mhurhangee/ep-ind-claims huggingface dataset:
A method of sending a falling body of a falling body viscometer when sending the falling body loaded in a loading unit of a loading holder to a measured substance, the loading unit including a falling body holding mechanism which allows the falling body to be movable with respect to the loading unit using an extruding device while holding the falling body in the loading unit, the extruding device including an extruding pin, whereby the method comprises the following steps: - a first step of setting a standby state in which a part of the falling body advances into a measuring container such that the measured substance infiltrates into a surface of the falling body; - a second step of maintaining the state of the falling body in the first step for a specified time, characterized in that in a third step the falling body is send out from the loading unit by pressing the falling body using the extruding pin, whereby the standby state of the first step is maintained by suppressing the falling of the falling body by a frictional force which is generated between protrusion formed in an inner peripheral surface of a vertical hole of the loading unit and a peripheral surface of the falling body in the falling body holding mechanism, whereby the extruding pin is operated by a driving device such that an operation of sending the falling body may be performed automatically. - a first step of setting a standby state in which a part of the falling body advances into a measuring container such that the measured substance infiltrates into a surface of the falling body; - a second step of maintaining the state of the falling body in the first step for a specified time,
A storage device (2, 4) with two pole storage elements for electrical charges, with inverter groups (11, 28, 35) including full bridges connected in series, wherein exactly one of the full bridges of each of the inverter groups (11, 28, 35) is connected with poles of each of the storage elements, with a control unit configured to determine storage conditions and optimize charge and discharge processes of the storage elements through the full bridges based on a respective storage condition, and with a respective two-pole connection at each of the inverter groups (11, 28, 35), characterized in that the control unit includes control modules connected with one another by a data bus, further characterized by storage modules, wherein the full bridges form part of the storage modules, each of the storage modules with a bus connection configured to connect with the data bus, further with exactly one of the storage elements, and further with one of the control modules that determines its storage condition and optimizes its charging and discharging processes and that includes an interface with four control conductors to one of the full bridges for each of the inverter groups (11, 28, 35), wherein the storage device (2, 4) is configured to apply a DC voltage at the connections of at least two of the inverter groups (11, 28, 35). with two pole storage elements for electrical charges, with inverter groups (11, 28, 35) including full bridges connected in series, wherein exactly one of the full bridges of each of the inverter groups (11, 28, 35) is connected with poles of each of the storage elements, with a control unit configured to determine storage conditions and optimize charge and discharge processes of the storage elements through the full bridges based on a respective storage condition, and with a respective two-pole connection at each of the inverter groups (11, 28, 35), characterized in that the control unit includes control modules connected with one another by a data bus, further characterized by storage modules, wherein the full bridges form part of the storage modules, each of the storage modules with a bus connection configured to connect with the data bus, further with exactly one of the storage elements, and further with one of the control modules that determines its storage condition and optimizes its charging and discharging processes and that includes an interface with four control conductors to one of the full bridges for each of the inverter groups (11, 28, 35), wherein the storage device (2, 4) is configured to apply a DC voltage at the connections of at least two of the inverter groups (11, 28, 35).
A method for optimizing the configuration of an optical network which is adapted to transport optical traffic along a path from a source node to a destination node, wherein the path can be routed via any one or more of a plurality of intermediate nodes in the optical network, the method comprising the steps of: receiving an operating parameter of an optical device monitored in a plurality of nodes; comparing the received operating parameter with a threshold value; determining an operating status of an operating node along the path from the source node to the destination node based on the comparison of the received operating parameter with the threshold value; and using the determined operating status of a node as a routing criteria for computing a path for routing traffic through the optical network. receiving an operating parameter of an optical device monitored in a plurality of nodes; comparing the received operating parameter with a threshold value; determining an operating status of an operating node along the path from the source node to the destination node based on the comparison of the received operating parameter with the threshold value; and using the determined operating status of a node as a routing criteria for computing a path for routing traffic through the optical network.
