mhurhangee/ep-ind-claims huggingface dataset:
An information transmission method, implemented in a Long Term Evolution, LTE, system or Long Term Evolution - Advanced, LTE-A, system, the method comprising: determining (S101, S201) a subframe for enhanced transmission of first information; repeatedly transmitting (S102, S202) the first information multiple times in the determined subframe for the enhanced transmission of the first information; and when a subframe for channel state information-reference signal, CSI-RS, transmission collides with the subframe for the enhanced transmission of the first information, the first information is not transmitted on a resource element occupied by the CSI-RS transmission in a subframe in which the enhanced transmission of the first information collides with the CSI-RS transmission, wherein the first information is a master information block, MIB, a quantity of times of repeatedly transmitting the MIB in the subframe is greater than one time; for a frequency division duplex, FDD, system, the subframe for enhanced transmission of the first information comprises: a subframe 9; or a subframe 4; or a subframe 4 and a subframe 9; or a subframe 0 and a subframe 9. determining (S101, S201) a subframe for enhanced transmission of first information; repeatedly transmitting (S102, S202) the first information multiple times in the determined subframe for the enhanced transmission of the first information; and when a subframe for channel state information-reference signal, CSI-RS, transmission collides with the subframe for the enhanced transmission of the first information, the first information is not transmitted on a resource element occupied by the CSI-RS transmission in a subframe in which the enhanced transmission of the first information collides with the CSI-RS transmission, wherein the first information is a master information block, MIB, a quantity of times of repeatedly transmitting the MIB in the subframe is greater than one time; for a frequency division duplex, FDD, system, the subframe for enhanced transmission of the first information comprises: a subframe 9; or a subframe 4; or a subframe 4 and a subframe 9; or a subframe 0 and a subframe 9. a subframe 9; or a subframe 4; or a subframe 4 and a subframe 9; or a subframe 0 and a subframe 9.
A method of communication, comprising: identifying at a network node a plurality of candidate target access points for a handoff operation for an access terminal, based on a report that the access terminal provided to a source access point and that the source access point forwarded to the network node, wherein the plurality of candidate target access points each transmit pilot signals having a defined characteristic that corresponds to a pilot signal detected at the access terminal; sending, by the network node, a message to each of the plurality of candidate target access points to request each candidate target access point to process an uplink signal from the access terminal; receiving at the network node at least one response to at least one of the messages; and identifying at the network node the one of the plurality of candidate target access points that transmitted the pilot signal detected at the access terminal for the handoff operation based on the at least one response. identifying at a network node a plurality of candidate target access points for a handoff operation for an access terminal, based on a report that the access terminal provided to a source access point and that the source access point forwarded to the network node, wherein the plurality of candidate target access points each transmit pilot signals having a defined characteristic that corresponds to a pilot signal detected at the access terminal; sending, by the network node, a message to each of the plurality of candidate target access points to request each candidate target access point to process an uplink signal from the access terminal; receiving at the network node at least one response to at least one of the messages; and identifying at the network node the one of the plurality of candidate target access points that transmitted the pilot signal detected at the access terminal for the handoff operation based on the at least one response.
A composition comprising a plurality of particles, wherein said particles comprise: 25% to 99% by weight a water soluble carrier, wherein the water soluble carrier is polyethylene glycol having a weight average molecular weight from 2000 to 20000 Da (g/mol); and 1% to 75% by weight a graft copolymer; wherein said graft copolymer comprises: (a) a polyalkylene oxide which has a number average molecular weight of from 1000 to 20000 Da (g/mol) and is based on ethylene oxide, propylene oxide, or butylene oxide; and (b) a vinyl ester derived from a saturated monocarboxylic acid containing from 1 to 6 carbon atoms; wherein (a) and (b) are present at a weight ratio of (a):(b) of from 1:0.1 to 1:2; and wherein each of said particles has a mass from 1 mg to 1 g. 25% to 99% by weight a water soluble carrier, wherein the water soluble carrier is polyethylene glycol having a weight average molecular weight from 2000 to 20000 Da (g/mol); and 1% to 75% by weight a graft copolymer; wherein said graft copolymer comprises: (a) a polyalkylene oxide which has a number average molecular weight of from 1000 to 20000 Da (g/mol) and is based on ethylene oxide, propylene oxide, or butylene oxide; and (b) a vinyl ester derived from a saturated monocarboxylic acid containing from 1 to 6 carbon atoms; (a) a polyalkylene oxide which has a number average molecular weight of from 1000 to 20000 Da (g/mol) and is based on ethylene oxide, propylene oxide, or butylene oxide; and (b) a vinyl ester derived from a saturated monocarboxylic acid containing from 1 to 6 carbon atoms; wherein (a) and (b) are present at a weight ratio of (a):(b) of from 1:0.1 to 1:2; and wherein each of said particles has a mass from 1 mg to 1 g.
