mhurhangee/ep-ind-claims huggingface dataset:
A moisture curable polyorganosiloxane composition comprising: about 17 to about 40 mass%, based on the combined mass of components to, of a polyorganosiloxane represented by the following general formula: X-(SiR 11 2 O) m -SiR 11 2 -X wherein each R 11 is the same or different monovalent hydrocarbon group lacking an aliphatic unsaturated bond, each X is an alkoxysilyl-containing group, and "m" is an integer of from 20 to 1000; about 5 to about 30 mass%, based on the combined mass of components to, of a polyorganosiloxane resin having a content of OZ in a range of from about 50 mol% to about 150 mol%, wherein each Z is H or an alkyl group such that OZ represents a silanol group and/or a silicon atom-bonded alkoxy group, and represented by the following average unit formula: (R 21 3 SiO 1/2) c (R 21 2 SiO 2/2) d (R 21 SiO 3/2) e (SiO 4/2) f wherein each R 21 is the same or different monovalent hydrocarbon group, and "c", "d", "e" and "f" are numbers satisfied by the following conditions: 0 ≤ c < 0.2, 0 ≤ d ≤ 0.5, 0.4 < e ≤ 1.0, 0 ≤ f < 0.2, and c + d + e + f = 1; and about 40 to about 70 mass%, based on the combined mass of components to, of a polyorganosiloxane resin represented by the following average unit formula: (R 31 3 SiO 1/2) g (SiO 4/2) 1 wherein each R 31 is the same or different, and selected from a monovalent hydrocarbon group or X as described above, provided however, at least one R 31 is X per molecule, and "g" is a number of about 0.5 to about 1.5. about 17 to about 40 mass%, based on the combined mass of components to, of a polyorganosiloxane represented by the following general formula: X-(SiR 11 2 O) m -SiR 11 2 -X wherein each R 11 is the same or different monovalent hydrocarbon group lacking an aliphatic unsaturated bond, each X is an alkoxysilyl-containing group, and "m" is an integer of from 20 to 1000; about 5 to about 30 mass%, based on the combined mass of components to, of a polyorganosiloxane resin having a content of OZ in a range of from about 50 mol% to about 150 mol%, wherein each Z is H or an alkyl group such that OZ represents a silanol group and/or a silicon atom-bonded alkoxy group, and represented by the following average unit formula: (R 21 3 SiO 1/2) c (R 21 2 SiO 2/2) d (R 21 SiO 3/2) e (SiO 4/2) f wherein each R 21 is the same or different monovalent hydrocarbon group, and "c", "d", "e" and "f" are numbers satisfied by the following conditions: 0 ≤ c < 0.2, 0 ≤ d ≤ 0.5, 0.4 < e ≤ 1.0, 0 ≤ f < 0.2, and c + d + e + f = 1; and about 40 to about 70 mass%, based on the combined mass of components to, of a polyorganosiloxane resin represented by the following average unit formula: (R 31 3 SiO 1/2) g (SiO 4/2) 1 wherein each R 31 is the same or different, and selected from a monovalent hydrocarbon group or X as described above, provided however, at least one R 31 is X per molecule, and "g" is a number of about 0.5 to about 1.5.
