mhurhangee/ep-ind-claims huggingface dataset:
An extract of Citrus depressa for use in the prevention or treatment of (i) muscle atrophy or (ii) reduction of muscle force resulting from muscle atrophy, wherein the muscle atrophy is any one of the following 1) to 4): 1) muscle atrophy resulting from aging, being bedridden, sedentary lifestyle, or spaceflight; 2) muscle atrophy resulting from immobilization of limbs, or postoperative rest; 3) muscle atrophy resulting from side reactions of drugs such as steroids; and 4) muscle atrophy resulting from osteoarthritis, rheumatoid arthritis, diabetes, thermal burn, infectious disease accompanied by inflammation, sepsis accompanying infectious disease, inflammatory bowel disease, connective tissue disease, renal failure, hepatic failure, cardiac failure, cancer, malignant tumor, cachexia, anorexia or hypercatabolism in terminal symptoms of a disease. 1) muscle atrophy resulting from aging, being bedridden, sedentary lifestyle, or spaceflight; 2) muscle atrophy resulting from immobilization of limbs, or postoperative rest; 3) muscle atrophy resulting from side reactions of drugs such as steroids; and 4) muscle atrophy resulting from osteoarthritis, rheumatoid arthritis, diabetes, thermal burn, infectious disease accompanied by inflammation, sepsis accompanying infectious disease, inflammatory bowel disease, connective tissue disease, renal failure, hepatic failure, cardiac failure, cancer, malignant tumor, cachexia, anorexia or hypercatabolism in terminal symptoms of a disease.
A device with multiple encapsulated functional layers, comprising: a substrate; a first functional layer including a first functional component positioned above a top surface of the substrate; a first thin-film encapsulating layer encapsulating the first functional component; a second functional layer including a second functional component positioned upon the first thin-film encapsulating layer; and a second thin-film encapsulating layer encapsulating the second functional component, wherein the first thin-film encapsulation layer is a substrate upon which the second functional component is formed; wherein the second functional component is located above the first functional component. a substrate; a first functional layer including a first functional component positioned above a top surface of the substrate; a first thin-film encapsulating layer encapsulating the first functional component; a second functional layer including a second functional component positioned upon the first thin-film encapsulating layer; and a second thin-film encapsulating layer encapsulating the second functional component, wherein the first thin-film encapsulation layer is a substrate upon which the second functional component is formed; wherein the second functional component is located above the first functional component.
A pharmaceutical composition for use in reducing hepatotoxicity caused by acetaminophen (APAP) comprising: (a) a pharmaceutically effective dose of APAP or pro-drug analogs of the analgesic APAP, and (b) mannitol.
A composition comprising (a) carbohydrate; (b) lipid, comprising from 0.25% to 2.5% lecithin by weight of total lipid; (c) from 90% to 97% of intact protein by weight of total protein; and (d) from 3% to 10% of hydrolyzed whey protein by weight of total protein; wherein the hydrolyzed whey protein has a degree of hydrolysis of between 23% and 90%, and wherein the composition is a nutritional powder. (a) carbohydrate; (b) lipid, comprising from 0.25% to 2.5% lecithin by weight of total lipid; (c) from 90% to 97% of intact protein by weight of total protein; and (d) from 3% to 10% of hydrolyzed whey protein by weight of total protein;
Dedusting system for dedusting raw gas, with a system housing delimited by housing walls, which has a raw gas inlet opening and a clean gas outlet opening and is subdivided by a filter arrangement into a raw gas chamber and a clean gas chamber, wherein the dedusting system comprises a fan arrangement for generating a gas flow from the raw gas inlet opening to the clean gas outlet opening with a series connection of at least two free-blowing radial fans (2', 2"), each of which has at least one radial impeller (21', 21") with blades, each driven directly by an electric motor (22', 22"), and an end-side fan intake opening, wherein at least one upstream radial fan is arranged in a housing with a housing intake opening and a housing discharge opening (13"), wherein the upstream radial fan is arranged with its fan intake opening in the region of the housing intake opening and a downstream radial fan (2") is arranged with its fan intake opening in the region of the housing discharge opening (13"), wherein flow guide elements are arranged in the housing such that the air volume flow from the circumference of the radial impeller of the upstream radial fan is guided through the flow guide elements in at least two partial volume flows along tapering helical lines into the fan intake opening of the downstream radial fan (22").
A method performed by a wireless device, characterized in that the method comprises: receiving, from a base station, a message listing that includes a plurality of message pointers, wherein each message pointer indicates data available for reception and includes carrier information and time slot information associated with receiving each of the data; determining that a message pointer, of the plurality of message pointers, is associated with an identifier of the wireless device; and receiving, from the base station based on the determination, information using the carrier information and the time slot information. receiving, from a base station, a message listing that includes a plurality of message pointers, wherein each message pointer indicates data available for reception and includes carrier information and time slot information associated with receiving each of the data; determining that a message pointer, of the plurality of message pointers, is associated with an identifier of the wireless device; and receiving, from the base station based on the determination, information using the carrier information and the time slot information.