A gas turbine engine comprising: a turbine section (28; 100) having a turbine rotor and at least one blade extending outwardly of said turbine rotor, said turbine rotor rotating about an axis of rotation; an axial seal (122; 128; 222), wherein said axial seal (122; 128; 222) is a bristle seal (122; 128; 222); and a blade outer air seal positioned radially outward of said at leat one blade, said blade outer air seal having an axially forward hook and an axially aft hook supported to a static structure, wherein the axial seal (122, 128; 222) is attached to said static structure forward of said forward hook, and has a sealing portion extending in an aft direction, characterised in that: the engine further comprises a sealing surface member (130; 230), wherein the sealing surface member (130; 230) is positioned intermediate an aft end of said axial seal (122, 128; 222) and a forward end of said forward hook to provide a sealing surface for sealing between said axial seal (122, 128; 222) and said blade outer air seal; said blade outer air seal is formed of ceramic matrix composite materials; and said axial bristle seal (122, 128; 222) has bristles with an aft end in contact with said sealing surface member (130; 230). a turbine section (28; 100) having a turbine rotor and at least one blade extending outwardly of said turbine rotor, said turbine rotor rotating about an axis of rotation; an axial seal (122; 128; 222), wherein said axial seal (122; 128; 222) is a bristle seal (122; 128; 222); and a blade outer air seal positioned radially outward of said at leat one blade, said blade outer air seal having an axially forward hook and an axially aft hook supported to a static structure, wherein the axial seal (122, 128; 222) is attached to said static structure forward of said forward hook, and has a sealing portion extending in an aft direction, the engine further comprises a sealing surface member (130; 230), wherein the sealing surface member (130; 230) is positioned intermediate an aft end of said axial seal (122, 128; 222) and a forward end of said forward hook to provide a sealing surface for sealing between said axial seal (122, 128; 222) and said blade outer air seal; said blade outer air seal is formed of ceramic matrix composite materials; and said axial bristle seal (122, 128; 222) has bristles with an aft end in contact with said sealing surface member (130; 230).
Use of a rubber blend composition for treads of tires or transmission systems, wherein the rubber blend composition contains trans-polynorbornenes in conjunction with process oils, characterised in that the rubber blend composition contains paraffinic oil as process oil having a glass transition of <-20°C, preferably <-70°C.
A system for damping undesired oscillations in a movably arranged crane structure being hydraulically driven by means of an arrangement comprising at least one hydraulic actuator (10, 10', 60) mechanically connected to an engagement structure attached to the crane structure, wherein the at least one hydraulic actuator (10, 10', 60) is in fluid communication with a hydraulic unit through one or more conduits (14, 14', 64, 66), wherein said hydraulic unit is connected to a hydraulic pressure source, wherein the hydraulic unit comprises a valve configured to direct hydraulic oil from the hydraulic pressure source, to the at least one hydraulic actuator (10, 10', 60), characterised in that the system comprises a damping member comprising an additional hydraulic unit hydraulically connected to the hydraulic pressure source and to the at least one hydraulic actuator (10, 10', 60), where the additional hydraulic unit is connected to the hydraulic pressure source via a conduit (38, 74) arranged in such a manner that the additional hydraulic oil flow can be delivered to the additional hydraulic unit by the hydraulic pressure source without flowing through the hydraulic unit, whereby the additional hydraulic unit is configured to deliver an additional hydraulic oil flow and hereby damp the motion of the at least one hydraulic actuator (10, 10', 60).
Motor vehicle, preferably utility vehicle: having - a securing device of a spare wheel of the motor vehicle, wherein the spare wheel is able to be removed from the securing device via an outlet opening, and - a retention device which is arranged on the motor vehicle, preferably on the motor vehicle front end, having: - a carrier portion, mounted on the motor vehicle, and - a retention portion on which a functional element is retained, wherein the retention portion is able to be pivoted about a pivot axis from a first state, in which it at least partially closes the outlet opening, into a second state, in which it opens the outlet opening in such a manner that the spare wheel can be removed, and wherein the retention portion is pivotably mounted on the carrier portion, characterized in that the functional element is a sensor device. - a securing device of a spare wheel of the motor vehicle, wherein the spare wheel is able to be removed from the securing device via an outlet opening, and - a retention device which is arranged on the motor vehicle, preferably on the motor vehicle front end, having: - a carrier portion, mounted on the motor vehicle, and - a retention portion on which a functional element is retained, wherein the retention portion is able to be pivoted about a pivot axis from a first state, in which it at least partially closes the outlet opening, into a second state, in which it opens the outlet opening in such a manner that the spare wheel can be removed, and wherein the retention portion is pivotably mounted on the carrier portion, characterized in that the functional element is a sensor device. - a carrier portion, mounted on the motor vehicle, and - a retention portion on which a functional element is retained, wherein the retention portion is able to be pivoted about a pivot axis from a first state, in which it at least partially closes the outlet opening, into a second state, in which it opens the outlet opening in such a manner that the spare wheel can be removed, and wherein the retention portion is pivotably mounted on the carrier portion, characterized in that the functional element is a sensor device.