A biaxially stretched article obtained by stretching a thermoplastic composition in a machine direction and a transverse direction at elevated temperature of 100 oC to 130 oC, said thermoplastic composition comprising: - a polyolefin phase containing at least one polyolefin, - a starch phase containing thermoplastic starch, - at least one compatibiliser, wherein the thermoplastic composition comprises - from 10 - 70 wt% of at least one polyolefin - from 10 - 70 wt% of thermoplastic starch - from 5 - 40 wt% of at least one compatibiliser the weight percentages being based on the weight of the thermoplastic composition, wherein the at least one polyolefin is selected from the group consisting of propylene homopolymers, ethylene propylene copolymers, polyethylene, high density polyethylene, medium density polyethylene, low density polyethylene, linear low density polyethylene and mixtures of at least two of the preceding polyolefins, wherein the article has a layered morphology with alternating layers of starch phase and polyolefin phase, said layers of starch phase and polyolefin phase extending in machine direction and transverse direction, and wherein the thermoplastic composition further comprises a thermoplastic polyester. - a polyolefin phase containing at least one polyolefin, - a starch phase containing thermoplastic starch, - at least one compatibiliser, wherein the thermoplastic composition comprises - from 10 - 70 wt% of at least one polyolefin - from 10 - 70 wt% of thermoplastic starch - from 5 - 40 wt% of at least one compatibiliser
Raised bed (100, 200) comprising at least one side wall (1.1, 1.2) extending in an upward direction and a longitudinal direction and a plurality of transverse struts extending in a transverse direction, in particular for supporting shelves (3.1), wherein the side wall (1.1, 1.2) comprises at longitudinal ends respectively an angled portion extending in the upward direction and the transverse direction for abutment against and connection with an angled portion of an adjacent side wall (1.1, 1.2) or end wall (2.1, 2.2), and wherein the angled portions have a plurality of recesses (5.1) distributed over the upward direction, and wherein receiving means for receiving a transverse strut is respectively arranged in at least one recess (5.1), characterized in that a transverse strut arranged at a receiving means rests on the receiving means in the upward direction, and in that the transverse strut comprises a first recess (9.3) for engaging behind the receiving means and is held with the first recess (9.3) in the transverse direction at the receiving means in a form-fitting manner at least away from the side wall (1.1, 1.2). wherein the side wall (1.1, 1.2) comprises at longitudinal ends respectively an angled portion extending in the upward direction and the transverse direction for abutment against and connection with an angled portion of an adjacent side wall (1.1, 1.2) or end wall (2.1, 2.2), and wherein the angled portions have a plurality of recesses (5.1) distributed over the upward direction, and wherein receiving means for receiving a transverse strut is respectively arranged in at least one recess (5.1), characterized in that a transverse strut arranged at a receiving means rests on the receiving means in the upward direction, and in that the transverse strut comprises a first recess (9.3) for engaging behind the receiving means and is held with the first recess (9.3) in the transverse direction at the receiving means in a form-fitting manner at least away from the side wall (1.1, 1.2).
A power supply module for a voltage supply device arranged in a vehicle, wherein the power supply module is constructed from a large number of structurally independent power supply cells, wherein the large number of power supply cells, stacked to form at least one row of cells, are arranged one behind another, wherein the power supply module cooperates with a temperature control means, wherein the temperature control means is designed to control the temperature of at least some of the power supply cells by means of a heating medium, with a bracing means (18, 18', 18") which is designed to brace the power supply cells of the at least one row of cells, wherein the bracing means (18, 18', 8") for this has at least two end plates (20, 20f, 20q, 20f, 20q') and a tensioning element (22, 22a, 22', 22a', 22", 22a"), wherein the at least two end plates (20, 20f, 20q, 20f, 20q') cooperate with the tensioning element (22, 22a, 22', 22a', 22", 22a") to form a bracing force acting on the power supply cells, wherein the tensioning element (22, 22a, 22', 22a', 22", 22a") is embodied as a functional component of the temperature control means and to this end has at least one infeed connection (26, 26a, 26b) for feeding heating medium into the tensioning element (22, 22a, 22', 22a', 22", 22a") and at least one discharge connection (28, 28a, 28b) for discharging the heating medium which has flowed through at least a partial region of the tensioning element (22, 22a, 22', 22a', 22", 22a"), characterised in that the tensioning element (22, 22a, 22', 22a', 22", 22a") is designed to be U-shaped or meandering and is constructed from at least one transverse element (42, 42a, 42*, 42a', 42", 42a") and at least two longitudinal elements (44, 44a, 44', 44a', 44", 44a"), produced monolithically with the transverse element (42, 42a, 42*, 42a', 42", 42a"), with in each case one end (46, 46a) on the transverse-element side and one free end (48, 48a), the infeed connection (26, 26a, 26b) and the discharge connection (28, 28a, 28b) being associated spatially with the free ends (48, 48a), the infeed connection (26, 26a, 26b) being associated with the free end (48, 48a) of the one longitudinal element (44, 44a, 44', 44a', 44", 44a") and the discharge connection (28, 28a, 28b) with the free end (48, 48a) of the other longitudinal element (44, 44a, 44', 44a', 44", 44a"), and the tensioning element (22, 22a, 22', 22a', 22", 22a") having at least one heating-medium channel (68, 68', 68") carrying the heating medium and connected to the infeed connection (26, 26a, 26b) and the discharge connection (28, 28a, 28b), which channel is designed such that it encompasses the row of cells along the two longitudinal elements (44, 44a, 44', 44a', 44", 44a") and the transverse element (42, 42a, 42*, 42a', 42", 42a").
