mhurhangee/ep-ind-claims huggingface dataset:
A method for operating a drive system of a submarine with at least one electrical traction network for supplying at least one consumer with electrical energy, wherein at least two parallel battery banks (11, 12), each of which is linked to the traction network by a DC-DC converter (13, 14), are assigned to each traction network, wherein the respective states of charge of the at least two battery banks (11, 12) of a traction network are synchronized with each other by the SOC of each battery bank (11, 12) being measured in each case by a battery management system, and a bank voltage of each battery bank (11, 12) being set by the respective DC-DC converter (13, 14) on the basis of a characteristic curve for the respective battery bank (11, 12) depending on the measured SOC, wherein the battery bank (11, 12), for which a higher SOC was measured than in the case of a parallel battery bank (11, 12) of the same traction network, feeds a higher current into the traction network, than the battery bank (11, 12) for which a lower SOC was measured characterized in that on a current limitation of the battery bank (11, 12) with the higher SOC being reached or on reduction of the SOC, the traction network voltage is reduced.
A probe holder for a measuring system, comprising: a first connector comprising electric and/or optical signal connections for attaching a measure probe electric and/or optical conductor for connecting to the measure probe by said first connector; a rotary actuator arranged to rotate said first connector relative to a reference system, the rotary actuator comprising a rotor capable of continuous rotation to which the first connector is attached and an electric motor; an electric and/or optical slip ring; an angle encoder providing information on an angular position of said rotor; wherein the probe holder is connectable to an articulated head of a measurement system; wherein the rotor has a hollow axle supported by two coaxial spaced-apart bearings; the electric motor is between said bearings, and the electric and/or optical conductor run inside said hollow axle; characterized by the axial distance between the bearings being at least 50 mm; and the electric and/or optical slip ring being in the hollow axle and between said bearings. a first connector comprising electric and/or optical signal connections for attaching a measure probe electric and/or optical conductor for connecting to the measure probe by said first connector; a rotary actuator arranged to rotate said first connector relative to a reference system, the rotary actuator comprising a rotor capable of continuous rotation to which the first connector is attached and an electric motor; an electric and/or optical slip ring; an angle encoder providing information on an angular position of said rotor; wherein the probe holder is connectable to an articulated head of a measurement system; wherein the rotor has a hollow axle supported by two coaxial spaced-apart bearings; the electric motor is between said bearings, and the electric and/or optical conductor run inside said hollow axle; characterized by the axial distance between the bearings being at least 50 mm; and the electric and/or optical slip ring being in the hollow axle and between said bearings.
A retrieval device for retrieving an object from a vasculature, to be side-mounted on an elongate member comprising: a retriever having a proximal end and a distal end and at least partially defining a tapered lumen there through; wherein the retriever comprises an interlocking section extending along at least portion of the retriever between the proximal end to the distal end. a retriever having a proximal end and a distal end and at least partially defining a tapered lumen there through; wherein the retriever comprises an interlocking section extending along at least portion of the retriever between the proximal end to the distal end.
A device for monitoring and/or signalling errors of a radiation therapy apparatus during delivery of a radiation treatment to a target, said radiation therapy apparatus being configurable for a given radiation treatment and comprising a radiation source and a beam shaping device being a multi-leat collimator, the device comprising: • a radiation transparent 2-dimensional 2-D array detector (T2D) located between said beam shaping device and said target, capable of providing for successive times of said radiation treatment a measured detector response of said radiation treatment in a plane perpendicular to the treatment beam; • processing means comprising: • means adapted to acquire in real time a measured 2-D detector response for successive times of said radiation treatment delivery; • a memory for storing a predicted 2-D detector response for corresponding successive times of said radiation treatment; • computing means adapted to compare the measured 2-D detector response and the corresponding predicted 2-D detector response in real time; • means adapted to signal, in real time, an error when said comparison results in a difference which exceeds a given threshold. • a radiation transparent 2-dimensional 2-D array detector (T2D) located between said beam shaping device and said target, capable of providing for successive times of said radiation treatment a measured detector response of said radiation treatment in a plane perpendicular to the treatment beam; • processing means comprising: • means adapted to acquire in real time a measured 2-D detector response for successive times of said radiation treatment delivery; • a memory for storing a predicted 2-D detector response for corresponding successive times of said radiation treatment; • computing means adapted to compare the measured 2-D detector response and the corresponding predicted 2-D detector response in real time; • means adapted to signal, in real time, an error when said comparison results in a difference which exceeds a given threshold. • means adapted to acquire in real time a measured 2-D detector response for successive times of said radiation treatment delivery; • a memory for storing a predicted 2-D detector response for corresponding successive times of said radiation treatment; • computing means adapted to compare the measured 2-D detector response and the corresponding predicted 2-D detector response in real time; • means adapted to signal, in real time, an error when said comparison results in a difference which exceeds a given threshold.
