mhurhangee/ep-ind-claims huggingface dataset:
A system for determining the integrity of a container containing at least one gas, said system comprises: an environment with a lower absolute gas pressure than the pressure inside the container; wherein said environment is an at least partially open enclosure or a closed enclosure; and wherein said at least partially open enclosure, or closed enclosure, is configured to have said container positioned therein, characterized in that the system further comprises a light source and a detector, wherein the said light source is arranged to transmit a light signal to said detector through said environment, but only outside of said container; wherein said light source and said detector are configured as an optical sensor using tunable diode laser absorption spectroscopy; and a control unit for determining, based on said transmitted light signal being detected, if a level of said at least one gas inside said container is altered in said environment. an environment with a lower absolute gas pressure than the pressure inside the container; wherein said environment is an at least partially open enclosure or a closed enclosure; and wherein said at least partially open enclosure, or closed enclosure, is configured to have said container positioned therein, characterized in that the system further comprises a light source and a detector, wherein the said light source is arranged to transmit a light signal to said detector through said environment, but only outside of said container; wherein said light source and said detector are configured as an optical sensor using tunable diode laser absorption spectroscopy; and a control unit for determining, based on said transmitted light signal being detected, if a level of said at least one gas inside said container is altered in said environment.
A mobile terminal device connectable to a network, comprising: a rechargeable battery serving as a power supply of the mobile terminal device; charger identification information reception means adapted to receive, from a charger connected to charge said rechargeable battery, charger identification information to be used to identify the charger; setting information storage means adapted to store setting information associated with the charger identification information; setting information extraction means adapted to extract, from said setting information storage means, the setting information corresponding to the charger identification information received by said charger identification information reception means; and setting means adapted to set, in the mobile terminal device, the setting information extracted by said setting information extraction means, wherein the setting information comprises function restriction setting information that restricts a function of the mobile terminal device, and wherein the charger identification information comprises information to identify an area where the charger is arranged, and wherein the setting is the silent mode. a rechargeable battery serving as a power supply of the mobile terminal device; charger identification information reception means adapted to receive, from a charger connected to charge said rechargeable battery, charger identification information to be used to identify the charger; setting information storage means adapted to store setting information associated with the charger identification information; setting information extraction means adapted to extract, from said setting information storage means, the setting information corresponding to the charger identification information received by said charger identification information reception means; and setting means adapted to set, in the mobile terminal device, the setting information extracted by said setting information extraction means, wherein the setting information comprises function restriction setting information that restricts a function of the mobile terminal device, and wherein the charger identification information comprises information to identify an area where the charger is arranged, and wherein the setting is the silent mode.
A method of opening a shunt switch (8, 9, 10, 11) carrying a current, the switch being connected in parallel with at least one thyristor (4, 5, 6, 7) of a high voltage DC network, interruption of the current flowing through the switch being initiated at the time of a current zero of the current flowing through the switch, the method being characterized in that it includes, based on a measurement effected by means for measuring the current flowing through the switch, a step of adjusting a control angle of the thyristor to position the current zero in a zone in which the time derivative of the measured current is a continuous function and the absolute value of a peak value of the measured current is substantially equal to the absolute value of the inaccuracy of the measurement of the current zero.
An elevator system comprising: a hoistway; one or more elevator system components fixed in the hoistway; an elevator car suspended in the hoistway via a suspension member and drivable along the hoistway, the elevator car including an access door openable from inside the elevator car to provide access to the one or more elevator system components in the hoistway, such that inspection, maintenance and/or repair can be performed on the one or more elevator system components from inside of the elevator car; characterized in that the elevator system further comprises a telescoping mechanism to urge the elevator system component away from a hoistway wall and toward the elevator car. a hoistway; one or more elevator system components fixed in the hoistway; an elevator car suspended in the hoistway via a suspension member and drivable along the hoistway, the elevator car including an access door openable from inside the elevator car to provide access to the one or more elevator system components in the hoistway, such that inspection, maintenance and/or repair can be performed on the one or more elevator system components from inside of the elevator car; characterized in that the elevator system further comprises a telescoping mechanism to urge the elevator system component away from a hoistway wall and toward the elevator car.