A fuel charging or electricity charging port lid lock, comprising: - an elevating shaft being provided with an elevating thread on an exterior wall thereof; - a worm gear configured to drive the elevating shaft, the worm gear being provided with an inner thread and an outer gear, the worm gear being sleeved outside of the elevating shaft, and the inner thread of the worm gear being engaged with the elevating thread of the elevating shaft; and - a worm configured to drive the worm gear, the worm being provided with helical teeth at an exterior thereof, and the helical teeth being engaged with the outer gear of the worm gear; wherein the elevating shaft is configured to be capable of moving up and moving down along an axial direction of the elevating shaft and rotating about the axial direction of the elevating shaft when driven by the worm; and wherein a head portion of the elevating shaft is used to drive a fuel charging or electricity charging port lid so as to control the opening and closing of the fuel charging or electricity charging port lid. - an elevating shaft being provided with an elevating thread on an exterior wall thereof; - a worm gear configured to drive the elevating shaft, the worm gear being provided with an inner thread and an outer gear, the worm gear being sleeved outside of the elevating shaft, and the inner thread of the worm gear being engaged with the elevating thread of the elevating shaft; and - a worm configured to drive the worm gear, the worm being provided with helical teeth at an exterior thereof, and the helical teeth being engaged with the outer gear of the worm gear;
A glass powder blend characterized by comprising glass powder and additives, wherein the additives comprise copper powder, the copper powder accounts for 2-3 mass% based on the total amount of the glass powder blend in 100 mass% and the copper powder has an average particle diameter between 1.0 μm and 2.5 μm. the additives comprise copper powder, the copper powder accounts for 2-3 mass% based on the total amount of the glass powder blend in 100 mass% and the copper powder has an average particle diameter between 1.0 μm and 2.5 μm.
An optical device comprising: a photoelectric conversion element having a photoelectric conversion portion which is formed on a substrate; an optical adjustment element formed on the substrate on the side opposite to the photoelectric conversion portion; a connection terminal electrically connected to the photoelectric conversion element; and a sealing material which seals the photoelectric conversion element, the optical adjustment element and the connection terminal, wherein the optical device comprises an aperture (6; 7) on one side of the optical device through which light is allowed to enter or exit, the bottom face of the aperture (6; 7) is an interface between the optical adjustment element which is the closest to the outside, and the outside, wherein the optical adjustment element is selected from any one of a light anti-reflection element, which prevents reflection of light in the aperture (6; 7), a filter, which controls a wavelength of received light or emitted light, and an optical lens, which controls detection of light, and an exiting direction of light, and condenses light. a photoelectric conversion element having a photoelectric conversion portion which is formed on a substrate; an optical adjustment element formed on the substrate on the side opposite to the photoelectric conversion portion; a connection terminal electrically connected to the photoelectric conversion element; and a sealing material which seals the photoelectric conversion element, the optical adjustment element and the connection terminal, wherein the optical device comprises an aperture (6; 7) on one side of the optical device through which light is allowed to enter or exit, the bottom face of the aperture (6; 7) is an interface between the optical adjustment element which is the closest to the outside, and the outside, wherein the optical adjustment element is selected from any one of a light anti-reflection element, which prevents reflection of light in the aperture (6; 7), a filter, which controls a wavelength of received light or emitted light, and an optical lens, which controls detection of light, and an exiting direction of light, and condenses light.
A gas burner with inward-facing flame, comprising a base body adapted for being disposed under a cooktop and a discoid lid disposed above said base body, said base body comprising: - a central chamber with cylindrical or truncated-conical shape, adapted for being connected to at least one horizontal Venturi tube fed by at least one gas injector; and - a peripheral annular chamber, - at least two partitions defining at least two apertures providing communication between said central chamber and said peripheral annular chamber, said lid comprising: - a central dish disposed onto said central chamber of the base body, - an intermediate toroidal portion disposed onto said partitions of the base body, and - a flame ring disposed onto said peripheral annular chamber of the base body and presenting an inclined surface where a plurality of ports is obtained, communicating with said peripheral annular chamber, said ports presenting an axis inclined upwards and towards the vertical axis of the burner for propagation of flame inwards. - a central chamber with cylindrical or truncated-conical shape, adapted for being connected to at least one horizontal Venturi tube fed by at least one gas injector; and - a peripheral annular chamber, - at least two partitions defining at least two apertures providing communication between said central chamber and said peripheral annular chamber, - a central dish disposed onto said central chamber of the base body, - an intermediate toroidal portion disposed onto said partitions of the base body, and - a flame ring disposed onto said peripheral annular chamber of the base body and presenting an inclined surface where a plurality of ports is obtained, communicating with said peripheral annular chamber, said ports presenting an axis inclined upwards and towards the vertical axis of the burner for propagation of flame inwards.
