mhurhangee/ep-ind-claims huggingface dataset:
A precision approach path indicator (PAPI, 100) comprising: - a first artificial light source comprising a plurality of semiconductor emitters (11, 12, 13), - a second artificial light source comprising a plurality of semiconductor emitters, - a first planar reflector for guiding light (L 1) received from the first artificial light source as output of the PAPI, - a second planar reflector for guiding light (L 2) received from the second artificial light source as output of the PAPI, - a first concave reflector adapted to collect light (L 1) emitted by the plurality of semiconductor emitters (11, 12, 13) of the first artificial light source and to gather the collected light (L 1) to the first planar reflector, - a second concave reflector adapted to collect light (L 2) emitted by the plurality of semiconductor emitters of the second artificial light source and to gather the collected light (L 2) to the second planar reflector, and - a projector lens, wherein the first and second planar reflector (50, 60) are configured to reflect the light (L 1, L 2) received from the first and second concave reflectors (30, 40), respectively, to the projector lens, characterized in that: - the light emitted by the plurality of semiconductor emitters (11, 12, 13) of the first artificial light source is firstly emitted away from the projector lens and from a center axis thereof and in that - the light emitted by the plurality of semiconductor emitters of the second artificial light source is firstly emitted away from the projector lens and from a center axis thereof. - a first artificial light source comprising a plurality of semiconductor emitters (11, 12, 13), - a second artificial light source comprising a plurality of semiconductor emitters, - a first planar reflector for guiding light (L 1) received from the first artificial light source as output of the PAPI, - a second planar reflector for guiding light (L 2) received from the second artificial light source as output of the PAPI, - a first concave reflector adapted to collect light (L 1) emitted by the plurality of semiconductor emitters (11, 12, 13) of the first artificial light source and to gather the collected light (L 1) to the first planar reflector, - a second concave reflector adapted to collect light (L 2) emitted by the plurality of semiconductor emitters of the second artificial light source and to gather the collected light (L 2) to the second planar reflector, and - a projector lens, wherein the first and second planar reflector (50, 60) are configured to reflect the light (L 1, L 2) received from the first and second concave reflectors (30, 40), respectively, to the projector lens, - the light emitted by the plurality of semiconductor emitters (11, 12, 13) of the first artificial light source is firstly emitted away from the projector lens and from a center axis thereof and in that - the light emitted by the plurality of semiconductor emitters of the second artificial light source is firstly emitted away from the projector lens and from a center axis thereof.
Operating device for mechanically controlling a membrane pump device for conveying fluids, in particular medical liquids for blood treatment, having a base body which comprises a mounting face for a membrane pump device and through which a control fluid line (33, 35) passes which extends from a control fluid port (78, 79) to a control fluid opening (34, 36) which opens at the mounting face, and having an adjustment device (9, 14) which comprises a working fluid valve (81, 82) which is designed to influence a cross section of a working fluid line (85, 86) which passes through the base body, and wherein the control fluid valve (74, 75) and the working fluid valve (81, 82) are electrically connected to a control device which is designed to electrically control the control fluid valve (74, 75) and the working fluid valve (81, 20, 82), wherein a control fluid valve (74, 75) is arranged in the control fluid line (33, 35), which control fluid valve is designed to influence a cross section of the control fluid line (33, 35), and characterized in that the adjustment device (9, 14) comprises a fluid actuator arranged on the mounting face for providing an adjustment movement.