A device for adjusting a base of a spring element for a vehicle, the device comprising a first wall element for connection to a vehicle, a second wall element spaced from the first wall element for connection to the spring element, and a chamber disposed between the first wall element and the second wall element for changing the distance between the first wall element and the second wall element by changing a volume of the chamber,wherein the chamber comprises an incompressible fluid and the first and/or second wall element comprises a passage opening for the incompressible fluid to the chamber, the passage opening being fluidly communicably connectable to an input/output device for the incompressible fluid for changing the volume of the chamber, wherein the chamber has a chamber wall with at least one third wall element extending from the first wall element to the second wall element, the mass of the third wall element being constant when the volume of the chamber is changed, wherein the device further comprises an axial guide being arranged in the chamber and comprising a centering element and a guide element, wherein the guide element is configured to guide the centering element in axial direction of the spring element and the centering element is slidingly connected to the guide element, wherein the centering element is connected to the first or the second wall element (14, 16) and the guide element is connected to the respective other wall element (14, 16) and wherein the third wall element extends around the axial guide, characterized in that the device further comprises a separate element which has a receiving geometry for the spring element, an additional receiving geometry for the second wall element and a part of the third wall element, and an outer guide for the third wall element, which extends over the spring element.
A method for operating an aircraft, comprising: receiving an input corresponding to an aircraft component structural response of an aircraft component to an aerodynamic load; and based at least in part on the input corresponding to the aircraft component structural response, reducing the aircraft component structural response to the aerodynamic load by activating at least one plasma actuator carried by the aircraft, in accordance with one or more activation parameters; wherein: receiving the input includes receiving the input that in turn includes an amplitude, frequency and phase of the aircraft component structural response; and reducing the aircraft component structural response includes altering the amplitude of the aircraft component structural response by generating an effect in a flowfield adjacent to the aircraft component as a result of activating the at least one plasma actuator. receiving an input corresponding to an aircraft component structural response of an aircraft component to an aerodynamic load; and based at least in part on the input corresponding to the aircraft component structural response, reducing the aircraft component structural response to the aerodynamic load by activating at least one plasma actuator carried by the aircraft, in accordance with one or more activation parameters; wherein: receiving the input includes receiving the input that in turn includes an amplitude, frequency and phase of the aircraft component structural response; and reducing the aircraft component structural response includes altering the amplitude of the aircraft component structural response by generating an effect in a flowfield adjacent to the aircraft component as a result of activating the at least one plasma actuator. receiving the input includes receiving the input that in turn includes an amplitude, frequency and phase of the aircraft component structural response; and reducing the aircraft component structural response includes altering the amplitude of the aircraft component structural response by generating an effect in a flowfield adjacent to the aircraft component as a result of activating the at least one plasma actuator.
Process for the acetoxylation of olefins in a gaseous reaction stream containing an olefin, acetic acid and an oxygen-containing gas, wherein the reaction gas is passed over at least two catalyst zones of differing reactivity arranged in series, where the catalyst zones are located in one or more reaction tubes arranged in parallel.
A compound of formula, or a salt thereof preferably of formula (XV-a) wherein R5 is selected from hydrogen and a group -CO-OR*, and Ra and R* are, independently of each other, selected from hydrogen, a carboxyl protecting group, and C 1 -C 6 -alkyl, preferably ethyl, wherein the carboxyl protecting group is selected from C 6 -C 10 -aryl-C 1 -C 6 -alkyl and SiR11R12R13, wherein R11, R12, and R13 are, independently of each other, C 1 -C 7 -alkyl, C 6 -C 10 -aryl or phenyl-C 1- C 4 -alkyl. R5 is selected from hydrogen and a group -CO-OR*, and Ra and R* are, independently of each other, selected from hydrogen, a carboxyl protecting group, and C 1 -C 6 -alkyl, preferably ethyl, wherein the carboxyl protecting group is selected from C 6 -C 10 -aryl-C 1 -C 6 -alkyl and SiR11R12R13, wherein R11, R12, and R13 are, independently of each other, C 1 -C 7 -alkyl, C 6 -C 10 -aryl or phenyl-C 1- C 4 -alkyl.
A cast resin transformer having a seismic structure to prevent detachment of a spacer by reducing a displacement occurring when an external force exerts on the cast resin transformer, comprising: a bed frame seated on a floor; a lower frame coupled to the top of the bed frame; at least one coil installed on the top of the lower frame; an upper frame installed on the top of the coil and located in parallel with the lower frame; a core connected to the coil; a spacer interposed between the coil and the lower frame; a protrusion part which protrudes from the top of the lower frame and is inserted in a groove formed in the lower end of the spacer so as to prevent the spacer interposed between the lower frame and the coil from being detached; and a reinforcement part connected between the bed frame and the lower frame so as to provide a reinforcing function against an external force, wherein the groove has a size larger than the width of the protrusion part and the spacer is formed so as to move within a clearance space in a state where the protrusion part is inserted in the groove. a bed frame seated on a floor; a lower frame coupled to the top of the bed frame; at least one coil installed on the top of the lower frame; an upper frame installed on the top of the coil and located in parallel with the lower frame; a core connected to the coil; a spacer interposed between the coil and the lower frame; a protrusion part which protrudes from the top of the lower frame and is inserted in a groove formed in the lower end of the spacer so as to prevent the spacer interposed between the lower frame and the coil from being detached; and a reinforcement part connected between the bed frame and the lower frame so as to provide a reinforcing function against an external force, wherein the groove has a size larger than the width of the protrusion part and the spacer is formed so as to move within a clearance space in a state where the protrusion part is inserted in the groove.
