mhurhangee/ep-ind-claims huggingface dataset:
A multi-beam antenna, MBA, system for a spacecraft, the MBA system including: a reflector; and a feed array of radiating feed elements configured as a phased array and illuminating the reflector, operable at a frequency having a characteristic wavelength, the feed array including a plurality of interchangeable modules, wherein: each of the plurality of interchangeable modules includes a first distal mounting panel and a proximal mounting panel, and at least six feed array elements; each feed array element is electrically coupled with a respective amplifier and mechanically coupled with an exterior surface of the first distal mounting panel; the respective amplifiers are thermally coupled with the proximal mounting panel and are coupled with an interior surface of the first distal mounting panel and an exterior surface of the proximal mounting panel; and an interior surface of the proximal mounting panel of each interchangeable module is mechanically and thermally coupled with a back plate. a reflector; and a feed array of radiating feed elements configured as a phased array and illuminating the reflector, operable at a frequency having a characteristic wavelength, the feed array including a plurality of interchangeable modules, wherein: each of the plurality of interchangeable modules includes a first distal mounting panel and a proximal mounting panel, and at least six feed array elements; each feed array element is electrically coupled with a respective amplifier and mechanically coupled with an exterior surface of the first distal mounting panel; the respective amplifiers are thermally coupled with the proximal mounting panel and are coupled with an interior surface of the first distal mounting panel and an exterior surface of the proximal mounting panel; and an interior surface of the proximal mounting panel of each interchangeable module is mechanically and thermally coupled with a back plate. each of the plurality of interchangeable modules includes a first distal mounting panel and a proximal mounting panel, and at least six feed array elements; each feed array element is electrically coupled with a respective amplifier and mechanically coupled with an exterior surface of the first distal mounting panel; the respective amplifiers are thermally coupled with the proximal mounting panel and are coupled with an interior surface of the first distal mounting panel and an exterior surface of the proximal mounting panel; and an interior surface of the proximal mounting panel of each interchangeable module is mechanically and thermally coupled with a back plate.
An apparatus for reducing the high transient mount load from an aircraft engine, the apparatus including an isolator housing (400, 600) filled with a material capable of flexibly accommodating dynamic load movement from the aircraft engine, the isolator housing having a through-hole to receive a yoke bolt therethrough, the through-hole having a through-hole axis, the isolator housing comprising: a first wall having a first opening; and a second wall opposite the first wall, having a second opening coaxial with the first opening; wherein the first opening and the second opening provide the through-hole; and the first opening and second opening each have a cross section that is continuous and substantially semi-circular according to a minor axis (406, 502) on a first half and substantially oval shaped having a major axis (408,504) on a second half, such that, when mounted to a circular engine mount frame, the major axes are oriented to align substantially tangentially with the circular engine mount frame, in a direction opposite to a direction of rotation of engine fan blades. a first wall having a first opening; and a second wall opposite the first wall, having a second opening coaxial with the first opening; wherein the first opening and the second opening provide the through-hole; and the first opening and second opening each have a cross section that is continuous and substantially semi-circular according to a minor axis (406, 502) on a first half and substantially oval shaped having a major axis (408,504) on a second half, such that, when mounted to a circular engine mount frame, the major axes are oriented to align substantially tangentially with the circular engine mount frame, in a direction opposite to a direction of rotation of engine fan blades.
