mhurhangee/patent-ind-claim-en huggingface dataset:
A packet backpressure detection method by a device having a Peripheral Component Interconnect Express, PCIe, port, and the method comprises: storing a plurality of packets that are to be transmitted via the PCIe port in a packet queue in a first buffer and storing a packet that is to be transmitted next in a second buffer ; recording a storage duration of each packet stored in the second buffer ; determining that packet backpressure occurs at the PCIe port and removing the packet from the second buffer after the packet is transmitted via the PCIe port, when recorded storage duration of any packet in the second buffer reaches a first value ; and generating an indication of packet backpressure at the PCIe port. storing a plurality of packets that are to be transmitted via the PCIe port in a packet queue in a first buffer and storing a packet that is to be transmitted next in a second buffer ; recording a storage duration of each packet stored in the second buffer ; determining that packet backpressure occurs at the PCIe port and removing the packet from the second buffer after the packet is transmitted via the PCIe port, when recorded storage duration of any packet in the second buffer reaches a first value ; and generating an indication of packet backpressure at the PCIe port.
Method for erecting an apparatus for dismantling an industrial plant, the industrial plant comprising a large number of industrial plant elements and the apparatus having a large number of disassembly stations for disassembling industrial plant elements, comprising the method steps of: - determining a dismantling sequence of the industrial plant elements and - determining disassembly stations that are required for dismantling at least the first industrial plant element, and - determining rooms within the industrial plant to be disassembled for erecting disassembly stations, based on the determined dismantling sequence, and - identifying placements in rooms within the industrial plant to be disassembled for disassembly stations, with a first group of disassembly stations being provided for processing reusable materials and a second group of disassembly stations being provided for processing waste materials, and - placing a first disassembly station for disassembling the industrial plant in a determined room of the industrial plant, characterized in that transport routes between disassembly stations of the first and the second group do not cross. - determining a dismantling sequence of the industrial plant elements and - determining disassembly stations that are required for dismantling at least the first industrial plant element, and - determining rooms within the industrial plant to be disassembled for erecting disassembly stations, based on the determined dismantling sequence, and - identifying placements in rooms within the industrial plant to be disassembled for disassembly stations, with a first group of disassembly stations being provided for processing reusable materials and a second group of disassembly stations being provided for processing waste materials, and - placing a first disassembly station for disassembling the industrial plant in a determined room of the industrial plant,
A method for reduction of start-up SO 2 , SO 3 and H 2 SO 4 emissions in sulfuric acid production, in which SO 2 is converted to SO 3 in n successive catalyst beds, where n is an integer >1, wherein - the final catalyst beds are used as absorbents for SO 2 and SO 3 during the start-up procedure, - one or more of the m beds downstream the first bed are purged, either separately or simultaneously, with hot gas, where m is an integer > 1 and m < n, during the previous shut-down, and - one separate purge with hot gas is used on the final bed. - the final catalyst beds are used as absorbents for SO 2 and SO 3 during the start-up procedure, - one or more of the m beds downstream the first bed are purged, either separately or simultaneously, with hot gas, where m is an integer > 1 and m < n, during the previous shut-down, and - one separate purge with hot gas is used on the final bed.
A method for defining a plurality of thrust limits for a wind turbine having a rotor with a plurality of blades and being located at a site, wherein the thrust limits define values of aerodynamic thrust on the rotor not to be exceeded in operation, the method characterized by comprising: providing a wind speed distribution representative for the site, defining one or more isolines of constant turbulence probability representing a turbulence parameter as a function of wind speed, wherein the isolines correspond to quantile levels of turbulence of the wind speed distribution and the turbulence parameter is indicative of wind speed variation; and defining turbulence ranges with respect to the isolines; and defining thrust limits for the turbulence ranges. providing a wind speed distribution representative for the site, defining one or more isolines of constant turbulence probability representing a turbulence parameter as a function of wind speed, wherein the isolines correspond to quantile levels of turbulence of the wind speed distribution and the turbulence parameter is indicative of wind speed variation; and defining turbulence ranges with respect to the isolines; and defining thrust limits for the turbulence ranges.
Method for cold stamping on a three-dimensional article , wherein the article is either rotatable about a rotation axis or is held fixed in place by a holding device , wherein, in a first step, an adhesive is applied onto the article at a first workstation and wherein, in a second step, a transfer film having a decorative layer and a carrier film is pressed by a pressing device onto the article at a second workstation , and the adhesive is simultaneously hardened, wherein the adhesive is a UV-adhesive, and wherein the hardening of the adhesive takes place by means of irradiation with UV-radiation.
