mhurhangee/ep-ind-claims huggingface dataset:
Spray gun for the discharge of spray product, comprising a housing; a receiving installation for optionally receiving spray-product containers (32a, 32b) of dissimilar heights; a handle for holding the spray gun, and an extension installation, provided on the handle, for extending the length of the handle so as to adapt the length of the handle to the height (H1, H2) of a spray-product container (32a, 32b), disposed on the receiving installation, in such a manner that the handle and the spray-product container (32a, 32b) conjointly form a placement space for placing the spray gun, wherein the extension installation has at least one extension element (38; 60) that is fastened to the handle so as to be adjustable thereon in the longitudinal direction thereof, wherein a locking installation with the aid of which the extension element (38; 60) is lockable in a plurality of positions is provided, wherein the positions which are lockable with the aid of the locking installation are defined positions, characterized in that the locking installation has at least two toothed components (38, 52, 46, 50; 60, 62, 68, 70) that are specified such that said toothed components may be caused to mutually engage or disengage, and that said toothed components define the plurality of positions, wherein locking is performed in the engaged state of the toothed components (38, 52, 46, 50; 60, 62, 68, 70), wherein the locking installation has at least one spring element (43; 72) which biases the toothed components (38, 52, 46, 50; 60, 62, 68, 70) towards the engaged state of the latter, and wherein the biasing force of the at least one spring element is chosen to be so large that the locked position of the extension element. is maintained when the spray gun is placed, and chosen to be so small that the locking of the extension element is capable of being overcome by a manual force acting on the extension element.
A fuel supply system for a gaseous fuelled internal combustion engine comprising: a. a gaseous fuel supply conduit; b. a fuel injector for injecting gaseous fuel into said internal combustion engine, said fuel injector having a first body comprising an inlet, and a nozzle chamber fluidly connected to said inlet and from which said gaseous fuel is injected into said internal combustion engine, and comprising a needle and a seat, an injection valve seal formed when said needle abuts said seat; c. a second body formed for installation between and fluidly connecting said gaseous fuel supply conduit and a gaseous fuel flow passage of a predetermined volume through which said gaseous fuel supply conduit is connected to said nozzle chamber, said second body defining a restricted fluid flow passage for delivering said gaseous fuel to said nozzle chamber; wherein said restricted fluid flow passage is located a predetermined distance from said injection valve seal, said predetermined distance calculated as a function of the speed of sound in the gaseous fuel and an opened time of the fuel injector. a. a gaseous fuel supply conduit; b. a fuel injector for injecting gaseous fuel into said internal combustion engine, said fuel injector having a first body comprising an inlet, and a nozzle chamber fluidly connected to said inlet and from which said gaseous fuel is injected into said internal combustion engine, and comprising a needle and a seat, an injection valve seal formed when said needle abuts said seat; c. a second body formed for installation between and fluidly connecting said gaseous fuel supply conduit and a gaseous fuel flow passage of a predetermined volume through which said gaseous fuel supply conduit is connected to said nozzle chamber, said second body defining a restricted fluid flow passage for delivering said gaseous fuel to said nozzle chamber; wherein said restricted fluid flow passage is located a predetermined distance from said injection valve seal, said predetermined distance calculated as a function of the speed of sound in the gaseous fuel and an opened time of the fuel injector.
A video encoding apparatus for subjecting a video image to motion compensated encoding, the apparatus comprising: an acquisition module configured to acquire available blocks having motion vectors and number of the available blocks from encoded blocks adjacent to a to-be-encoded block; a selection module configured to select one available block from the available blocks; a selection information encoding module configured to select one selection code table from a plurality of code tables depending on the number of the available blocks and to encode selection information specifying the selected block using the selected code table, the selected code table having the same number of entries as the number of available blocks; and an image encoding module to subject the to-be-encoded block to a motion compensated prediction encoding using a motion vector of the selected block. an acquisition module configured to acquire available blocks having motion vectors and number of the available blocks from encoded blocks adjacent to a to-be-encoded block; a selection module configured to select one available block from the available blocks; a selection information encoding module configured to select one selection code table from a plurality of code tables depending on the number of the available blocks and to encode selection information specifying the selected block using the selected code table, the selected code table having the same number of entries as the number of available blocks; and an image encoding module to subject the to-be-encoded block to a motion compensated prediction encoding using a motion vector of the selected block.