An electronic apparatus comprising: a first integrated circuit semiconductor die (511, 611) including a first portion (501, 601a) of a first signal conditioning circuit integrated within the first integrated circuit semiconductor die (511, 611) and disposed along a first signal path, the first integrated circuit semiconductor die (511, 611) derived from a first semiconductor wafer that is comprised of one of silicon, silicon-germanium, gallium arsenide, indium phosphide, and gallium nitride; a second integrated circuit semiconductor die (512, 612) including a second portion (505, 605) of the first signal conditioning circuit integrated within the second integrated circuit semiconductor die (512, 612) and disposed along the first signal path for performing a first signal conditioning function along with the first portion (501, 601a) of the first signal conditioning circuit for a signal propagating along the first signal path, the second integrated circuit semiconductor die (512, 612) derived from a second semiconductor wafer that is comprised of a different one of silicon, silicon-germanium, gallium arsenide, indium phosphide, and gallium nitride; and a substrate for supporting the first and second integrated circuit semiconductor dies and for providing electrical connection to and from the first and second integrated circuit semiconductor dies. a first integrated circuit semiconductor die (511, 611) including a first portion (501, 601a) of a first signal conditioning circuit integrated within the first integrated circuit semiconductor die (511, 611) and disposed along a first signal path, the first integrated circuit semiconductor die (511, 611) derived from a first semiconductor wafer that is comprised of one of silicon, silicon-germanium, gallium arsenide, indium phosphide, and gallium nitride; a second integrated circuit semiconductor die (512, 612) including a second portion (505, 605) of the first signal conditioning circuit integrated within the second integrated circuit semiconductor die (512, 612) and disposed along the first signal path for performing a first signal conditioning function along with the first portion (501, 601a) of the first signal conditioning circuit for a signal propagating along the first signal path, the second integrated circuit semiconductor die (512, 612) derived from a second semiconductor wafer that is comprised of a different one of silicon, silicon-germanium, gallium arsenide, indium phosphide, and gallium nitride; and a substrate for supporting the first and second integrated circuit semiconductor dies and for providing electrical connection to and from the first and second integrated circuit semiconductor dies.
Cosmetic composition for making up and/or caring for the lips, which is in the form of a liquid emulsion, having a viscosity at 25°C between 0.05 and 8 Pa.s, comprising: a) at least 8% by weight, relative to the total weight of the composition, of one or more non-volatile oils, chosen from phenylated non-volatile silicone oils, from polar non-volatile hydrocarbon-based oils, and also mixtures thereof b) 3 to 5 % by weight of active substance, relative to the total weight of the composition, of at least one film-forming agent chosen from vinyl polymers comprising at least one carbosiloxane dendrimer-based unit chosen from vinyl polymer containing at least one carbosiloxane dendrimer-based unit having a molecular side chain containing a carbosiloxane dendrimer structure, and being the product of polymerization of: from 0 to 99.9 parts by weight of a vinyl monomer; and from 100 to 0.1 parts by weight of a carbosiloxane dendrimer of formula represented by one of the following formulae: c) at least 10% by weight of water relative to the total weight of the composition, d) at least one coloring material. a) at least 8% by weight, relative to the total weight of the composition, of one or more non-volatile oils, chosen from phenylated non-volatile silicone oils, from polar non-volatile hydrocarbon-based oils, and also mixtures thereof b) 3 to 5 % by weight of active substance, relative to the total weight of the composition, of at least one film-forming agent chosen from vinyl polymers comprising at least one carbosiloxane dendrimer-based unit chosen from vinyl polymer containing at least one carbosiloxane dendrimer-based unit having a molecular side chain containing a carbosiloxane dendrimer structure, and being the product of polymerization of: from 0 to 99.9 parts by weight of a vinyl monomer; and from 100 to 0.1 parts by weight of a carbosiloxane dendrimer of formula represented by one of the following formulae: from 0 to 99.9 parts by weight of a vinyl monomer; and from 100 to 0.1 parts by weight of a carbosiloxane dendrimer of formula represented by one of the following formulae: c) at least 10% by weight of water relative to the total weight of the composition, d) at least one coloring material.
