mhurhangee/ep-ind-claims huggingface dataset:
A rotorcraft, comprising: a body; a power train coupled to the body and comprising an engine and a drive shaft coupled to the engine; a main rotor system coupled to the power train, the main rotor system comprising at least one main rotor blade; a pilot input device disposed within the body and comprising an engine throttle adjustable among a neutral position, an increase position, and a decrease position, the engine throttle configured to transmit a first signal in response to a pilot selection of the increase position and transmit a second signal in response to a pilot selection of the decrease position a curved control stick and a transmission wire disposed within the curved control stick and configured to electronically communicate signals from the engine throttle to an engine control unit; and the engine control unit; wherein the engine control unit is in communication with the engine throttle and operable to: instruct the engine to increase power output in response to receipt of the first signal via the transmission wire; and instruct the engine to decrease power output in response to receipt of the second signal via the transmission wire. a body; a power train coupled to the body and comprising an engine and a drive shaft coupled to the engine; a main rotor system coupled to the power train, the main rotor system comprising at least one main rotor blade; a pilot input device disposed within the body and comprising an engine throttle adjustable among a neutral position, an increase position, and a decrease position, the engine throttle configured to transmit a first signal in response to a pilot selection of the increase position and transmit a second signal in response to a pilot selection of the decrease position a curved control stick and a transmission wire disposed within the curved control stick and configured to electronically communicate signals from the engine throttle to an engine control unit; and the engine control unit; wherein the engine control unit is in communication with the engine throttle and operable to: instruct the engine to increase power output in response to receipt of the first signal via the transmission wire; and instruct the engine to decrease power output in response to receipt of the second signal via the transmission wire. instruct the engine to increase power output in response to receipt of the first signal via the transmission wire; and instruct the engine to decrease power output in response to receipt of the second signal via the transmission wire.
A process for the preparation of 2-(2-amino propan-2-yl)-N-(4-fluorobenzyl)-5-hydroxy-1-methyl-6-oxo-1,6-dihydro pyrimidine-4-carboxamide of formula III, comprising: a. debenzylation of benzyl(2-{4-[(4-fluorobenzyl)carbamoyl]-5-hydroxy-1-methyl-6-oxo-1,6-dihydropyrimidin-2-yl}propan-2-yl)carbamate (Formula IV) in the presence of an acid; and b. isolating 2-(2-amino propan-2-yl)-N-(4-fluorobenzyl)-5-hydroxy-1-methyl-6-oxo-1,6-dihydro pyrimidine-4-carboxamide (Formula III). wherein the acid is hydrobromic acid; and wherein debenzylation of compound of Formula IV is carried out at a temperature between 40 °C and 100 °C. a. debenzylation of benzyl(2-{4-[(4-fluorobenzyl)carbamoyl]-5-hydroxy-1-methyl-6-oxo-1,6-dihydropyrimidin-2-yl}propan-2-yl)carbamate (Formula IV) in the presence of an acid; and b. isolating 2-(2-amino propan-2-yl)-N-(4-fluorobenzyl)-5-hydroxy-1-methyl-6-oxo-1,6-dihydro pyrimidine-4-carboxamide (Formula III). wherein the acid is hydrobromic acid; and wherein debenzylation of compound of Formula IV is carried out at a temperature between 40 °C and 100 °C.
An information processing system comprising: circuitry configured to: acquire image data corresponding to a target object that is a target for gesture recognition captured by an imaging device; calculate, based on the acquired image data, motion information corresponding to motion of the target object, wherein the motion information comprises a motion vector; determine a motion direction based on the motion vector; calculate an area of a region in the image corresponding to the motion direction; determine, based on the calculated area, whether a distance between the target object and the imaging device is inadequate for recognition of a gesture made by the target object, wherein the distance between the target object and the imaging device is considered inadequate if the calculated area exceeds a predefined threshold; output a notification when the determining determines that the distance between the target object and the imaging device is inadequate for recognition of a gesture made by the target object; and control a display to display the acquired image data and, as the notification, a graphic notification corresponding to a trajectory of the motion of the target image based on the motion information. acquire image data corresponding to a target object that is a target for gesture recognition captured by an imaging device; calculate, based on the acquired image data, motion information corresponding to motion of the target object, wherein the motion information comprises a motion vector; determine a motion direction based on the motion vector; calculate an area of a region in the image corresponding to the motion direction; determine, based on the calculated area, whether a distance between the target object and the imaging device is inadequate for recognition of a gesture made by the target object, wherein the distance between the target object and the imaging device is considered inadequate if the calculated area exceeds a predefined threshold; output a notification when the determining determines that the distance between the target object and the imaging device is inadequate for recognition of a gesture made by the target object; and control a display to display the acquired image data and, as the notification, a graphic notification corresponding to a trajectory of the motion of the target image based on the motion information.