Trailing-edge segment (2, 112) of a wind-turbine rotor blade for increasing a profile depth of the rotor blade (1, 108) of a wind turbine, comprising: - at least one inner blade segment (6, 7, 8), having an inner blade shell, - at least one middle blade segment, having a middle blade shell, the at least one middle blade segment and the at least one inner blade segment (6, 7, 8) being able to be coupled to each other via a coupling means, and characterized in that the coupling means having two shell elements (13, 53), having two inner sides (22, 62) that are parallel to each other each forming a receiving space, wherein the receiving space each being designed to receive at least one of the inner blade shell or middle blade shell, and wherein the two receiving spaces are adapted with the two inner sides (22, 62) to a thickness of the inner blade shell or the middle blade shell, wherein the two inner sides (22, 62) at least partly enclose the inner blade shell or the middle blade shell inserted into the receiving space, in such a manner that a force acting upon the trailing-edge segment (2, 112) is introduced via the two inner sides (22, 62) centrically into the coupling means, wherein the two shell elements (13, 53) each having a recess and first coupling elements (15, 65), wherein the first coupling elements (15, 65) of a shell element (13, 53) are arranged in the recesses of the other shell element (13, 53). - at least one inner blade segment (6, 7, 8), having an inner blade shell, - at least one middle blade segment, having a middle blade shell, the at least one middle blade segment and the at least one inner blade segment (6, 7, 8) being able to be coupled to each other via a coupling means, and characterized in that the coupling means having two shell elements (13, 53), having two inner sides (22, 62) that are parallel to each other each forming a receiving space, wherein the receiving space each being designed to receive at least one of the inner blade shell or middle blade shell, and wherein the two receiving spaces are adapted with the two inner sides (22, 62) to a thickness of the inner blade shell or the middle blade shell, wherein the two inner sides (22, 62) at least partly enclose the inner blade shell or the middle blade shell inserted into the receiving space, in such a manner that a force acting upon the trailing-edge segment (2, 112) is introduced via the two inner sides (22, 62) centrically into the coupling means, wherein the two shell elements (13, 53) each having a recess and first coupling elements (15, 65), wherein the first coupling elements (15, 65) of a shell element (13, 53) are arranged in the recesses of the other shell element (13, 53).
Assembly for aircraft comprising: - an aircraft wing comprising a wing box that consists in part of a forward stringer and an intermediate stringer; - an engine mounting pylon arranged beneath the wing, the pylon comprising a primary structure in the form of a box having an upper stringer extending at least in part beneath the wing box, and also having a lower stringer, lateral panels and transverse reinforcing ribs (36, 36a, 36b); and - attachment means (40, 42) for attaching the primary structure of the mounting pylon to the wing box, characterized in that said attachment means comprise a line of bolts along which each bolt passes both through a structural component (36, 136a, 136b) of the pylon and through a fitting attached to one of said forward and intermediate stringers (16, 18), and in that said structural component of the pylon corresponds to one of the transverse reinforcing ribs (36, 36a, 36b) and the line of bolts is parallel to that of the forward and intermediate stringers (16, 18) to which the fitting is attached. - an aircraft wing comprising a wing box that consists in part of a forward stringer and an intermediate stringer; - an engine mounting pylon arranged beneath the wing, the pylon comprising a primary structure in the form of a box having an upper stringer extending at least in part beneath the wing box, and also having a lower stringer, lateral panels and transverse reinforcing ribs (36, 36a, 36b); and - attachment means (40, 42) for attaching the primary structure of the mounting pylon to the wing box,
A method for machining the end faces of workpieces made from wood, plastic and the like, in which the end faces of the workpieces, which are clamped by at least one clamping device, are milled by at least one rotatably driven milling cutter, characterized in that two workpieces (1, 1') are clamped with a lateral distance therebetween and offset lengthwise with respect to one another, and the end faces thereof are machined with the milling tool.
Process for the preparation of a support impregnated with clay, comprising stages where: - a pasty mixture comprising a filler essentially comprising clay is prepared, - the pasty mixture is sprayed onto a dry flexible support having a fibrous structure, - then the said support provided with this mixture is dried, characterized in that, so that the filler does not significantly separate off from the dry support when the support is subsequently immersed in distilled water, at ambient temperature: - the pasty mixture which is prepared is prepared with non-swelling phyllitic clay representing between 30% and 60% by weight of mixture, - the pasty mixture is prepared in a tank where a pressure of air of between 1.5 and 7 x 10 5 Pa has been established and/or the mixture is sprayed at a distance from the support of between 5 cm and 30 cm, - the said support onto which the mixture is sprayed is taut, of nonwoven type comprising natural or synthetic fibres and obtained by an aerodynamic and dry-route process, the mixture which is sprayed being devoid of polymerization agent capable of bringing about polymerization within the mixture or in the presence of the support provided with the sprayed mixture, - the said mixture is sprayed in order to impregnate the support with it, - and, before being dried, the impregnated support is not rolled between ramming rollers or scraped in order to further ram the mixture into the support. - a pasty mixture comprising a filler essentially comprising clay is prepared, - the pasty mixture is sprayed onto a dry flexible support having a fibrous structure, - then the said support provided with this mixture is dried, - the pasty mixture which is prepared is prepared with non-swelling phyllitic clay representing between 30% and 60% by weight of mixture, - the pasty mixture is prepared in a tank where a pressure of air of between 1.5 and 7 x 10 5 Pa has been established and/or the mixture is sprayed at a distance from the support of between 5 cm and 30 cm, - the said support onto which the mixture is sprayed is taut, of nonwoven type comprising natural or synthetic fibres and obtained by an aerodynamic and dry-route process, the mixture which is sprayed being devoid of polymerization agent capable of bringing about polymerization within the mixture or in the presence of the support provided with the sprayed mixture, - the said mixture is sprayed in order to impregnate the support with it, - and, before being dried, the impregnated support is not rolled between ramming rollers or scraped in order to further ram the mixture into the support.