A light emitting device, comprising: - a first light emitting diode; and - a surface-modified luminophore configured to absorb light emitted from the first light emitting diode and configured to emit light having a different wavelength from the absorbed light, the surface-modified luminophore comprising: - a silicate luminophore; and - a fluorinated coating arranged on the silicate luminophore wherein the silicate luminophore comprises an alkaline earth metal silicate luminophore, wherein the fluorinated coating comprises a fluorinated barrier layer formed by fluorinating the alkaline earth metal silicate luminophore using fluorine - functionalized organosilane comprising the general formula Si 3 X where R = CH 3, C 2 H 5, or higher alkanes, and X comprises a fluorine-functionalized organic ligand, and wherein the fluorinated coating is configured to generate hydrophobic surface sitesand, wherein the surface-modified luminophore further comprises a moisture barrier layer comprising an oxide arranged on the fluorinated coating or arranged between the fluorinated coating and the silicate luminophore. - a first light emitting diode; and - a surface-modified luminophore configured to absorb light emitted from the first light emitting diode and configured to emit light having a different wavelength from the absorbed light, the surface-modified luminophore comprising: - a silicate luminophore; and - a fluorinated coating arranged on the silicate luminophore - a silicate luminophore; and - a fluorinated coating arranged on the silicate luminophore
Method for manufacturing containers filled with a liquid filling material out of preforms made of a thermoplastic material, wherein the respective preform is thermally conditioned and then formed into the container within a mould during a forming and filling phase, thereby being filled with at least one liquid filling material (21, 21.1) as a pressure medium at a filling pressure p 2, characterized in that the filling material (21, 21.1) or proportions of the filling material (21, 21.1) are supplied in at least two process phases with different levels of carbon dioxide and/or at different temperatures, wherein the container formed during the first process phase relieves the filling pressure p 2 to attain a pressure p 1, and filling material is supplied during the second process phase, after which the container is relieved to attain atmospheric pressure p 0 and wherein, during the first process phase, previously degassed water is supplied as filling material.
A seismic sensor (100, 200) for a seismic survey, the seismic sensor (100, 200) comprising: an outer housing (101, 201) having a central axis (105, 205), a first end (101a, 201a), and a second end (101b, 201b) opposite the first end (101a, 201a); a proof mass (170, 190, 195; 190 263, 290) moveably disposed in the outer housing (101, 201), wherein the proof mass (170, 190, 195; 190 263, 290) includes a power source; a sensor element disposed in the outer housing (101, 201) and configured to detect the movement of the outer housing (101, 201) relative to the proof mass (170, 190, 195; 190 263, 290); and electronic circuitry coupled to the sensor element and the power source, the electronic circuitry being configured to emit light; characterized in that the first end (101a, 201a) comprises a portion (120, 221) made of a clear material configured to transmit light having a frequency in the visible or infrared range of the electromagnetic spectrum, wherein the seismic sensor (100, 200) further comprises a light guide assembly (127, 143; 228) having a first end (127a, 228b) adjacent the clear portion (120, 221) of the first end (101a, 201a) of the outer housing (101, 201) and a second end (143a, 228a) adjacent the electronic circuitry, wherein the light guide assembly (127, 143; 228) is configured to transmit light in an axial direction between the first end (127a, 228b) of the light guide assembly and the clear portion (120, 221) and to transmit light in a non-axial direction between the second end (143a, 228a) of the light guide assembly (127, 143; 228) and the electronic circuitry. an outer housing (101, 201) having a central axis (105, 205), a first end (101a, 201a), and a second end (101b, 201b) opposite the first end (101a, 201a); a proof mass (170, 190, 195; 190 263, 290) moveably disposed in the outer housing (101, 201), wherein the proof mass (170, 190, 195; 190 263, 290) includes a power source; a sensor element disposed in the outer housing (101, 201) and configured to detect the movement of the outer housing (101, 201) relative to the proof mass (170, 190, 195; 190 263, 290); and electronic circuitry coupled to the sensor element and the power source, the electronic circuitry being configured to emit light; characterized in that the first end (101a, 201a) comprises a portion (120, 221) made of a clear material configured to transmit light having a frequency in the visible or infrared range of the electromagnetic spectrum, wherein the seismic sensor (100, 200) further comprises a light guide assembly (127, 143; 228) having a first end (127a, 228b) adjacent the clear portion (120, 221) of the first end (101a, 201a) of the outer housing (101, 201) and a second end (143a, 228a) adjacent the electronic circuitry, wherein the light guide assembly (127, 143; 228) is configured to transmit light in an axial direction between the first end (127a, 228b) of the light guide assembly and the clear portion (120, 221) and to transmit light in a non-axial direction between the second end (143a, 228a) of the light guide assembly (127, 143; 228) and the electronic circuitry.