An environmental control system, comprising environmental air compressors (EACs) (101, 102), a first regenerative heat exchanger, a primary heat exchanger, a condenser, a water extractor and a reheater, wherein the environmental air compressors (EACs) (101, 102) operate in parallel and receive an outside air (103, 104), wherein each EAC (101, 102) includes a respective EAC compressor (101a, 102a) and EAC turbine (101c, 102c) and an EAC motor (101b,102b) therebetween; wherein the first regenerative heat exchanger is downstream of the EAC compressors (101a, 102a) and upstream of the EAC turbines (101c, 102c), the environmental control system being characterized in comprising an air cycle machine, a secondary heat exchanger downstream of the ACM, wherein the secondary heat exchanger receives the outside air; and an actuated door (125, 126) that controls an amount of the outside air to the primary heat exchanger and to the secondary heat exchanger, wherein the primary heat exchanger is downstream of the secondary heat exchanger; and the environmental control system being further characterized in that in use the first regenerative heat exchanger receives an environmental air from an enclosure for occupants; the primary heat exchanger is downstream of the first regenerative heat exchanger, wherein in use the primary heat exchanger receives the outside air (103, 104); the air cycle machine is downstream of the primary heat exchanger; the condenser is downstream of the ACM, wherein in use conditioned air exits the condenser and into the enclosure; the water extractor is downstream of the condenser; the reheater is downstream of the water extractor and upstream of the ACM.
A method of operating an electronic device to launch an application, comprising: detecting a notification alert of a message that can be accessed by the application, loading the application in the background upon detecting the notification alert, if the application has not been loaded; and when motion of the electronic device is detected within a predetermined period of time after the notification alert, bringing the application to the foreground. detecting a notification alert of a message that can be accessed by the application, loading the application in the background upon detecting the notification alert, if the application has not been loaded; and when motion of the electronic device is detected within a predetermined period of time after the notification alert, bringing the application to the foreground.
A method for operating a hybrid-electric propulsion system of an aircraft, the hybrid-electric propulsion system comprising a gas turbine engine having a high pressure system, a low pressure system, an electric machine coupled to at least the low pressure system, and an energy storage unit, the method comprising: operating the electric machine as an electric generator to charge the energy storage unit during a flight operation of the aircraft; switching the gas turbine engine to an electric operating mode during or after a landing operation of the aircraft; driving a system of the gas turbine engine with the electric machine using power from the energy storage unit while in the electric operating mode to provide or assist with providing ground operations the aircraft; wherein driving the system of the gas turbine engine comprises driving the low pressure system, the high pressure system, or both, wherein the ground operations include driving the low pressure system of the aircraft with the electric machine to mitigate engine soak-back, and wherein the method further comprises: parking the aircraft, wherein driving the low pressure system of the aircraft with the electric machine to mitigate engine soak-back comprises driving the low pressure system of the aircraft with the electric machine to mitigate engine soak-back after parking the aircraft. operating the electric machine as an electric generator to charge the energy storage unit during a flight operation of the aircraft; switching the gas turbine engine to an electric operating mode during or after a landing operation of the aircraft; driving a system of the gas turbine engine with the electric machine using power from the energy storage unit while in the electric operating mode to provide or assist with providing ground operations the aircraft; wherein driving the system of the gas turbine engine comprises driving the low pressure system, the high pressure system, or both, wherein the ground operations include driving the low pressure system of the aircraft with the electric machine to mitigate engine soak-back, and wherein the method further comprises: parking the aircraft, wherein driving the low pressure system of the aircraft with the electric machine to mitigate engine soak-back comprises driving the low pressure system of the aircraft with the electric machine to mitigate engine soak-back after parking the aircraft.