Pipe clamp for fastening a pipe to a wall; having a wall mounting section comprising a fastening means for wall mounting; having two clamping legs which extend arcuately in each case from a first end (4.1, 5.1) to a second end (4.2, 5.2), are connected to one another in an articulated or detachable manner at the second end (4.2, 5.2), are arranged to engage around the pipe together in an arcuate manner and of which at least one comprises the wall-mounting section ; having a connecting device for releasably connecting the two first ends (4.1, 5.1) of the clamping legs ; wherein the connecting device has in each case a radially inwardly directed bend at each first end (4.1, 5.1) of the clamping legs , and the two bends are braced against each other in the circumferential direction by means of a screw connection extending in the circumferential direction; and wherein the pipe clamp has one or more elastic pressure elements, wherein the clamping legs have a C-shape, with radially inwardly directed folded edges extending along their circumference, between which the one or more elastic pressure elements are arranged, which project inwardly in the radial direction beyond the folded edges and the bends for frictionally engaged contact with the pipe. having a wall mounting section comprising a fastening means for wall mounting; having two clamping legs which extend arcuately in each case from a first end (4.1, 5.1) to a second end (4.2, 5.2), are connected to one another in an articulated or detachable manner at the second end (4.2, 5.2), are arranged to engage around the pipe together in an arcuate manner and of which at least one comprises the wall-mounting section ; having a connecting device for releasably connecting the two first ends (4.1, 5.1) of the clamping legs ; wherein the connecting device has in each case a radially inwardly directed bend at each first end (4.1, 5.1) of the clamping legs , and the two bends are braced against each other in the circumferential direction by means of a screw connection extending in the circumferential direction; and wherein the pipe clamp has one or more elastic pressure elements, wherein the clamping legs have a C-shape, with radially inwardly directed folded edges extending along their circumference, between which the one or more elastic pressure elements are arranged, which project inwardly in the radial direction beyond the folded edges and the bends for frictionally engaged contact with the pipe.
A unit for filling a succession of tubular wrappers (T) of the tobacco industry, of the type extending along a main axis of extension (X) and internally defining respective containment chambers adapted to contain a filling material of the tobacco industry, the unit comprising: - a filling station comprising a plurality of filling means configured to insert the filling material into respective containment chambers of the succession of tubular wrappers (T) through a filling end of the tubular wrappers (T). - a closing station disposed downstream of the filling station and comprising a plurality of closing means configured to make respective walls which close the filling ends and which are transverse to the respective main axes of extension (X); characterized in that the closing station comprises at least one feed drum on which the plurality of closing means are mounted. - a filling station comprising a plurality of filling means configured to insert the filling material into respective containment chambers of the succession of tubular wrappers (T) through a filling end of the tubular wrappers (T). - a closing station disposed downstream of the filling station and comprising a plurality of closing means configured to make respective walls which close the filling ends and which are transverse to the respective main axes of extension (X);
A biopsy needle that is to be inserted into an endoscope forceps channel, the biopsy needle comprising: a hollow tube which includes a distal end opening portion and a proximal end opening portion and of which the distal end opening portion and the proximal end opening portion communicate with each other, wherein the tube includes a puncture portion that is provided at a distal end portion of the tube and has a plurality of blade distal end points, a slit that extends toward the proximal end opening portion from the distal end opening portion , and a tissue excision cutter that is provided at a proximal end of the slit and is formed in a shape tapered toward a distal end of the slit from the proximal end of the slit, wherein the puncture portion includes a first blade distal end point , a second blade distal end point , and a third blade distal end point , in a case where the tube is viewed in a direction orthogonal to an axial direction of the tube, the first blade distal end point is formed closer to a distal end side of the tube than the second blade distal end point and the third blade distal end point , and in a case where the tube is viewed in the axial direction of the tube, the first blade distal end point is disposed to face the slit in a radial direction of the tube, and the second blade distal end point and the third blade distal end point are disposed to face each other with the slit interposed therebetween, characterized in that the slit is an elongated through-hole that is formed in the shape of a line extending in the axial direction of the tube . a hollow tube which includes a distal end opening portion and a proximal end opening portion and of which the distal end opening portion and the proximal end opening portion communicate with each other, wherein the tube includes a puncture portion that is provided at a distal end portion of the tube and has a plurality of blade distal end points, a slit that extends toward the proximal end opening portion from the distal end opening portion , and a tissue excision cutter that is provided at a proximal end of the slit and is formed in a shape tapered toward a distal end of the slit from the proximal end of the slit, wherein the puncture portion includes a first blade distal end point , a second blade distal end point , and a third blade distal end point , in a case where the tube is viewed in a direction orthogonal to an axial direction of the tube, the first blade distal end point is formed closer to a distal end side of the tube than the second blade distal end point and the third blade distal end point , and in a case where the tube is viewed in the axial direction of the tube, the first blade distal end point is disposed to face the slit in a radial direction of the tube, and the second blade distal end point and the third blade distal end point are disposed to face each other with the slit interposed therebetween, characterized in that the slit is an elongated through-hole that is formed in the shape of a line extending in the axial direction of the tube .
