first travel distance history; characterised by : detecting at least one of a temperature of a fuel or a pressure of the fuel; and storing the at least one of the temperature of the fuel or the pressure of the fuel to the memory to create at least one of a fuel temperature history or a fuel pressure history, wherein the determining the level of degradation of the fuel actuation system is further based on the at least one of the fuel temperature history or the fuel pressure history. detecting at least one of a temperature of a fuel or a pressure of the fuel; and storing the at least one of the temperature of the fuel or the pressure of the fuel to the memory to create at least one of a fuel temperature history or a fuel pressure history, wherein the determining the level of degradation of the fuel actuation system is further based on the at least one of the fuel temperature history or the fuel pressure history.
Method for preparing for a navigation manoeuvre of a vehicle by controlling a contact analogue display of navigation information by an augmented reality display device , comprising the steps of: determining a target manoeuvre and a manoeuvre point of the target manoeuvre; (S2) determining a first display point with a first fixed spacing from the manoeuvre point on a road used by the vehicle and between a current vehicle position and the manoeuvre point; (S3) generating and outputting a first contact analogue display element for display at the first display point by the augmented reality display device ; (S4) determining a second display point with a second fixed spacing from the manoeuvre point on the road used by the vehicle and between the current vehicle position and the manoeuvre point; and (S5) generating and outputting a second contact analogue display element for display at the second display point by the augmented reality display device ; wherein the first fixed spacing is determined on the basis of a position and a speed of the vehicle , wherein the first fixed spacing is determined to be greater at a high speed than at a lower speed, and wherein the second fixed spacing is shorter than the first fixed spacing , and wherein the first display element is output in a first period of time and sections of the second display element are output in a second period of time after the first period of time. wherein the first fixed spacing is determined on the basis of a position and a speed of the vehicle , wherein the first fixed spacing is determined to be greater at a high speed than at a lower speed, and wherein the second fixed spacing is shorter than the first fixed spacing , and wherein the first display element is output in a first period of time and sections of the second display element are output in a second period of time after the first period of time.
A lifting assembly for a jump elevator characterized in that it comprises: a supporting platform provided with a plurality of first pawls ; an operating platform comprising a machine room platform and provided with a plurality of second pawls ; at least one screw mechanism comprising a screw and a sleeve , the screw and the sleeve are provided with an external thread and an internal thread matching with each other, respectively; a driving mechanism configured to drive one of the screw and the sleeve to rotate in relative to the other, such that the screw mechanism extends or retracts; wherein the screw mechanism is connected between the supporting platform and the operating platform , one of the screw and the sleeve is configured to be rotatably attached to one of the supporting platform or the operating platform . a supporting platform provided with a plurality of first pawls ; an operating platform comprising a machine room platform and provided with a plurality of second pawls ; at least one screw mechanism comprising a screw and a sleeve , the screw and the sleeve are provided with an external thread and an internal thread matching with each other, respectively; a driving mechanism configured to drive one of the screw and the sleeve to rotate in relative to the other, such that the screw mechanism extends or retracts; wherein the screw mechanism is connected between the supporting platform and the operating platform , one of the screw and the sleeve is configured to be rotatably attached to one of the supporting platform or the operating platform .
Pressure-actuated tripping device for an electrical line protection apparatus, of the circuit breaker type, the electrical apparatus comprising an arc extinguishing chamber in which gases (G) are generated which escape at a flow velocity, said tripping device comprising a case and comprising, inside the case : - an upstream chamber , - return means , - an inlet orifice for the gases (G) opening onto the upstream chamber and having a predetermined cross section; - a downstream chamber ; - an actuator able to rotate counter to said return means between a rest position and a trip position, said actuator being positioned between the upstream chamber and the downstream chamber and in itself partially delimiting the upstream chamber as well as the downstream chamber , characterized in that the tripping device further comprises means for recovering residual polluting particles present in the gases (G) consisting of at least a first baffle and a second baffle which are designed to trap the particles by reducing the flow velocity of the gases (G), said first baffle being located in the continuation of the upstream chamber , the actuator having a first protuberance able to be inserted into the first baffle and a second protuberance able to be inserted into the second baffle , the second baffle opening onto an aperture in the downstream chamber through which a tripping end piece of the actuator emerges, the sets of protuberances and baffles being sized so that a stream of gases (G) can flow through the baffles ; and, in the rest position, the actuator being arranged to rest on the walls defining the second baffle , such that the stream of gases (G) then remains confined in the baffles . - an upstream chamber , - return means , - an inlet orifice for the gases (G) opening onto the upstream chamber and having a predetermined cross section; - a downstream chamber ; - an actuator able to rotate counter to said return means between a rest position and a trip position,
A multifunctional controller for a satellite, comprising: - reconfiguration functions for reconfiguring components of an onboard computer, OBC, of the satellite in an event of a mal-function, wherein the components of the OBC include central processing units, CPUs; - control functions for controlling a distribution of energy to satellite components, - wherein the reconfiguration functions and the control functions are implemented together in a single chip, characterized in that the chip is integrated in a separate housing and separated from the CPUs by the housing. - reconfiguration functions for reconfiguring components of an onboard computer, OBC, of the satellite in an event of a mal-function, wherein the components of the OBC include central processing units, CPUs; - control functions for controlling a distribution of energy to satellite components, - wherein the reconfiguration functions and the control functions are implemented together in a single chip,
An apparatus comprising: a first part configured to form at least part of a case of the apparatus; a second part configured to form at least part of a display for the apparatus; a coupling configured to couple the first part to the second part ; at least two actuators coupled to the second part and configured to apply a force to the second part to generate a displacement of the second part ; and a mode determiner configured to determine a mode of operation of the apparatus in dependence on at least one proximity sensor, wherein the apparatus is configured to: in a hands-free mode of operation, operate the at least two actuators to generate a translational displacement of the second part relative to the first part to provide a first acoustic amplitude of sound from the translational displacement of the second part ; and in a hands-portable mode of operation, operate a sub-group of the at least two actuators to generate a localized displacement of the second part relative to the first part to provide a second acoustic amplitude of sound from the localized displacement of the second part which is less than the first acoustic amplitude of sound. a first part configured to form at least part of a case of the apparatus; a second part configured to form at least part of a display for the apparatus; a coupling configured to couple the first part to the second part ; at least two actuators coupled to the second part and configured to apply a force to the second part to generate a displacement of the second part ; and a mode determiner configured to determine a mode of operation of the apparatus in dependence on at least one proximity sensor, wherein the apparatus is configured to: in a hands-free mode of operation, operate the at least two actuators to generate a translational displacement of the second part relative to the first part to provide a first acoustic amplitude of sound from the translational displacement of the second part ; and in a hands-portable mode of operation, operate a sub-group of the at least two actuators to generate a localized displacement of the second part relative to the first part to provide a second acoustic amplitude of sound from the localized displacement of the second part which is less than the first acoustic amplitude of sound. in a hands-free mode of operation, operate the at least two actuators to generate a translational displacement of the second part relative to the first part to provide a first acoustic amplitude of sound from the translational displacement of the second part ; and in a hands-portable mode of operation, operate a sub-group of the at least two actuators to generate a localized displacement of the second part relative to the first part to provide a second acoustic amplitude of sound from the localized displacement of the second part which is less than the first acoustic amplitude of sound.