A cosmetic active substance characterized in that it is the product obtained through bioconversion by Lactobacillus arizonensis of Simmondsia chinensis.
Baler device provided for successively forming bales one after the other, comprising: a pre-pressing station having a hingeable pressing door, a main pressing station and a connecting duct between the pre-pressing station and main pressing station along which the pre-pressed material is displaced from the pre-pressing station to the main pressing station and which is formed by an upper wall and a lower wall, characterized in that the pressing door is plate-shaped and forms, together with a panel-shaped element which is rotatable about a horizontal axis, the upper and the lower wall of the connecting duct during the displacement of the pre-pressed material from the pre-pressing station to the main pressing station and that the angle formed by the plane of the pressing door and the plane of the panel-shaped element when the pressing door is in the closed position is greater than or equal to 90°.
Method for displaying a settings menu, the method comprising a step for displaying at least one three-dimensional image and steps for: - displaying (61, 71) said settings menu comprising a three-dimensional graphical element of which one of the dimensions extends according to a depth direction (z), the three-dimensional graphical element comprising a plurality of unitary graphical elements (201 to 208) corresponding to a maximum amplitude of the depth that it is possible to set for the at least one three-dimensional image, each unitary graphical element (201 to 208) being associated with a respective level of depth setting corresponding to its relative depth position, - selecting at least one unitary graphical element (203, 204, 205) among said plurality of unitary graphical elements (201 to 208) and applying at least one setting associated with the corresponding at least one respective level of depth setting to the at least one three-dimensional image. - displaying (61, 71) said settings menu comprising a three-dimensional graphical element of which one of the dimensions extends according to a depth direction (z), the three-dimensional graphical element comprising a plurality of unitary graphical elements (201 to 208) corresponding to a maximum amplitude of the depth that it is possible to set for the at least one three-dimensional image, each unitary graphical element (201 to 208) being associated with a respective level of depth setting corresponding to its relative depth position, - selecting at least one unitary graphical element (203, 204, 205) among said plurality of unitary graphical elements (201 to 208) and applying at least one setting associated with the corresponding at least one respective level of depth setting to the at least one three-dimensional image.
An in vitro method of preparing an extracellular matrix material, comprising: a. incubating vascular adventitial tissue in a zwitterionic detergent, wherein the vascular adventitial tissue is optionally bovine, ovine, or porcine, and wherein the adventitial tissue is optionally aortic adventitia; b. incubating the tissue in Trypsin-EDTA; c. incubating the tissue with an anionic detergent; d. disinfecting the tissue, optionally with peracetic acid, producing a decellularized ECM material; e. lyophilizing the decellularized ECM material; f. comminuting the decellularized ECM material; g. partially or completely solubilizing the decellularized ECM material with an acid protease to produce solubilized ECM; h. neutralizing the solubilized ECM to produce an ECM pre-gel; and i. optionally, gelling the ECM pre-gel at a temperature at which the ECM pre-gel gels to produce an ECM gel. a. incubating vascular adventitial tissue in a zwitterionic detergent, wherein the vascular adventitial tissue is optionally bovine, ovine, or porcine, and wherein the adventitial tissue is optionally aortic adventitia; b. incubating the tissue in Trypsin-EDTA; c. incubating the tissue with an anionic detergent; d. disinfecting the tissue, optionally with peracetic acid, producing a decellularized ECM material; e. lyophilizing the decellularized ECM material; f. comminuting the decellularized ECM material; g. partially or completely solubilizing the decellularized ECM material with an acid protease to produce solubilized ECM; h. neutralizing the solubilized ECM to produce an ECM pre-gel; and i. optionally, gelling the ECM pre-gel at a temperature at which the ECM pre-gel gels to produce an ECM gel.
