mhurhangee/ep-ind-claims huggingface dataset:
A packet forwarding method, comprising the steps of: receiving, by a network device, a first packet, wherein the first packet comprises a first tunnel identifier; obtaining, by the network device, the first tunnel identifier of the first packet; and forwarding, by the network device, the first packet based on a first routing group in a virtual routing and forwarding, VRF, table, when the first tunnel identifier is a first value, or forwarding, by the network device, the first packet based on the first routing group and a second routing group of the VRF table, when the first tunnel identifier is a second value, wherein the VRF table comprises the first routing group and the second routing group, wherein the first routing group consists of one or more local routes, each next-hop outbound interface of the one or more local routes is a local outbound interface, and the second routing group comprises at least one remote route whose next-hop outbound interface is a remote outbound interface, wherein at least one next-hop of the one or more local routes and at least one next-hop of the one or more remote routes share a same destination address receiving, by a network device, a first packet, wherein the first packet comprises a first tunnel identifier; obtaining, by the network device, the first tunnel identifier of the first packet; and forwarding, by the network device, the first packet based on a first routing group in a virtual routing and forwarding, VRF, table, when the first tunnel identifier is a first value, or forwarding, by the network device, the first packet based on the first routing group and a second routing group of the VRF table, when the first tunnel identifier is a second value, wherein the VRF table comprises the first routing group and the second routing group, wherein the first routing group consists of one or more local routes, each next-hop outbound interface of the one or more local routes is a local outbound interface, and the second routing group comprises at least one remote route whose next-hop outbound interface is a remote outbound interface, wherein at least one next-hop of the one or more local routes and at least one next-hop of the one or more remote routes share a same destination address
Overvoltage protection device, consisting of an insulating housing for receiving at least one surge arrestor, in particular a spark gap and/or a varistor, wherein the housing has openings for the electrical connection and for the mechanical fixing and at least one flat housing underside, characterized in that the housing underside has apertures, of which the contour and spacing is designed to correspond to the grip tabs of a low-voltage power fuse insert, in such a way that the housing can be attached to a low-voltage power fuse insert or a group of low-voltage power fuse inserts and connected to the latter, wherein at least one of the grip tabs can be contacted electrically by means of connection elements located in the housing interior, wherein means for receiving a neutral conductor and/or connecting the surge arrestor having a neutral conductor, in particular a neutral conductor rail, are provided on or in the housing.
A stiffener skeleton that is configured to be mounted to an upper deck of a rotary wing aircraft in a maintenance phase and to be removed from the upper deck after the maintenance phase, comprising: an upper stiffening structure with a plurality of supporting arms (32a, 32b, 32c) for providing upside stiffening support; and a lateral stiffening structure with a plurality of supporting legs (33a, 33b, 34a, 34b) for providing lateral stiffening support; wherein the plurality of supporting arms (32a, 32b, 32c) and the plurality of supporting legs (33a, 33b, 34a, 34b) form a self-supporting frame structure; and wherein the self-supporting frame structure is configured to be arranged in the maintenance phase on a firewall arrangement provided on an upper deck of a rotary wing aircraft for supporting and stiffening at least a front firewall, a rear firewall, and a mid firewall of the firewall arrangement. an upper stiffening structure with a plurality of supporting arms (32a, 32b, 32c) for providing upside stiffening support; and a lateral stiffening structure with a plurality of supporting legs (33a, 33b, 34a, 34b) for providing lateral stiffening support; wherein the plurality of supporting arms (32a, 32b, 32c) and the plurality of supporting legs (33a, 33b, 34a, 34b) form a self-supporting frame structure; and wherein the self-supporting frame structure is configured to be arranged in the maintenance phase on a firewall arrangement provided on an upper deck of a rotary wing aircraft for supporting and stiffening at least a front firewall, a rear firewall, and a mid firewall of the firewall arrangement.