Compressor rotor blade for a compressor of axial design, having a blade profile which has a transonic section, and a profile section of the blade profile, which profile section extends in the transonic section and, on its suction side, has a concave suction side region and a convex suction side region which is arranged downstream of the concave suction side region, and which, on its pressure side, has a convex pressure side region and a concave pressure side region which is arranged downstream of the convex pressure side region, characterized in that a curvature progression on the pressure side of the profile section and a curvature progression on the suction side of the profile section are constant in each case plotted over a profile chord of the profile section, in that the positions of the minimum values of the curvature progressions (27, 28) differ from one another by no more than 10% of the length of the profile chord, and the positions of the maximum values of the curvature progressions (27, 28) differ from one another by no more than 10% of the length of the profile chord, and in that the minimum values multiplied by the length of the profile chord are from - 1.2 to - 0.5, and the maximum values multiplied by the length of the profile chord are from 1.5 to 4.
Operating lever with corresponding link system, the link system having at least a first link part and restoring means which act on the at least one link part and transfer the latter into a zero position, and wherein the operating lever is guided in the link system, the first link part being mounted movably such that a change in position of the operating lever relative to the link system results in a movement of the at least one link part in the direction of the restoring means acting on the at least one link part, wherein the link system has at least a first link part and a second link part, which are movably mounted in such a way that a change in position of the operating lever relative to the link system results in the two link parts (3, 4) moving apart perpendicular to the pivoting plane, wherein the link parts (3, 4) have recesses which together form a link in which the operating lever is guided, characterized in that the width of the link in the region of the zero position of the operating lever is designed to decrease in the radial direction with respect to the pivoting movement of the operating lever with increasing distance from the latter, so that pressing the operating lever in the radial direction with respect to the pivoting movement results in the two link parts (3, 4) moving apart.
A silicone resin comprising constitutional units represented by the compositional formula and having a weight average molecular weight of 3,000 to 500,000, containing (A-1) a first silicone resin having a silicone content of 10 to 40% by weight of the first silicone resin, and (A-2) a second silicone resin having a silicone content of 50 to 80% by weight of the second silicone resin, the weight content of first silicone resin (A-1) being 10 to 50% by weight of the total weight of the silicone resin, wherein R 1 to R 4 are each independently a monovalent C 1 -C 8 hydrocarbon group, excluding that R 3 and R 4 are methyl at the same time, m and n each are an integer of 0 to 300, a and b are positive numbers, a+b = 1, X is a divalent linking group having the general formula or, c indicative of moles of the group of formula and d indicative of moles of the group of formula are in the range of 0/1 ≤ d/c ≤ 1/1, wherein V is a divalent organic group selected from the following: p is 0 or 1, R 5 is hydrogen or methyl, f is an integer of 0 to 7, R 6 and R 7 are each independently C 1 -C 4 alkyl or alkoxy, h is 0, 1 or 2, wherein R 3 and R 4 are each independently a monovalent C 1 -C 8 hydrocarbon group, excluding that R 3 and R 4 are methyl at the same time, q and r each are an integer of 0 to 300, R 8 is hydrogen or methyl, and k is an integer of 0 to 7. wherein R 1 to R 4 are each independently a monovalent C 1 -C 8 hydrocarbon group, excluding that R 3 and R 4 are methyl at the same time, m and n each are an integer of 0 to 300, a and b are positive numbers, a+b = 1, X is a divalent linking group having the general formula or, c indicative of moles of the group of formula and d indicative of moles of the group of formula are in the range of 0/1 ≤ d/c ≤ 1/1, wherein V is a divalent organic group selected from the following: p is 0 or 1, R 5 is hydrogen or methyl, f is an integer of 0 to 7, R 6 and R 7 are each independently C 1 -C 4 alkyl or alkoxy, h is 0, 1 or 2, wherein R 3 and R 4 are each independently a monovalent C 1 -C 8 hydrocarbon group, excluding that R 3 and R 4 are methyl at the same time, q and r each are an integer of 0 to 300, R 8 is hydrogen or methyl, and k is an integer of 0 to 7.
