mhurhangee/ep-ind-claims huggingface dataset:
A holder for at least one cassette (400, 500, 600), with the holder having at least one shaft holder, at least one shaft element (200, 250) and at least one cassette (400, 500, 600), with the at least one cassette (400, 500, 600) being attached to the shaft element (200, 250) such that it can pivot about a pivoting axis, with the at least one shaft element (200, 250) being attached to the shaft holder, with the at least one shaft element (200, 250) having a guidance channel (212, 212a), with the guidance channel (212, 212a) running at least partially parallel to the pivoting axis, with the cassette (400, 500, 600) having at least one element (515, 515a) for rotatable mounting, characterized in, that the at least one element (515, 515a) for rotatable mounting comprises a first element for rotatable mounting and a second element for rotatable mounting, each being hollow-cylindrical and having an envelope surface with slots (518, 518a) which extends in the direction of the entire longitudinal extent along the at least one element (515, 515a), so that the first and second element (515, 515a) for rotatable mounting form a first and a second shaft channel (516, 516a), and the at least one shaft element (200, 250) comprises a first shaft element and a second shaft element, each being hollow-cylindrical and having a guidance channel (212, 212a) for guiding an optical waveguide in the cassette (400, 500, 600), the guidance channels (212, 212a) run along the entire longitudinal extent of the shaft elements (208, 208a) and along the central longitudinal axis parallel to the privoting axis, the at least one element (515, 515a) for rotatable mounting being pluggable or latchable on the circumferential profile of the shaft elements (208, 208a) by the slots (518, 518a), so that the at least one element (515, 515a) is detachable mounted with the shaft element (200, 250), so that the each hollow cylindrical guidance channel (212, 212a) in the shaft elements (208, 208a) for guiding optical waveguides in the cassette (400, 500, 600) being independent of the rotation of the cassette (400, 500, 600) about a pivot axis corresponding with the central longitudinal axis.
A latch for a cargo management system of a cargo hold, the latch comprising: a base plate configured for rigid attachment to a surface of the cargo hold; a latch head attached to the base plate and configured to prevent a movement of at least one cargo unit in a lateral Y-direction and a vertical Z-direction and to allow a movement of the at least one cargo unit in a longitudinal X-direction along the length of an aircraft; and a roller assembly attached to the base plate, opposite the latch head, and comprising at least one roller, the roller being configured to provide a vertical support to the at least one cargo unit in the Z-direction while allowing the movement of the at least one cargo unit in the X-direction, wherein the latch head comprises a latch toe on an edge thereof, the latch toe configured to engage against a base-latch heel formed in the base plate to secure the latch head within a latch head slot formed in the base plate, wherein the base plate and the latch head comprise corresponding latch-base alignment features, including a protuberance on the base plate and a cavity formed in a bottom surface of the latch head, wherein, when the latch toe is engaged against the base-latch heel, the latch head is configured to pivotably rotate into an installed position, in which the protuberance is located within the cavity. a base plate configured for rigid attachment to a surface of the cargo hold; a latch head attached to the base plate and configured to prevent a movement of at least one cargo unit in a lateral Y-direction and a vertical Z-direction and to allow a movement of the at least one cargo unit in a longitudinal X-direction along the length of an aircraft; and a roller assembly attached to the base plate, opposite the latch head, and comprising at least one roller, the roller being configured to provide a vertical support to the at least one cargo unit in the Z-direction while allowing the movement of the at least one cargo unit in the X-direction, wherein the latch head comprises a latch toe on an edge thereof, the latch toe configured to engage against a base-latch heel formed in the base plate to secure the latch head within a latch head slot formed in the base plate, wherein the base plate and the latch head comprise corresponding latch-base alignment features, including a protuberance on the base plate and a cavity formed in a bottom surface of the latch head, wherein, when the latch toe is engaged against the base-latch heel, the latch head is configured to pivotably rotate into an installed position, in which the protuberance is located within the cavity.