A zinc finger protein that binds to an EPSPS target genomic region of interest, the ZFP comprising one or more zinc finger binding domains, wherein the ZFP comprises the recognition helix regions shown in a single row of Table A.
An axial fan comprising an essentially circular-cylindrical blower pipe configured about a centre axis and having an inner side and an outer side; and wherein the blower pipe is configured with a fan rotor, which fan rotor has a rotor shaft which essentially coincides with the centre axis of the circular-cylindrical blower pipe; and wherein the fan comprises one or more plates that are bent and subsequently joined at opposing plate rims for forming the circular-cylindrical blower pipe; and wherein the circular-cylindrical blower pipe has two opposing ends; wherein the blower pipe is, at least at its one end, bent outwards essentially at right angles to the outside of the blower pipe for forming a mounting flange on which means are provided for mounting of the axial fan in a tubing system, the plate or the plates comprised by the blower pipe comprises a rust-resistant metal plate or a steel plate which is coated with a rust-resistant material at least on the outside and the inside of the blower pipe; characterised in that the plate rims are joined in a rim-by-rim manner, without overlap, by soldering with a rust-resistant filler material.
An expandable cell matrix system for a mattress, pillow or cushion structure, comprising a plurality of cells; a port for introducing fluid into and withdrawing fluid from the plurality of cells; wherein the cell matrix system is formed by sealing together a plurality of sheets (150, 152, 164, 180) of material to form a mattress, pillow or cushion structure; wherein the plurality of cells creates an array of cells at least two of which are in fluid communication with each other to allow for introduction and withdrawal of fluid to the array of cells via the port; and characterized in that the cell matrix is manufactured using a continuous manufacturing process comprising creating a plurality of folds in the plurality of sheets (150, 152, 164, 180) of material and gusset sealing each fold combined with cross sealing, vertical sealing and/or donut sealing to create a cell shape; and in that the cell matrix is adapted to be stored in a substantially flat form when un-inflated; and wherein the cell matrix is adapted to provide support when inflated with a fluid. a plurality of cells; a port for introducing fluid into and withdrawing fluid from the plurality of cells; wherein the cell matrix system is formed by sealing together a plurality of sheets (150, 152, 164, 180) of material to form a mattress, pillow or cushion structure; wherein the plurality of cells creates an array of cells at least two of which are in fluid communication with each other to allow for introduction and withdrawal of fluid to the array of cells via the port; and characterized in that the cell matrix is manufactured using a continuous manufacturing process comprising creating a plurality of folds in the plurality of sheets (150, 152, 164, 180) of material and gusset sealing each fold combined with cross sealing, vertical sealing and/or donut sealing to create a cell shape; and in that the cell matrix is adapted to be stored in a substantially flat form when un-inflated; and wherein the cell matrix is adapted to provide support when inflated with a fluid.
Timepiece striking mechanism including a mechanism for controlling at least one hammer which includes a first striking area arranged to strike, in a first direction of travel, a first resonant component on a first striking surface when said at least one hammer moves from a recoiled position to a first impact position, wherein said at least one hammer includes, opposite to said first striking area, a second striking area arranged to strike, in a second direction of travel opposite to said first direction of travel, when said at least one hammer recoils from said first impact position to said recoiled position, a second striking surface included in said first resonant component, characterised in that when said first resonant component includes said second striking surface in immediate proximity to said first striking surface from which it is separated by the thickness of said first resonant component.