A high-pressure fuel pump actuator used in an engine, which is used in a fuel injection system of an engine, is mounted on between a driving cam and a fuel pump plunger, the pump actuator comprising: a guide sleeve, a U-shaped holder, and a pin shaft roller set, wherein the pin shaft roller set is mounted on the U-shaped holder, and wherein the U-shaped holder is mounted in the guide sleeve; wherein symmetrical positions on a left and a right side walls of the guide sleeve are provided with windows (1.4), wherein a left and a right side walls are provided with two flanges (1.1) respectively, wherein the U-shaped holder includes a bottom plate (2.1) and side plates (2.2) that are located on a left and a right side of the bottom plate (2.1), wherein upon assembly, the side plate (2.2) is locked between two flanges (1.1); characterized in that, an internal wall of the guide sleeve is provided with a ring groove (1.2) forming a recess, wherein a back side of the bottom plate (2.1) is provided with a tail portion (2.4) whose end surface is arc-shaped, wherein upon assembly, the tail portion (2.4) is locked in the ring groove (1.2).
A method for bonding gas turbine engine airfoil sections to form an airfoil, the method comprising: placing a stub airfoil section having stub airfoil pressure and suction sides (26, 27) between pressure and suction side stub electrodes (86, 88), placing an upper airfoil section having upper airfoil pressure and suction sides (24, 25) between pressure and suction side upper airfoil electrodes (90, 92), aligning the upper airfoil section with the stub airfoil section, the aligning including aligning upper and stub airfoil cross sections (28, 29) spaced at upper and stub airfoil distal ends (68, 69) of the upper and stub airfoil sections respectively (15, 16), the stub and upper airfoil cross sections (29, 28) being spaced apart from the stub and upper electrodes respectively, pressing together the upper and stub airfoil cross sections (28, 29), and solid state resistance welding the upper and stub airfoil sections (15, 16) together along the upper and stub airfoil cross sections (28, 29) by passing electrical current across the upper and stub airfoil cross sections while the upper and stub airfoil cross sections are being pressed together, the method including applying the electrical current to the electrodes during the solid state resistance welding. placing a stub airfoil section having stub airfoil pressure and suction sides (26, 27) between pressure and suction side stub electrodes (86, 88), placing an upper airfoil section having upper airfoil pressure and suction sides (24, 25) between pressure and suction side upper airfoil electrodes (90, 92), aligning the upper airfoil section with the stub airfoil section, the aligning including aligning upper and stub airfoil cross sections (28, 29) spaced at upper and stub airfoil distal ends (68, 69) of the upper and stub airfoil sections respectively (15, 16), the stub and upper airfoil cross sections (29, 28) being spaced apart from the stub and upper electrodes respectively, pressing together the upper and stub airfoil cross sections (28, 29), and solid state resistance welding the upper and stub airfoil sections (15, 16) together along the upper and stub airfoil cross sections (28, 29) by passing electrical current across the upper and stub airfoil cross sections while the upper and stub airfoil cross sections are being pressed together, the method including applying the electrical current to the electrodes during the solid state resistance welding.
A system for moving items on a rig floor, the system comprising a plurality of skids (30,31,32,33,34,35,37) and a network of rails for guiding the plurality of skids, each skid of said plurality of skids for supporting an item (47,112,125,130), and each skid having rail engagement members for engaging at least one rail of said network of rails wherein said network of rails further comprises at least one predetermined parking spot, characterised in that the system further comprises a master computer control system, wherein a parking sensor is provided to obtain parking location information to indicate that the skid is parked at said predetermined parking spot and relaying the parking location information to the master computer control system.
A liquid developer comprising a dispersion of toner particles comprising a polyester resin P having an acid value of 3 mgKOH/g or more and 80 mgKOH/g or less and a pigment in an insulating liquid in the presence of a dispersant, wherein the dispersant comprises a copolymer C obtained by polymerizing monomers comprising a monomer having a basic functional group and a monomer having a silicone chain, wherein the monomer having a silicone chain has a weight-average molecular weight of 1,000 or more and 10,000 or less, and the copolymer C has a weight-average molecular weight of 10,000 or more and 80,000 or less, and wherein a mass ratio of the monomer having a basic functional group to the monomer having a silicone chain is 3/97 or more and 50/50 or less.
