mhurhangee/ep-ind-claims huggingface dataset:
A method of determining a total mass of an aircraft comprising: determining an acceleration of a pushback vehicle while moving the aircraft; determining a pushback force applied by the pushback vehicle while moving the aircraft; and determining the total mass of the aircraft based on the pushback force, the acceleration of the pushback vehicle, and a coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves; wherein determining the acceleration of the pushback vehicle while moving the aircraft comprises determining a first acceleration, and wherein determining the pushback force applied by the pushback vehicle while moving the aircraft comprises determining a first pushback force, and wherein the method further comprises: applying a known mass to the aircraft; determining a second acceleration of the pushback vehicle while moving the aircraft with the known mass; determining a second pushback force applied by the pushback vehicle while moving the aircraft with the known mass; and determining the coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves based on the known mass, the first acceleration, the first pushback force, the second acceleration, and the second pushback force. determining an acceleration of a pushback vehicle while moving the aircraft; determining a pushback force applied by the pushback vehicle while moving the aircraft; and determining the total mass of the aircraft based on the pushback force, the acceleration of the pushback vehicle, and a coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves; wherein determining the acceleration of the pushback vehicle while moving the aircraft comprises determining a first acceleration, and wherein determining the pushback force applied by the pushback vehicle while moving the aircraft comprises determining a first pushback force, and wherein the method further comprises: applying a known mass to the aircraft; determining a second acceleration of the pushback vehicle while moving the aircraft with the known mass; determining a second pushback force applied by the pushback vehicle while moving the aircraft with the known mass; and determining the coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves based on the known mass, the first acceleration, the first pushback force, the second acceleration, and the second pushback force. applying a known mass to the aircraft; determining a second acceleration of the pushback vehicle while moving the aircraft with the known mass; determining a second pushback force applied by the pushback vehicle while moving the aircraft with the known mass; and determining the coefficient of static friction between tires of the aircraft and a surface on which the aircraft moves based on the known mass, the first acceleration, the first pushback force, the second acceleration, and the second pushback force.
A three-part ammunition cartridge casing body comprising: a base portion, made of metal or polymeric resin, having a closed end and an open end; a substantially cylindrical case portion, open on both ends, joined to the open end of the base portion and comprising a nanocomposite material of a nanoclay dispersed in a polyamide resin matrix; and a cap portion, made of a nanocomposite material of a nanoclay dispersed in a polyamide resin matrix and glass fibers, joined to the other end of the case portion, wherein the case portion is more ductile than the cap portion. a base portion, made of metal or polymeric resin, having a closed end and an open end; a substantially cylindrical case portion, open on both ends, joined to the open end of the base portion and comprising a nanocomposite material of a nanoclay dispersed in a polyamide resin matrix; and a cap portion, made of a nanocomposite material of a nanoclay dispersed in a polyamide resin matrix and glass fibers, joined to the other end of the case portion, wherein the case portion is more ductile than the cap portion.
Electronic module for accommodating electronic components, with a housing which is bounded in a longitudinal direction by two end faces, each comprising an opening, such that the housing can be fitted via the openings with at least one first circuit board equipped with electronic components and with at least one second circuit board equipped with plug and/or clamp connectors, whereby on the at least one second circuit board additional plug and/or clamp connectors (35, 38) are arranged in such a way that plug and/or clamp connectors (35, 38) of another electronic module can be wirelessly connected to the at least one second circuit board via plug and/or clamp connectors for the transmission of electrical power and communication signals, characterized in that the housing, on the inner side of a housing wall, exhibits at least one dome configured in a longitudinal direction to which the at least one first circuit board can be attached essentially transversely to the longitudinal direction, and the housing further exhibits, on two opposite-facing inner sides and/or two opposite-facing domes, a retaining groove in each case for the insertion of at least one second circuit board in the longitudinal direction, wherein the at least one first circuit board and the at least one second circuit board are wirelessly electrically connected to each other inside the housing via plug and/or clamp connectors (35, 38) for the transmission of electrical power and communication signals.