A method for launching an unmanned rotorcraft (1002, 902, 802) comprising a visual sensor (1305, 1405, 1505, 1705) and one or more rotor blades (201, 801, 901), said method comprising: (a) detecting, by the rotorcraft (1002, 902, 802), a visual signal (1310, 1410, 1510) generated by an operator (1001, 1301, 1401, 1501, 1601) of said rotorcraft (1002, 902, 802); and (b) detecting a release of grip of the unmanned rotorcraft (1002, 902, 802) by a hand (906, 1003); and (c) in response to the detected visual signal (1310, 1410, 1510) and the release of grip of the unmanned rotorcraft, activating the one or more rotor blades (201, 801, 901) to generate a lift and/or thrust. (a) detecting, by the rotorcraft (1002, 902, 802), a visual signal (1310, 1410, 1510) generated by an operator (1001, 1301, 1401, 1501, 1601) of said rotorcraft (1002, 902, 802); and (b) detecting a release of grip of the unmanned rotorcraft (1002, 902, 802) by a hand (906, 1003); and (c) in response to the detected visual signal (1310, 1410, 1510) and the release of grip of the unmanned rotorcraft, activating the one or more rotor blades (201, 801, 901) to generate a lift and/or thrust.
A disinfection system for a cabin of an aircraft, the disinfection system comprising: a stowable item; a housing defining a compartment within which the stowable item is configured to be at least partially retained, wherein the housing is a section of a cabin structure of the aircraft; an electromagnetic radiation source coupled to the housing and configured to operably emit disinfecting electromagnetic radiation to the compartment to deliver a disinfecting treatment to the stowable item; a controller electrically coupled to the electromagnetic radiation source, the controller comprising a processor and a tangible, non-transitory computer-readable storage medium having instructions stored thereon that, in response to execution by the processor, cause the processor to perform various operations comprising controlling, by the processor, emission of the disinfecting electromagnetic radiation; and a detector coupled to the housing and electrically coupled to the controller, the detector configured to determine, by the processor, at least one of a presence, a position, and an orientation of the stowable item, wherein controlling the emission of the disinfecting electromagnetic radiation is based on at least one of the presence, the position, and the orientation of the stowable item; characterized in that, the housing comprises a refractive material configured to direct emission of the disinfecting electromagnetic radiation. a stowable item; a housing defining a compartment within which the stowable item is configured to be at least partially retained, wherein the housing is a section of a cabin structure of the aircraft; an electromagnetic radiation source coupled to the housing and configured to operably emit disinfecting electromagnetic radiation to the compartment to deliver a disinfecting treatment to the stowable item; a controller electrically coupled to the electromagnetic radiation source, the controller comprising a processor and a tangible, non-transitory computer-readable storage medium having instructions stored thereon that, in response to execution by the processor, cause the processor to perform various operations comprising controlling, by the processor, emission of the disinfecting electromagnetic radiation; and a detector coupled to the housing and electrically coupled to the controller, the detector configured to determine, by the processor, at least one of a presence, a position, and an orientation of the stowable item, wherein controlling the emission of the disinfecting electromagnetic radiation is based on at least one of the presence, the position, and the orientation of the stowable item; characterized in that, the housing comprises a refractive material configured to direct emission of the disinfecting electromagnetic radiation.
Method for producing a housing of an energy collection device by means of additive manufacture, in particular by means of 3D dispensing, comprising at least the following method steps: a) producing a layer construction of the housing in a spatial direction, b) creating fixing regions for energy collection structures, bending beams, comb structures (80, 82) with at least one additional mass, separating levels and at least one printed circuit board by additive layer construction while carrying out method step a), c) materially joining the components, mentioned in method step b), in the fixing regions by arranging the components between UV-precrosslinked levels produced by additive layer construction and wet layers in the layer construction. a) producing a layer construction of the housing in a spatial direction, b) creating fixing regions for energy collection structures, bending beams, comb structures (80, 82) with at least one additional mass, separating levels and at least one printed circuit board by additive layer construction while carrying out method step a), c) materially joining the components, mentioned in method step b), in the fixing regions by arranging the components between UV-precrosslinked levels produced by additive layer construction and wet layers in the layer construction.
