mhurhangee/ep-ind-claims huggingface dataset:
A data storage method, characterized in that, the data storage method comprises steps of: receiving (S 102), by a base station, a storage request for storing a content source sent by a service capability exposure function, wherein the content source comes from a third-party server; and storing (S 104), by the base station, the content source according to the storage request in a local storage space, wherein the method further comprises at least one of: detecting, by the base station, the storage space of the base station when the base station is restarted, and sending detected information with respect of the storage space to the service capability exposure function; detecting, by the base station, the storage space of the base station according to a predetermined period, and sending the detected information with respect of the storage space to the service capability exposure function; receiving, by the base station, a query request for querying the storage space of the base station sent by the service capability exposure function, detecting the storage space of the base station according to the query request, and sending the detected information with respect to the storage space to the service capability exposure function. receiving (S 102), by a base station, a storage request for storing a content source sent by a service capability exposure function, wherein the content source comes from a third-party server; and storing (S 104), by the base station, the content source according to the storage request in a local storage space, wherein the method further comprises at least one of: detecting, by the base station, the storage space of the base station when the base station is restarted, and sending detected information with respect of the storage space to the service capability exposure function; detecting, by the base station, the storage space of the base station according to a predetermined period, and sending the detected information with respect of the storage space to the service capability exposure function; receiving, by the base station, a query request for querying the storage space of the base station sent by the service capability exposure function, detecting the storage space of the base station according to the query request, and sending the detected information with respect to the storage space to the service capability exposure function. detecting, by the base station, the storage space of the base station when the base station is restarted, and sending detected information with respect of the storage space to the service capability exposure function; detecting, by the base station, the storage space of the base station according to a predetermined period, and sending the detected information with respect of the storage space to the service capability exposure function; receiving, by the base station, a query request for querying the storage space of the base station sent by the service capability exposure function, detecting the storage space of the base station according to the query request, and sending the detected information with respect to the storage space to the service capability exposure function.
A cableway cabin with a floor which can be walked on at least during boarding the cableway cabin and with at least two seats which, in a side view of the cableway cabin, are arranged on both sides of an imaginary vertical line on which the centre of gravity is located during operation of the cableway cabin, wherein the viewing direction of seated passengers respectively corresponding to the seats is at least temporarily facing away from each other with respect to the imaginary vertical line in the side view and the seats are respectively outermost seats with respect to the imaginary vertical line in the side view, to thereby offer passengers a view not obstructed by other passengers, characterized in that the seats are movable between a viewing position, in which the viewing direction of the passengers sitting on the seats is at least partially, preferably completely, facing away from each other with respect to the imaginary vertical line, and a boarding position, in which the viewing direction of the passengers with respect to the imaginary vertical line is preferably facing each other.
A touch sensor assembly comprising: a sensor housing provided behind an exterior surface of a household appliance in which a touch input area is provided; a sensor PCB provided inside the sensor housing and having a top surface on which a conductive layer is formed; a touch sensor, the touch sensor including a metal plate having a bottom surface in contact with the conductive layer, wherein the touch sensor further includes: a ceramic element provided on a top surface of the metal plate, characterised by a spacer having a sensor hole formed at a position corresponding to the sensor and having a bottom surface attached to a top surface of the conductive layer; a conductive foil attached to a top surface of the spacer and having a bottom surface on which an inner guide line configured to apply an electric current to the ceramic element and an outer guide line configured to apply an electric current to the metal plate are printed; and a contact layer (745; 746) formed on a top surface of the conductive foil, wherein the contact layer (745; 746) is configured to protrude at a position corresponding to a position of the inner guide line. a sensor housing provided behind an exterior surface of a household appliance in which a touch input area is provided; a sensor PCB provided inside the sensor housing and having a top surface on which a conductive layer is formed; a touch sensor, the touch sensor including a metal plate having a bottom surface in contact with the conductive layer, wherein the touch sensor further includes: a ceramic element provided on a top surface of the metal plate, characterised by a spacer having a sensor hole formed at a position corresponding to the sensor and having a bottom surface attached to a top surface of the conductive layer; a conductive foil attached to a top surface of the spacer and having a bottom surface on which an inner guide line configured to apply an electric current to the ceramic element and an outer guide line configured to apply an electric current to the metal plate are printed; and a contact layer (745; 746) formed on a top surface of the conductive foil, a ceramic element provided on a top surface of the metal plate, characterised by a spacer having a sensor hole formed at a position corresponding to the sensor and having a bottom surface attached to a top surface of the conductive layer; a conductive foil attached to a top surface of the spacer and having a bottom surface on which an inner guide line configured to apply an electric current to the ceramic element and an outer guide line configured to apply an electric current to the metal plate are printed; and a contact layer (745; 746) formed on a top surface of the conductive foil, wherein the contact layer (745; 746) is configured to protrude at a position corresponding to a position of the inner guide line.