Method for manufacturing a wound fuel cell comprising: - a supporting strip, - an anodic insulating band, - a H 2 diffusion band, - a electrochemical cell carrying band, the anodes of which are on a first side of the carrier band and the cathodes of which are on a second side of the carrier band, and - a corrugated cathodic separating band, characterised in that it comprises: - a step of producing a winding mandrel including a device for H 2 fluid connection and for electric connection of a first end of the cell and including assembling a start end of the supporting strip to a holding flange (11, 11a, 11b) integral with a winding spindle of the cell, the mandrel provided with the holding flange receiving first endings of said supporting strip, anodic insulating band, H 2 diffusion band, electrochemical cell carrying band and corrugated cathodic separating band, - a step of winding the cell for which the tension of the supporting strip between an unwinder and the mandrel is controlled so as to apply a calibrated pressure to the wound layers of the cell. - a supporting strip, - an anodic insulating band, - a H 2 diffusion band, - a electrochemical cell carrying band, the anodes of which are on a first side of the carrier band and the cathodes of which are on a second side of the carrier band, and - a corrugated cathodic separating band, - a step of producing a winding mandrel including a device for H 2 fluid connection and for electric connection of a first end of the cell and including assembling a start end of the supporting strip to a holding flange (11, 11a, 11b) integral with a winding spindle of the cell, the mandrel provided with the holding flange receiving first endings of said supporting strip, anodic insulating band, H 2 diffusion band, electrochemical cell carrying band and corrugated cathodic separating band, - a step of winding the cell for which the tension of the supporting strip between an unwinder and the mandrel is controlled so as to apply a calibrated pressure to the wound layers of the cell.
A method of sorbing carbon dioxide on a porous polymeric sorbent, the method comprising: providing the porous polymeric sorbent, wherein the porous polymeric sorbent has a BET specific surface area equal to at least 250 m 2 /gram, the porous polymeric sorbent comprising (a) 8 to 40 weight percent of a first monomeric unit of Formula; (b) 48 to 75 weight percent of a second monomeric unit of Formula; (c) 0 to 20 weight percent of a third monomeric unit of Formula wherein R 1 is hydrogen or alkyl; and (d) 0 to 8 weight percent of a fourth monomeric unit of Formula; exposing the porous polymeric sorbent to a gas mixture comprising carbon dioxide; and sorbing carbon dioxide on the porous polymeric sorbent. providing the porous polymeric sorbent, wherein the porous polymeric sorbent has a BET specific surface area equal to at least 250 m 2 /gram, the porous polymeric sorbent comprising (a) 8 to 40 weight percent of a first monomeric unit of Formula; (b) 48 to 75 weight percent of a second monomeric unit of Formula; (c) 0 to 20 weight percent of a third monomeric unit of Formula wherein R 1 is hydrogen or alkyl; and (d) 0 to 8 weight percent of a fourth monomeric unit of Formula; (a) 8 to 40 weight percent of a first monomeric unit of Formula; (b) 48 to 75 weight percent of a second monomeric unit of Formula; (c) 0 to 20 weight percent of a third monomeric unit of Formula wherein R 1 is hydrogen or alkyl; and (d) 0 to 8 weight percent of a fourth monomeric unit of Formula; exposing the porous polymeric sorbent to a gas mixture comprising carbon dioxide; and sorbing carbon dioxide on the porous polymeric sorbent.
A computer-implemented system for executing macros on a hosted computer system, comprising: a plurality of hosted applications operable from the hosted computer system; a macro data store storing a plurality of macros that are each associated with a registered user of the hosted computer system and that each define a series of actions to be executed by at least one of the plurality of hosted applications; a processor to operate a scheduling module that identifies triggering events in the system and begins execution of one of the plurality of macros in response to an identified triggering event that corresponds to the one of the plurality of macros; and a processor permitting the registered user associated with the macros to identify other users who are authorized to use the registered user's macros. a plurality of hosted applications operable from the hosted computer system; a macro data store storing a plurality of macros that are each associated with a registered user of the hosted computer system and that each define a series of actions to be executed by at least one of the plurality of hosted applications; a processor to operate a scheduling module that identifies triggering events in the system and begins execution of one of the plurality of macros in response to an identified triggering event that corresponds to the one of the plurality of macros; and a processor permitting the registered user associated with the macros to identify other users who are authorized to use the registered user's macros.
An apparatus for separating feed for livestock along a cutting face, the apparatus being provided with at least two cutter blades which extend in a width direction of the cutting face and which are angled with respect to each other as seen in side view, characterised in that at least one of the cutter blades has an end which crosses the plane of the other cutter blade as seen in side view.
A method of embedding a pattern as a watermark into a content segment, comprising modifying the content segment by inserting a set of substantially imperceptible features that relate to the pattern, characterised in, determining an impulse response of a filter to be used for detecting the pattern; inserting the time-reversed impulse response of the filter into the segment as the set of imperceptible features; wherein the filter is an infinite impulse response filter; wherein the infinite impulse response filter comprises a semi-white frequency spectrum and provides a pseudo-random time-domain response.