An aircraft landing gear comprising: a shock-absorbing main leg having a sprung part for attachment to an aircraft and an un-sprung part including a slider and an axle carrying at least one wheel (3a, 3b), the wheel having a toothed ring gear (7a, 7b); a drive transmission mounted externally on the sprung part, or on the un-sprung part, of the main leg, the drive transmission having at least one motor and a drive pinion for meshing with the toothed ring of the wheel; and an actuator for lifting the drive transmission into and out of driving engagement with the toothed ring and for maintaining the driving engagement as the landing gear deflects during a ground taxiing operation, wherein the drive transmission is detachably mounted, wherein the drive transmission is supported by an articulating mechanism and wherein the articulating mechanism and the actuator are mounted on the main leg by mounting brackets (12, 15), and wherein the mounting brackets include release mechanisms to permit detachment of the articulating mechanism and actuator from the main leg and wherein the articulating mechanism and the actuator are mounted in flexible or spherical bearings in the mounting brackets. a shock-absorbing main leg having a sprung part for attachment to an aircraft and an un-sprung part including a slider and an axle carrying at least one wheel (3a, 3b), the wheel having a toothed ring gear (7a, 7b); a drive transmission mounted externally on the sprung part, or on the un-sprung part, of the main leg, the drive transmission having at least one motor and a drive pinion for meshing with the toothed ring of the wheel; and an actuator for lifting the drive transmission into and out of driving engagement with the toothed ring and for maintaining the driving engagement as the landing gear deflects during a ground taxiing operation, wherein the drive transmission is detachably mounted, wherein the drive transmission is supported by an articulating mechanism and wherein the articulating mechanism and the actuator are mounted on the main leg by mounting brackets (12, 15), and wherein the mounting brackets include release mechanisms to permit detachment of the articulating mechanism and actuator from the main leg and wherein the articulating mechanism and the actuator are mounted in flexible or spherical bearings in the mounting brackets.
A display device, comprising: a display panel configured to display images and comprising outer portions; a light irradiating part configured to irradiate light toward a back surface of the display panel; an electrically grounded heat radiating plate configured to radiate heat generated by the light irradiating part; a plurality of protective members (12A, 12B, 12C, 12D) configured to form a frame provided along the outer portions of the display panel, wherein at least one of the plurality of protective members (12A, 12B, 12C, 12D) is an opposing protective member that opposes the heat radiating plate; and a conductive member interposed between and electrically connecting the opposing protective member and the heat radiating plate, wherein the conductive member contacts a front portion of the opposing protective member. a display panel configured to display images and comprising outer portions; a light irradiating part configured to irradiate light toward a back surface of the display panel; an electrically grounded heat radiating plate configured to radiate heat generated by the light irradiating part; a plurality of protective members (12A, 12B, 12C, 12D) configured to form a frame provided along the outer portions of the display panel, wherein at least one of the plurality of protective members (12A, 12B, 12C, 12D) is an opposing protective member that opposes the heat radiating plate; and a conductive member interposed between and electrically connecting the opposing protective member and the heat radiating plate, wherein the conductive member contacts a front portion of the opposing protective member.
An LC medium comprising - a polymerisable component A) comprising one or more polymerisable compounds, preferably selected from reactive mesogens (RMs), and - a liquid crystalline component B), also referred to below as "LC host mixture", comprising one or more, preferably two or more, low-molecular-weight (monomeric and unpolymerisable) compounds selected from mesogenic or liquid crystal compounds, characterized in that component B comprises one or more compounds of formula I wherein denotes R 1 and R 2 each, independently of one another, denote alkyl having 1 to 12 C atoms, where, in addition, one or two non-adjacent CH 2 groups may be replaced by -O-, -CH=CH-, -CO-, -OCO- or -COO- in such a way that O atoms are not linked directly to one another, preferably alkyl or alkoxy having 1 to 6 C atoms, L 1-4 each, independently of one another, denote F, Cl, OCF 3, CF 3, CH 3, CH 2 F, CHF 2, wherein at least one of L 1-4 is different from H and preferably denotes F, and component B does not contain a terphenyl compound wherein one or more phenyl rings are fluorinated in 2- and/or 3 position, and wherein the proportion of compounds of formula I in the mixture as a whole is from 1 to 45%, and the content of an individual compound of formula I is in each case from 1 to 20%. - a polymerisable component A) comprising one or more polymerisable compounds, preferably selected from reactive mesogens (RMs), and - a liquid crystalline component B), also referred to below as "LC host mixture", comprising one or more, preferably two or more, low-molecular-weight (monomeric and unpolymerisable) compounds selected from mesogenic or liquid crystal compounds, R 1 and R 2 each, independently of one another, denote alkyl having 1 to 12 C atoms, where, in addition, one or two non-adjacent CH 2 groups may be replaced by -O-, -CH=CH-, -CO-, -OCO- or -COO- in such a way that O atoms are not linked directly to one another, preferably alkyl or alkoxy having 1 to 6 C atoms, L 1-4 each, independently of one another, denote F, Cl, OCF 3, CF 3, CH 3, CH 2 F, CHF 2, wherein at least one of L 1-4 is different from H and preferably denotes F,