Motor vehicle comprising a bodywork structure, a hood and at least one hinge connecting said hood to a support integral with the structure, the at least one hinge comprising: - a fixed blade configured to be fixed to the support; and - a movable blade pivotally mounted on the fixed blade and configured to be attached to the door; the fixed blade comprising, at one end, a finger able to engage with the support in order to ensure, during the mounting of said blade, a temporary fixing before a fitting of clamping fixing means, said at least one hinge has a center of gravity G situated, longitudinally, beyond said support, the cover being at the front of the vehicle, characterized in that for the at least one hinge, the end of the fixed blade comprising the finger is a front end, centre of gravity G being located at the rear of the support. - a fixed blade configured to be fixed to the support; and - a movable blade pivotally mounted on the fixed blade and configured to be attached to the door;
A support structure for a rostrum, comprising: a first A-frame; and at least a second A-frame, nestable into the first A-frame, each A-frame (10, 12) comprising two limbs, each limb being spaced apart at a lower portion and connected to one another at an upper portion, characterized in that, at least the second A-frame is retractable into the first A-frame, and in that when the second A-frame is nested in the first A-frame, the limbs of the first and second A-frames (10, 12) lie in the same vertical plane, and when the support structure is in the expanded position for use, the limbs of the first A-frame lie in a different vertical plane from the limbs of the second A-frame. a first A-frame; and at least a second A-frame, nestable into the first A-frame, each A-frame (10, 12) comprising two limbs, each limb being spaced apart at a lower portion and connected to one another at an upper portion, characterized in that, at least the second A-frame is retractable into the first A-frame, and in that when the second A-frame is nested in the first A-frame, the limbs of the first and second A-frames (10, 12) lie in the same vertical plane, and when the support structure is in the expanded position for use, the limbs of the first A-frame lie in a different vertical plane from the limbs of the second A-frame.
An apparatus to treat an eye with a therapeutic agent (702, 110), the apparatus comprising: a therapeutic device configured to be implanted in the eye, the therapeutic device comprising: a reservoir chamber (130, 140) having reservoir volume extending between a proximal end and a distal end of the reservoir chamber (130, 140); and a rigid porous structure coupled to the distal end of the reservoir chamber (130, 140); and an injector configured to fill the reservoir chamber (130, 140) with an amount of the therapeutic agent (702, 110) while the therapeutic device is at least partially implanted in the eye comprising: a needle (189, 189L) having an injection lumen (705, 189B) and a vent lumen (706, 189A); an injection chamber configured to be in fluid communication with the reservoir chamber (130, 140) via the injection lumen (705, 189B); a vent chamber configured to be in fluid communication with the reservoir chamber (130, 140) via the vent lumen (706, 189A); and a piston movable within the injection chamber; wherein the injector is configured to place the amount of the therapeutic agent (702, 110) into the reservoir chamber (130, 140) without delivering a substantial bolus from the reservoir chamber (130, 140) into the eye. a therapeutic device configured to be implanted in the eye, the therapeutic device comprising: a reservoir chamber (130, 140) having reservoir volume extending between a proximal end and a distal end of the reservoir chamber (130, 140); and a rigid porous structure coupled to the distal end of the reservoir chamber (130, 140); and a reservoir chamber (130, 140) having reservoir volume extending between a proximal end and a distal end of the reservoir chamber (130, 140); and a rigid porous structure coupled to the distal end of the reservoir chamber (130, 140); and an injector configured to fill the reservoir chamber (130, 140) with an amount of the therapeutic agent (702, 110) while the therapeutic device is at least partially implanted in the eye comprising: a needle (189, 189L) having an injection lumen (705, 189B) and a vent lumen (706, 189A); an injection chamber configured to be in fluid communication with the reservoir chamber (130, 140) via the injection lumen (705, 189B); a vent chamber configured to be in fluid communication with the reservoir chamber (130, 140) via the vent lumen (706, 189A); and a piston movable within the injection chamber; a needle (189, 189L) having an injection lumen (705, 189B) and a vent lumen (706, 189A); an injection chamber configured to be in fluid communication with the reservoir chamber (130, 140) via the injection lumen (705, 189B); a vent chamber configured to be in fluid communication with the reservoir chamber (130, 140) via the vent lumen (706, 189A); and a piston movable within the injection chamber; wherein the injector is configured to place the amount of the therapeutic agent (702, 110) into the reservoir chamber (130, 140) without delivering a substantial bolus from the reservoir chamber (130, 140) into the eye.
A heat dissipation enclosure for a heat generation device of a wind power generator set, wherein the heat dissipation enclosure comprises an enclosure body defining an intermediate space, and a thermal radiation absorption coating is at least partially applied on an inner wall of the enclosure body, wherein a thermal radiation dissipation coating is at least partially applied on an outer wall of the enclosure body, wherein the thermal radiation dissipation coating is arranged on an outer wall, at a shady side, of the enclosure body.