Cooling system for a galley for installation in a transportation means, in particular an aircraft, comprising: - a cooling device which comprises a coolant circuit adapted to be flowed through with a coolant, - a fluid line which is adapted to be flowed through with a fluid to be cooled and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the fluid to be cooled flowing through the fluid line to the coolant circulating in the coolant circuit, - an air line which is adapted to be flowed through with air and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the coolant circulating in the coolant circuit to the air flowing through the air line, - wherein the air line, downstream of the thermal coupling of the air line with the coolant circuit of the cooling device, is connectable to a cabin region of the transportation means accommodating the galley in order to supply the cabin region with air warmed by heat transfer from the coolant circulating in the coolant circuit of the cooling device, and - wherein the air line, upstream of the thermal coupling of the air line with the coolant circuit of the cooling device, is connectable to an interior of the galley in order to supply the air line with air to be discharged from the interior of the galley. - a cooling device which comprises a coolant circuit adapted to be flowed through with a coolant, - a fluid line which is adapted to be flowed through with a fluid to be cooled and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the fluid to be cooled flowing through the fluid line to the coolant circulating in the coolant circuit, - an air line which is adapted to be flowed through with air and which is thermally coupled with the coolant circuit of the cooling device in order to transfer heat from the coolant circulating in the coolant circuit to the air flowing through the air line, - wherein the air line, downstream of the thermal coupling of the air line with the coolant circuit of the cooling device, is connectable to a cabin region of the transportation means accommodating the galley in order to supply the cabin region with air warmed by heat transfer from the coolant circulating in the coolant circuit of the cooling device, and - wherein the air line, upstream of the thermal coupling of the air line with the coolant circuit of the cooling device, is connectable to an interior of the galley in order to supply the air line with air to be discharged from the interior of the galley.
A method for producing atomized powder for glassy aluminum-based alloys, comprising the steps of: providing a positive pressure of inert gas in a melt chamber having a closed top using an inert gas inlet; supplying inert gas to the inlet from a source of inert gas; melting an aluminum alloy in a crucible and delivering molten aluminum alloy out of the crucible; receiving the molten aluminum alloy from the crucible into an atomization chamber and forming fine aluminum alloy powder from the molten alloy, while maintaining a positive pressure of inert gas in the atomization chamber; and receiving powder produced in the atomization chamber in at least one catch tank (33, 37, 41) while maintaining a positive pressure of inert gas therein. providing a positive pressure of inert gas in a melt chamber having a closed top using an inert gas inlet; supplying inert gas to the inlet from a source of inert gas; melting an aluminum alloy in a crucible and delivering molten aluminum alloy out of the crucible; receiving the molten aluminum alloy from the crucible into an atomization chamber and forming fine aluminum alloy powder from the molten alloy, while maintaining a positive pressure of inert gas in the atomization chamber; and receiving powder produced in the atomization chamber in at least one catch tank (33, 37, 41) while maintaining a positive pressure of inert gas therein.
A process for patterning a liquid crystal polymer layer, the processing comprising: contacting a liquid crystal polymer layer and a reusable alignment template (1330, 1501) comprising a surface alignment pattern such that liquid crystal molecules of the liquid crystal polymer layer are aligned to the surface alignment pattern of the reusable alignment template (1330, 1501) primarily via chemical, steric, or other intermolecular interaction; polymerizing the liquid crystal polymer layer to form a patterned polymerized liquid crystal polymer layer; and separating the patterned polymerized liquid crystal polymer layer and the reusable alignment template (1330, 1501), wherein the reusable alignment template comprises a photo-alignment layer comprising the surface alignment pattern; wherein contacting the liquid crystal polymer layer and the reusable alignment template (1330, 1501) comprises depositing the liquid crystal polymer layer on a surface of the reusable alignment template (1330, 1501), wherein depositing the liquid crystal polymer layer further comprises jet depositing the liquid crystal polymer layer; and wherein the reusable alignment template further comprises a release layer disposed over the photo-alignment layer and a second liquid crystal polymer layer disposed between the photo-alignment layer and the release layer. contacting a liquid crystal polymer layer and a reusable alignment template (1330, 1501) comprising a surface alignment pattern such that liquid crystal molecules of the liquid crystal polymer layer are aligned to the surface alignment pattern of the reusable alignment template (1330, 1501) primarily via chemical, steric, or other intermolecular interaction; polymerizing the liquid crystal polymer layer to form a patterned polymerized liquid crystal polymer layer; and separating the patterned polymerized liquid crystal polymer layer and the reusable alignment template (1330, 1501), wherein the reusable alignment template comprises a photo-alignment layer comprising the surface alignment pattern; wherein contacting the liquid crystal polymer layer and the reusable alignment template (1330, 1501) comprises depositing the liquid crystal polymer layer on a surface of the reusable alignment template (1330, 1501), wherein depositing the liquid crystal polymer layer further comprises jet depositing the liquid crystal polymer layer; and wherein the reusable alignment template further comprises a release layer disposed over the photo-alignment layer and a second liquid crystal polymer layer disposed between the photo-alignment layer and the release layer.
