mhurhangee/ep-ind-claims huggingface dataset:
A computer system for distributed shared execution of one or more shared processes, comprising: first program code for the one or more shared processes that comprises one or more shared code segments shared between a first authorizing node and a second authorizing node, wherein the one or more shared code segments are executable by one or more executing nodes; a distributed ledger that provides a record of valid code segments of the first program code; and second program code comprising instructions that, when executed by the first and/or second authorizing nodes, validates that an anticipated execution result of the one or more shared code segments satisfies shared authorization conditions and, if satisfied, authorizes the execution of the one or more shared code segments by the one or more executing nodes. first program code for the one or more shared processes that comprises one or more shared code segments shared between a first authorizing node and a second authorizing node, wherein the one or more shared code segments are executable by one or more executing nodes; a distributed ledger that provides a record of valid code segments of the first program code; and second program code comprising instructions that, when executed by the first and/or second authorizing nodes, validates that an anticipated execution result of the one or more shared code segments satisfies shared authorization conditions and, if satisfied, authorizes the execution of the one or more shared code segments by the one or more executing nodes.
A comfortable restraint system located in a vehicle incorporating an electronic braking system governed by a control unit, and comprising a safety belt configured by a textile strap, a permanent anchoring device which comprises means for coupling an anchor tongue joined to one end of the textile strap, a removable anchoring device and a retractor for the safety belt, wherein: - the safety belt comprises a chamber attached longitudinally on each side of the textile strap, and - the permanent anchoring device comprises connector outlets for the supply of pressurised air through a compression system, and - each one of the chambers comprises an adapter intended to be joined to a connector outlet, such that the chambers are pneumatically connected to the compression system with a proportional valve, in charge of supplying and extracting air to and from the chambers, which is governed by the vehicle control unit, the restraint system being characterised in that it is synchronised with the electronic braking system, such that the air extraction flow of the chambers is proportional to the braking intensity. - the safety belt comprises a chamber attached longitudinally on each side of the textile strap, and - the permanent anchoring device comprises connector outlets for the supply of pressurised air through a compression system, and - each one of the chambers comprises an adapter intended to be joined to a connector outlet, such that the chambers are pneumatically connected to the compression system with a proportional valve, in charge of supplying and extracting air to and from the chambers, which is governed by the vehicle control unit,
A method comprising: receiving, at a port, a reflected signal generated by an interrogation signal being reflected off a remote vibrating target; propagating the reflected signal down a first waveguide; splitting, by a first beam splitter, the reflected signal into a first portion propagating down the first waveguide and a second portion propagating down a second waveguide; delaying, by a delay element, a phase of one of the first and second portions of the reflected signal; spatially phase shifting, by one or more spatial phase shifters (318-1, 318-2), one or both of the first or second portions of the reflected signal; splitting, by a second beam splitter, the first and second portions of the reflected signal into a third portion propagating down the first waveguide and a fourth portion propagating down the second waveguide; detecting, by a split detector, an intensity difference between a first lobe and a second lobe of the third portion of the reflected signal; and calculating a Doppler frequency based on the intensity difference. receiving, at a port, a reflected signal generated by an interrogation signal being reflected off a remote vibrating target; propagating the reflected signal down a first waveguide; splitting, by a first beam splitter, the reflected signal into a first portion propagating down the first waveguide and a second portion propagating down a second waveguide; delaying, by a delay element, a phase of one of the first and second portions of the reflected signal; spatially phase shifting, by one or more spatial phase shifters (318-1, 318-2), one or both of the first or second portions of the reflected signal; splitting, by a second beam splitter, the first and second portions of the reflected signal into a third portion propagating down the first waveguide and a fourth portion propagating down the second waveguide; detecting, by a split detector, an intensity difference between a first lobe and a second lobe of the third portion of the reflected signal; and calculating a Doppler frequency based on the intensity difference.