A process for recovering acetic acid and other valuable materials from cellulose acetate waste, characterized in that it includes: a) subjecting the cellulose acetate waste to a hydrothermal process operating at high pressure between 5 and 15 Mpa , at a temperature between 190 and 250 °C with reaction times between 10 and 240 min, feeding the reactor with a feed of cellulose acetate and water having a weight ratio between 1:5 and 1:10, in presence of acidic and basic catalysts; b) separating the liquid phase from the residual solid; c) sending the separated liquid phase to a process for recovering acetic acid and diethyl phthalate; and d) sending the recovered acetic acid to the plant for the traditional production of cellulose acetate. a) subjecting the cellulose acetate waste to a hydrothermal process operating at high pressure between 5 and 15 Mpa , at a temperature between 190 and 250 °C with reaction times between 10 and 240 min, feeding the reactor with a feed of cellulose acetate and water having a weight ratio between 1:5 and 1:10, in presence of acidic and basic catalysts; b) separating the liquid phase from the residual solid; c) sending the separated liquid phase to a process for recovering acetic acid and diethyl phthalate; and d) sending the recovered acetic acid to the plant for the traditional production of cellulose acetate.
Process for carrying out an allergy test, in which a blood sample with at least one allergen is contacted in vitro ; and in which one allergic reaction or an absence of the at least one allergic reaction of immune cells is directly optically observed by means of a microscope , characterised in that in the at least one allergic reaction a degranulation of the immune cells is observed, the immune cells may be arranged in different heights or planes, the position of granules being observed by means of the microscope , wherein the granules are observed in various heights or height planes, and that a position of the granules in the immune cells, a movement and/or a degranulation of the granules is observed in an observation time of up to 10 minutes or 60 seconds to 300 seconds.
A multi-domain polypeptide comprising (i) a first complement control protein repeat (CCP) domain being a convertase decay accelerating domain for convertases of the classical and alternative pathways of complement activation, (ii) a host cell recognition domain, and (iii) a second CCP-comprising domain, wherein said host cell recognition domain comprises CCPs 6 to 8 and/or 19 to 20 of a complement Factor H. (i) a first complement control protein repeat (CCP) domain being a convertase decay accelerating domain for convertases of the classical and alternative pathways of complement activation, (ii) a host cell recognition domain, and (iii) a second CCP-comprising domain, wherein said host cell recognition domain comprises CCPs 6 to 8 and/or 19 to 20 of a complement Factor H.
Cleaning device for cleaning a transparent element of an optical or optoelectronic device with a fluid cleaning agent, comprising a housing in which the device is arranged, with at least one fluid inlet arranged in the housing and at least one nozzle fed from the fluid inlet , wherein the nozzle is configured so as to direct a cleaning agent jet onto the transparent element , and wherein the jet direction of the cleaning agent jet is provided substantially transversely with respect to an optical axis of the transparent element , wherein the fluid inlet is configured for being flowed through by a cleaning liquid from a hydraulic channel and by compressed air from a pneumatic channel , wherein the hydraulic channel has a hydraulic check valve and the pneumatic channel has a pneumatic check valve , and the check valves open the channels in the direction of the nozzle and block in the opposite direction, characterized in that the pneumatic check valve and/or the hydraulic check valve is designed to be electrically controlled.