Device having at least one elastically deformable component as a structural part and/or bearing part, on which various deformation forces that are dependent on changing operating states and lead to component wear, which limits the component service life, act over the course of operation, characterized in that the device has a recording unit designed to detect and record a predetermined operating state that recurs at staggered times and is the same in each case, and which has an associated identical deformation force in each case, in that the device has a component-associated sensor and a downstream measuring and evaluation unit, wherein detection and recording of a predetermined operating state of this kind by the recording unit results in a measurement process being automatically startable and performable by means of a starting signal, and a component deformation being measurable by means of the sensor and the measuring and evaluation unit as a characteristic quantity for a present component rigidity for component monitoring, and the measured value being storable, in that the measuring and evaluation unit has a comparator unit by means of which a comparison of a present deformation measured value with preceding, stored deformation measured values is performable with the result that the deformation measured values stored over a relatively long service life, or corresponding characteristic quantities for the component rigidity, are approximately identical and a measurement curve formed from the measured values results in a plateau region with a small rise in inclination for the component deformation over the course of this service life, or a small drop in inclination for the component rigidity, whereupon further reliable component operation is apparent, or that, alternatively, successively and progressively increasing deformation measured values are recordable in succession over a short service life in comparison with the service life of the plateau region, so that the plateau region is exited with a larger rise in inclination for a measurement curve relating to the component deformation in comparison with the plateau region, or with a larger drop in inclination for a measurement curve relating to the component rigidity in comparison with the inclination of the plateau region, as a result of which the start of a wear-induced prescribable remaining component service life is apparent and appropriate warning information is outputtable when a rise in inclination or drop in inclination, prescribed as a threshold value, of the measurement curve is reached.
Light component for a bodywork of a motor vehicle, with a support frame having four frame parts (5, 6, 7, 8), which substantially spans over a square, and has at least two intersecting struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20) which are designed according to bionic aspects and are connected at the intersection point(s) (15, 18), and which respectively interconnect two of the frame parts (5, 6, 7, 8) arranged perpendicularly to each other, and with a panelling arranged on the support frame, wherein the support frame is formed from a fibre-reinforced plastic, characterised in that the frame parts (5, 6, 7, 8) and the struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20) are arranged mirror symmetrically to an axis of symmetry, and - wherein a part of the support frame is designed in the direction of the axis of symmetry on one side predominantly free from struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20), while the part lying opposite in the direction of the axis of symmetry has the majority of the struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20) and all intersection points (15, 18) of the struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20) with each other, - wherein the support frame is longer in the direction of the axis of symmetry than transversely to the axis of symmetry, - wherein curved struts (16, 17, 19) are provided between the struts (9, 10, 11, 12, 13, 14) which extend from the respectively longer frame part (6, 8) and at least one of the shorter frame parts in an arc back to the same frame part (6, 7, 8). - wherein a part of the support frame is designed in the direction of the axis of symmetry on one side predominantly free from struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20), while the part lying opposite in the direction of the axis of symmetry has the majority of the struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20) and all intersection points (15, 18) of the struts (9, 10, 11, 12, 13, 14, 16, 17, 19, 20) with each other, - wherein the support frame is longer in the direction of the axis of symmetry than transversely to the axis of symmetry, - wherein curved struts (16, 17, 19) are provided between the struts (9, 10, 11, 12, 13, 14) which extend from the respectively longer frame part (6, 8) and at least one of the shorter frame parts in an arc back to the same frame part (6, 7, 8).
A selective solidification apparatus comprising a build chamber, a build platform lowerable in the build chamber, a wiper for spreading powder material across the build platform to form successive powder layers of a powder bed, an energy beam unit for generating an energy beam for consolidating the powder material, a scanner for directing and focussing the energy beam onto each powder layer and a processor for controlling the scanner, wherein the processor is arranged to control the scanner to scan the energy beam across the powder bed to consolidate powder material each side of the wiper when the wiper is moving across the powder bed, characterised in that the processor is further arranged to control movement of the wiper to vary a time the wiper is stationary between strokes or a speed of the wiper based upon a size of an area to be solidified in a layer and/or scan paths for the energy beam to take in solidifying the powder material.