A local error generation device comprising an estimation unit to estimate and generate local errors that influence positioning accuracy in a second region remote from a first region, based on global errors included in positioning augmentation information (81, 82) for positioning that is generated by a network configured for the first region, the global errors being caused by satellites to transmit positioning signals, and on observed data generated based on the positioning signals received by a receiver that does not belong to the network and is installed at an electronic reference point located in the second region, the local errors depending on the second region where the receiver exists and caused by propagation paths of the positioning signals; characterized in that the estimation unit is configured to generate the local errors for each satellite of a plurality of satellites; and wherein a supplementary information generation unit is configured to select a plurality of satellites that are available for positioning in the second region based on the local errors for each satellite. an estimation unit to estimate and generate local errors that influence positioning accuracy in a second region remote from a first region, based on global errors included in positioning augmentation information (81, 82) for positioning that is generated by a network configured for the first region, the global errors being caused by satellites to transmit positioning signals, and on observed data generated based on the positioning signals received by a receiver that does not belong to the network and is installed at an electronic reference point located in the second region, the local errors depending on the second region where the receiver exists and caused by propagation paths of the positioning signals; characterized in that the estimation unit is configured to generate the local errors for each satellite of a plurality of satellites; and wherein a supplementary information generation unit is configured to select a plurality of satellites that are available for positioning in the second region based on the local errors for each satellite.
A method for Internet key exchange protocol, IKE, authentication messaging using a certificate, comprising: parsing, by a first device, a certificate of the first device to obtain signature information in the certificate; filling, by the first device, an AUTH payload field in an Internet key exchange protocol, IKE, identity authentication, AUTH, message based on the signature information in the certificate, wherein signature information indicated by the AUTH payload field matches the signature information in the certificate; and sending, by the first device, the IKE AUTH message to a second device; wherein the first device is an initiator of authentication and the second device is a responder of the authentication; wherein the AUTH payload field indicates a signature information type supported by the first device in the authentication, and there is a mapping relationship between a filling value of the AUTH payload field and the signature information in the certificate; wherein the signature information type indicates whether a digital signature is supported. parsing, by a first device, a certificate of the first device to obtain signature information in the certificate; filling, by the first device, an AUTH payload field in an Internet key exchange protocol, IKE, identity authentication, AUTH, message based on the signature information in the certificate, wherein signature information indicated by the AUTH payload field matches the signature information in the certificate; and sending, by the first device, the IKE AUTH message to a second device; wherein the first device is an initiator of authentication and the second device is a responder of the authentication; wherein the AUTH payload field indicates a signature information type supported by the first device in the authentication, and there is a mapping relationship between a filling value of the AUTH payload field and the signature information in the certificate; wherein the signature information type indicates whether a digital signature is supported.
A shoe comprising: an upper; and a sole, wherein the upper is formed from a web including one or a plurality of randomly layered thermoplastic fine strands, the web includes a first region in which the thermoplastic fine strand is point-bonded to each other at contact portions and a three-dimensional shape of the thermoplastic fine strand is maintained and a second region formed in a sheet form in which the thermoplastic fine strand is fused and a three-dimensional shape of the thermoplastic fine strand disappears or is deformed, the second region having an apparent density higher than an apparent density of the first region, wherein a thickness of the first region is 5 mm to 30 mm, and a diameter of the thermoplastic fine strand in the first region ranges from 0.2 mm to 2 mm, and the apparent density of the first region ranges from 0.005 g/cm 3 to 0.2 g/cm 3. an upper; and a sole, wherein the upper is formed from a web including one or a plurality of randomly layered thermoplastic fine strands, the web includes a first region in which the thermoplastic fine strand is point-bonded to each other at contact portions and a three-dimensional shape of the thermoplastic fine strand is maintained and a second region formed in a sheet form in which the thermoplastic fine strand is fused and a three-dimensional shape of the thermoplastic fine strand disappears or is deformed, the second region having an apparent density higher than an apparent density of the first region, wherein a thickness of the first region is 5 mm to 30 mm, and a diameter of the thermoplastic fine strand in the first region ranges from 0.2 mm to 2 mm, and the apparent density of the first region ranges from 0.005 g/cm 3 to 0.2 g/cm 3.
Floor covering consisting of rectangular hard panels, wherein these panels are provided, on a first pair of opposite edges (3-4, 5-6), with coupling means, so that several of such panels can be mutually coupled; wherein these coupling means provide for an interlocking in a direction perpendicular to the plane of the floor covering, as well as in a direction perpendicular to the edges (3-4, 5-6) concerned and parallel to the plane of the floor covering; wherein the above-mentioned coupling means comprise a tongue and a groove and whereby the lip which is situated on the bottom side of the groove, hereafter called the lower lip, is longer than the lip on the top side, hereafter called the upper lip; wherein the coupling means consist at least of first coupling parts, formed of contact surfaces working in conjunction with one another, on the top side of the tongue and the bottom side of the upper lip respectively, second coupling parts formed of contact surfaces, on the top side of the lower lip and an opposite part of the other panel respectively, and third coupling parts providing for the horizontal interlocking, which are situated on the lower lip, yet further than the free end of the upper lip, wherein these third coupling parts are situated between the first and second ones; wherein the panels are provided with coupling means on a second pair of opposite edges which allow for a vertical and a horizontal interlocking and which make it possible for the panels concerned to be assembled along their top edges, disassembled respectively, at least by means of a movement of rotation, characterized in that at the first pair of edges a free space is provided under the tongue extending as of the tip of the tongue up to the third coupling parts.