An armored vehicle turret able to accommodate a crew including a shooter, comprising a fixed roof with an opening and a retractable protection system in the form of an armored cover or dome, able to be moved pivotably around a horizontal axis and/or in vertical translation, characterized in that: - the retractable armored cover or dome can assume at least four positions, a first position in which the retractable system is retracted against the roof and provides closing of the opening, a second partial opening position in which the retractable system is partially deployed in upward vertical translation and makes it possible to protect a soldier in the observation position, a third partial opening position in which the retractable system is partially deployed in upward vertical translation, but more than in the second position, and makes it possible to protect a soldier in the sniper position, and a fourth complete opening position in which the retractable system is fully deployed by pivoting and/or upward vertical translation while exposing the opening in order to allow an evacuation of the crew; - the turret is provided with a mechanism ensuring, during use and depending on the needs, the movement of the retractable protection system between the aforementioned four positions and in the second position, the retractable dome exposes a lateral peripheral space closed off by protective plates with murder holes, allowing the soldier to assume an observation position of up to 360°. - the retractable armored cover or dome can assume at least four positions, a first position in which the retractable system is retracted against the roof and provides closing of the opening, a second partial opening position in which the retractable system is partially deployed in upward vertical translation and makes it possible to protect a soldier in the observation position, a third partial opening position in which the retractable system is partially deployed in upward vertical translation, but more than in the second position, and makes it possible to protect a soldier in the sniper position, and a fourth complete opening position in which the retractable system is fully deployed by pivoting and/or upward vertical translation while exposing the opening in order to allow an evacuation of the crew; - the turret is provided with a mechanism ensuring, during use and depending on the needs, the movement of the retractable protection system between the aforementioned four positions and in the second position, the retractable dome exposes a lateral peripheral space closed off by protective plates with murder holes, allowing the soldier to assume an observation position of up to 360°.
A method of allocating one or more uplink radio resources in a mobile communication system, the method comprising: allocating the uplink radio resources for a terminal before the terminal transmits a measurement report; transmitting information related to the allocated uplink radio resources to the terminal, wherein the information is measurement control information and the measurement control information is transmitted using a system information block 11, SIB 11, or a system information block 12, SIB 12; receiving the measurement report from the terminal that used the allocated uplink radio resources to transmit the measurement report, determining a type of the measurement report transmitted by the terminal; and transmitting information related to optimized uplink radio resources to the terminal based on the determined type of the measurement report, wherein the information related to the optimized uplink radio resources includes certain information within a preamble of a random access channel, RACH, and wherein a priority for traffic data and the measurement report is assigned based on the type of the measurement report. allocating the uplink radio resources for a terminal before the terminal transmits a measurement report; transmitting information related to the allocated uplink radio resources to the terminal, wherein the information is measurement control information and the measurement control information is transmitted using a system information block 11, SIB 11, or a system information block 12, SIB 12; receiving the measurement report from the terminal that used the allocated uplink radio resources to transmit the measurement report, determining a type of the measurement report transmitted by the terminal; and transmitting information related to optimized uplink radio resources to the terminal based on the determined type of the measurement report, wherein the information related to the optimized uplink radio resources includes certain information within a preamble of a random access channel, RACH, and wherein a priority for traffic data and the measurement report is assigned based on the type of the measurement report.
Electric motor having an inner stator and an outer rotor, which outer rotor has a rotor housing and a plurality of magnets and is formed for rotation about a rotation axis, which magnets are in the form of bar magnets, which rotor housing has an inner surface, a first end and a second end opposite the first end, which inner surface has receiving surfaces for receiving the magnets, which receiving surfaces each serve to arrange one of the magnets, and which magnets are each fixed to one of the receiving surfaces with the aid of an adhesive fixing means, characterized in that a first bearing seat for receiving a first bearing cage is formed at the second end of the rotor housing, which rotor housing has a first rotor housing portion with an inner diameter at the second end, which inner diameter is smaller than the inner diameter of the rotor housing in a second rotor housing portion in which the magnets are fixed, thereby forming the rotor seat at the second end, and that the receiving surfaces each have a groove-like recess, the groove-like recesses extend in a direction parallel to the rotation axis and the groove-like recesses have a first length in the direction parallel to the rotation axis which is greater than a second length of the plurality of magnets extending in the direction parallel to the rotation axis, so that an excess adhesive fastener can collect in the recess in the areas not covered by the bar magnets, without a planar fixing of the bar magnet to the magnet seat being cancelled out by the excess adhesive fastener.