A method of performing duplicate detection for a hybrid automatic repeat request (HARQ) transmission, comprising: receiving subpackets on frames of an ARQ channel, wherein subpackets containing sufficient information to decode a same packet are assigned sequential identifiers and are received in sequential order; decoding a first packet based on a subpacket received on a current frame of the ARQ channel; if the first packet is correctly decoded, obtaining the identifier of the subpacket received on the current frame of the ARQ channel and setting an unexpected identifier for the ARQ channel, the unexpected identifier being for a subpacket not expected to be received on the ARQ channel, to the identifier of the subpacket received on the current frame on the ARQ channel plus one; decoding a second packet based on a subpacket received on the next frame of the ARQ channel; and if the second packet is correctly decoded, obtaining the identifier of the subpacket received on the next frame of the ARQ channel and declaring the second packet to be a duplicate of the first packet if the identifier of the subpacket received on the next frame is equal to the unexpected identifier. receiving subpackets on frames of an ARQ channel, wherein subpackets containing sufficient information to decode a same packet are assigned sequential identifiers and are received in sequential order; decoding a first packet based on a subpacket received on a current frame of the ARQ channel; if the first packet is correctly decoded, obtaining the identifier of the subpacket received on the current frame of the ARQ channel and setting an unexpected identifier for the ARQ channel, the unexpected identifier being for a subpacket not expected to be received on the ARQ channel, to the identifier of the subpacket received on the current frame on the ARQ channel plus one; decoding a second packet based on a subpacket received on the next frame of the ARQ channel; and if the second packet is correctly decoded, obtaining the identifier of the subpacket received on the next frame of the ARQ channel and declaring the second packet to be a duplicate of the first packet if the identifier of the subpacket received on the next frame is equal to the unexpected identifier.
A fuzing system for a signal flare for use on a submarine vessel, said system comprising an ignition system that is operationally connected to a signalling substance in such a way that said signalling substance can be ignited by activating said ignition system, wherein a hydrostatic device is arranged to activate said ignition system at a predetermined surrounding pressure, and wherein said system comprises a movable central piston member associated with the hydrostatic device, whereby said hydrostatic device comprises a movable member which in one end is arranged with a hydrostatic spring device exerting a predetermined force onto the movable member, and which movable member in its other end is subjected to a pressure which equals the pressure surrounding said fuzing system, characterized in that said spring device is preloaded so that it upon launch of the fusing system from a submarine immediately exerts a pushing force against the movable member in a direction towards an activating position, wherein further the piston member upon launch is arranged to be pushed downwards with respect to the launching direction, simultaneously compressing an ignition spring member and locking the ignition spring member in a compressed position until a point where said predetermined surrounding pressure leads to that the movable member reaches an activating position, in which position said movable member is arranged to cause release of the ignition spring member thereby causing ignition of the ignition system.
Device for adjustable fixing of a panel, which comprises two glass plates (1a, 1b) connected to one another, which comprise at least two recesses (11a, 11b) that correspond to one another, to a frame element provided with a lower assembly profile, with an anchoring bolt serving to hold the panel which comprises anchoring pins on both sides which are insertable into grooves which lie opposite each other within the assembly profile, and which eccentrically holds two cylindrical outer eccentric elements (2a, 2b), which are insertable each in one of the cylindrical openings (21a, 21b) preferably without play, which comprise cylindrical openings (21a, 21b), characterised in that in the cylindrical openings (21a, 21b) of the outer eccentric elements (2a, 2b), which are orientated concentrically with each other after assembly, a shaft of an inner eccentric element is held inserted therein preferably without play, which comprises an eccentrically arranged, preferably cylindrical opening, in which the anchoring bolt is held and that the inner eccentric element comprises on at least one side of the shaft a coupling element, such as a polygonal nut, which corresponds to an adjusting tool.