Thread separation mechanism for a weft feeder device with a winding drum having an axial direction and a winding circumference for storing a weft thread, the thread separation mechanism comprises a separation element arranged at the winding circumference and extending in the axial direction of the winding drum, and a drive system for moving the separation element relative to the winding drum along a trajectory having radial and axial components for advancing windings of the weft thread in the axial direction along the winding drum, wherein the drive system comprises a first carrier element and a second carrier element, the first carrier element and the second carrier element are actuated to move to-and-fro in the axial direction with a phase shift between the to-and-fro movement of the first carrier element and the second carrier element, characterized in that the separation element is coupled to the first carrier element and the second carrier element via a linkage system in such manner that the relative movement between the first carrier element and the second carrier element in the axial direction causes a radial movement of the separation element and a conjoint movement of the first carrier element and the second carrier element in the axial direction causes an axial movement of the separation element.
An apparatus (20; 50; 60; 120) for detecting an edge of a material web, comprising: either an ultrasound sensor which comprises two or more separately readable ultrasound receiver elements (2; 2'; 2"...2 'n) and an ultrasound transmitter element (3; 3'; 3"), characterized in that two or more ultrasound receiver elements (2; 2'; 2"...2 'n) have a common ultrasound transducer element or an ultrasound sensor which comprises one or more separately readable ultrasound receiver elements (2; 2'; 2"...2 'n) and two or more separately actuatable ultrasound transmitter elements (3; 3'; 3"), characterized in that two or more ultrasound transmitter elements (3; 3'; 3") have a common ultrasound transducer element. either an ultrasound sensor which comprises two or more separately readable ultrasound receiver elements (2; 2'; 2"...2 'n) and an ultrasound transmitter element (3; 3'; 3"), characterized in that two or more ultrasound receiver elements (2; 2'; 2"...2 'n) have a common ultrasound transducer element or an ultrasound sensor which comprises one or more separately readable ultrasound receiver elements (2; 2'; 2"...2 'n) and two or more separately actuatable ultrasound transmitter elements (3; 3'; 3"), characterized in that two or more ultrasound transmitter elements (3; 3'; 3") have a common ultrasound transducer element.
Paramotor with dynamic torque compensation comprising: a frame, a harness or seat, a power unit, a propeller which rotates and a cage, wherein said propeller is protected by said cage, wherein said propeller is an unducted propeller, characterised by one or more surfaces on said cage positioned such that when air flows over them a compensating torque is generated in an opposite direction to that of the propeller torque, said cage basically consisting of a main ring and arms, said surfaces being integrated into the arms of said paramotor cage, wherein the arms of said cage are formed from asymmetric profile with non-zero angle of attack or from symmetric profile with non-zero angle of attack. a frame, a harness or seat, a power unit, a propeller which rotates and a cage, wherein said propeller is protected by said cage, wherein said propeller is an unducted propeller, characterised by one or more surfaces on said cage positioned such that when air flows over them a compensating torque is generated in an opposite direction to that of the propeller torque, said cage basically consisting of a main ring and arms, said surfaces being integrated into the arms of said paramotor cage, wherein the arms of said cage are formed from asymmetric profile with non-zero angle of attack or from symmetric profile with non-zero angle of attack.
An articulating medical instrument comprising of: a substantially straight proximal segment (130, 510); a substantially straight distal segment (140, 530) connected to the proximal segment; an articulation mechanism for changing an articulation angle between the proximal and distal segments and providing a straight configuration in which the proximal and distal segments form a substantially straight line and at least one articulated configuration in which the proximal and distal segments form an articulation angle of less than 180 degrees between the segments, the articulation mechanism being configured for increasing or decreasing the articulation angle; and one or more drive mechanisms (150, 220, 320, 420, 520, 580) configured for transferring rotary movement from the proximal segment to the distal segment, characterized in that said at least one drive mechanism (150, 220, 320, 420, 520, 580) for transferring rotary movement is contained within the segments in the straight configuration, wherein at least a portion of said at least one drive mechanism for transferring rotary movement is external to at least a portion of at least one segment adjacent to the connection between the segments in the articulated configuration. a substantially straight proximal segment (130, 510); a substantially straight distal segment (140, 530) connected to the proximal segment; an articulation mechanism for changing an articulation angle between the proximal and distal segments and providing a straight configuration in which the proximal and distal segments form a substantially straight line and at least one articulated configuration in which the proximal and distal segments form an articulation angle of less than 180 degrees between the segments, the articulation mechanism being configured for increasing or decreasing the articulation angle; and one or more drive mechanisms (150, 220, 320, 420, 520, 580) configured for transferring rotary movement from the proximal segment to the distal segment, characterized in that said at least one drive mechanism (150, 220, 320, 420, 520, 580) for transferring rotary movement is contained within the segments in the straight configuration, wherein at least a portion of said at least one drive mechanism for transferring rotary movement is external to at least a portion of at least one segment adjacent to the connection between the segments in the articulated configuration.