A system comprising one or more evolved NodesB, eNB,; one or more WLAN access points, AP,; a WLAN element manager, EM,, a network manager, NM,; a 3GPP Domain Manager, DM,; the AP(s) being linked indirectly to the eNB(s) through the WLAN EM, the NM and the 3GPP DM; the, WLAN EM comprising: a polling module configured to poll the WLAN AP(s), said polling to request traffic load data from said WLAN AP(s); a timer module configured to trigger said polling module to poll at periodic intervals; a logging module configured to receive and log said requested traffic load data; and an integration reference point, IRP, agent comprising a reporting module configured to generate a traffic load report for transmission to the network manager, NM, said traffic load report based on said logged traffic load data; wherein said periodic interval for polling is configured based on traffic load management requirements of the eNB(s); and the eNB(s) configured to receive the traffic load report(s) from the NM through the 3GPP DM and each of the eNBs configured to select some of the WLAN AP(s) based on the received traffic load report(s) as candidates for traffic offloading. a polling module configured to poll the WLAN AP(s), said polling to request traffic load data from said WLAN AP(s); a timer module configured to trigger said polling module to poll at periodic intervals; a logging module configured to receive and log said requested traffic load data; and an integration reference point, IRP, agent comprising a reporting module configured to generate a traffic load report for transmission to the network manager, NM, said traffic load report based on said logged traffic load data; wherein said periodic interval for polling is configured based on traffic load management requirements of the eNB(s); and the eNB(s) configured to receive the traffic load report(s) from the NM through the 3GPP DM and each of the eNBs configured to select some of the WLAN AP(s) based on the received traffic load report(s) as candidates for traffic offloading.
A method for the preparation of an edible product or a pharmaceutical composition, said method comprising incorporating 0.5-10% by weight of a polysaccharide having a backbone comprising alternating rhamnogalacturonan-I cores and alpha(1,4)-linked polygalacturonic acid or alpha(1,4)-linked oligogalacturonic acid cores or having a backbone consisting of a rhamnogalacturonan-I core; wherein the polysaccharide has a molecular weight of at least 70 kD; and wherein the polysaccharide is obtained from plants of the species Camellia sinensis and wherein the molar ratio of galacturonyl acid residues to rhamnosyl residues in the backbone of the polysaccharide ranges from 2.5:1 to 1:1; wherein the molar ratio of galacturonyl acid residues to rhamnosyl residues in the backbone of the polysaccharide is determined using the NMR method described in the Examples.
A structural assembly for supporting electrical and/or electronic modules, the structural assembly comprising: - a longitudinally extending tubular structure defining a support end (1.1) and an operational end (1.2), axially opposed to the support end (1.1); and - a base (2; 3) for holding the tubular structure by the support end (1.1); wherein the tubular structure comprises: - at least one longitudinally extending groove (1.3) configured to exert angular retention of the electrical and/or electronic modules such that they are prevented from being rotationally moved; - at least one longitudinally extending cavity (1.4) configured to house at least one power or data cable; and - at least one flange for each cavity (1.4), the at least one flange being arranged to cover access to the cavity (1.4) whereon it is arranged; characterised in that: the at least one flange is elastically deformable in order to simultaneously establish a passage to the cavity (1.4); and there are two flanges, the flanges being arranged in each cavity (1.4) such that they jointly cover the access to the cavity (1.4). - a longitudinally extending tubular structure defining a support end (1.1) and an operational end (1.2), axially opposed to the support end (1.1); and - a base (2; 3) for holding the tubular structure by the support end (1.1); wherein the tubular structure comprises: - at least one longitudinally extending groove (1.3) configured to exert angular retention of the electrical and/or electronic modules such that they are prevented from being rotationally moved; - at least one longitudinally extending cavity (1.4) configured to house at least one power or data cable; and - at least one flange for each cavity (1.4), the at least one flange being arranged to cover access to the cavity (1.4) whereon it is arranged; - at least one longitudinally extending groove (1.3) configured to exert angular retention of the electrical and/or electronic modules such that they are prevented from being rotationally moved; - at least one longitudinally extending cavity (1.4) configured to house at least one power or data cable; and - at least one flange for each cavity (1.4), the at least one flange being arranged to cover access to the cavity (1.4) whereon it is arranged; characterised in that: the at least one flange is elastically deformable in order to simultaneously establish a passage to the cavity (1.4); and there are two flanges, the flanges being arranged in each cavity (1.4) such that they jointly cover the access to the cavity (1.4). the at least one flange is elastically deformable in order to simultaneously establish a passage to the cavity (1.4); and there are two flanges, the flanges being arranged in each cavity (1.4) such that they jointly cover the access to the cavity (1.4).