An autonomous, transportable ground station for an unmanned aerial vehicle, comprising: a support structure configured to support a UAV and a recharging station; a container comprising an openable top panel; a solar panel in communication with the recharging station; characterized by further comprising wheels, rollers, or a marine propulsion system on the container, wherein the wheels, rollers, or the marine propulsion system are configured to propel the container; and circuitry in or on the container, said circuitry being configured to control the ground station via remote control or autonomously without the need for human intervention at the ground-station site and during transportation. a support structure configured to support a UAV and a recharging station; a container comprising an openable top panel; a solar panel in communication with the recharging station; characterized by further comprising wheels, rollers, or a marine propulsion system on the container, wherein the wheels, rollers, or the marine propulsion system are configured to propel the container; and circuitry in or on the container, said circuitry being configured to control the ground station via remote control or autonomously without the need for human intervention at the ground-station site and during transportation.
Use of a carrier comprising at least one take-up region based on a non-woven polyolefin or use of the take-up region for semi-quantitatively, preferably quantitatively determining the concentration of an analyte in a blood sample.
A method of making an unsaturated dibasic ester, comprising: providing a reactant composition comprising a terminal olefin ester and an internal olefin ester, wherein the terminal olefin ester is a compound according to the following chemical formula: wherein, X is C 3-18 alkylene, which optionally comprises unsaturation; and R is alkyl, which optionally comprises unsaturation or ether linkages; and reacting the terminal olefin ester with the internal olefin ester in a reactor in the presence of a first metathesis catalyst to form an unsaturated dibasic ester and a first terminal olefin, and wherein at least a portion of the first terminal olefin is removed from the reactor during the reacting; and further reacting the terminal olefin ester with an internal olefin in the presence of a second metathesis catalyst to form at least a portion of the internal olefin ester in the reaction composition. providing a reactant composition comprising a terminal olefin ester and an internal olefin ester, wherein the terminal olefin ester is a compound according to the following chemical formula: wherein, X is C 3-18 alkylene, which optionally comprises unsaturation; and R is alkyl, which optionally comprises unsaturation or ether linkages; and X is C 3-18 alkylene, which optionally comprises unsaturation; and R is alkyl, which optionally comprises unsaturation or ether linkages; and reacting the terminal olefin ester with the internal olefin ester in a reactor in the presence of a first metathesis catalyst to form an unsaturated dibasic ester and a first terminal olefin, and wherein at least a portion of the first terminal olefin is removed from the reactor during the reacting; and further reacting the terminal olefin ester with an internal olefin in the presence of a second metathesis catalyst to form at least a portion of the internal olefin ester in the reaction composition.
An apparatus (136; 236; 336; 436) for compensating transmitter quadrature imbalances over an optical signal (S(t)) received at an optical coherent receiver of a node of an optical communication network, said optical signal (S(t)) comprising a sequence of symbols comprising received information symbols and received pilot symbols, said receiver being configured to store a sequence of reference pilot symbols, the apparatus (136, 236, 336, 436) comprising: - an absolute phase estimating circuit (141; 251; 341, 351; 441) configured to estimate a phase error between a received pilot symbol (Zdp(k) and a corresponding pilot symbol of said sequence of reference pilot symbols (P(k)); - a phase correcting module (142; 242; 358; 442) configured to remove said phase error from said received pilot symbol (Zdp(k)) and a number of received information symbols associated with said received pilot symbol; - a quadrature imbalance detection circuit (145; 245; 345; 445) configured to estimate said transmitter quadrature imbalances on the basis of at least said phase-corrected pilot symbol; and - a quadrature imbalance compensation circuit (143; 243; 347, 348, 349; 460) configured to compensate said estimated transmission quadrature imbalances over said number of phase-corrected information symbols. - an absolute phase estimating circuit (141; 251; 341, 351; 441) configured to estimate a phase error between a received pilot symbol (Zdp(k) and a corresponding pilot symbol of said sequence of reference pilot symbols (P(k)); - a phase correcting module (142; 242; 358; 442) configured to remove said phase error from said received pilot symbol (Zdp(k)) and a number of received information symbols associated with said received pilot symbol; - a quadrature imbalance detection circuit (145; 245; 345; 445) configured to estimate said transmitter quadrature imbalances on the basis of at least said phase-corrected pilot symbol; and - a quadrature imbalance compensation circuit (143; 243; 347, 348, 349; 460) configured to compensate said estimated transmission quadrature imbalances over said number of phase-corrected information symbols.