A vehicle intended to mainly move in a longitudinal direction, the vehicle comprising: • a chassis; • two independent swing arms (22, 24), each of the swing arms (22, 24) being rotationally movable relative to the chassis about a transverse axis perpendicular to the longitudinal direction, each of the swing arms (22, 24) supporting a wheel (18, 20) of the vehicle, • two independent rockers (32, 34), each being rotationally movable relative to the chassis about an axis (38, 40), the axes of rotation (38, 40) of the two rockers (32, 34) being distinct from each other and parallel to each other, • a first link element (36; 102) disposed between the two rockers (32, 34), • two second link elements (52, 54) each linking one of the rockers (32, 34) to one of the swing arms (22, 24), characterised in that each rocker (32, 34) comprises: • two first parallel plates (70, 72; 74, 76) extending between the rotational link relative to the chassis and a link with the first link element • two second parallel plates (78, 80; 82; 84) fixed to the first plates (70, 72; 74, 76) and allowing to space apart the link (46; 48) to the first link element and the link (56, 58) to the second link element (52, 54). • a chassis; • two independent swing arms (22, 24), each of the swing arms (22, 24) being rotationally movable relative to the chassis about a transverse axis perpendicular to the longitudinal direction, each of the swing arms (22, 24) supporting a wheel (18, 20) of the vehicle, • two independent rockers (32, 34), each being rotationally movable relative to the chassis about an axis (38, 40), the axes of rotation (38, 40) of the two rockers (32, 34) being distinct from each other and parallel to each other, • a first link element (36; 102) disposed between the two rockers (32, 34), • two second link elements (52, 54) each linking one of the rockers (32, 34) to one of the swing arms (22, 24), • two first parallel plates (70, 72; 74, 76) extending between the rotational link relative to the chassis and a link with the first link element • two second parallel plates (78, 80; 82; 84) fixed to the first plates (70, 72; 74, 76) and allowing to space apart the link (46; 48) to the first link element and the link (56, 58) to the second link element (52, 54).
A hollow securing element having: - a locking end arranged to be temporarily arrested into a locking device in dependence on a locking mechanism of the locking device; - a filling end arranged for at least temporarily supporting the securing element in the locking device; and - a hollow space arranged between the locking end and the filling end, in which a pressurised fluid is included as a protective agent, - wherein the hollow space is lockable at the filling end by a filling valve for introducing the fluid into the hollow space; characterised in that the filling end has a thread, in particular a threaded insert, for fixing the filling valve to the filling end and - the protective agent has a non-flammable propellant. - a locking end arranged to be temporarily arrested into a locking device in dependence on a locking mechanism of the locking device; - a filling end arranged for at least temporarily supporting the securing element in the locking device; and - a hollow space arranged between the locking end and the filling end, in which a pressurised fluid is included as a protective agent, - wherein the hollow space is lockable at the filling end by a filling valve for introducing the fluid into the hollow space; - the protective agent has a non-flammable propellant.
A method for controlling a wind turbine during a safety operation, said wind turbine comprising at least two wind turbine blades adapted to be pitched individually, the method comprising the steps of: - providing a safety pitch control system adapted to pitch the blades individually at a number of pre-set approximately constant pitch rates including a first pitch rate and a second pitch rate lower than the first pitch rate; - providing a safety pitch strategy wherein for all the blades, the pitch rate is alternating between the first pitch rate and the second pitch rate according to a function of each blade azimuthal position, where each blade follows the same pitch rate function one after the other at regular angular intervals during the rotation, such that each blade in turn is closer to the feathering position than the others; - receiving a command for initiating the safety operation of the wind turbine whereupon the blades are pitched towards a feathering position by the safety pitch control system; - before initiating the safety pitch strategy, pitching the blades at an identical pitch rate for a first period of time; - pitching the blades according to the safety pitch strategy; and - the safety pitch strategy being performed while pitching the blades towards a feathering position. - providing a safety pitch control system adapted to pitch the blades individually at a number of pre-set approximately constant pitch rates including a first pitch rate and a second pitch rate lower than the first pitch rate; - providing a safety pitch strategy wherein for all the blades, the pitch rate is alternating between the first pitch rate and the second pitch rate according to a function of each blade azimuthal position, where each blade follows the same pitch rate function one after the other at regular angular intervals during the rotation, such that each blade in turn is closer to the feathering position than the others; - receiving a command for initiating the safety operation of the wind turbine whereupon the blades are pitched towards a feathering position by the safety pitch control system; - before initiating the safety pitch strategy, pitching the blades at an identical pitch rate for a first period of time; - pitching the blades according to the safety pitch strategy; and - the safety pitch strategy being performed while pitching the blades towards a feathering position.