A computer-implemented method of providing data relating to atmospheric conditions in an airspace using observations of aircraft trajectories through the airspace, the method comprising a computer system: (a) identifying aircraft flying within the airspace; (b) for at least some of the aircraft identified, processing the aircraft by determining an observed trajectory of the aircraft, determining initial conditions of the aircraft, determining the type of the aircraft and retrieving from memory aircraft performance data relating to that type of aircraft, and retrieving from memory aircraft intent data relating to the aircraft stored therein, wherein the aircraft intent data provides an unambiguous description of the aircraft's trajectory through the airspace expressed, for example, using a formal language; (c) using as inputs the observed trajectories, the initial conditions, the aircraft performance data, and the aircraft intent data for the processed aircraft; (d) inferring from the inputs atmospheric conditions data that, in combination with the aircraft intent data and the aircraft performance data, would give rise to the observed trajectory for each of the processed aircraft; and (e) providing as an output the inferred atmospheric conditions data for the airspace. (a) identifying aircraft flying within the airspace; (b) for at least some of the aircraft identified, processing the aircraft by determining an observed trajectory of the aircraft, determining initial conditions of the aircraft, determining the type of the aircraft and retrieving from memory aircraft performance data relating to that type of aircraft, and retrieving from memory aircraft intent data relating to the aircraft stored therein, wherein the aircraft intent data provides an unambiguous description of the aircraft's trajectory through the airspace expressed, for example, using a formal language; determining an observed trajectory of the aircraft, determining initial conditions of the aircraft, determining the type of the aircraft and retrieving from memory aircraft performance data relating to that type of aircraft, and retrieving from memory aircraft intent data relating to the aircraft stored therein, wherein the aircraft intent data provides an unambiguous description of the aircraft's trajectory through the airspace expressed, for example, using a formal language; (c) using as inputs the observed trajectories, the initial conditions, the aircraft performance data, and the aircraft intent data for the processed aircraft; (d) inferring from the inputs atmospheric conditions data that, in combination with the aircraft intent data and the aircraft performance data, would give rise to the observed trajectory for each of the processed aircraft; and (e) providing as an output the inferred atmospheric conditions data for the airspace.
Slipper comprising: - a sole having a plurality of holes; - an upper anchored to said sole by means of said holes which comprises at least a lace and one or more anchorage elements of said lace to said sole, each of said anchorage elements comprising a respective base housed in one of said holes and a respective projection overhanging from said base and having at least one through hole through which said lace is inserted; wherein at least one of said anchorage elements comprises retention means (53, 63, 73) suitable for securing the position of the anchorage element itself with respect to said sole and characterized by the fact that said retention means (53, 63, 73) comprise at least a protrusion defined by said projection and having a truncated cone shape. - a sole having a plurality of holes; - an upper anchored to said sole by means of said holes which comprises at least a lace and one or more anchorage elements of said lace to said sole, each of said anchorage elements comprising a respective base housed in one of said holes and a respective projection overhanging from said base and having at least one through hole through which said lace is inserted; wherein at least one of said anchorage elements comprises retention means (53, 63, 73) suitable for securing the position of the anchorage element itself with respect to said sole and
An in vitro method for inducing T cells for a cell-based immunotherapy, comprising the steps of: providing Rag1 and/or Rag2 gene knockout human pluripotent stem cells bearing genes encoding a T cell receptor specific for a desired antigen, inducing CD4CD8 double positive T cells from the pluripotent stem cells of step, and inducing CD8 single positive T cells from the CD4CD8 double positive cells of step. providing Rag1 and/or Rag2 gene knockout human pluripotent stem cells bearing genes encoding a T cell receptor specific for a desired antigen, inducing CD4CD8 double positive T cells from the pluripotent stem cells of step, and inducing CD8 single positive T cells from the CD4CD8 double positive cells of step.
