mhurhangee/ep-ind-claims huggingface dataset:
A solid electrolyte membrane including a non-woven fabric made of fibers serving as a support and a solid electrolyte serving as a matrix component, wherein the fibers are made of a thermoplastic polymer to which nanocellulose is added, the nanocellulose has a fiber length of 0.5 μm or more and 10 μm or less and a fiber diameter of 0.001 μm or more and 10 μm or less, wherein the amount of the nanocellulose added to the thermoplastic polymer is 0.1 vol% or more and 10 vol% or less, wherein the thermoplastic polymer is selected from high-density polyethylene, polypropylene, polymethylpentene, polyethylene terephthalate, polybutylene terephthalate, polyvinylidene fluoride, polyamide, and polyphenylene sulfide, and wherein an average fiber diameter of the fibers is 5 μm or less. wherein the fibers are made of a thermoplastic polymer to which nanocellulose is added, the nanocellulose has a fiber length of 0.5 μm or more and 10 μm or less and a fiber diameter of 0.001 μm or more and 10 μm or less, wherein the amount of the nanocellulose added to the thermoplastic polymer is 0.1 vol% or more and 10 vol% or less, wherein the thermoplastic polymer is selected from high-density polyethylene, polypropylene, polymethylpentene, polyethylene terephthalate, polybutylene terephthalate, polyvinylidene fluoride, polyamide, and polyphenylene sulfide, and wherein an average fiber diameter of the fibers is 5 μm or less.
A core for an airfoil comprising a refractory metal structure having a variable thickness, wherein the structure is a unitary body having uniform material properties throughout the structure, the structure having at least one portion with a thickness of less than 1.52 mm (0.060 inch), characterised in that: the structure includes a first portion and a second portion in spaced apart and overlapping relationship with one another, wherein the structure is tapered between first and second portions (77, 79), with the second portion having a thickness less than 0.51 mm (0.020 inch), and the structure includes a standoff interconnecting the first and second portions (77, 79).
A lubricating grease composition comprising a complex metal soap thickener of aliphatic dicarboxylic acid and monoamide monocarboxylic acid obtainable by amidation of a monocarboxylic group of a saturated or unsaturated aliphatic dicarboxylic acid having 2 to 20 carbon atoms, and a fluororesin powder contained in a base oil mixture of a non-fluorine-based base oil and a fluorine-based base oil, which are incompatible with each other, i.e. a homogeneous base oil mixture cannot be formed by simply mixing these two base oils, wherein the non-fluorine-based base oil is contained in an amount of 5 to 90 wt.%, wherein the fluorine-based base oil is contained in an amount of 5 to 90 wt.%, wherein the complex metal soap is contained in an amount of 1.5 to 30 wt.% and wherein the fluororesin powder is contained in an amount of 0.1 to 50 wt.% in the lubricating grease composition.
A rod-shaped cosmetic material feeding container (100; 200), comprising: a tubular-shaped container with a front container part and a rear container part, the rear container part being mounted rotatable with respect to the front container part around an axis line and immovable in an axial direction; a movable body with a male thread at an outer peripheral part, the movable body being unrotatable around the axis line and movable in the axial direction with respect to the front container part, the movable body supporting a rod-shaped cosmetic material at a distal end; a female thread part with a female thread at an inner peripheral part, the female thread part being unrotatable with respect to the rear container part around the axis line, the female thread being screwed with the male thread; a first elastic body configured to reduce rearward movement of the female thread part in the axial direction; and a second elastic body configured to reduce frontward movement of the female thread part in the axial direction, wherein the male thread and the female thread constitute a thread engagement part, the thread engagement part acts by relative rotation of the front container part and the rear container part, the relative rotation advancing and retreating the movable body causes the rod-shaped cosmetic material to appear and disappear from an opening at a distal end of a container, the female thread part is movable in the axial direction, characterized in that the first elastic body and/or the second elastic body is a coil spring. a tubular-shaped container with a front container part and a rear container part, the rear container part being mounted rotatable with respect to the front container part around an axis line and immovable in an axial direction; a movable body with a male thread at an outer peripheral part, the movable body being unrotatable around the axis line and movable in the axial direction with respect to the front container part, the movable body supporting a rod-shaped cosmetic material at a distal end; a female thread part with a female thread at an inner peripheral part, the female thread part being unrotatable with respect to the rear container part around the axis line, the female thread being screwed with the male thread; a first elastic body configured to reduce rearward movement of the female thread part in the axial direction; and a second elastic body configured to reduce frontward movement of the female thread part in the axial direction, wherein the male thread and the female thread constitute a thread engagement part, the thread engagement part acts by relative rotation of the front container part and the rear container part, the relative rotation advancing and retreating the movable body causes the rod-shaped cosmetic material to appear and disappear from an opening at a distal end of a container, the female thread part is movable in the axial direction, characterized in that the first elastic body and/or the second elastic body is a coil spring.