A cone radiator sub-reflector assembly for a reflector antenna with a sub-reflector supported by a waveguide, comprising: a unitary dielectric block; a sub-reflector provided at a distal end of the unitary dielectric block; a waveguide transition portion of the unitary dielectric block dimensioned for insertion coupling into an end of the waveguide; and a sub-reflector support portion of the unitary dielectric block supporting the sub-reflector; wherein the sub-reflector support portion and the waveguide transition portion are provided with a plurality of longitudinal ribs and longitudinal grooves coaxial with a longitudinal axis of the cone radiator sub-reflector assembly; wherein the longitudinal grooves open to a proximal end of the unitary dielectric block; and wherein a longitudinal extent of the longitudinal ribs of the sub-reflector support portion toward the proximal end of the unitary dielectric block shortens between an inner diameter and a periphery of the sub-reflector support portion; and wherein a leading edge of the longitudinal ribs of the sub-reflector support portion is angled to form a conical surface with a maximum diameter toward the distal end of the unitary dielectric block. a unitary dielectric block; a sub-reflector provided at a distal end of the unitary dielectric block; a waveguide transition portion of the unitary dielectric block dimensioned for insertion coupling into an end of the waveguide; and a sub-reflector support portion of the unitary dielectric block supporting the sub-reflector; wherein the sub-reflector support portion and the waveguide transition portion are provided with a plurality of longitudinal ribs and longitudinal grooves coaxial with a longitudinal axis of the cone radiator sub-reflector assembly; wherein the longitudinal grooves open to a proximal end of the unitary dielectric block; and wherein a longitudinal extent of the longitudinal ribs of the sub-reflector support portion toward the proximal end of the unitary dielectric block shortens between an inner diameter and a periphery of the sub-reflector support portion; and wherein a leading edge of the longitudinal ribs of the sub-reflector support portion is angled to form a conical surface with a maximum diameter toward the distal end of the unitary dielectric block.
An exhaust apparatus of an internal combustion engine, comprising; an expansion chamber (36, 37; 86) in which an exhaust flow discharged from the internal combustion engine is introduced to extend the exhaust flow and to mute exhaust gas sounds, a sound deadening device (27; 81) having a resonance chamber (38; 87) adjacent to the expansion chamber (36, 37; 86) to mute the exhaust gas sounds of a specific frequency, an exhaust pipe (51, 53; 90, 91) having at its one end portion (51 A; 90A) an upstream open end (51 a; 90a) connected with the expansion chamber (36, 37; 86) of the sound deadening device (27; 81) at the upstream side of exhaust gas flow in the exhaust gas flow direction, and at its other end potion (53B; 91 B) a downstream open end (53b; 91 b) through which the exhaust gas discharged from the sound deadening device (27; 81) is discharged to the atmosphere at the downstream side of exhaust gas flow in the exhaust gas flow direction, and a hollow member (52; 89) disposed in the exhaust pipe (51, 53; 90, 91) and having a downstream end forming an open end (52b; 89b), and an upstream end forming an open end (52a; 89a) protruded outwardly from the inside of the exhaust pipe (51, 53; 90, 91) communicating with the resonance chamber (38; 87) through the upstream open end (51a, 90a) of the exhaust pipe and being located in a closed space surrounded by the wall portion (31, 32, 34; 82, 84, 85) of the sound deadening device (27; 81) defining the resonance chamber (38; 87), characterized in that the exhaust pipe (51, 53; 90, 91) is constituted by an outer pipe (51; 90) provided in the sound deadening device (27; 81), and a tail pipe (53; 91) connected to the outer pipe (51; 90) and extending toward the downstream side of the sound deadening device (27; 81), and the hollow member (52; 89) is constituted by an outlet pipe (52; 89) provided in the outer pipe (51; 90), and the downstream portion (52B; 89B) of the outlet pipe (52; 89) is connected with the upstream portion (53A; 91A) of the tail pipe (53; 91), and is formed with at least one through-bore (52c; 89c) allowing the inside of the outlet pipe (52; 89) to be held in communication with the inside of the outer pipe (51; 90).
A system provided with panels, for example, glass sheets, and with substantially steel elements (1, 3) extending parallel to edges of the panels, wherein thermally insulating parts extend between said steel elements (1, 3) and are connected by means of connecting means to connecting surfaces of the steel elements (1, 3), said connecting means comprising connecting elements that are provided with steel connecting flanges that have been fixed to the connecting surfaces of the steel elements (1, 3), characterized in that the insulating parts are integrally fixed to respective connecting elements by means of clamping fixation, with deformation of the insulating parts.