A modified mineral filler particle comprising a filler particle modified with discrete functional particles that are sufficiently bound, adhered, or otherwise associated to the surface of the filler via interaction such that they are able to remain associated during subsequent manufacturing steps, wherein the discrete functional particles are pigment particles, and wherein the particle size distribution for the filler is in a range from 10 to 50 microns and the particle size distribution for the pigment particles is in a range from 0.01 to 3 microns, the particle size being measured by SEM.
A method for monitoring of fabrication of integrated computational elements comprising: receiving, by a fabrication system, a design of an integrated computational element, the ICE design comprising specification of a substrate and a plurality of layers, their respective target thicknesses and complex refractive indices, wherein complex refractive indices of adjacent layers are different from each other, and wherein a notional ICE fabricated in accordance with the ICE design is related to a characteristic of a sample; forming, by the fabrication system, at least some of the layers of a plurality of ICEs in accordance with the ICE design using a deposition source associated with the fabrication system, wherein the layers of the ICEs being formed are supported on a support that is moved with a periodic motion relative to the deposition source during said forming; monitoring, by a measurement system associated with the fabrication system, characteristics of the layers of the ICEs during said forming, wherein said monitoring the characteristics is performed using a timing of the periodic motion of the support relative to the deposition source; and adjusting said forming based on results of said monitoring. receiving, by a fabrication system, a design of an integrated computational element, the ICE design comprising specification of a substrate and a plurality of layers, their respective target thicknesses and complex refractive indices, wherein complex refractive indices of adjacent layers are different from each other, and wherein a notional ICE fabricated in accordance with the ICE design is related to a characteristic of a sample; forming, by the fabrication system, at least some of the layers of a plurality of ICEs in accordance with the ICE design using a deposition source associated with the fabrication system, wherein the layers of the ICEs being formed are supported on a support that is moved with a periodic motion relative to the deposition source during said forming; monitoring, by a measurement system associated with the fabrication system, characteristics of the layers of the ICEs during said forming, wherein said monitoring the characteristics is performed using a timing of the periodic motion of the support relative to the deposition source; and adjusting said forming based on results of said monitoring.
An ear simulator representing an average acoustic ear drum impedance of ears of a population of humans, comprising: - a sound entrance plane, - a sound termination plane for arrangement of a diaphragm of a measurement microphone, - a frontal cavity of predetermined volume extending between the sound entrance plane and the sound termination plane, - a plurality of air cavities (22, 24, 26, 28) acoustically coupled to the sound termination plane through respective sound channels (22a, 24a, 26a, 28a), characterized in that: - at least one air cavity of the plurality of air cavities is situated behind the sound termination plane. - a sound entrance plane, - a sound termination plane for arrangement of a diaphragm of a measurement microphone, - a frontal cavity of predetermined volume extending between the sound entrance plane and the sound termination plane, - a plurality of air cavities (22, 24, 26, 28) acoustically coupled to the sound termination plane through respective sound channels (22a, 24a, 26a, 28a), characterized in that: - at least one air cavity of the plurality of air cavities is situated behind the sound termination plane.
A method for interface refresh synchronization, comprising: obtaining, in a user space of an operating system, refresh information of a plurality of interface refresh operations, when the plurality of interface refresh operations are initiated by a plurality of foreground applications in the user space, wherein the refresh information comprises a thread number of each interface refresh operation, refresh time and refresh contents corresponding to each thread number; and transmitting the obtained refresh information of the plurality of interface refresh operations to a kernel space of the operating system. obtaining, in a user space of an operating system, refresh information of a plurality of interface refresh operations, when the plurality of interface refresh operations are initiated by a plurality of foreground applications in the user space, wherein the refresh information comprises a thread number of each interface refresh operation, refresh time and refresh contents corresponding to each thread number; and transmitting the obtained refresh information of the plurality of interface refresh operations to a kernel space of the operating system.