A pivot and swivel joint comprising a rotary sleeve having an axially continuous recess and a swivel sleeve connected thereto via a swivel axis having an axially continuous recess, which is swivelable relative to the rotary sleeve about the swivel axis, wherein at the axial end of the rotary sleeve facing away from the swivel axis a rotary axis is configured, characterized in that a sealing hose is disposed between the rotary sleeve and the swivel sleeve, which by a first axial end sealingly abuts at the recess of the rotary sleeve and by the opposite second axial end is sealingly disposed at the axial end of the swivel sleeve.
A control surface for an aircraft, comprising: an outer skin; and a core coupled to the outer skin, the core including a plurality of folded corrugations, wherein a height of the core decreases in a direction extending from a leading edge of the control surface to a trailing edge of the control surface; wherein the plurality of folded corrugations comprises a plurality of ridges and a plurality of grooves, the plurality of ridges being located at the outer skin and the plurality of grooves being located at an inner skin, characterised in that a pitch of the ridges proximate the trailing edge is less than a pitch of the ridges proximate the leading edge. an outer skin; and a core coupled to the outer skin, the core including a plurality of folded corrugations, wherein a height of the core decreases in a direction extending from a leading edge of the control surface to a trailing edge of the control surface; wherein the plurality of folded corrugations comprises a plurality of ridges and a plurality of grooves, the plurality of ridges being located at the outer skin and the plurality of grooves being located at an inner skin, characterised in that a pitch of the ridges proximate the trailing edge is less than a pitch of the ridges proximate the leading edge.
A method of preparing silver-coated copper nanowires having a core-shell structure comprising: (a) stirring an aqueous solution containing an alkali, a copper compound and a capping agent in water; (b) producing copper nanowires by adding a reducing agent to the aqueous solution to reduce copper ions; (c) washing and drying produced copper nanowires; (d) removing an oxide film from the copper nanowires produced in step (c) in a copper nanowire solution; (e) adding a reducing agent to the solution of step (d), adjusting pH 8 to 11 and then forming a silver coating while adding a silver nitrate-ammonia complex solution dropwise; and (f) washing and drying silver-coated copper nanowires prepared in step (e). (a) stirring an aqueous solution containing an alkali, a copper compound and a capping agent in water; (b) producing copper nanowires by adding a reducing agent to the aqueous solution to reduce copper ions; (c) washing and drying produced copper nanowires; (d) removing an oxide film from the copper nanowires produced in step (c) in a copper nanowire solution; (e) adding a reducing agent to the solution of step (d), adjusting pH 8 to 11 and then forming a silver coating while adding a silver nitrate-ammonia complex solution dropwise; and (f) washing and drying silver-coated copper nanowires prepared in step (e).