A method for manufacturing a tower structure, the method comprising: printing, via an additive printing device, a plurality of concentric sections of the tower structure of the wind turbine, wherein an inner section of the plurality of concentric sections defines a locking flange extending outward along a radial direction from a radially outer surface and an adjacent outer section of the plurality of concentric sections defines an elongated recess extending along a vertical direction on a radially inner surface, the locking flange being positioned within the elongated recess after printing; raising the inner section of the plurality of concentric sections to position a bottom portion of the inner section proximate a top portion of an adjacent outer section of the plurality of concentric sections, by sliding the locking flange within the elongated recess; rotating the inner section of the plurality of concentric sections after raising the inner section such that the locking flange is no longer aligned with the elongated recess; and joining the inner section of the plurality of concentric sections to the adjacent outer section of the plurality of concentric sections. printing, via an additive printing device, a plurality of concentric sections of the tower structure of the wind turbine, wherein an inner section of the plurality of concentric sections defines a locking flange extending outward along a radial direction from a radially outer surface and an adjacent outer section of the plurality of concentric sections defines an elongated recess extending along a vertical direction on a radially inner surface, the locking flange being positioned within the elongated recess after printing; raising the inner section of the plurality of concentric sections to position a bottom portion of the inner section proximate a top portion of an adjacent outer section of the plurality of concentric sections, by sliding the locking flange within the elongated recess; rotating the inner section of the plurality of concentric sections after raising the inner section such that the locking flange is no longer aligned with the elongated recess; and joining the inner section of the plurality of concentric sections to the adjacent outer section of the plurality of concentric sections.
A tension measurement system for measuring a tension force in a cable comprising: a sheave comprising a first radius and a second radius, the sheave configured to rotate about an axis to orient the first radius or the second radius toward the cable; an adjustable support comprising a first end to mount the sheave and a second end to control movement of the first end relative to the cable; and a plurality of tensioners configured to engage with the cable to provide a contact force between the sheave and the cable when the adjustable support positions the sheave adjacent to the cable. a sheave comprising a first radius and a second radius, the sheave configured to rotate about an axis to orient the first radius or the second radius toward the cable; an adjustable support comprising a first end to mount the sheave and a second end to control movement of the first end relative to the cable; and a plurality of tensioners configured to engage with the cable to provide a contact force between the sheave and the cable when the adjustable support positions the sheave adjacent to the cable.
A mobile vacuum cleaning device comprising a vacuum cleaner having an intake air inlet, an exhaust air outlet and a particle separator, the device further comprising • a housing containing said vacuum cleaner and having an aperture to allow either a suction hose or a connection therefor to be led therethrough and coupled to said intake air inlet of the vacuum cleaner and at least one opening to direct air exhausted by the exhaust air outlet of the vacuum cleaner out of the housing, at least one portion of the housing being separable from the rest of the housing in order to uncover an opening for providing access to the interior of the housing, • a suction hose connected to either the intake air inlet of the vacuum cleaner or said connection, said housing having members making it movable, and • a trolley carrying said housing and provided with said members, such as wheels, for moving said housing, characterized in that said trolley has means configured to receive and contain equipment and utensils useful for cleaning work and expendable supplies associated with such work, such as soap, toilet paper, etc, and that said suction hose is extraordinary long and has a length of at least 3 meters counted from said aperture of the housing. • a housing containing said vacuum cleaner and having an aperture to allow either a suction hose or a connection therefor to be led therethrough and coupled to said intake air inlet of the vacuum cleaner and at least one opening to direct air exhausted by the exhaust air outlet of the vacuum cleaner out of the housing, at least one portion of the housing being separable from the rest of the housing in order to uncover an opening for providing access to the interior of the housing, • a suction hose connected to either the intake air inlet of the vacuum cleaner or said connection, said housing having members making it movable, and • a trolley carrying said housing and provided with said members, such as wheels, for moving said housing, characterized in that said trolley has means configured to receive and contain equipment and utensils useful for cleaning work and expendable supplies associated with such work, such as soap, toilet paper, etc, and that said suction hose is extraordinary long and has a length of at least 3 meters counted from said aperture of the housing.