A method of cutting a glass laminate comprising: forming a trench line in a surface of a glass substrate that is an uppermost layer of a glass laminate to a depth ranging from 10% to 20% of the thickness of the glass substrate by scoring the surface of the glass substrate; and cutting the glass laminate using a router bit in a direction parallel to the trench line at a distance of 10μm to 100μm from the center of the trench line. forming a trench line in a surface of a glass substrate that is an uppermost layer of a glass laminate to a depth ranging from 10% to 20% of the thickness of the glass substrate by scoring the surface of the glass substrate; and cutting the glass laminate using a router bit in a direction parallel to the trench line at a distance of 10μm to 100μm from the center of the trench line.
A gas turbine engine comprising: an oil tank storing lubricating oil; a cylindrical external case accommodating a compressor, a combustor, and a turbine; and a fan that includes fan blades and is accommodated in the external case, characterized in that the oil tank is arranged along an outer peripheral surface of the external case so as to surround the external case and is arranged at an axial position corresponding radially to the axial position of the fan that is configured to rotate to take in air and supplies the air to the compressor and a bypass passage located outside the compressor in a radial direction. an oil tank storing lubricating oil; a cylindrical external case accommodating a compressor, a combustor, and a turbine; and a fan that includes fan blades and is accommodated in the external case, characterized in that the oil tank is arranged along an outer peripheral surface of the external case so as to surround the external case and is arranged at an axial position corresponding radially to the axial position of the fan that is configured to rotate to take in air and supplies the air to the compressor and a bypass passage located outside the compressor in a radial direction.
Method for anticipating the entry of a rotorcraft into a vortex domain, the rotorcraft comprising a main rotor equipped with blades, characterised in that said method comprises the following steps: a) acquiring measurements of at least one parameter serving to characterise variation in the flow of air in the environment of the main rotor, b) analysing the measurements in order to isolate frequencies that are characteristic of the variation of each parameter, and c) detecting a specific frequency f characterising the proximity of a vortex domain, the specific frequency f being lower than 1 Hertz (Hz). a) acquiring measurements of at least one parameter serving to characterise variation in the flow of air in the environment of the main rotor, b) analysing the measurements in order to isolate frequencies that are characteristic of the variation of each parameter, and c) detecting a specific frequency f characterising the proximity of a vortex domain, the specific frequency f being lower than 1 Hertz (Hz).
An engine powered machine with safety system comprising: an engine configured to rotate a shaft coupled to a working tool; a fuel-air mixer fluidly coupled to the engine to provide a mixture of fuel and air; an ignition coil operatively connected to the engine to provide a plurality of sparks; a fuel supply fluidly coupled to the fuel-air mixer; a fuel solenoid operatively connected between the fuel supply and the fuel-air mixer, the fuel solenoid controlling a flow of fuel to the engine and movable between an open position in which fuel flows from the fuel supply through the fuel solenoid to the fuel-air mixer while the engine is in a running state, and a closed position in which the solenoid interrupts fuel flow to the fuel-air mixer while the engine is in an off state; and a safety switch operatively connected to the fuel solenoid and the ignition coil; wherein, upon activation of the safety switch, the ignition coil is disabled so that it no longer provides the plurality of sparks to the engine and the fuel solenoid simultaneously moves to the closed position to interrupt the flow of fuel from the fuel supply to the fuel-air mixer, characterized by further comprising a first relay that provides power to the fuel solenoid while the engine is in a running state and interrupts power to the fuel solenoid upon activation of the safety switch. an engine configured to rotate a shaft coupled to a working tool; a fuel-air mixer fluidly coupled to the engine to provide a mixture of fuel and air; an ignition coil operatively connected to the engine to provide a plurality of sparks; a fuel supply fluidly coupled to the fuel-air mixer; a fuel solenoid operatively connected between the fuel supply and the fuel-air mixer, the fuel solenoid controlling a flow of fuel to the engine and movable between an open position in which fuel flows from the fuel supply through the fuel solenoid to the fuel-air mixer while the engine is in a running state, and a closed position in which the solenoid interrupts fuel flow to the fuel-air mixer while the engine is in an off state; and a safety switch operatively connected to the fuel solenoid and the ignition coil; wherein, upon activation of the safety switch, the ignition coil is disabled so that it no longer provides the plurality of sparks to the engine and the fuel solenoid simultaneously moves to the closed position to interrupt the flow of fuel from the fuel supply to the fuel-air mixer, characterized by further comprising a first relay that provides power to the fuel solenoid while the engine is in a running state and interrupts power to the fuel solenoid upon activation of the safety switch.