A cleaning tool for cleaning an optical connector (91; 96) and, optionally, an optical plug or an optical adapter, the cleaning tool comprising: a tool body; and an extension part that extends from the tool body, the extension part including a head that presses a cleaning element onto a cleaning target on a pressing surface, wherein the extension part includes an inner guide part through which the head is inserted, and an outer guide part through which the inner guide part is inserted, the outer guide part comprises an outer peripheral portion and an outer guide end surface, the outer peripheral portion having a peripheral surface adapted to guide the head along an inner wall surface of a receptacle housing of a first optical connector to be cleaned with respect to a ferrule endface of a first optical connector, and the cleaning tool being adapted to fit the inner guide part inside a second optical connector to be cleaned when the outer guide part retracts and the outer guide end surface abuts a housing of a second optical connector. a tool body; and an extension part that extends from the tool body, the extension part including a head that presses a cleaning element onto a cleaning target on a pressing surface, wherein the extension part includes an inner guide part through which the head is inserted, and an outer guide part through which the inner guide part is inserted, the outer guide part comprises an outer peripheral portion and an outer guide end surface, the outer peripheral portion having a peripheral surface adapted to guide the head along an inner wall surface of a receptacle housing of a first optical connector to be cleaned with respect to a ferrule endface of a first optical connector, and the cleaning tool being adapted to fit the inner guide part inside a second optical connector to be cleaned when the outer guide part retracts and the outer guide end surface abuts a housing of a second optical connector.
A separating device with a separating unit for separating and sealing two chambers (111, 112) of a container, wherein the separating unit comprises a main body which has a radial outer peripheral surface which is designed as a sealing surface, wherein the separating unit comprises a support structure which is arranged in the region of the outer periphery and which each comprises a support structure unit (125, 126) which is arranged above and below the main body, and wherein the main body with the support structure forms a receiving space which at least partly receives a inflatable seal, and the separating unit in the installed state is arranged in the container which comprises a container wall which forms the counter sealing surface, in a manner such that the sealing surface is annularly enclosed by the counter sealing surface, so that the inflatable seal in the pressure-free, relaxed state is arranged loosely in the receiving space and in the state in which it is subjected to pressure is expanded and bears on the sealing surface as well as the counter sealing surface, so that the inflatable seal separates the container into two chambers (111, 112) and seals these with respect to one another characterised in that the support structure units (125, 126) are each designed in a grid-like manner.
A composition comprising free N-glycans, wherein the free N-glycans are generated by contacting a glycoprotein comprising a high mannose, complex, or hybrid N-glycan with a GH18 endoglycosidase from B. longum bv infantis, wherein the glycoprotein is a milk, plant, or egg glycoprotein.
A method of manufacturing an embossing element for decorative surfaces including the steps of: a) UV curable inkjet printing a decorative pattern on a metallic surface; and b) forming a relief by etching metal from the metallic surface. a) UV curable inkjet printing a decorative pattern on a metallic surface; and b) forming a relief by etching metal from the metallic surface.
