mhurhangee/ep-ind-claims huggingface dataset:
Sensor synchronization method having the following method steps: a) determining at least a first latency of a first sensor and a second latency of a second sensor, b) capturing at least a first data rate of the first sensor and a second data rate of the second sensor, wherein the first data rate is in a ratio of 2 n with respect to the second data rate, where n is an element from the set of natural numbers N 0, including the number zero, c) starting a central timer, d) generating a countdown timer on the basis of a value of the central timer and the first data rate, and generating a second countdown timer on the basis of the value of the central timer and the second data rate, and e) providing the first countdown timer for the first sensor and the second countdown timer for the second sensor, wherein the first sensor begins the measurement at the latest when the first latency is equal to the value of the first countdown timer, and wherein the second sensor begins the measurement at the latest when the second latency is equal to the value of the second countdown timer, f) outputting a first measured value from the first sensor and a second measured value from the second sensor in a synchronized manner. a) determining at least a first latency of a first sensor and a second latency of a second sensor, b) capturing at least a first data rate of the first sensor and a second data rate of the second sensor, wherein the first data rate is in a ratio of 2 n with respect to the second data rate, where n is an element from the set of natural numbers N 0, including the number zero, c) starting a central timer, d) generating a countdown timer on the basis of a value of the central timer and the first data rate, and generating a second countdown timer on the basis of the value of the central timer and the second data rate, and e) providing the first countdown timer for the first sensor and the second countdown timer for the second sensor, wherein the first sensor begins the measurement at the latest when the first latency is equal to the value of the first countdown timer, and wherein the second sensor begins the measurement at the latest when the second latency is equal to the value of the second countdown timer, f) outputting a first measured value from the first sensor and a second measured value from the second sensor in a synchronized manner.
A spout (200, 600) for a container (100, 500), comprising: a central duct (230, 630) defining a pouring passage (240, 640) configured to communicate with an interior of the container (100, 500) and extend through an opening (120, 520) of the container (100, 500); an outer sidewall (210, 610) extending around the central duct (230, 630), the outer sidewall (210, 610) configured to engage an interior surface (112, 512) of the container (100, 500) and having an upper end (212, 612) and a flange projecting in a radial direction from the upper end; (212, 612) and a seal ring (250, 650) disposed on the flange of the outer sidewall (210, 610), wherein the central duct (230, 630) and the outer sidewall (210, 610) comprise a first material having a first durometer and the seal ring (250, 650) comprises a second material having a second durometer less than the first durometer, characterized in that an interior surface of the seal ring (250, 650) is flush with an interior surface of the outer sidewall (210, 610). a central duct (230, 630) defining a pouring passage (240, 640) configured to communicate with an interior of the container (100, 500) and extend through an opening (120, 520) of the container (100, 500); an outer sidewall (210, 610) extending around the central duct (230, 630), the outer sidewall (210, 610) configured to engage an interior surface (112, 512) of the container (100, 500) and having an upper end (212, 612) and a flange projecting in a radial direction from the upper end; (212, 612) and a seal ring (250, 650) disposed on the flange of the outer sidewall (210, 610), wherein the central duct (230, 630) and the outer sidewall (210, 610) comprise a first material having a first durometer and the seal ring (250, 650) comprises a second material having a second durometer less than the first durometer, characterized in that an interior surface of the seal ring (250, 650) is flush with an interior surface of the outer sidewall (210, 610).
A sterile drape for covering a surgical robotic arm and preventing contamination of a sterile field, the sterile drape comprising a flexible covering with a sterile outer surface and a sterile drape sleeve configured to receive an electrical plug therethrough, said covering being at least partially conformable to a surgical robotic arm, wherein the sterile drape sleeve is configured to be sealed around a portion of the electrical plug using a sterile adhesive tape, wherein the sterile drape sleeve is configured to surround at least a portion of a connector of the surgical robotic arm and extend outwardly from the connector, wherein the sterile drape includes a drape stiffener in the form of a supporting tube configured to allow the plug to pass through the sterile drape sleeve.