Booster assembly for a combustion engine, comprising an air-booster turbocompressor and a discharge valve (20, 21) of the turbocompressor, the discharge valve (20, 21) comprising a tilting arm (20, 21) and the booster assembly comprising an actuator having an actuation rod (10, 11, 12) connected to the tilting arm (20, 21) so that the actuation rod (10, 11, 12) drives the tilting arm (20, 21), the actuation rod (10, 11, 12) and the tilting arm (20, 21) being connected together by a pair consisting of a spindle hole and a spindle introduced into this spindle hole with a dimensional clearance of the spindle in the spindle hole, the booster assembly further comprising an elastic element (30, 40) exerting a force on the spindle so that the spindle is held in abutment against an internal wall of the spindle hole counter to a movement within the dimensional clearance, characterised in that an anchoring orifice is present in the spindle and the elastic element (30, 40) is anchored in the anchoring orifice.
A polarizing plate, comprising: a polarizing film in which a light absorption axis is formed in one in-plane direction; a protective film formed on only one side of the polarizing film; and a pressure-sensitive adhesive layer formed on the other side of the polarizing film, wherein the polarizing plate has a total thickness of 200 μm or less, wherein a ratio of a shrinkage force of the protective film in an in-plane direction perpendicular to the light absorption axis direction relative to a shrinkage force of the polarizing film in an in-plane direction parallel to the light absorption axis direction is in a range of 0.1 to 5; wherein a shrinkage force of the polarizing film in the light absorption axis direction is in a range of 8 N to 15 N per 5.3 mm width, wherein the shrinkage force is measured by means of a dynamic mechanical analysis instrument, wherein a specimen is produced to have a width of about 5.3 mm and a length of about 15 mm, and both ends of the specimen in the longitudinal direction are fixed to the clamp of the measuring instrument and then the contractile force is measured, wherein the length 15 mm of the specimen is the length excluding the portion to be fixed to the clamp, wherein after fixing the specimen to the clamp, the specimen is pulled and fixed to maintain strain 0.1 % in the state of preload ON, and then the shrinkage force applied when the strain 0.1 % is kept at an elevated temperature of 80 °C is measured 120 minutes after 80 °C stabilisation. a polarizing film in which a light absorption axis is formed in one in-plane direction; a protective film formed on only one side of the polarizing film; and a pressure-sensitive adhesive layer formed on the other side of the polarizing film, wherein the polarizing plate has a total thickness of 200 μm or less, wherein a ratio of a shrinkage force of the protective film in an in-plane direction perpendicular to the light absorption axis direction relative to a shrinkage force of the polarizing film in an in-plane direction parallel to the light absorption axis direction is in a range of 0.1 to 5; wherein a shrinkage force of the polarizing film in the light absorption axis direction is in a range of 8 N to 15 N per 5.3 mm width, wherein the shrinkage force is measured by means of a dynamic mechanical analysis instrument, wherein a specimen is produced to have a width of about 5.3 mm and a length of about 15 mm, and both ends of the specimen in the longitudinal direction are fixed to the clamp of the measuring instrument and then the contractile force is measured, wherein the length 15 mm of the specimen is the length excluding the portion to be fixed to the clamp, wherein after fixing the specimen to the clamp, the specimen is pulled and fixed to maintain strain 0.1 % in the state of preload ON, and then the shrinkage force applied when the strain 0.1 % is kept at an elevated temperature of 80 °C is measured 120 minutes after 80 °C stabilisation.
An optical component comprising: a substrate; and a metasurface disposed on the substrate, the metasurface comprising a plurality of repeating and adjacent tessellated grating unit cells which each comprise a grid of linearly birefringent elements, wherein the linearly birefringent elements of each tessellated grating unit cell diffract at least four different polarizations of incident light into four different directions, and characterized in that, in each tessellated grating unit cell, the angular orientation of at least one element of the linearly birefringent elements is different from another element of the linearly birefringent elements. a substrate; and a metasurface disposed on the substrate, the metasurface comprising a plurality of repeating and adjacent tessellated grating unit cells which each comprise a grid of linearly birefringent elements, wherein the linearly birefringent elements of each tessellated grating unit cell diffract at least four different polarizations of incident light into four different directions, and characterized in that, in each tessellated grating unit cell, the angular orientation of at least one element of the linearly birefringent elements is different from another element of the linearly birefringent elements.