A device for measuring phase retardation distribution and fast axis azimuth angle distribution of a sample in real time, comprising: a collimating light source, a circular polarizer, a diffractive beam-splitting component, a quarter wave plate, an analyzer array, a CCD image sensor and a computer equipped with an image acquisition card; wherein the analyzer array is composed of a first analyzer, a second analyzer, a third analyzer and a fourth analyzer, whose polarization direction angle successively increases by 45°; wherein the quarter wave plate is located in a same path as the first analyzer between the diffractive beam-splitting component and the analyzer array and the angle between the fast axis of the quarter wave plate and the transmission direction of the first analyzer is 45° or 135°; wherein the system is configured such that in use the light emitted from the collimating light source passes through the circular polarizer and then the diffractive beam-splitting component and is split into four sub-beams by the diffractive beam-splitting component, and only one of the sub-beams passes through the quarter wave plate and then is analyzed by the first analyzer, and the other three sub-beams are directly analyzed by the second analyzer, the third analyzer and the fourth analyzer, respectively; wherein an output port of the image sensor is connected to an input port of the computer; and wherein a means for accommodating a measuring sample is arranged between the circular polarizer and the diffractive beam-splitting component. a collimating light source, a circular polarizer, a diffractive beam-splitting component, a quarter wave plate, an analyzer array, a CCD image sensor and a computer equipped with an image acquisition card; wherein the analyzer array is composed of a first analyzer, a second analyzer, a third analyzer and a fourth analyzer, whose polarization direction angle successively increases by 45°; wherein the quarter wave plate is located in a same path as the first analyzer between the diffractive beam-splitting component and the analyzer array and the angle between the fast axis of the quarter wave plate and the transmission direction of the first analyzer is 45° or 135°; wherein the system is configured such that in use the light emitted from the collimating light source passes through the circular polarizer and then the diffractive beam-splitting component and is split into four sub-beams by the diffractive beam-splitting component, and only one of the sub-beams passes through the quarter wave plate and then is analyzed by the first analyzer, and the other three sub-beams are directly analyzed by the second analyzer, the third analyzer and the fourth analyzer, respectively; wherein an output port of the image sensor is connected to an input port of the computer; and wherein a means for accommodating a measuring sample is arranged between the circular polarizer and the diffractive beam-splitting component.
A valve comprising a longitudinal axis, for inflation and deflation of air bags configured to utilize a turning tool having a circular edge, said valve comprising: a body; an insert; an o-ring; and a spring disposed between said body and said insert; characterized in that said insert has a first end and a second end, said insert having panels disposed between said first end and said second end, said panels having openings disposed between said panels, and wherein said first end has at least two diametrically-opposed longitudinal slots positioned on an inside of said insert, wherein said insert is dimensioned to receive the circular edge of the turning tool and is adapted to engage said at least two diametrically-opposed longitudinal slots. a body; an insert; an o-ring; and a spring disposed between said body and said insert; characterized in that said insert has a first end and a second end, said insert having panels disposed between said first end and said second end, said panels having openings disposed between said panels, and wherein said first end has at least two diametrically-opposed longitudinal slots positioned on an inside of said insert, wherein said insert is dimensioned to receive the circular edge of the turning tool and is adapted to engage said at least two diametrically-opposed longitudinal slots.
An aircraft which includes: a tailless fuselage which has a body which includes a transverse trailing edge, the body having a fineness ratio of between 3 and 7; and a wing having two sides (14.1) which protrude from opposite sides of the fuselage, characterised in that the width of the trailing edge of the fuselage is adjustable, for changing the position of the neutral point to adjust the static margin. a tailless fuselage which has a body which includes a transverse trailing edge, the body having a fineness ratio of between 3 and 7; and a wing having two sides (14.1) which protrude from opposite sides of the fuselage, characterised in that the width of the trailing edge of the fuselage is adjustable, for changing the position of the neutral point to adjust the static margin.
Membrane pump for fluidising and conveying dust at pressures of up to 7 MPa, in which - in a housing, a membrane separates a hydraulic compartment from a dust compartment, characterised in that - the housing is formed by a pressure-resistant hydraulic half-shell facing the hydraulic compartment and a pressure-resistant dust half-shell facing the dust compartment, - a gas-permeable, half-shell-shaped fluidising surface is arranged in the dust compartment, which surface is made of porous material and is curved, - a gas compartment for supplying gas is provided between the dust half-shell and the half-shell-shaped fluidising surface, - a support element is arranged between the dust half-shell and the half-shell-shaped fluidising surface. - in a housing, a membrane separates a hydraulic compartment from a dust compartment, characterised in that - the housing is formed by a pressure-resistant hydraulic half-shell facing the hydraulic compartment and a pressure-resistant dust half-shell facing the dust compartment, - a gas-permeable, half-shell-shaped fluidising surface is arranged in the dust compartment, which surface is made of porous material and is curved, - a gas compartment for supplying gas is provided between the dust half-shell and the half-shell-shaped fluidising surface, - a support element is arranged between the dust half-shell and the half-shell-shaped fluidising surface.