A base station, BS, for handling buffer status reporting for data duplication, comprising: a storage device; and a processing circuit, coupled to the storage device, wherein the storage device stores, and the processing circuit is configured to execute, instructions of: configuring a radio bearer, RB, and configuring a first logical channel, LC, and a second LC associated to the RB, to a communication device; configuring the communication device to report separate buffer statuses for the first LC and the second LC associated to the RB; receiving a first buffer status comprising a volume of data associated to the first LC and a second buffer status comprising a volume of data associated to the second LC, from the communication device; transmitting a first UL grant to the communication device according to the first buffer status; and transmitting a second UL grant to the communication device according to the second buffer status. a storage device; and a processing circuit, coupled to the storage device, wherein the storage device stores, and the processing circuit is configured to execute, instructions of: configuring a radio bearer, RB, and configuring a first logical channel, LC, and a second LC associated to the RB, to a communication device; configuring the communication device to report separate buffer statuses for the first LC and the second LC associated to the RB; receiving a first buffer status comprising a volume of data associated to the first LC and a second buffer status comprising a volume of data associated to the second LC, from the communication device; transmitting a first UL grant to the communication device according to the first buffer status; and transmitting a second UL grant to the communication device according to the second buffer status. configuring a radio bearer, RB, and configuring a first logical channel, LC, and a second LC associated to the RB, to a communication device; configuring the communication device to report separate buffer statuses for the first LC and the second LC associated to the RB; receiving a first buffer status comprising a volume of data associated to the first LC and a second buffer status comprising a volume of data associated to the second LC, from the communication device; transmitting a first UL grant to the communication device according to the first buffer status; and transmitting a second UL grant to the communication device according to the second buffer status.
A method for a seeker, in a missile in flight, to locate a moving target, the method comprising: (a) measuring, at a plurality of moments during the flight of the missile, the location of the missile and the range to the target; (b) calculating the location of the target from the measured ranges and the measured missile locations; and (c) measuring Doppler information to determine a closing velocity of the missile relative to the target and using the Doppler information, in synthetic aperture radar processing, to separate the target from other targets and clutter in the calculation of the location of the target and in calculation of a velocity of the target. (a) measuring, at a plurality of moments during the flight of the missile, the location of the missile and the range to the target; (b) calculating the location of the target from the measured ranges and the measured missile locations; and (c) measuring Doppler information to determine a closing velocity of the missile relative to the target and using the Doppler information, in synthetic aperture radar processing, to separate the target from other targets and clutter in the calculation of the location of the target and in calculation of a velocity of the target.
A method of performing an injection molding cycle in an injection molding apparatus comprising a manifold that receives an injection fluid, the manifold distributing injection fluid to a fluid delivery channel that delivers the injection fluid under an injection pressure to a gate of a mold cavity and a valve pin having an axis and a tip end, the valve pin being slidably mounted for movement along the axis within the fluid delivery channel, whereas the method comprises, drivably interconnecting the valve pin to an electric motor driven by a source of electrical power or energy in an arrangement wherein the electric motor drives the valve pin along the axis and drives the tip end of the valve pin between a first position where the tip end of the valve pin obstructs the gate to prevent the injection fluid from flowing into the cavity, a second position upstream of the first position wherein the tip end of the valve pin restricts flow of the injection fluid along at least a portion of the length of the drive path (RP, RP2) extending between the first position and the second position, and a third maximum upstream position where the injection fluid material flows freely without restriction from the tip end of the pin through the first gate, the electric motor being electrically operable to drive the valve pin at one or more intermediate rates of upstream and downstream travel extending between zero and a maximum rate of upstream travel and a maximum rate of downstream travel, characterized in that the method comprises controllably operating the electric motor to drive the valve pin at one or more intermediate rates of downstream travel that are less than the maximum rate of downstream travel beginning when the valve pin is disposed at the third maximum upstream position during the course of an injection cycle to drive the tip end of the valve pin continuously downstream from the third position along at least a portion (RP, RP2) of the length of the drive path extending between the first position and the third position where the tip end of the valve pin restricts flow of the injection fluid to the first position where the gate is closed at the one or more intermediate rates of downstream travel.