A multi-ply security paper for manufacturing security or value documents, such as banknotes or identification cards, in which - into a first paper ply is introduced an endless security element (54; 66) that is freely accessible on at least one side of the paper ply, - the first paper ply is covered on the freely accessible side of the security element (54; 66) by a second paper ply, characterized in that the first paper ply exhibits a watermark, the second paper ply is interrupted in the region of the watermark, and the second paper ply exhibits one or more openings in the region of the security element (54; 66). - the first paper ply is covered on the freely accessible side of the security element (54; 66) by a second paper ply,
A method of detecting quenches in a superconducting magnet comprising a plurality of cables comprising HTS material in a coil, the method comprising: providing a plurality of optical fibres, wherein each cable of the coil of the superconducting magnet is in thermal contact with at least one of the optical fibres; monitoring backscattered light from each of the optical fibres; comparing changes in wavelength of backscattered light from each optical fibre; detecting a change in temperature of a cable of the coil on the basis of a change in wavelength observed in one or more first optical fibres of the plurality of optical fibres which are in thermal contact with the cable, but not observed in second optical fibres of the plurality of optical fibres which are not in thermal contact with the cable; in response to said detection of a change in temperature, determining that the cable has quenched; characterized in that the method further comprises the step of monitoring strain of the superconducting magnet by analysing changes in wavelength of backscattered light which are observed in substantially all of the optical fibres. providing a plurality of optical fibres, wherein each cable of the coil of the superconducting magnet is in thermal contact with at least one of the optical fibres; monitoring backscattered light from each of the optical fibres; comparing changes in wavelength of backscattered light from each optical fibre; detecting a change in temperature of a cable of the coil on the basis of a change in wavelength observed in one or more first optical fibres of the plurality of optical fibres which are in thermal contact with the cable, but not observed in second optical fibres of the plurality of optical fibres which are not in thermal contact with the cable; in response to said detection of a change in temperature, determining that the cable has quenched; characterized in that the method further comprises the step of monitoring strain of the superconducting magnet by analysing changes in wavelength of backscattered light which are observed in substantially all of the optical fibres. monitoring strain of the superconducting magnet by analysing changes in wavelength of backscattered light which are observed in substantially all of the optical fibres.
An intracellular Calcium signaling inhibitor for use in a method of ameliorating the symptoms of pancreatitis in a patient in need thereof, wherein said intracellular Calcium signaling inhibitor is a compound having the structure of: N -(5-(6-ethoxy-4-methylpyridin-3-yl)pyrazin-2-yl)-2,6-difluorobenzamide, N -(5-(2-ethyl-6-methylbenzo[ d]oxazol-5-yl)pyridin-2-yl)-3,5-difluoroisonicotinamide, N -(4-(1-ethyl-3-(thiazol-2-yl)-1 H -pyrazol-5-yl)phenyl)-2-fluorobenzamide, N -(5-(1-ethyl-3-(triflouromethyl)-1 H -pyrazol-5-yl)pyrazin-2-yl)-2,4,6-trifluorobenzamide, N -(4-(3-(difluoromethyl)-5-methyl-1 H -pyrazol-1-yl)-3-fluorophenyl)-2,6-difluorobenzamide, N -(4-(3-(difluoromethyl)-5-methyl-1 H -pyrazol-1-yl)-3-fluorophenyl)-2,4,6-trifluorobenzamide, N -(4-(3-(difluoromethyl)-1-methyl-1 H -pyrazol-5-yl)-3-fluorophenyl)-2,4,6-trifluorobenzamide, 3-fluoro-4-(1-methyl-3-(trifluoromethyl)-1 H -pyrazol-5-yl)- N -((3-methylisothiazol-4-yl)methyl)aniline, N -(2,6-difluorobenzyl)-5-(1-ethyl-3-(thiazol-2-yl)-1 H -pyrazol-5-yl)pyrimidin-2-amine, 3,5-difluoro- N -(3-fluoro-4-(3-methyl-1-(thiazol-2-yl)-1 H -pyrazol-4-yl)phenyl)isonicotinamide, N -(5-(1-ethyl-3-(trifluoromethyl)-1 H -pyrazol-5-yl)pyridin-2-yl)-2,4,6-trifluorobenzamide, N -(5-(5-chloro-2-methylbenzo[d]oxazol-6-yl)pyrazin-2-yl)-2,6-difluorobenzamide, N -(5-(6-ethoxy-4-methylpyridin-3-yl)thiazol-2-yl)-2,3,6-trifluorobenzamide, N -(5-(1-ethyl-3-(trifluoromethyl)-1 H -pyrazol-5-yl)pyridin-2-yl)-2,3,6-trifluorobenzamide, or N -(5-(6-chloro-2,2-difluorobenzo[ d][1,3]dioxol-5-yl)pyrazin-2-yl)-2-fluoro-6-methylbenzamide, or a pharmaceutically acceptable salt thereof. N -(5-(6-ethoxy-4-methylpyridin-3-yl)pyrazin-2-yl)-2,6-difluorobenzamide, N -(5-(2-ethyl-6-methylbenzo[ d]oxazol-5-yl)pyridin-2-yl)-3,5-difluoroisonicotinamide, N -(4-(1-ethyl-3-(thiazol-2-yl)-1 H -pyrazol-5-yl)phenyl)-2-fluorobenzamide, N -(5-(1-ethyl-3-(triflouromethyl)-1 H -pyrazol-5-yl)pyrazin-2-yl)-2,4,6-trifluorobenzamide, N -(4-(3-(difluoromethyl)-5-methyl-1 H -pyrazol-1-yl)-3-fluorophenyl)-2,6-difluorobenzamide, N -(4-(3-(difluoromethyl)-5-methyl-1 H -pyrazol-1-yl)-3-fluorophenyl)-2,4,6-trifluorobenzamide, N -(4-(3-(difluoromethyl)-1-methyl-1 H -pyrazol-5-yl)-3-fluorophenyl)-2,4,6-trifluorobenzamide, 3-fluoro-4-(1-methyl-3-(trifluoromethyl)-1 H -pyrazol-5-yl)- N -((3-methylisothiazol-4-yl)methyl)aniline, N -(2,6-difluorobenzyl)-5-(1-ethyl-3-(thiazol-2-yl)-1 H -pyrazol-5-yl)pyrimidin-2-amine, 3,5-difluoro- N -(3-fluoro-4-(3-methyl-1-(thiazol-2-yl)-1 H -pyrazol-4-yl)phenyl)isonicotinamide, N -(5-(1-ethyl-3-(trifluoromethyl)-1 H -pyrazol-5-yl)pyridin-2-yl)-2,4,6-trifluorobenzamide, N -(5-(5-chloro-2-methylbenzo[d]oxazol-6-yl)pyrazin-2-yl)-2,6-difluorobenzamide, N -(5-(6-ethoxy-4-methylpyridin-3-yl)thiazol-2-yl)-2,3,6-trifluorobenzamide, N -(5-(1-ethyl-3-(trifluoromethyl)-1 H -pyrazol-5-yl)pyridin-2-yl)-2,3,6-trifluorobenzamide, or N -(5-(6-chloro-2,2-difluorobenzo[ d][1,3]dioxol-5-yl)pyrazin-2-yl)-2-fluoro-6-methylbenzamide, or a pharmaceutically acceptable salt thereof.
A process for producing a rubber composition comprising a rubber component comprising at least one selected from natural rubbers and synthetic diene rubbers, a filler containing an inorganic filler, a silane coupling agent, and at least two kinds of chemical agents and selected from guanidines, sulfenamides, thiazoles, thiurams, dithiocarbamates, thioureas, and xanthates, wherein the rubber composition is kneaded in a plurality of stages wherein, in the first stage of kneading, the rubber component, all or a portion of the inorganic filler, all or a portion of the silane coupling agent, and at least two kinds of the chemical agents and are added and kneaded, wherein the maximum temperature of the rubber composition in the first stage of kneading is 120 to 190°C.
A method for evaluating a lifetime of a turbomachine part, comprising the following steps: S1: determining an average damage of the part as a function of time (E_moy(t)) based on a relationship expressing the stresses applied to the part as a function of a wear of the part (σ(u)) and of a relationship expressing the wear of the part as a function of time (u(t)); S2: determining a damage at failure (E_rupt) of the part; S3: determining a cumulative damage (E_cum) of the part corresponding to the damage at failure (E_rupt) of the part, said cumulative damage (E_cum) corresponding to the integral of the average damage as a function of time (E_moy(t)) between an initial time (t_0) and a final time t_rupt: E _ cum = E _ rupt = ∫ t _ 0 t _ rupt E _ moy t dt; and S4: deducing therefrom the lifetime of the part, said lifetime corresponding to the final time (t_rupt). S1: determining an average damage of the part as a function of time (E_moy(t)) based on a relationship expressing the stresses applied to the part as a function of a wear of the part (σ(u)) and of a relationship expressing the wear of the part as a function of time (u(t)); S2: determining a damage at failure (E_rupt) of the part; S3: determining a cumulative damage (E_cum) of the part corresponding to the damage at failure (E_rupt) of the part, said cumulative damage (E_cum) corresponding to the integral of the average damage as a function of time (E_moy(t)) between an initial time (t_0) and a final time t_rupt: E _ cum = E _ rupt = ∫ t _ 0 t _ rupt E _ moy t dt; and S4: deducing therefrom the lifetime of the part, said lifetime corresponding to the final time (t_rupt).