An extruded thermoplastic composition comprising: a) from 20 wt % to 75 wt % of a ceramic fiber component; b) from 15 wt % to 70 wt % of a polybutylene terephthalate component comprising a high molecular weight PBT and a low molecular weight PBT; c) from 5 wt % to 23 wt % of a polycarbonate component; and d) from 1 wt % to 10 wt % of a compatibilizer component, wherein the extruded thermoplastic composition is extruded under conditions that apply a specific energy of less than 90 W-Hr/kg to the extruded thermoplastic composition, the high molecular weight PBT has a Mw of greater than 100,000 grams per mole (g/mol) and the low molecular weight PBT has a Mw of less than 70,000 g/mol, molecular weight is determined by gel permeation chromatography, the combined weight percent value of all components does not exceed 100 wt %, and all weight percent values are based on the total weight of the extruded thermoplastic composition. a) from 20 wt % to 75 wt % of a ceramic fiber component; b) from 15 wt % to 70 wt % of a polybutylene terephthalate component comprising a high molecular weight PBT and a low molecular weight PBT; c) from 5 wt % to 23 wt % of a polycarbonate component; and d) from 1 wt % to 10 wt % of a compatibilizer component, the extruded thermoplastic composition is extruded under conditions that apply a specific energy of less than 90 W-Hr/kg to the extruded thermoplastic composition, the high molecular weight PBT has a Mw of greater than 100,000 grams per mole (g/mol) and the low molecular weight PBT has a Mw of less than 70,000 g/mol, molecular weight is determined by gel permeation chromatography, the combined weight percent value of all components does not exceed 100 wt %, and all weight percent values are based on the total weight of the extruded thermoplastic composition.
Method to provide a winding structure for an electrical machine using the needle winding technique, the method comprising: - winding in a first direction a number of coil-forming loops around a first tooth group (5,4,3) resulting in a first partial coil; - leading the coil-forming wire to bypass an odd number of teeth (6,7,8); - winding in the same direction a predetermined number of coil-forming loops around another tooth group (9,10,11) resulting in another partial coil; - optionally, repeating once or multiple times the previous two steps; - connecting the first partial coil to a corresponding commutator hook and connecting the last partial coil to a corresponding commutator hook (1,7); - repeating the aforementioned steps, beginning with a tooth group (10,9,8) following the last tooth group wrapped or provided with windings in the previous step until a uniform coil configuration is obtained in at least all tooth groups, wherein the adjacent partial coils (10,9,8; 9,10,11) do not lie directly on top of one another. - winding in a first direction a number of coil-forming loops around a first tooth group (5,4,3) resulting in a first partial coil; - leading the coil-forming wire to bypass an odd number of teeth (6,7,8); - winding in the same direction a predetermined number of coil-forming loops around another tooth group (9,10,11) resulting in another partial coil; - optionally, repeating once or multiple times the previous two steps; - connecting the first partial coil to a corresponding commutator hook and connecting the last partial coil to a corresponding commutator hook (1,7); - repeating the aforementioned steps, beginning with a tooth group (10,9,8) following the last tooth group wrapped or provided with windings in the previous step until a uniform coil configuration is obtained in at least all tooth groups, wherein the adjacent partial coils (10,9,8; 9,10,11) do not lie directly on top of one another.