mhurhangee/ep-ind-claims huggingface dataset:
A method for monitoring a dual-stage shock strut, comprising: measuring a first primary chamber pressure of a primary gas chamber of the dual-stage shock strut when the dual-stage shock strut is in a first state: measuring a first secondary chamber pressure of a secondary gas chamber of the dual-stage shock strut when the dual-stage shock strut is in the first state: measuring a shock strut stroke when the dual-stage shock strut is in the first state: measuring a first ambient temperature corresponding to that of the dual stage shock strut when the dual stage shock strut is in the first state using a temperature sensor installed on the fuselage or the wings of an aircraft; measuring a second primary chamber pressure of the primary gas chamber when the dual-stage shock strut is in a second state; measuring a second secondary chamber pressure of the secondary gas chamber when the dual-stage shock strut is in the second state; measuring a second ambient temperature corresponding to that of the dual stage shock strut when the dual stage shock strut is in the second state using the temperature sensor; determining a servicing condition of the shock strut based upon at least the first primary chamber pressure, the first secondary chamber pressure, the shock strut stroke, the first ambient temperature, the second primary chamber pressure, the second secondary chamber pressure, and the second ambient temperature; and wherein the secondary gas chamber is separated from the primary gas chamber via a separator piston measuring a first primary chamber pressure of a primary gas chamber of the dual-stage shock strut when the dual-stage shock strut is in a first state: measuring a first secondary chamber pressure of a secondary gas chamber of the dual-stage shock strut when the dual-stage shock strut is in the first state: measuring a shock strut stroke when the dual-stage shock strut is in the first state: measuring a first ambient temperature corresponding to that of the dual stage shock strut when the dual stage shock strut is in the first state using a temperature sensor installed on the fuselage or the wings of an aircraft; measuring a second primary chamber pressure of the primary gas chamber when the dual-stage shock strut is in a second state; measuring a second secondary chamber pressure of the secondary gas chamber when the dual-stage shock strut is in the second state; measuring a second ambient temperature corresponding to that of the dual stage shock strut when the dual stage shock strut is in the second state using the temperature sensor; determining a servicing condition of the shock strut based upon at least the first primary chamber pressure, the first secondary chamber pressure, the shock strut stroke, the first ambient temperature, the second primary chamber pressure, the second secondary chamber pressure, and the second ambient temperature; and wherein the secondary gas chamber is separated from the primary gas chamber via a separator piston
A photocatalytic coating composition comprising 5 to 20% by weight of a hydroxyapatite-coated photocatalyst, 5 to 15% by weight of a silica-based binder, 1 to 5% by weight of an acrylic emulsion, 0.1 to 1% by weight of a thickener and 54 to 85% by weight of water, wherein the hydroxyapatite-coated photocatalyst has a coverage ratio in the range of 5 to 36%, wherein the hydroxyapatite-coated photocatalyst has an average particle diameter in the range of 1 to 250 nm, wherein the photocatalyst is selected from titanium dioxide, zinc oxide, zirconium oxide, tin oxide, vanadium trioxide, wherein the thickener is xanthan gum.
A system for incubating and hatching eggs wherein the system comprises: (i) a first zone, (ii) an egg carrier, (iii) an egg transport system, (iv) an egg transferring system and (v) a first carrier support configured in the first zone, wherein: - the first zone comprises an egg placing zone; - the egg carrier is configured to carry the eggs during incubation and hatching; wherein the egg carrier comprises a conveyor belt, wherein the egg carrier is a linear egg carrier comprising a beginning and an end, wherein the egg carrier is not circular defining an infinite loop; - the egg transport system is configured to move in an operational mode of the system the egg carrier along a track from the first zone to a second zone; - the egg transferring system is configured to transfer eggs from an egg support element onto the egg carrier in the egg placing zone, wherein one or more of the eggs is at least partly in direct contact with the egg carrier; and - wherein during the operational mode, the system is configured to unroll the egg carrier from the first carrier support. - the first zone comprises an egg placing zone; - the egg carrier is configured to carry the eggs during incubation and hatching; wherein the egg carrier comprises a conveyor belt, wherein the egg carrier is a linear egg carrier comprising a beginning and an end, wherein the egg carrier is not circular defining an infinite loop; - the egg transport system is configured to move in an operational mode of the system the egg carrier along a track from the first zone to a second zone; - the egg transferring system is configured to transfer eggs from an egg support element onto the egg carrier in the egg placing zone, wherein one or more of the eggs is at least partly in direct contact with the egg carrier; and - wherein during the operational mode, the system is configured to unroll the egg carrier from the first carrier support.