Method for operating a multi-gas burner in a low-calorific operation with a low-calorific combustion gas and in a high-calorific operation with a high-calorific combustion gas, wherein the multi-gas burner has - at least one burner lance with a first, a second and a third nozzle, - a first, a second and a third feed chamber which are each connected in terms of flow to a respective nozzle (11, 12, 13) and - a combustion chamber, into which the at least one burner lance projects, wherein in a high-calorific operation air is fed via the first nozzle and simultaneously O 2 -depleted gas via the second nozzle and a high-calorific combustion gas via the third nozzle into the combustion chamber, where they are combusted, the air and the O 2 -depleted gas being used as oxygen carriers for the combustion, characterised in that in a low-calorific operation air is fed via the first nozzle as an oxygen carrier for the combustion and simultaneously a low-calorific combustion gas is fed via the second nozzle into the combustion chamber, where they are combusted. - at least one burner lance with a first, a second and a third nozzle, - a first, a second and a third feed chamber which are each connected in terms of flow to a respective nozzle (11, 12, 13) and - a combustion chamber, into which the at least one burner lance projects, wherein in a high-calorific operation air is fed via the first nozzle and simultaneously O 2 -depleted gas via the second nozzle and a high-calorific combustion gas via the third nozzle into the combustion chamber, where they are combusted, the air and the O 2 -depleted gas being used as oxygen carriers for the combustion, characterised in that in a low-calorific operation air is fed via the first nozzle as an oxygen carrier for the combustion and simultaneously a low-calorific combustion gas is fed via the second nozzle into the combustion chamber, where they are combusted.
An ophthalmic composition in the form of an oil-in-water emulsion comprising a mucomimetic polymer selected from hyaluronic acid and salts thereof and lipoic acid.
A macerator comprising a housing, an opening in the housing providing access to its interior, a releasably securable closure for releasably closing the opening in the housing, movable blade means within the housing, means for supplying water to the interior of the housing, an exit aperture in the housing and a lock means for releasably securing the closure in a closed position, characterised by a contactless switch operable by a user for controlling a function of the macerator, wherein actuation of the switch is adapted to control the operation of the lock means.
A vehicle steering system (10, 10'), comprising: - a steering wheel, - a first steering assembly, comprising • a first steering linkage mechanically connected to a first road wheel at a first end of a wheel axle, • a first support motor operatively connected to the steering wheel and the first steering linkage, wherein the steering wheel is configured to control a steering angle of the first road wheel via the first support motor actuating the first steering linkage, - a second steering assembly, comprising • a second steering linkage mechanically connected to a second road wheel at a second end of said wheel axle, • a second support motor operatively connected to the second steering linkage, characterized in that the vehicle steering system comprises: - a processing circuitry configured to receive from the first steering assembly first input signals, the first input signals comprising one or more steering parameter values measured for the first steering assembly, wherein, based on the received first input signals, the processing circuitry is configured to calculate a desired steering angle of the second road wheel and to send control signals to the second support motor so as to actuate the second steering linkage such that said desired steering angle of the second road wheel is obtained. - a steering wheel, - a first steering assembly, comprising • a first steering linkage mechanically connected to a first road wheel at a first end of a wheel axle, • a first support motor operatively connected to the steering wheel and the first steering linkage, wherein the steering wheel is configured to control a steering angle of the first road wheel via the first support motor actuating the first steering linkage, • a first steering linkage mechanically connected to a first road wheel at a first end of a wheel axle, • a first support motor operatively connected to the steering wheel and the first steering linkage, - a second steering assembly, comprising • a second steering linkage mechanically connected to a second road wheel at a second end of said wheel axle, • a second support motor operatively connected to the second steering linkage, • a second steering linkage mechanically connected to a second road wheel at a second end of said wheel axle, • a second support motor operatively connected to the second steering linkage, - a processing circuitry configured to receive from the first steering assembly first input signals, the first input signals comprising one or more steering parameter values measured for the first steering assembly,