A method for manufacture of a composite blade with an airfoil and a root , the blade comprising a core of chopped fibre composite material and a textile composite material encasing the chopped fibre core, the method comprising: forming a blade insert using chopped fibre composite; surrounding the blade insert with a plurality of layers of a textile in a textile composite material ; and thermoforming the blade insert and the surrounding textile composite material in a thermoforming mould in order to consolidate the part, wherein the blade insert is situated at a location where the cross-sectional area of the blade changes significantly, wherein the blade insert is located at the root of the blade where the cross-section increases compared to the cross-section of the airfoil , and characterized in that the shape of the blade insert extends further toward the airfoil tip at its centre in a dorsal fin shape with the upper tip of the dorsal fin shape extending into the airfoil from the root along the centre line of the airfoil. forming a blade insert using chopped fibre composite; surrounding the blade insert with a plurality of layers of a textile in a textile composite material ; and thermoforming the blade insert and the surrounding textile composite material in a thermoforming mould in order to consolidate the part, wherein the blade insert is situated at a location where the cross-sectional area of the blade changes significantly, wherein the blade insert is located at the root of the blade where the cross-section increases compared to the cross-section of the airfoil , and characterized in that the shape of the blade insert extends further toward the airfoil tip at its centre in a dorsal fin shape with the upper tip of the dorsal fin shape extending into the airfoil from the root along the centre line of the airfoil. characterized in that the shape of the blade insert extends further toward the airfoil tip at its centre in a dorsal fin shape with the upper tip of the dorsal fin shape extending into the airfoil from the root along the centre line of the airfoil.
An absorbent article comprising, on a skin contact side thereof, a sheet having a region where, when rubbed under the conditions below, a friction coefficient or a mean deviation of the friction coefficient decreases by 5% or more or 15% or more, respectively, compared to before the rubbing, and having a longitudinal direction corresponding to a front-to-back direction of a wearer and a lateral direction perpendicular to the longitudinal direction, wherein the sheet is a three-dimensionally shaped laminate sheet composed of a skin contact side sheet and a non-skin contact side sheet , the skin contact side sheet and the non-skin contact side sheet being united to each other at a plurality of bonds , the skin contact side sheet forming a plurality of projections protruding away from the non-skin contact side sheet in portions other than the bonds , and the region being designed such that the skin contact side sheet and the non-skin contact side sheet peel from each other at the bond when rubbed, wherein the bond in the region comprises portions having different thicknesses, and peel-apart separation between the skin contact side sheet and the non-skin contact side sheet is designed to initiate from between the portions having different thicknesses by the rubbing: conditions: a wet collagen film is reciprocated 10 times on the sheet in the longitudinal direction of the sheet under a load of 3.0 kPa; and the wet collagen film has a water content of 100 to 150 mass% relative to a dry weight thereof and is prepared by immersing a collagen film in ion-exchanged water for 1 minute, taking out the collagen film, and removing excess water; wherein the friction coefficient and the mean deviation of the friction coefficient are measured according to the method of the description. conditions: a wet collagen film is reciprocated 10 times on the sheet in the longitudinal direction of the sheet under a load of 3.0 kPa; and the wet collagen film has a water content of 100 to 150 mass% relative to a dry weight thereof and is prepared by immersing a collagen film in ion-exchanged water for 1 minute, taking out the collagen film, and removing excess water; wherein the friction coefficient and the mean deviation of the friction coefficient are measured according to the method of the description.
Aircraft pylon fairing extending along a longitudinal axis and comprising a wall having at least two opposite flanks oriented respectively one on each side of said longitudinal axis , and a central interior cavity, the two opposite flanks meeting in the lower or upper part of said fairing , said fairing being such that it comprises: - a front transverse rib securely fixed to said wall and extending perpendicularly on each side of said longitudinal axis , said front transverse rib comprising a through opening configured to accept a peg of an exterior structure by push-fitting in a direction (X) parallel to said longitudinal axis , and comprising two yokes each having bores along a longitudinal axis oriented perpendicular to said longitudinal axis of the fairing and arranged facing a through opening in one of said opposing flanks , and - a rear transverse rib securely fixed to said wall and extending perpendicularly on each side of said longitudinal axis and comprising two yokes each having bores along a longitudinal axis oriented perpendicular to said longitudinal axis of the fairing and arranged facing a through opening in one of said opposing flanks . - a front transverse rib securely fixed to said wall and extending perpendicularly on each side of said longitudinal axis , said front transverse rib comprising a through opening configured to accept a peg of an exterior structure by push-fitting in a direction (X) parallel to said longitudinal axis , and comprising two yokes each having bores along a longitudinal axis oriented perpendicular to said longitudinal axis of the fairing and arranged facing a through opening in one of said opposing flanks , and - a rear transverse rib securely fixed to said wall and extending perpendicularly on each side of said longitudinal axis and comprising two yokes each having bores along a longitudinal axis oriented perpendicular to said longitudinal axis of the fairing and arranged facing a through opening in one of said opposing flanks .