A system for processing a workpiece, said system comprising: a support surface for supporting a workpiece and defining a processing path; a processing tool movable with respect to said processing path; and a gas mixture system for controlling a gas used by said processing tool, said system characterized in that said gas mixture system controls the flow of a gas based on historical three-dimensional coordinates of said processing tool. a support surface for supporting a workpiece and defining a processing path; a processing tool movable with respect to said processing path; and a gas mixture system for controlling a gas used by said processing tool,
Recovery system allowing a carrier aircraft to at least recover a carrier-borne aircraft in flight, the recovery system comprising a receiver able to be carried by the carrier aircraft and an attachment able to be carried by the carrier-borne aircraft, said receiver having an internal volume emerging into an external environment via a through surface, said receiver comprising a hollow guide section, said guide section being flared, said attachment comprising a flared connection section able to be at least partially contained in said internal volume, said recovery system comprising a fixing device reversibly fixing the attachment to the receiver, characterised in that said attachment is rigidly connected to a mast configured to be attached to the carrier-borne aircraft, said mast comprising a segment arranged outside said receiver when said attachment is stowed in the receiver, said guide section being asymmetrical.
An image processing apparatus comprising: generating means arranged to generate an object distance map by extracting each object and its associated object distance included in a blurred image; a blur restoration means arranged to set one of the object distances as a blur restoration distance and to restore an image from the blurred image by performing deconvolution processing as blur restoration processing on the blurred image according to the blur restoration distance; an instruction means arranged to instruct the blur restoration means to change the blur restoration distance; and characterized in that if a fine correction instruction is issued by the instruction means in response to an operation of the photographer if a difference between at least one of the object distances and the blur restoration distance is lower than a predetermined threshold, the blur restoration means changes the blur restoration distance with a first change amount, otherwise the blur restoration means changes the blur restoration distance with a second change amount larger than said first change amount, the blur restoration means restores the image from the blurred image according to the changed blur restoration distance. generating means arranged to generate an object distance map by extracting each object and its associated object distance included in a blurred image; a blur restoration means arranged to set one of the object distances as a blur restoration distance and to restore an image from the blurred image by performing deconvolution processing as blur restoration processing on the blurred image according to the blur restoration distance; an instruction means arranged to instruct the blur restoration means to change the blur restoration distance; and
An energy absorber (10,10',1010,1110), comprising: a monolithic length of ductile material (20,1020,1120) comprising a first end (20a,1020a,1120a) and a second end (20b,1020b,1120b), the monolithic length of ductile material (20,1020,1120) being formed to comprise at least a first longitudinally extending section (40,40',1040,1140) that extends continuously between the first end (20a,1020a,1120a) and the second end (20b,1020b,1120b), the first longitudinally extending section (40,40',1040,1140) being deformed over at least a portion thereof out of a plane running through the first end (20a,1020a,1120a) and the second end (20b,1020b,1120b), a first section (50a,50a',1050a,1150a) extending longitudinally from the first end (20a,1020a,1120a) toward the second end (20b,1020b,1120b) to a first terminal end, and at least a second section (50b,50b',1050b,1150b) extending longitudinally from the second end (20b,1020b,1120b) toward the first end (20a,1020a,1120a) to a second terminal end, wherein the first terminal end is located longitudinally between the second terminal end and the second end (20b,1020b,1120b) such that a portion of the first section (50a,50a',1050a,1150a) and second section (50b,50b',1050b,1150b) overlap, the first section (50a,50a',1050a,1150a) and the second section (50b,50b',1050b,1150b) are connected such that tensile force of a threshold magnitude is required between the first end (20a,1020a,1120a) and the second end (20b,1020b,1120b) to disconnect the first section (50a,50a',1050a,1150a) from the second section (50b,50b',1050b,1150b), upon disconnection of the first section (50a,50a',1050a,1150a) from the second section (50b,50b',1050b,1150b), the first longitudinally extending section (40,40',1040,1140) being free to deform under tensile force to absorb energy.
Mounting apparatus for mounting an item of furniture against a vertical wall surface, the apparatus including an engagement facility configured to engage an item of furniture to be mounted; and a plurality of fixings, each fixing being configured to receive a fastener whereby the fixings may be fixed to the wall, wherein said apparatus includes connecting means connecting said fixings along a connection axis, said connecting means and said fixings being configured such that a fixing can be located with respect to another at substantially any position along said connecting axis, wherein said connecting means includes a pair of spaced, facing, channels extending in the direction of said connection axis, and wherein at least one of said fixings includes lugs engageable within said channels, said channels and said lugs being configured so that said at least one of said fixings is retained within but is slidable along said channels, wherein when mounted in a functional position, said engagement facility defines or is included in an upper boundary of said connecting means, wherein a surface of each of said fixings and a surface of said connecting means lie in a substantially common surface contact plane, for contacting the vertical wall surface.