A chair, comprising: a seat frame having a front edge, a rear edge, a first lateral edge, a second lateral edge, a bottom side, and a top side; a seat base disposed on the top side of the seat frame that is pivotally coupled to the front edge of the seat frame, the seat base being moveable with respect to the seat frame between a depressed position and an extended position; a first arm support having a proximate end that is coupled to the first lateral edge of the seat frame and a distal end that extends from the top side of the seat frame; a first arm having a front end and a rear end, the first arm being pivotally coupled to the first arm support about a point located between the front end and the rear end of the first arm; and a component coupling the first arm to the seat base in a manner that permits movement of the first arm to translate into movement of the seat base; a base having a top side and a bottom side, the base being disposed on a bottom side of the seat frame; and a swivel mounted to the top side of the base and coupled to the seat frame. a seat frame having a front edge, a rear edge, a first lateral edge, a second lateral edge, a bottom side, and a top side; a seat base disposed on the top side of the seat frame that is pivotally coupled to the front edge of the seat frame, the seat base being moveable with respect to the seat frame between a depressed position and an extended position; a first arm support having a proximate end that is coupled to the first lateral edge of the seat frame and a distal end that extends from the top side of the seat frame; a first arm having a front end and a rear end, the first arm being pivotally coupled to the first arm support about a point located between the front end and the rear end of the first arm; and a component coupling the first arm to the seat base in a manner that permits movement of the first arm to translate into movement of the seat base; a base having a top side and a bottom side, the base being disposed on a bottom side of the seat frame; and a swivel mounted to the top side of the base and coupled to the seat frame.
A method for performing low-density parity-check (LDPC) decoding, the method comprising: receiving log-likelihood ratios (LLRs) corresponding to bits encoded using LDPC encoding; updating the LLRs for each of the encoded bits corresponding to columns of a parity check matrix, the bit LLRs indicating a probability of a value of each of the encoded bits; determining, for each of the encoded bits, an a posteriori LLR for a row of the PCM by processing each LLR within the row, wherein for a first set of the encoded bits, determining the a posteriori LLR comprises using a first number of outdated LLRs, and wherein for a second set of the encoded bits, determining the a posteriori LLR comprises using a second number of updated LLRs, wherein the first set of the encoded bits and the second set of the encoded bits comprise all of the encoded bits; utilizing the LLRs to decode the encoded bits. receiving log-likelihood ratios (LLRs) corresponding to bits encoded using LDPC encoding; updating the LLRs for each of the encoded bits corresponding to columns of a parity check matrix, the bit LLRs indicating a probability of a value of each of the encoded bits; determining, for each of the encoded bits, an a posteriori LLR for a row of the PCM by processing each LLR within the row, wherein for a first set of the encoded bits, determining the a posteriori LLR comprises using a first number of outdated LLRs, and wherein for a second set of the encoded bits, determining the a posteriori LLR comprises using a second number of updated LLRs, wherein the first set of the encoded bits and the second set of the encoded bits comprise all of the encoded bits; utilizing the LLRs to decode the encoded bits.
Rotatable propulsion unit for propulsion and maneuvering of a maritime vessel, which includes a nozzle wherein is arranged a propeller section (13, 13a), which propeller section being electrically or hydraulically driven, which propulsion unit includes a fastening device arranged for arrangement to a steering device arranged for steering and/or moving the propulsion unit, which propeller section is rotatably arranged about a hub being arranged to the nozzle by means of stays (15, 16), characterized in that the nozzle exhibits a curved following edge at outlet of the nozzle, which results in that length of the nozzle is longer at upper part of the nozzle and shortest at outermost points of a horizontal central axis through the nozzle, when the nozzle is seen from behind.
An injection molding method for molding a resin-made interior panel into a thin-plate shape by using an injection molding die, wherein the injection molding die includes a pair of dies, the pair of dies comprising: a cavity die for forming a front surface side of the panel and a core die for forming a back surface side of the panel, one of which is a fixed die having a molten resin supply channel structure integrated therein and the other one of which is a movable die opposing thereto; wherein portions which correspond to undercut portions with respect to the die-cutting direction of the molding die in the original shape of the panel include on the back surface side of the panel a flat bottom portion having a shape which cancels an entire undercut space on the side of the core die; wherein a portion of the cavity-die corresponds to a rib structure portion on the front surface side of the panel, said rib structure portion having the flat bottom portion and a plurality of ribs projecting in the shape of plugging back the undercut space on the side of the core die and having a plurality of grooves extending from the bottom portion in the die-cut direction; and wherein the injection molding method comprises: injecting and filling molten resin in a state in which the distance between the cavity die and the core die each having a configuration required for molding the interior panel is slightly increased, bringing the core die toward the cavity die, filling the molten resin entirely in the interior of the cavity, and covering at least the rib structure portion with a surface material layer. injecting and filling molten resin in a state in which the distance between the cavity die and the core die each having a configuration required for molding the interior panel is slightly increased, bringing the core die toward the cavity die, filling the molten resin entirely in the interior of the cavity, and covering at least the rib structure portion with a surface material layer.