A control channel allocation method for a flying device, the method comprising: allocating a received task to a corresponding flying device; determining, according to flight information in the task, a flight time of the flying device flying from a departure station to an arrival station; and allocating, according to logistics information and the flight time, a target control channel meeting a preset control condition to the flying device, characterized in that the allocating, according to logistics information and the flight time, a target control channel meeting a preset control condition to the flying device comprises: searching for one or more control channels at the departure station and the arrival station that are idle during the flight time as one or more candidate channels; and selecting, from the one or more candidate channels, a channel having the longest distance from all channels in use as a target channel for controlling the flying device at the departure station and the arrival station, the channels in use comprising control channels at least having a corresponding non-idle state at the departure station or the arrival station during the flight time. allocating a received task to a corresponding flying device; determining, according to flight information in the task, a flight time of the flying device flying from a departure station to an arrival station; and allocating, according to logistics information and the flight time, a target control channel meeting a preset control condition to the flying device, characterized in that the allocating, according to logistics information and the flight time, a target control channel meeting a preset control condition to the flying device comprises: searching for one or more control channels at the departure station and the arrival station that are idle during the flight time as one or more candidate channels; and selecting, from the one or more candidate channels, a channel having the longest distance from all channels in use as a target channel for controlling the flying device at the departure station and the arrival station, the channels in use comprising control channels at least having a corresponding non-idle state at the departure station or the arrival station during the flight time.
A method for handling data for use in wireless devices, the method comprising: predicting whether said wireless device is engaged in a personal, business or leisure activity when generating or maintaining said data, based upon behavioral pattern recognition of behavioral biometric data acquired by a biometric sensor; generating context data tags based on user preference information and said predicted activity; and tagging said data, generated or maintained in said wireless mobile communication device, with said context data tags. predicting whether said wireless device is engaged in a personal, business or leisure activity when generating or maintaining said data, based upon behavioral pattern recognition of behavioral biometric data acquired by a biometric sensor; generating context data tags based on user preference information and said predicted activity; and tagging said data, generated or maintained in said wireless mobile communication device, with said context data tags.
Method of obtaining helium from a helium-containing feed gas, comprising the following steps: feeding the helium-containing feed gas to a prepurifying unit, with removal of undesirable components from the helium-containing feed gas in a pressure swing adsorption process with the aid of the prepurifying unit, in order to obtain a prepurified feed gas; feeding the prepurified feed gas to a membrane unit which is connected downstream of the prepurifying unit and has at least one membrane (8, 15) which is more readily permeable to helium than to at least one further component present in the prepurified feed gas; feeding a pressurized low-helium retentate stream from the membrane unit that has not passed through the at least one membrane (8, 15) to the prepurifying unit; and displacing helium-rich gas with the aid of the pressurized low-helium retentate stream from an adsorber (E2B, E3B) to be regenerated in the prepurifying unit into an already regenerated adsorber (R2, R3) of the prepurifying unit. feeding the helium-containing feed gas to a prepurifying unit, with removal of undesirable components from the helium-containing feed gas in a pressure swing adsorption process with the aid of the prepurifying unit, in order to obtain a prepurified feed gas; feeding the prepurified feed gas to a membrane unit which is connected downstream of the prepurifying unit and has at least one membrane (8, 15) which is more readily permeable to helium than to at least one further component present in the prepurified feed gas; feeding a pressurized low-helium retentate stream from the membrane unit that has not passed through the at least one membrane (8, 15) to the prepurifying unit; and displacing helium-rich gas with the aid of the pressurized low-helium retentate stream from an adsorber (E2B, E3B) to be regenerated in the prepurifying unit into an already regenerated adsorber (R2, R3) of the prepurifying unit.