Heat exchanger device, comprising a plurality of cassettes (11, 21), where a first cassette comprises two plates of a first type and a second cassette comprises two plates of a second type, where each plate is provided with at least four portholes constituting inlet and outlet ports (14, 15, 16, 17) and a heat transfer surface, and a corrugated pattern having a plurality of ridges (19, 24) and valleys (20, 25) with side walls (22, 23, 26, 27) there between, where the corrugated pattern comprises undulations parallel to the direction of the corrugated pattern, and where the cassettes are mounted adjacent each other at a predefined distance, wherein the perpendicular distance (a 2) between the side walls (22, 23, 26, 27) of two adjacent cassettes (11, 21) is substantially constant over the width of the heat exchanger device, and that the corrugated pattern of the heat exchanger plates is substantially perpendicular to the main flow direction of the heat exchanger, characterized in that there are no contact points between the first cassette and the second cassette at the heat transfer surface.
Portable device for assisting with a vibroacoustic diagnosis for the analysis of noises in particular emitted by a motor vehicle, comprising a source of electric current supply, a loudspeaker, sensor s sound s clamp-type (14, 16, 18, 20) and a sensor audible type microphone and a connecting housing provided with sockets (28, 30, 32, 34, 36) electrical connection of the loudspeaker and of said at least one clamp (14, 16, 18, 20) and of the microphone-type sound sensor, the source of electric current supply being integrated into the connection box, the connection box 24 comprising several sockets (28, 30, 32, 34, 36, 38) for connection to different sound sensors (14, 16, 18, 20, 22), the sound sensors (14, 16, 18, 20, 22) being connectable simultaneously via the connection sockets (28, 30, 32, 34, 36, 38) and a switch for selecting the transmission of sound signals from the any of these sensors to the speaker, characterized in that the clip-type sound sensors (14, 16, 18, 20) are of different sizes and in that the connection box comprises means processing the signals supplied by the sensor sound (14, 16, 18, 20, 22) into at least one data file in a readable predetermined format by a computer and means for connecting to this computer.
A method of detecting one or more properties of a structure, wherein the method comprises: generating and storing calibration data determined from one or more test structures, wherein the one or more test structures are formed from a material that forms the structure; emitting X-ray radiation into the structure to scan the structure; detecting X-ray scatter from the structure; and determining the one or more properties of the structure based on a comparison of the detected X-ray scatter and the calibration data, characterized by that the one or more properties are at least one of mechanical and thermal properties and include a variation level of polymeric bonds within the structure. generating and storing calibration data determined from one or more test structures, wherein the one or more test structures are formed from a material that forms the structure; emitting X-ray radiation into the structure to scan the structure; detecting X-ray scatter from the structure; and determining the one or more properties of the structure based on a comparison of the detected X-ray scatter and the calibration data, characterized by that the one or more properties are at least one of mechanical and thermal properties and include a variation level of polymeric bonds within the structure.