A transmission apparatus for transmitting a signalling frame and a data frame to a reception apparatus in a Code Division Multiple Access, CDMA, mobile communication system having an ALL-IP network, comprising: a signalling frame transmitter for transmitting header information for a data frame to be transmitted to the reception apparatus through a signalling frame over a first channel during a call setup for a call attempt request of a user; and a voice frame transmitter for constructing the data frame including a terminal identification code and data to be transmitted, after the call setup, and means for transmitting the data frame to the reception apparatus over a second channel different from the first channel, wherein the terminal identification code is used to retrieve the header information transmitted through the first channel. a signalling frame transmitter for transmitting header information for a data frame to be transmitted to the reception apparatus through a signalling frame over a first channel during a call setup for a call attempt request of a user; and a voice frame transmitter for constructing the data frame including a terminal identification code and data to be transmitted, after the call setup, and means for transmitting the data frame to the reception apparatus over a second channel different from the first channel, wherein the terminal identification code is used to retrieve the header information transmitted through the first channel.
A flight control system for a rotary aircraft (101; 201), the rotary aircraft comprising: a rotor blade; an actuator operably associated with the rotor blade, the actuator being configured to change the pitch of the rotor blade; a controller to be commanded by a pilot and operably associated with the actuator to control the pitch of the rotor blade, characterized by the flight control system comprising: a subsystem configured to modify flight control limits for a displacement of the controller based upon detection of an impending hazardous flight condition, the impending hazardous flight condition being detected as an excessive flapping of the rotor blade; and a display configured to display a symbol identifying the displacement of the controller relative to the flight control limits, the display showing a flight control envelope defined by the flight control limits, the flight control envelope being configured to morph in response to the aircraft approaching the impending hazardous flight condition. a rotor blade; an actuator operably associated with the rotor blade, the actuator being configured to change the pitch of the rotor blade; a controller to be commanded by a pilot and operably associated with the actuator to control the pitch of the rotor blade, characterized by the flight control system comprising: a subsystem configured to modify flight control limits for a displacement of the controller based upon detection of an impending hazardous flight condition, the impending hazardous flight condition being detected as an excessive flapping of the rotor blade; and a display configured to display a symbol identifying the displacement of the controller relative to the flight control limits, the display showing a flight control envelope defined by the flight control limits, the flight control envelope being configured to morph in response to the aircraft approaching the impending hazardous flight condition. a subsystem configured to modify flight control limits for a displacement of the controller based upon detection of an impending hazardous flight condition, the impending hazardous flight condition being detected as an excessive flapping of the rotor blade; and a display configured to display a symbol identifying the displacement of the controller relative to the flight control limits, the display showing a flight control envelope defined by the flight control limits, the flight control envelope being configured to morph in response to the aircraft approaching the impending hazardous flight condition.
Medical appliance having at least one coupling element and one line element connected to the coupling element, wherein at least one part of the coupling element and at least one portion of the line element are enclosed in a gas-tight manner by means of a gas-tight sealing device, wherein the sealing device, at a first sealing location, connects circumferentially in a gas-tight manner, on all sides, to the line element, wherein the sealing device, at a second sealing location, connects circumferentially in a gas-tight manner, on all sides, to the coupling element or to a wall in or at which the coupling element is mounted, and wherein the sealing device, between the first sealing location and the second sealing location, encloses in a gas-tight manner a volume defined by the geometry of the sealing device.