Process for preparing aminomethylated bead polymers, characterized in that a) monomer droplets composed of a mixture comprising at least one monovinylaromatic compound, at least one polyvinylaromatic compound and at least one initiator are converted to a bead polymer and b) the bead polymer from step a) is reacted with compounds of the formula or salts thereof where R 1 = C 1 -C 3 -alkyl or H and compounds of the formula where n = 2 to 100, in the presence of aliphatic saturated or unsaturated carboxylic anhydrides or in the presence of mixtures of aliphatic saturated or unsaturated carboxylic anhydrides and at least one aliphatic saturated or unsaturated carboxylic acid, and in the presence of at least one Friedel-Crafts catalyst, to give a phthalimidomethylated bead polymer, and the amount of the compounds of the formula and of the formula used, the bead polymer, and the aliphatic saturated or unsaturated carboxylic anhydrides, Friedel-Crafts catalysts and any carboxylic acids together in the reaction mixture is greater than 80% by weight based on the total amount of the reaction mixture, and c) the phthalimidomethylated bead polymer is hydrolysed to give an aminomethylated bead polymer. a) monomer droplets composed of a mixture comprising at least one monovinylaromatic compound, at least one polyvinylaromatic compound and at least one initiator are converted to a bead polymer and b) the bead polymer from step a) is reacted with compounds of the formula or salts thereof where R 1 = C 1 -C 3 -alkyl or H and compounds of the formula where n = 2 to 100, in the presence of aliphatic saturated or unsaturated carboxylic anhydrides or in the presence of mixtures of aliphatic saturated or unsaturated carboxylic anhydrides and at least one aliphatic saturated or unsaturated carboxylic acid, and in the presence of at least one Friedel-Crafts catalyst, to give a phthalimidomethylated bead polymer, and the amount of the compounds of the formula and of the formula used, the bead polymer, and the aliphatic saturated or unsaturated carboxylic anhydrides, Friedel-Crafts catalysts and any carboxylic acids together in the reaction mixture is greater than 80% by weight based on the total amount of the reaction mixture, and c) the phthalimidomethylated bead polymer is hydrolysed to give an aminomethylated bead polymer.
A method of controlling landing of an aerostat with a computerized flight controller, the aerostat being attached to a ground station with one or more tethers, the method comprising: (a) retracting the one or more tethers to bring the aerostat toward the ground station during a descend phase; (b) upon sensing that the aerostat has reached a specified altitude, automatically transitioning the flight controller to a capture mode during which the ground station makes physical contact with the aerostat and/or bridles attached to the aerostat; (c) after sensing initial contact of the ground station with the aerostat and/or bridles attached to the aerostat, automatically transitioning the flight controller to a dock mode during which the aerostat is moved from an initial ground station contact position to a docked position on a cradle of the ground station. (a) retracting the one or more tethers to bring the aerostat toward the ground station during a descend phase; (b) upon sensing that the aerostat has reached a specified altitude, automatically transitioning the flight controller to a capture mode during which the ground station makes physical contact with the aerostat and/or bridles attached to the aerostat; (c) after sensing initial contact of the ground station with the aerostat and/or bridles attached to the aerostat, automatically transitioning the flight controller to a dock mode during which the aerostat is moved from an initial ground station contact position to a docked position on a cradle of the ground station.
An apparatus for reducing jet noise generated by a gas turbine engine exhaust plume, the apparatus comprising: a variable geometry gas turbine engine nozzle comprising a circumferentially distributed array of nozzle flap panels supported for alternate collective splaying and gathering motion, the collective splaying motion of the flap panels being from a narrow position defining a minimum cross-sectional area at a nozzle exit plane, to a wide position defining a maximum cross-sectional area at the nozzle exit plane; a plurality of nozzle seal panels supported in a circumferentially distributed array within the array of nozzle flap panels; and said apparatus being characterized by: a seal panel actuator operatively engageable with at least one seal panel of the array of nozzle seal panels and configured to deflect the at least one seal panel radially inward toward a fully deployed position to reduce jet noise by increasing exhaust stream mixing with ambient air. a variable geometry gas turbine engine nozzle comprising a circumferentially distributed array of nozzle flap panels supported for alternate collective splaying and gathering motion, the collective splaying motion of the flap panels being from a narrow position defining a minimum cross-sectional area at a nozzle exit plane, to a wide position defining a maximum cross-sectional area at the nozzle exit plane; a plurality of nozzle seal panels supported in a circumferentially distributed array within the array of nozzle flap panels; and said apparatus being characterized by: a seal panel actuator operatively engageable with at least one seal panel of the array of nozzle seal panels and configured to deflect the at least one seal panel radially inward toward a fully deployed position to reduce jet noise by increasing exhaust stream mixing with ambient air.
Stackable crate made of cardboard and comprising two side walls which are connected to a front wall and have an outer edge which slopes in relation to the lower front wall from an engaging protrusion which projects vertically and corresponds to a base recess, wherein the sloping outer edges and the connected engaging protrusions are reinforced by inwardly folded adhesive tabs (12, 13) which, in the flat blank, leave free therebetween a gusset which tapers in relation to the transition between the engaging protrusion and the sloping outer edge, characterised in that the adhesive tabs (12, 13) for the sloping outer edge on the one hand and the connected engaging protrusion on the other hand are connected on the side opposite the tip of the gusset by an edge web to form a common fold-in tab, and in that the edge web forms two folding lines starting from the corners of the remaining triangular gusset recess for the counter-directional folding-in of the edge web in relation to the two portions of the fold-in tab producing the adhesive tabs (12, 13).