Voltage measurement apparatus comprising: a potential attenuator configured to be electrically connected between first and second conductors (206, 208), the first and second conductors being electrically coupled to a source, the potential attenuator comprising: a first impedance and a reference impedance arrangement (319, 429) in series with each other, and a processing arrangement configured to acquire at least one signal from the reference impedance arrangement, and to determine a voltage between the first and second conductors based on the at least one signal, characterised by the voltage measuring apparatus further comprising an offset voltage circuit, wherein the reference impedance arrangement (319, 419) comprises a second impedance connected between the first impedance, and an output of the offset voltage circuit (404, 452, 462) such that a voltage across a potential divider comprising the first impedance and the second impedance can be changed in response to known voltage changes at the offset voltage circuit. a first impedance and a reference impedance arrangement (319, 429) in series with each other, and a processing arrangement configured to acquire at least one signal from the reference impedance arrangement, and to determine a voltage between the first and second conductors based on the at least one signal, characterised by the voltage measuring apparatus further comprising an offset voltage circuit, wherein the reference impedance arrangement (319, 419) comprises a second impedance connected between the first impedance, and an output of the offset voltage circuit (404, 452, 462) such that a voltage across a potential divider comprising the first impedance and the second impedance can be changed in response to known voltage changes at the offset voltage circuit.
An integrated solvent deasphalting and steam pyrolysis process for the direct processing of a crude oil to produce olefinic and aromatic petrochemicals, the process comprising: a. charging the crude oil to a solvent deasphalting zone with an effective amount of solvent to produce a deasphalted and demetalized oil stream and a bottom asphalt phase; b. thermally cracking the deasphalted and demetalized oil stream in the presence of steam to produce a mixed product stream; c. separating the thermally cracked mixed product stream; d. recovering olefins and aromatics from the separated mixed product stream; and e. recovering pyrolysis fuel oil from the separated mixed product stream. a. charging the crude oil to a solvent deasphalting zone with an effective amount of solvent to produce a deasphalted and demetalized oil stream and a bottom asphalt phase; b. thermally cracking the deasphalted and demetalized oil stream in the presence of steam to produce a mixed product stream; c. separating the thermally cracked mixed product stream; d. recovering olefins and aromatics from the separated mixed product stream; and e. recovering pyrolysis fuel oil from the separated mixed product stream.
A lumen stent, comprising a tubular body, two inner branches and two outer branches which are respectively communicated with the tubular body, the tubular body comprising a first body segment, a tapered segment and a second body segment which are connected in sequence, wherein the tapered segment is provided with outer branch windows and inner branch windows, wherein a proximal end of the outer branches are connected to the outer branch windows and a distal end of the outer branches are located outside the tubular body, wherein a distal end of the inner branches are connected to the inner branch windows and the proximal end of the inner branches are located inside of the tubular body, and wherein the area of the inner branch windows is larger than that of the outer branch windows. wherein the tapered segment is provided with outer branch windows and inner branch windows, wherein a proximal end of the outer branches are connected to the outer branch windows and a distal end of the outer branches are located outside the tubular body, wherein a distal end of the inner branches are connected to the inner branch windows and the proximal end of the inner branches are located inside of the tubular body, and wherein the area of the inner branch windows is larger than that of the outer branch windows.
A method of preparing a reassortant influenza virus comprising the steps of (i) infecting a culture host with a first influenza strain and a second influenza strain; (ii) contacting the culture host of step (i) with an inhibitory agent wherein said inhibitory agent preferentially reduces the transcription and/or translation of the hemagglutinin and/or neuraminidase genes of the first influenza strain relative to the second influenza strain; (iii) culturing the culture host in order to produce reassortant virus and optionally further comprising the step (iv) of purifying the virus obtained in step (iii).
Electrolysis system for low-pressure PEM electrolysis, having at least two electrolysis modules each having at least one electrolysis cell and each having at least one connection device, each of which is connected in a fluidically conductive manner to the respective at least one electrolysis cell and via which the respective electrolysis module is connected to a tank for storing a fluid, wherein the connection devices of the at least two electrolysis modules are connected by a common duct element via which the electrolysis modules are connected to the tank, and the duct element has an inclination by means of which a preferred flow direction can be imposed on the fluid in the duct element, and the duct element has a withdrawal device for discharge of the fluid from the electrolysis system, and the duct element has a venting device by means of which the duct element can be fluidically coupled to an environment at its highest point in relation to a field of gravity.