A thrust reverser assembly for a gas turbine engine, the thrust reverser comprising: a hinge with a centre; a propulsion system duct through which bypass air and gas path air travel, the propulsion system duct having an intake inlet and an exhaust outlet; a kicker blocker that is a single component, the kicker blocker having a kicker portion and a blocker portion, the kicker blocker being rotatably attached to the hinge and rotatable about the centre of the hinge, the kicker blocker being movable between a stowed position and a deployed position; wherein the blocker portion is configured to extend into the propulsion system duct when the kicker blocker is in the deployed position to block bypass air and gas path air traveling through the propulsion system duct in a first direction prior to the exhaust outlet, thereby redirecting the bypass air and the gas path air in a second direction; and wherein the kicker portion is configured to extend out of the propulsion system duct when the kicker blocker is in the deployed position. a hinge with a centre; a propulsion system duct through which bypass air and gas path air travel, the propulsion system duct having an intake inlet and an exhaust outlet; a kicker blocker that is a single component, the kicker blocker having a kicker portion and a blocker portion, the kicker blocker being rotatably attached to the hinge and rotatable about the centre of the hinge, the kicker blocker being movable between a stowed position and a deployed position; wherein the blocker portion is configured to extend into the propulsion system duct when the kicker blocker is in the deployed position to block bypass air and gas path air traveling through the propulsion system duct in a first direction prior to the exhaust outlet, thereby redirecting the bypass air and the gas path air in a second direction; and wherein the kicker portion is configured to extend out of the propulsion system duct when the kicker blocker is in the deployed position.
A belt-type continuously variable transmission comprising a fixed sheave that is fixed to a crankshaft, a movable sheave that is supported on the crankshaft so as to be movable in an axial direction of the crankshaft while being made to face the fixed sheave, a belt that is wound around a pulley formed by the fixed sheave and the movable sheave, a speed change member that is relatively non-displaceably disposed with respect to the fixed sheave in the axial direction and has a cam face that is configured to approach the fixed sheave in going away from a rotational axis (Xis) of the crankshaft, a centrifugal weight that is sandwiched between the speed change member and the movable sheave and that is configured to move along the cam face in a centrifugal direction in response to an increase in centrifugal force to thus drive the movable sheave in the axial direction, an amplification member (93, 164) that is mechanically linked to the movable sheave and that rotates around a rotational axis (Xp) and that has a plurality of restriction bodies (92, 163), which are arranged in one line so as to cover a speed range from a lowest speed level to a highest speed level along an arc (118a, 172) that is concentric with the rotational axis (Xp) and which are configured to move on a specific trajectory with an amount of displacement that is obtained by amplifying the amount of displacement in the axial direction of the movable sheave, and a lock member (94, 165) that is linked to a solenoid actuator (78, 173) comprising an operating shaft that has an axis parallel to the rotational axis (Xp), wherein the lock member (94, 165) is configured to be displaced linearly between a first position at which the lock member (94, 165) comes into contact with any one of the restriction bodies (92, 163) of the amplification member (93, 164)to thus restrict movement of the restriction body (92, 163), restrict rotation of the amplification member (93, 164) and prevent movement of the movable sheave, thereby fixing a gear ratio corresponding to the one restriction body (92, 163), and a second position at which the lock member (94, 165) disengages from the restriction body (92, 163) to thus allow movement of the restriction body (92, 163). a first position at which the lock member (94, 165) comes into contact with any one of the restriction bodies (92, 163) of the amplification member (93, 164)to thus restrict movement of the restriction body (92, 163), restrict rotation of the amplification member (93, 164) and prevent movement of the movable sheave, thereby fixing a gear ratio corresponding to the one restriction body (92, 163), and a second position at which the lock member (94, 165) disengages from the restriction body (92, 163) to thus allow movement of the restriction body (92, 163).
A method for controlling a transmit power of a wireless device in a wireless local area network, the method comprising: receiving a frame comprising transmit power information element comprising one or more maximum transmit power fields (631b, 731b); and determining an actual maximum of transmit power level from the transmit power information element, wherein the actual maximum of transmission power level is based on channel bandwidth and a maximum transmit power per transmission channel, wherein the transmit power information element comprises maximum transmit power information for channel bandwidths for a plurality of transmission channels supported by a basic service set to which the wireless device is associated; and wherein the transmit power information element comprises transmit power below the maximum transmit power information for a channel bandwidth for each transmission channel of the plurality of transmission channels. receiving a frame comprising transmit power information element comprising one or more maximum transmit power fields (631b, 731b); and determining an actual maximum of transmit power level from the transmit power information element, wherein the actual maximum of transmission power level is based on channel bandwidth and a maximum transmit power per transmission channel, wherein the transmit power information element comprises maximum transmit power information for channel bandwidths for a plurality of transmission channels supported by a basic service set to which the wireless device is associated; and wherein the transmit power information element comprises transmit power below the maximum transmit power information for a channel bandwidth for each transmission channel of the plurality of transmission channels.