A power converter configured for being connected to an AC grid having three phases (a, b, c), the converter comprising: a full-bridge director switch arrangement; and a chain-link leg comprising a first arm of bi-polar chain-linked converter cells connected between a top point (p) and a middle point (b) in series with a second arm of bi-polar chain-linked converter cells connected between a bottom point (q) and said middle point (b); wherein the director switch arrangement comprises first and second parallel director switch legs (2a, 2b) connected across the chain-link leg, of which the first director switch leg comprises a first director switch in series with a fourth director switch, and the second director switch leg comprises a second director switch in series with a third director switch; wherein the converter is configured to be connected to the AC grid such that a first phase (a) of the AC grid is connected to the first director switch leg between the first and fourth director switches (D1, D4), a second phase (b) of the AC grid is connected to the chain-link leg between the first and second chain-link arms (3a, 3b), and a third phase (c) of the AC grid is connected to the second director switch leg between the second and third director switches (D2, D3); and wherein the director switch arrangement is arranged to alternately connect the first and third phases (a, c) to the top point (p) and the bottom point (q), respectively, and to the bottom point (q) and the top point (p), respectively, by switching the director switches every half fundamental frequency cycle. a full-bridge director switch arrangement; and a chain-link leg comprising a first arm of bi-polar chain-linked converter cells connected between a top point (p) and a middle point (b) in series with a second arm of bi-polar chain-linked converter cells connected between a bottom point (q) and said middle point (b); wherein the director switch arrangement comprises first and second parallel director switch legs (2a, 2b) connected across the chain-link leg, of which the first director switch leg comprises a first director switch in series with a fourth director switch, and the second director switch leg comprises a second director switch in series with a third director switch; wherein the converter is configured to be connected to the AC grid such that a first phase (a) of the AC grid is connected to the first director switch leg between the first and fourth director switches (D1, D4), a second phase (b) of the AC grid is connected to the chain-link leg between the first and second chain-link arms (3a, 3b), and a third phase (c) of the AC grid is connected to the second director switch leg between the second and third director switches (D2, D3); and wherein the director switch arrangement is arranged to alternately connect the first and third phases (a, c) to the top point (p) and the bottom point (q), respectively, and to the bottom point (q) and the top point (p), respectively, by switching the director switches every half fundamental frequency cycle.
Pivot bearing for a front wheel suspension system of a motor bike, comprising a first bearing part which permits a component to pivot about a first pivot axis, and a second bearing part which permits a component to pivot about a second pivot axis, wherein the two pivot axes (M1, M2) intersect, and wherein the two bearing parts (36, 38) are connected to each other and form a structural unit, characterized in that the second bearing part is centred with respect to its extent in the direction of the second pivot axis relative to the first pivot axis.
A tool system for agricultural soil tillage, the tool system comprising: a soil tillage unit comprising at least one rotatably mounted soil tillage tool and an electric drive for rotating the at least one rotatably mounted soil tillage tool, wherein the soil tillage unit is configured to change a rotational speed (w) of the at least one rotatably mounted soil tillage tool by means of the electric drive for generating a soil tillage result depending on the rotational speed (w) within a soil tillage region cultivated by means of the soil tillage unit, wherein the soil tillage unit further comprises at least one trailing tool for cultivating the soil tillage region, wherein the at least one trailing tool is driven electrically for generating a propelling force; a sensor system which is configured to determine an actual soil tillage result within the soil tillage region cultivated by means of the soil tillage unit; and a control system which is configured to change the rotational speed (ω) of the at least one rotatably mounted soil tillage tool based on the determined actual soil tillage result and a target soil tillage result to reduce a deviation of the actual soil tillage result from the target soil tillage result. a soil tillage unit comprising at least one rotatably mounted soil tillage tool and an electric drive for rotating the at least one rotatably mounted soil tillage tool, wherein the soil tillage unit is configured to change a rotational speed (w) of the at least one rotatably mounted soil tillage tool by means of the electric drive for generating a soil tillage result depending on the rotational speed (w) within a soil tillage region cultivated by means of the soil tillage unit, wherein the soil tillage unit further comprises at least one trailing tool for cultivating the soil tillage region, wherein the at least one trailing tool is driven electrically for generating a propelling force; a sensor system which is configured to determine an actual soil tillage result within the soil tillage region cultivated by means of the soil tillage unit; and a control system which is configured to change the rotational speed (ω) of the at least one rotatably mounted soil tillage tool based on the determined actual soil tillage result and a target soil tillage result to reduce a deviation of the actual soil tillage result from the target soil tillage result.