A drag reducing system for trailers comprising a first and a second air flow redirection means, each having a first end part and a second end part, wherein the first and second air flow redirection means respectively extending from its first to its second end part, and a plurality of connection brackets, wherein the plurality of connection brackets are arranged to be connected to a first and a second rear door of a trailer, and the first and the second air flow redirection means are connected to the plurality of connection brackets, wherein the first and the second air flow redirection means comprise a plurality of magnetic connection devices permitting the first and the second air flow redirection means to be kept in an active mode or in an inactive mode, wherein in the active mode the first air flow redirection means is substantially directed from its first end part towards its second end part away from the first rear door of the trailer, and wherein in the active mode the second air flow redirection means is substantially directed from its first end part towards its second end part away from the second rear door of the trailer, and wherein in the inactive mode the first air flow redirection means is substantially directed from its first end part towards its second end part along the first rear door of the trailer, and wherein in the inactive mode the second air flow redirection means is substantially directed from its first end part towards its second end part along the second rear door of the trailer, characterised in that the plurality of magnetic connection devices comprise a first group of magnetic connection devices arranged at a short side at the first end part of each of the first and the second air flow redirection means, the short side extending substantially perpendicular to the extension from the first end part to the second end part, so that the short side of the first end part of the first air flow redirection means is facing the first rear door of the trailer and so that the short side of the first end part of the second air flow redirection means is facing the second rear door of the trailer when the first and the second air flow redirection means are in the active mode, permitting to keep the first and the second air flow redirection means in the active mode.
An apparatus (11, 12, 50, 60, 100, 200) for transmitting a reference signal, comprising: N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt); and a processor (51, 61) operatively coupled with the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt) and configured to: generate K reference signal sequence vectors based on K reference signal sequences and K virtual antenna vectors, where K<N; and transmit the K reference signal sequence vectors through the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt), wherein the K reference signal sequence vectors are transmitted during a first period; characterized in that the processor (51, 61) is further configured to: generate N-K reference signal sequence vectors based on N-K reference signal sequences and N-K virtual antenna vectors; and transmit the N-K reference signal sequence vectors through the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt) during a second period, wherein the K virtual antenna vectors and the N-K virtual antenna vectors are different column vectors selected from a virtual antenna matrix having N*N size. N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt); and a processor (51, 61) operatively coupled with the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt) and configured to: generate K reference signal sequence vectors based on K reference signal sequences and K virtual antenna vectors, where K<N; and transmit the K reference signal sequence vectors through the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt), wherein the K reference signal sequence vectors are transmitted during a first period; generate K reference signal sequence vectors based on K reference signal sequences and K virtual antenna vectors, where K<N; and transmit the K reference signal sequence vectors through the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt), wherein the K reference signal sequence vectors are transmitted during a first period; characterized in that the processor (51, 61) is further configured to: generate N-K reference signal sequence vectors based on N-K reference signal sequences and N-K virtual antenna vectors; and transmit the N-K reference signal sequence vectors through the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt) during a second period, wherein the K virtual antenna vectors and the N-K virtual antenna vectors are different column vectors selected from a virtual antenna matrix having N*N size. generate N-K reference signal sequence vectors based on N-K reference signal sequences and N-K virtual antenna vectors; and transmit the N-K reference signal sequence vectors through the N antennas (59; 69; 190-1, 190-2, 190-Nt; 290-1, 290-Nt) during a second period, wherein the K virtual antenna vectors and the N-K virtual antenna vectors are different column vectors selected from a virtual antenna matrix having N*N size.
A method of coating an article comprising the steps of: providing a powder comprising coated particles, wherein coated particles consist of a calcium phosphate core and a coating consisting of titanium or titanium alloy; and spray coating the powder onto a surface of a said article to form a composite coating which comprises a well-mixed matrix of the particle core material and of the particle coat material. providing a powder comprising coated particles, wherein coated particles consist of a calcium phosphate core and a coating consisting of titanium or titanium alloy; and spray coating the powder onto a surface of a said article to form a composite coating which comprises a well-mixed matrix of the particle core material and of the particle coat material.