A microorganism from the species Sphingopyxis sp. deposited in the Spanish Type Culture Collection (CECT) with accession number CECT 8967 or a mutant thereof which maintains the ability of degrading microcystins.
Apparatus including inductive coupling communication means (D2, ACT) designed to communicate in peer-to-peer mode with another identical apparatus (DV'), and a housing, said communication means including a flat antenna coil (AC, AC1-AC7) tuned to a working frequency, the antenna coil being arranged near a wall of the housing of the apparatus, characterized in that: - the antenna coil is asymmetrical relative to a central longitudinal axis or central transverse axis of the wall of the housing of the apparatus, - the asymmetry of the antenna coil is designed such that when the wall of the housing of the apparatus is positioned so as to face the same wall of the other identical apparatus (DV'), the ratio between the sum of the mutually facing surfaces of loops of the same row of the antenna coil and of the antenna coil of the other identical apparatus, and the sum of the surfaces of the loops (Wi) of the antenna coil, is always less than or equal to: - 0.6 if the coil comprises 4 or more loops, - 0.7 if the coil comprises 3 loops, or - 0.8 if the coil comprises 1 or 2 loops. - the antenna coil is asymmetrical relative to a central longitudinal axis or central transverse axis of the wall of the housing of the apparatus, - the asymmetry of the antenna coil is designed such that when the wall of the housing of the apparatus is positioned so as to face the same wall of the other identical apparatus (DV'), the ratio between the sum of the mutually facing surfaces of loops of the same row of the antenna coil and of the antenna coil of the other identical apparatus, and the sum of the surfaces of the loops (Wi) of the antenna coil, is always less than or equal to: - 0.6 if the coil comprises 4 or more loops, - 0.7 if the coil comprises 3 loops, or - 0.8 if the coil comprises 1 or 2 loops.
A method comprising: providing a fixture including a target in a field of view of a sensor mounted to a vehicle, wherein the target is detectable by the sensor, and the fixture includes a first rangefinding device and a second rangefinding device spaced from the first rangefinding device; measuring a first angle (α 1) and first distance (d 1) from the first rangefinding device to a first known point on the vehicle; measuring a second angle (α 2) and second distance (d 2) from the second rangefinding device to a second known point on the vehicle; determining a position (x, y, z) v and orientation (φ, θ, ψ) v of the target in a coordinate system relative to the vehicle based on the first angle (α 1), the first distance (d 1), the second angle (α 2), and the second distance (d 2); and calibrating the sensor based on the position (x, y, z) v and orientation (φ, θ, ψ) v of the target. providing a fixture including a target in a field of view of a sensor mounted to a vehicle, wherein the target is detectable by the sensor, and the fixture includes a first rangefinding device and a second rangefinding device spaced from the first rangefinding device; measuring a first angle (α 1) and first distance (d 1) from the first rangefinding device to a first known point on the vehicle; measuring a second angle (α 2) and second distance (d 2) from the second rangefinding device to a second known point on the vehicle; determining a position (x, y, z) v and orientation (φ, θ, ψ) v of the target in a coordinate system relative to the vehicle based on the first angle (α 1), the first distance (d 1), the second angle (α 2), and the second distance (d 2); and calibrating the sensor based on the position (x, y, z) v and orientation (φ, θ, ψ) v of the target.
A housing (200; 600) having a plastic top portion (202, 208; 702) and a metal bottom portion and at least a mounting foot (206; 602) for attaching the housing (200; 600) to a surface, the mounting foot (206; 602) being formed by assembly of the plastic top portion (202, 208; 702) and the metal bottom portion, wherein the mounting foot (206; 602) comprises: a first cylindrical part (220; 704) comprising a cylindrical hole (218; 712) formed in the plastic top portion (202; 702); and a second cylindrical part (224; 702) formed on the metal bottom portion by stamping, the second cylindrical part (224; 702) extending inside the first cylindrical part (220; 704) when the plastic top portion (202, 208; 702) is joined with the metal bottom portion and configured to limit deformation of the first cylindrical part (220; 704) responsive to a compressive load impressed on the mounting foot (206; 602). a first cylindrical part (220; 704) comprising a cylindrical hole (218; 712) formed in the plastic top portion (202; 702); and a second cylindrical part (224; 702) formed on the metal bottom portion by stamping, the second cylindrical part (224; 702) extending inside the first cylindrical part (220; 704) when the plastic top portion (202, 208; 702) is joined with the metal bottom portion and configured to limit deformation of the first cylindrical part (220; 704) responsive to a compressive load impressed on the mounting foot (206; 602).