A wind turbine rotor blade comprising a rotor blade tip and a rotor blade root as well as a lightning protection system, wherein the lightning protection system has a lightning protection conductor and a heatable coating in the form of a paint on the surface of the rotor blade, wherein the heatable coating is galvanically coupled to the lightning protection conductor, wherein the heatable coating is based on an acrylate basis and has carbon nanomaterials and graphite. a rotor blade tip and a rotor blade root as well as a lightning protection system, wherein the lightning protection system has a lightning protection conductor and a heatable coating in the form of a paint on the surface of the rotor blade, wherein the heatable coating is galvanically coupled to the lightning protection conductor, wherein the heatable coating is based on an acrylate basis and has carbon nanomaterials and graphite.
A computer-implemented method for performing communications between a first computer and second computer, the method comprising performing, by the second computer: receiving a first message including a first computer blinded public key and first encrypted authentication information from the first computer, wherein the first computer blinded public key is generated by the first computer using a first computer blinding factor and a first computer public key; in response to receiving the first message, generating a first shared secret using the first computer blinded public key and a second computer private key; decrypting the first encrypted authentication information using the first shared secret to obtain first authentication information of the first computer; and authenticating the first computer using the first authentication information; in response to the authenticating of the first computer, encrypting second authentication information of the second computer to obtain second encrypted authentication information, the encrypting of the second authentication information based on the second computer private key and the first computer public key; and sending a second message including the second encrypted authentication information to the first computer, thereby enabling the first computer to authenticate the second computer using the second authentication information. receiving a first message including a first computer blinded public key and first encrypted authentication information from the first computer, wherein the first computer blinded public key is generated by the first computer using a first computer blinding factor and a first computer public key; in response to receiving the first message, generating a first shared secret using the first computer blinded public key and a second computer private key; decrypting the first encrypted authentication information using the first shared secret to obtain first authentication information of the first computer; and authenticating the first computer using the first authentication information; in response to the authenticating of the first computer, encrypting second authentication information of the second computer to obtain second encrypted authentication information, the encrypting of the second authentication information based on the second computer private key and the first computer public key; and sending a second message including the second encrypted authentication information to the first computer, thereby enabling the first computer to authenticate the second computer using the second authentication information.
An apparatus for preparing a pre-form comprising at least one layer of fibre tows being at least partly fixed by a resin, wherein the apparatus comprises: - a work surface; - a fibre tow distribution device comprising a plurality of distribution passages, each distribution passage being adapted for receiving and delivering a fibre tow, and the passages being arranged to provide a distribution distance between the delivered fibre tows; - a fibre tow retention device adapted to retain a plurality of fibre tows; and - a manipulation device adapted to move the fibre tow distribution device relative to the fibre tow retention device; wherein the apparatus is arranged so that free ends of the fibre tows can be delivered from the fibre tow distribution device to the fibre tow retention device, and the fibre tow retention device is adapted for retention of the free ends at the distribution distance so that mutual movement of the fibre tow distribution device and the fibre tow retention device away from each other causes drawing of the fibre tows through the distribution passages and distribution of the fibre tows onto the work surface. - a work surface; - a fibre tow distribution device comprising a plurality of distribution passages, each distribution passage being adapted for receiving and delivering a fibre tow, and the passages being arranged to provide a distribution distance between the delivered fibre tows; - a fibre tow retention device adapted to retain a plurality of fibre tows; and - a manipulation device adapted to move the fibre tow distribution device relative to the fibre tow retention device;
A method of scheduling performed by a network node comprising a distributed local oscillator architecture in which elements (18 1,.., 18 i,.., 18 N) of an antenna array, for simultaneously transmitting multiple layers, through multiple beams in case of line-of-sight communication or through multi-user MIMO, have at least partly uncorrelated local oscillator signals, the network node having wireless connectivity to at least two transmitter nodes (2a, 2b), the method comprising: - calculating a phase noise value between one or more layers received in each element (18 1,.., 18 i,.., 18 N) from a first transmitter node and one or more layers received in each element (18 1,.., 18 i,.., 18 N) from a second transmitter node, and - determining a scheduling allocation for the at least two transmitter nodes (2a, 2b), taking the calculated phase noise value into account. - calculating a phase noise value between one or more layers received in each element (18 1,.., 18 i,.., 18 N) from a first transmitter node and one or more layers received in each element (18 1,.., 18 i,.., 18 N) from a second transmitter node, and - determining a scheduling allocation for the at least two transmitter nodes (2a, 2b), taking the calculated phase noise value into account.