A baggage tag to be wrapped around and fastened to a luggage, such that the luggage can be tracked and traced via the baggage tag, the baggage tag comprising: - a face material made of paper with a first side and a second side; - a liner with a first side and a second side, wherein the first side is siliconized and facing against the second side of the face material; and - a pressure sensitive adhesive layer, which is arranged between the second side of the face material and the siliconized first side of the liner; characterized in that the baggage tag further comprising an RFID tag which tag comprises an RFID antenna and an IC, which IC is attached onto the antenna such that the antenna and the IC form the RFID tag and wherein the RFID antenna is formed directly onto the non-siliconized second side of the liner. - a face material made of paper with a first side and a second side; - a liner with a first side and a second side, wherein the first side is siliconized and facing against the second side of the face material; and - a pressure sensitive adhesive layer, which is arranged between the second side of the face material and the siliconized first side of the liner;
Combustion chamber of a turbine, in particular of a turbine having a thermodynamic cycle with a recuperator, for the production of energy, in particular electrical energy, having a housing accommodating a flame tube with a diffusion partition bearing a flame stabilizer comprising a perforated air diffuser and a mixing tube, said chamber also having a means for injecting at least one fuel, the perforated diffuser comprising at least two circumferential rows (C1, C2) of holes (84; 84a, 84b) and the housing, of cylindrical shape, being closed at one of its ends by an injector-bearing partition and at the other of its ends by a partition having an opening with a diameter less than that of said housing, characterized in that said injector-bearing partition comprises a plate, through which said means for injecting at least one fuel is mounted, in the form of an injector coaxial with the flame tube, said plate being surrounded by a semi-toric air-deflecting wall, the concavity of which is directed towards the flame tube and which is connected to the periphery of the housing.
Coupling unit (10, 10a, 10b) for transmitting torques from a drive (11, 11b) to an output (12, 12a, 12b), the coupling comprising a drive-side connector device, such as a flange, having a plurality of drive-side fixing means (15a, 15b, 15c) disposed around a drive-side axis of rotation assigned to the drive-side connector device, and comprising an output-side connector device, such as a flange, having a plurality of output-side fixing means (16a, 16b, 16c), and having connecting elements (19, 19a, 19b, 19c), such as connecting rods, which are disposed on the one hand on a drive-side fixing means and on the other hand on an output-side fixing means by means of an articulated joint, and the articulated joint is provided in the form of several joints (21, 22, 23) connected in series, characterised in that the drive-side fixing means and the output-side fixing means coupled with the latter by means of a connecting element are disposed circumferentially spaced apart from one another relative to the drive-side axis of rotation by 80° to 100°, in particular by 85° to 95°, more particularly by substantially 90°.
A combination of a detachable seat cover and a vehicle seat having a covering member, the seat having an outer surface which includes a depressed surface portion, side top surfaces, and side transition surfaces extending from the depressed surface portion to the side top surfaces, the detachable seat cover comprising: a seat cover body that is shaped to cover the outer surface of the seat; and a pair of elastic bands that are attached to a rear surface of the seat cover body; wherein the pair of elastic bands are configured to be stretched so as to follow the contours of the outer surface of the seat when the seat cover body is applied to the seat, wherein the seat cover body is configured to follow the contours of the outer surface of the seat with the pair of elastic bands when the pair of elastic bands are stretched, and wherein the pair of elastic bands are respectively positioned so as to extend along both sides of the depressed surface portion characterised in that the pair of elastic bands are respectively positioned to partially cover the side transition surfaces when the seat cover body is attached to the seat, and in that each of the elastic bands has a length shorter than the distance between one end portion of the seat cover body on which one end portion of each of the elastic bands is sewed and the other end portion of the seat cover body on which the other end portion of each of the elastic bands is sewed. a seat cover body that is shaped to cover the outer surface of the seat; and a pair of elastic bands that are attached to a rear surface of the seat cover body; wherein the pair of elastic bands are configured to be stretched so as to follow the contours of the outer surface of the seat when the seat cover body is applied to the seat, wherein the seat cover body is configured to follow the contours of the outer surface of the seat with the pair of elastic bands when the pair of elastic bands are stretched, and wherein the pair of elastic bands are respectively positioned so as to extend along both sides of the depressed surface portion characterised in that the pair of elastic bands are respectively positioned to partially cover the side transition surfaces when the seat cover body is attached to the seat, and in that each of the elastic bands has a length shorter than the distance between one end portion of the seat cover body on which one end portion of each of the elastic bands is sewed and the other end portion of the seat cover body on which the other end portion of each of the elastic bands is sewed.