An apparatus, comprising: a processing module (222, 224, 322, 422), disposed within a first switch fabric element (202, 204, 302, 402), configured to detect a second switch fabric element (202, 204, 302, 402) having a routing module (222, 224, 322, 422) when the second switch fabric element is operatively coupled to the first switch fabric element, the processing module configured to define, at the first switch fabric element a virtual processing module (242, 244, 246, 252, 254, 256, 342, 344, 346) configured to be operatively coupled to the second switch fabric element; the virtual processing module configured to receive a request from the second switch fabric element for forwarding information, the virtual processing module configured to send the forwarding information to the routing module; and the processing module configured to select the virtual processing module as a master virtual processor of the first switch fabric element based on at least one of: a number of master virtual processors currently being operated by the processing module; a historic reliability of the processing module; a historic reliability of the first switch fabric element; or an age of the first switch fabric element. a processing module (222, 224, 322, 422), disposed within a first switch fabric element (202, 204, 302, 402), configured to detect a second switch fabric element (202, 204, 302, 402) having a routing module (222, 224, 322, 422) when the second switch fabric element is operatively coupled to the first switch fabric element, the processing module configured to define, at the first switch fabric element a virtual processing module (242, 244, 246, 252, 254, 256, 342, 344, 346) configured to be operatively coupled to the second switch fabric element; the virtual processing module configured to receive a request from the second switch fabric element for forwarding information, the virtual processing module configured to send the forwarding information to the routing module; and the processing module configured to select the virtual processing module as a master virtual processor of the first switch fabric element based on at least one of: a number of master virtual processors currently being operated by the processing module; a historic reliability of the processing module; a historic reliability of the first switch fabric element; or an age of the first switch fabric element.
A production process of a gas turbine including a multistage compressor and a multistage turbine, each of them comprising a number of stages, the process comprising the steps of: designing in advance the compressor and the turbine so as to provide an optimal pressure ratio and an optimal expansion ratio for the simple gas turbine cycle, respectively, wherein the compressor and the turbine can be applied to various cycles by reducing the numbers of their active stages; reducing (S105, S106, S110) the number of active stages of the compressor to a particular number of active stages suitable for a desired cycle; inserting a disk-shaped member in each disk-mount position of the inactive stages, the disk-shaped member having a blade mount groove on it and a dummy key fitted in that groove, such that the outer peripheries of the disk-shaped member and the dummy key form a part of an inner peripheral wall of an annular flow passage of the compressor; and constructing the gas turbine by combining the compressor and the turbine with each other. designing in advance the compressor and the turbine so as to provide an optimal pressure ratio and an optimal expansion ratio for the simple gas turbine cycle, respectively, wherein the compressor and the turbine can be applied to various cycles by reducing the numbers of their active stages; reducing (S105, S106, S110) the number of active stages of the compressor to a particular number of active stages suitable for a desired cycle; inserting a disk-shaped member in each disk-mount position of the inactive stages, the disk-shaped member having a blade mount groove on it and a dummy key fitted in that groove, such that the outer peripheries of the disk-shaped member and the dummy key form a part of an inner peripheral wall of an annular flow passage of the compressor; and constructing the gas turbine by combining the compressor and the turbine with each other.
A method for detecting blood in a dialysate circuit of a dialysis system, comprising: substantially filling a first portion of a chamber with used dialysate, the chamber having a movable membrane that fluidly separates the first portion of the chamber from a second portion of the chamber; transmitting light through the first portion of the chamber while the first portion is substantially filled with used dialysate; detecting a first light level for light transmitted through the first portion of the chamber; substantially filling the second portion of the chamber with clean dialysate; transmitting light through the second portion while the second portion is substantially filled with clean dialysate; detecting a second light level for light transmitted through the second portion of the chamber; and determining a presence of blood in the first portion based on a comparison of the detected first and second light levels. substantially filling a first portion of a chamber with used dialysate, the chamber having a movable membrane that fluidly separates the first portion of the chamber from a second portion of the chamber; transmitting light through the first portion of the chamber while the first portion is substantially filled with used dialysate; detecting a first light level for light transmitted through the first portion of the chamber; substantially filling the second portion of the chamber with clean dialysate; transmitting light through the second portion while the second portion is substantially filled with clean dialysate; detecting a second light level for light transmitted through the second portion of the chamber; and determining a presence of blood in the first portion based on a comparison of the detected first and second light levels.