A method for estimating a time offset of a transmitted signal which comprises pilot symbols and data symbols received by a receiver, the method comprising: receiving and sampling, by the receiver the transmitted signal to produce a received signal; and processing an optimising function of the received signal at a finite number of possible time offsets to produce an estimate of the time offset wherein the optimising function is a function of both pilot symbols and data symbols wherein the optimising function is processed at the finite number of possible time offsets τ 1, τ 2,..., τ K for some positive integer K where τ i +1 - τ i =Δ, and Δ= T / c where T is the symbol period of the pilot symbols and data symbols, and c is a positive integer. receiving and sampling, by the receiver the transmitted signal to produce a received signal; and processing an optimising function of the received signal at a finite number of possible time offsets to produce an estimate of the time offset wherein the optimising function is a function of both pilot symbols and data symbols wherein the optimising function is processed at the finite number of possible time offsets τ 1, τ 2,..., τ K for some positive integer K where τ i +1 - τ i =Δ, and Δ= T / c where T is the symbol period of the pilot symbols and data symbols, and c is a positive integer.
A luminaire housing formed by a cover or by a cover cooperating with a base and the luminaire housing comprising a light chamber at least partially delimited by a light-transmissive wall with a thickness Tw of said cover comprising at least one rounded corner section in between two further linear, planar sections, said light chamber comprising a mounting region in which at least one solid state lighting element is mounted, wherein the rounded corner section has an inner surface having opposing inner endpoints (103, 105) and an outer surface having opposing outer endpoints (113, 115), wherein the light-transmissive cover comprises a pair of said rounded corner sections, and wherein one of said further sections is located in between the pair of rounded corner sections, and wherein the light transmissive wall is of constant thickness, characterized in that - a plane (P1,P2) under critical angle θc at the inner surface at an inner endpoint (103,105) does not extend through the outer surface of the rounded corner section, such that no ray of light (301, 301') emitted by the at least one solid state lighting element entering the light-transmissive cover via the further inner surface of the further section exits the light-transmissive cover from the outer surface of the rounded corner section. - a plane (P1,P2) under critical angle θc at the inner surface at an inner endpoint (103,105) does not extend through the outer surface of the rounded corner section, such that no ray of light (301, 301') emitted by the at least one solid state lighting element entering the light-transmissive cover via the further inner surface of the further section exits the light-transmissive cover from the outer surface of the rounded corner section.
A device for holding LED luminous elements comprising: a. a carrier element connectable to the power supply with contact surfaces, and b. a clamping element connectable with the carrier element for holding an LED chip with contact elements for electrically connecting the contact surfaces of the carrier element with connection points of the LED chip characterised in that the contact elements are formed integrally with the clamping element. a. a carrier element connectable to the power supply with contact surfaces, and b. a clamping element connectable with the carrier element for holding an LED chip with contact elements for electrically connecting the contact surfaces of the carrier element with connection points of the LED chip characterised in that the contact elements are formed integrally with the clamping element.
An assembly for a combustion chamber of a turbomachine, comprising an annular shell (3, 4) extending along a longitudinal axis, said shell (3, 4) comprising an inner wall intended to be turned towards a furnace of the combustion chamber and an outer wall opposite the inner wall, a projecting element extending radially from an area of the outer wall, characterized in that the shell (3, 4) has at least one plurality of deflectors projecting from the outer wall and located downstream of the projecting element with respect to a direction of gas flow along the outer wall, oriented along the longitudinal axis, each deflector extending circumferentially, the deflectors being axially offset from each other, perforations being provided in the shell (3, 4), axially between the projecting element and the or each deflector, and axially between the deflectors, with the perforations opening at the inner wall and the outer wall, at least one deflector being inclined axially in the upstream direction with respect to the outer wall.
A power generation facility comprising: a plurality of exhaust gas generating sources (11, 31); a plurality of turbochargers (14, 34) driven by exhaust gas from the plurality of exhaust gas generating sources (11, 31); a plurality of power generators (20, 40) connected to the plurality of turbochargers (14, 34); a plurality of converters (22, 42) for converting AC power generated by the plurality of power generators (20, 40) to DC power; one inverter for converting the DC power outputted from the plurality of converters (22, 42) to AC power; and a control device for controlling the plurality of exhaust gas generating sources (11, 31) or the plurality of turbochargers (14, 34) in accordance with the AC power from the inverter, whereby the plurality of exhaust gas generating sources (11, 31) are engines, and the control device is configured to control the engines so that the AC power from the inverter becomes constant. a plurality of exhaust gas generating sources (11, 31); a plurality of turbochargers (14, 34) driven by exhaust gas from the plurality of exhaust gas generating sources (11, 31); a plurality of power generators (20, 40) connected to the plurality of turbochargers (14, 34); a plurality of converters (22, 42) for converting AC power generated by the plurality of power generators (20, 40) to DC power; one inverter for converting the DC power outputted from the plurality of converters (22, 42) to AC power; and a control device for controlling the plurality of exhaust gas generating sources (11, 31) or the plurality of turbochargers (14, 34) in accordance with the AC power from the inverter,
A pressure sensitive adhesive foam comprising a foam comprising a non-syntactic foam blend of styrenic block copolymer and acrylic copolymer wherein the pressure-sensitive adhesive foam has an elongation of greater than 600%, wherein the non-syntactic foam blend is a hot melt formed foam.