Method of quantifying the intrinsic dimensions of a radiation sensor, the method comprising the following steps: - defining and producing of a model of the sensor, starting from a block diagram of the sensor, - using a digital calculation, identifying the influential elements of the sensor, through the use of the experience plans theory, - making measurements, for each particular position in the space around the sensor, using a standard multifrequency source of said radiation, and - determining the sizes of the elements that influence the response of the sensor, through the use of the experience plans theory. - defining and producing of a model of the sensor, starting from a block diagram of the sensor, - using a digital calculation, identifying the influential elements of the sensor, through the use of the experience plans theory, - making measurements, for each particular position in the space around the sensor, using a standard multifrequency source of said radiation, and - determining the sizes of the elements that influence the response of the sensor, through the use of the experience plans theory.
An electrophotographic photosensitive member comprising a conductive substrate and a photosensitive layer, wherein the photosensitive layer contains at least a charge generating material, a hole transport material, and a binder resin, and the hole transport material is a compound represented by the following general formula: where in general formula, R 1 and R 3 each independently represent an alkyl group, an aryl group, an aralkyl group, or an alkoxy group; and R 2 and R 4 each independently represent an alkyl group, or an alkoxy group, and the binder resin is a resin represented by the following general formula: where in general formula, R 23, R 24, and R 25 each independently represent a hydrogen atom, or an alkyl group having a carbon number of at least 1 and no greater than 4, at least one of R 23, R 24, and R 25 representing an alkyl group having a carbon number of at least 1 and no greater than 4; p + q = 1.00, and 0.35 ≤ p < 1.00; and n represents 2 or 3.
A process of preparing transiently transfected recombinant cells which transiently overexpress one or more genes encoding a drug transporter protein, wherein the drug transporter protein is MATE2K/Mate2K, said process comprising transiently transfecting cells by electroporation with one or more genes encoding MATE2K/Mate2K, and cryopreserving the transiently transfected recombinant cells within 48 hours of transfection.
Application machine for applying granular goods, in particular seeds and/or fertilizer grains, with conveyor lines for conveying the goods from a distributor head to application elements, by means of which the goods can be laid on/in the ground, wherein an acoustic detection device having at least one microphone for acoustically detecting the goods run-through the conveyor line is assigned to at least one conveyor line, wherein the microphone is arranged outside the conveyor line which is guided past the microphone contiguously at a uniform wall configuration, wherein the microphone is attached to a sound-absorbing and vibration-reducing coupling element which at least partially encompasses the conveyor line on the outer side thereof, characterized in that the line wall of the conveyor line is formed without interruptions and in that the microphone is attachable at various positions along the conveyor line.
An air compression device for use in driving a device such as a vehicle brake device or a door opening/closing device, comprising: a scroll compressor driven by an electric motor; a discharge flow channel connected to a discharge portion of the compressor and to a check valve; a downstream flow channel connected to the check valve and to an air tank, a release flow channel disposed to be connectable to the discharge flow channel; and an operation control unit configured to perform a release operation of releasing a part or all of compressed air remaining in the discharge flow channel through the release flow channel when the operation control unit controls to stop the compressor. a scroll compressor driven by an electric motor; a discharge flow channel connected to a discharge portion of the compressor and to a check valve; a downstream flow channel connected to the check valve and to an air tank, a release flow channel disposed to be connectable to the discharge flow channel; and an operation control unit configured to perform a release operation of releasing a part or all of compressed air remaining in the discharge flow channel through the release flow channel when the operation control unit controls to stop the compressor.
A gas turbine engine comprising: a combustor; a turbine section in fluid communication with the combustor, the turbine section including a first vane stage aft of the combustor; and a seal assembly disposed between the combustor and a forward face of the first vane stage, the seal assembly including a radially outer surface and a radially inner surface, characterised in that: the seal assembly further includes a plurality of circumferentially spaced apart slots and a first plurality of openings that extend from the radially outer surface to the radially inner surface at an angle relative to the radially outer surface, within each of the plurality of circumferentially spaced apart slots, for communicating cooling airflow into a gap between the aft end of the combustor and the forward face of the first vane stage, wherein the first vane stage includes a second plurality of openings communicating cooling airflow into the gap. a combustor; a turbine section in fluid communication with the combustor, the turbine section including a first vane stage aft of the combustor; and a seal assembly disposed between the combustor and a forward face of the first vane stage, the seal assembly including a radially outer surface and a radially inner surface, characterised in that: the seal assembly further includes a plurality of circumferentially spaced apart slots and a first plurality of openings that extend from the radially outer surface to the radially inner surface at an angle relative to the radially outer surface, within each of the plurality of circumferentially spaced apart slots, for communicating cooling airflow into a gap between the aft end of the combustor and the forward face of the first vane stage, wherein the first vane stage includes a second plurality of openings communicating cooling airflow into the gap.