A vehicle voice control system comprising: a voice actuation unit including at least one microphone (16, 16', 16", 16′′′, 34) that listens for a voiced command and on receipt of the voiced command the voice actuation unit generates an activation signal; a key fob transponder that receives the activation signal and outputs an identification code and a key fob activation signal; and a receiver-processor that receives the identification code and the key fob activation signal and verifies the identification code is an authorizing code and when the identification code is an authorizing code, the receiver-processor sends an actuator activation signal to a mechanical system of the vehicle. a voice actuation unit including at least one microphone (16, 16', 16", 16′′′, 34) that listens for a voiced command and on receipt of the voiced command the voice actuation unit generates an activation signal; a key fob transponder that receives the activation signal and outputs an identification code and a key fob activation signal; and a receiver-processor that receives the identification code and the key fob activation signal and verifies the identification code is an authorizing code and when the identification code is an authorizing code, the receiver-processor sends an actuator activation signal to a mechanical system of the vehicle.
A method for coating a turbine engine component, said method comprising the steps of: placing said component into a chamber; injecting a non-reactive carrier gas containing a coating material into said chamber; and forming a coating on a desired portion (61; 62) of said component by locally heating said desired portion of said component by redirecting a directed energy beam onto said desired portion of said component; wherein the method further comprises maintaining said non-reactive carrier gas containing said coating material at a temperature lower than the deposition temperature of said coating material; wherein said component placing step comprises placing a turbine vane pack having a plurality of airfoils in said chamber; wherein said coating forming step comprises forming a coating on hidden portions (61, 62) of said airfoils; wherein said redirecting step comprises articulating a redirecting surface mounted within the chamber so that the directed energy beam is directed onto said desired portion of said component; wherein said chamber has a transparent layer through which said energy beam is directed to the redirecting surface; and wherein said redirecting surface is mounted within the chamber to a wall of said chamber. placing said component into a chamber; injecting a non-reactive carrier gas containing a coating material into said chamber; and forming a coating on a desired portion (61; 62) of said component by locally heating said desired portion of said component by redirecting a directed energy beam onto said desired portion of said component; wherein the method further comprises maintaining said non-reactive carrier gas containing said coating material at a temperature lower than the deposition temperature of said coating material; wherein said component placing step comprises placing a turbine vane pack having a plurality of airfoils in said chamber; wherein said coating forming step comprises forming a coating on hidden portions (61, 62) of said airfoils; wherein said redirecting step comprises articulating a redirecting surface mounted within the chamber so that the directed energy beam is directed onto said desired portion of said component; wherein said chamber has a transparent layer through which said energy beam is directed to the redirecting surface; and wherein said redirecting surface is mounted within the chamber to a wall of said chamber.
A battery comprising: a first electrical contact; at least one cell structure comprising a cathode, an anode and an electrolyte; a bonding layer coupled with said first electrical contact and comprising an embedded conductor, wherein said embedded conductor contacts said cell structure and wherein said embedded conductor contacts said first electrical contact; and a second electrical contact; wherein said bonding layer and said at least one cell structure are sandwiched between said first electrical contact and said second electrical contact; and wherein said bonding layer comprises a plurality of layers (1110A, 1110B, 1110D-1110I) in which the cell structure is within one of the plurality of layers (1110A, 1110B, 1110D-1110I). a first electrical contact; at least one cell structure comprising a cathode, an anode and an electrolyte; a bonding layer coupled with said first electrical contact and comprising an embedded conductor, wherein said embedded conductor contacts said cell structure and wherein said embedded conductor contacts said first electrical contact; and a second electrical contact; wherein said bonding layer and said at least one cell structure are sandwiched between said first electrical contact and said second electrical contact; and wherein said bonding layer comprises a plurality of layers (1110A, 1110B, 1110D-1110I) in which the cell structure is within one of the plurality of layers (1110A, 1110B, 1110D-1110I).