A wireless electrical power transmission system, comprising a transmitting coil frequency generating circuit and a coil frequency phase tracking and feedback circuit, wherein the transmitting coil frequency generating circuit includes a control circuit, a driving circuit and an inverter circuit, the control circuit is configured to be controlled by software to output two opposite control signals, each of which controls the opening and closing of a switching tube after passing through the driving circuit, to form high-frequency oscillation in the transmitting coil; characterized in that the coil frequency phase tracking and feedback circuit comprises: a voltage comparison circuit, configured to compare voltages V1 and V2 at both ends of the transmitting coil to obtain an oscillation frequency f in the transmitting coil; a phase comparator and a Voltage Controlled Oscillator, configured to process the oscillation frequency f of the transmitting coil to obtain a frequency f0; the phase comparator is further configured to do a comparison between the frequencies f and f0 to generate a phase difference signal Δφ; the control circuit receives the oscillation frequency f and the phase difference signal Δφ, and finely tunes and outputs a delay of outputting signals P1 and P2 using the phase difference signal Δφ. a voltage comparison circuit, configured to compare voltages V1 and V2 at both ends of the transmitting coil to obtain an oscillation frequency f in the transmitting coil; a phase comparator and a Voltage Controlled Oscillator, configured to process the oscillation frequency f of the transmitting coil to obtain a frequency f0; the phase comparator is further configured to do a comparison between the frequencies f and f0 to generate a phase difference signal Δφ; the control circuit receives the oscillation frequency f and the phase difference signal Δφ, and finely tunes and outputs a delay of outputting signals P1 and P2 using the phase difference signal Δφ.
Beam comprising at least one first part having a main body of a general straight U-shaped cross section provided with lateral flanges (140, 150) protruding outwards from the sides of the U, the main body further comprising a part bottom as well as two wings (120, 130) forming the sides of the U, - the central portion of the main body defining cells (114, 128, 138) acting respectively in tension and compression on both sides of a neutral axis of main flexure (A-A, A'-A'), two of said cells being formed by two transition zones (125, 126, 127; 135, 136, 137) which are each located between the U-shaped element and a lateral flange (140, 150); characterised in that - the part bottom of the main body comprises one or several stiffening ribs that are directed towards the inside of the U; - at least one wing (120, 130) comprises at least one transition (121, 131) in the shape of a double rounded bending that comprises a point of inflexion, or one transition (121, 131) that forms a straight segment which connects each of the ends of said at least one wing (120, 130) by forming an angle; - at least one lateral flange (140, 150) comprises at least one zone of lower mechanical strength than the rest of the main body, said at least one zone of lower mechanical strength being made on the same side of the U as the wing (120, 130) comprising said at least one transition (121, 131). - the central portion of the main body defining cells (114, 128, 138) acting respectively in tension and compression on both sides of a neutral axis of main flexure (A-A, A'-A'), two of said cells being formed by two transition zones (125, 126, 127; 135, 136, 137) which are each located between the U-shaped element and a lateral flange (140, 150); - the part bottom of the main body comprises one or several stiffening ribs that are directed towards the inside of the U; - at least one wing (120, 130) comprises at least one transition (121, 131) in the shape of a double rounded bending that comprises a point of inflexion, or one transition (121, 131) that forms a straight segment which connects each of the ends of said at least one wing (120, 130) by forming an angle; - at least one lateral flange (140, 150) comprises at least one zone of lower mechanical strength than the rest of the main body, said at least one zone of lower mechanical strength being made on the same side of the U as the wing (120, 130) comprising said at least one transition (121, 131).