mhurhangee/ep-ind-claims huggingface dataset:
A mobile terminal (100, 200), comprising: a neck band unit comprising a main power supply unit and configured to be wearable on a user's neck in a separated configuration; a frame configured to be wearable on a user's head in the separated configuration; and an input/output module located at a portion of the frame, wherein the frame is electrically coupled to the neck band unit in a connected configuration and is electrically disconnected from the neck band unit in the separated configuration, wherein during the connected configuration, the main power supply unit provides power to the input/output module, wherein the neck band unit further comprises accommodation recesses corresponded to the exterior shape of a portion of the frame to receive the portion of the frame to facilitate the connected configuration, wherein the neck band unit comprises a first accommodation portion extending from the accommodation recesses and a connector protruding from the first accommodation portion, and the input/output module comprises a port for electrical coupling with the connector corresponding to the connector such that the connector is insertable into the port to be in the connected configuration, and wherein the neck band unit and the frame are wearable on the user's neck or head in the connected configuration. a neck band unit comprising a main power supply unit and configured to be wearable on a user's neck in a separated configuration; a frame configured to be wearable on a user's head in the separated configuration; and an input/output module located at a portion of the frame, wherein the frame is electrically coupled to the neck band unit in a connected configuration and is electrically disconnected from the neck band unit in the separated configuration, wherein during the connected configuration, the main power supply unit provides power to the input/output module, wherein the neck band unit further comprises accommodation recesses corresponded to the exterior shape of a portion of the frame to receive the portion of the frame to facilitate the connected configuration, wherein the neck band unit comprises a first accommodation portion extending from the accommodation recesses and a connector protruding from the first accommodation portion, and the input/output module comprises a port for electrical coupling with the connector corresponding to the connector such that the connector is insertable into the port to be in the connected configuration, and wherein the neck band unit and the frame are wearable on the user's neck or head in the connected configuration.
A fuel pump assembly comprising a spring seat, the fuel pump assembly further including a pump housing, a pump head (22a', 22b', 22c'), a tappet, a plunger, and a return spring, the pump housing including a bore (20a', 20b', 20c') for receiving the tappet, the pump head (22a', 22b', 22c') including a plunger bore, the plunger being driven in a reciprocal manner within the plunger bore by a drive arrangement to pressurise fuel disposed within a pumping chamber defined by the pump head (22a', 22b', 22c') and the plunger, the tappet including at least one vent for allowing the passage of fuel from the upper cam box to a lower cam box.formed circumferentially around a side wall portion and/or a base portion of the tappet and being operably disposed between the drive arrangement and the plunger, the spring seat is coupled with the plunger and disposed within the side wall portion and the base portion defining an upper cam box defined within the tappet, the return spring disposed between the spring seat and the pump head (22a', 22b', 22c') to bias the plunger against the tappet at an interface, the spring seat characterised by the spring seat comprising a deflector surface including an annularly tapered portion which is used to direct high temperature fuel outwardly through plunger tappet vents and the lower cam box during the pumping stroke and, wherein the spring seat is coupled with the plunger at a distance from the interface between the plunger and the tappet along a longitudinal axis of the plunger, the distance is between 3.0mm to 4.0mm.
An airfoil comprising: an airfoil wall defining a leading end, a trailing end, and first and second sides (62c, 62d) joining the leading end and the trailing end; first and second ribs each connecting the first and second sides of the airfoil wall (62c, 62d), each of the first and second ribs defining a tube portion circumscribing a rib passage and including cooling apertures, and first and second connector arms (70a, 70b) solely joining the tube portion to, respectively, the first and second sides of the airfoil wall (62c, 62d), the airfoil wall and the first and second ribs bounding a cooling channel there between, characterized by the cooling apertures of the first and second ribs opening at the cooling channel such that there is a cooling circuit in which the rib passage of the first rib is fluidly connected to the rib passage of the second rib through the cooling apertures of the first rib, then from the cooling apertures of the first rib to the cooling channel, and then from the cooling channel to the cooling apertures of the second rib. an airfoil wall defining a leading end, a trailing end, and first and second sides (62c, 62d) joining the leading end and the trailing end; first and second ribs each connecting the first and second sides of the airfoil wall (62c, 62d), each of the first and second ribs defining a tube portion circumscribing a rib passage and including cooling apertures, and first and second connector arms (70a, 70b) solely joining the tube portion to, respectively, the first and second sides of the airfoil wall (62c, 62d), a tube portion circumscribing a rib passage and including cooling apertures, and first and second connector arms (70a, 70b) solely joining the tube portion to, respectively, the first and second sides of the airfoil wall (62c, 62d), the airfoil wall and the first and second ribs bounding a cooling channel there between, characterized by the cooling apertures of the first and second ribs opening at the cooling channel such that there is a cooling circuit in which the rib passage of the first rib is fluidly connected to the rib passage of the second rib through the cooling apertures of the first rib, then from the cooling apertures of the first rib to the cooling channel, and then from the cooling channel to the cooling apertures of the second rib.
A cooling channel for a gas turbine engine comprising: a first surface to be cooled by a flow of cooling air, the first surface including: a pedestal array physically connected to the first surface, the pedestal array including: a first row of pedestals extending from the first surface; and a second row of pedestals extending from the first surface and running in a direction generally parallel to the first row of pedestals; and a first row of contour bumps extending from the first surface between the first row of pedestals and the second row of pedestals and running in a direction generally parallel to the first row of pedestals; the first row of contour bumps aligned such that at least one contour bump of the first row of contour bumps is positioned immediately downstream of a pedestal of the first row of pedestals or immediately upstream of a pedestal of the second row of pedestals; characterized in that, the first row of contour bumps extends a first distance from the first surface, the first row of pedestals extends a second distance from the first surface; the second row of pedestals extends a third distance from the first surface, and the first distance is less than 40% and more than 5% of the second distance and the third distance, and/or wherein the first row of contour bumps restricts the flow of cooling air between the first row of pedestals and the second row of pedestals to an extent less than the first row of pedestals and the second row of pedestals restrict the flow of cooling air. a first row of pedestals extending from the first surface; and a second row of pedestals extending from the first surface and running in a direction generally parallel to the first row of pedestals; and a first row of contour bumps extending from the first surface between the first row of pedestals and the second row of pedestals and running in a direction generally parallel to the first row of pedestals; the first row of contour bumps aligned such that at least one contour bump of the first row of contour bumps is positioned immediately downstream of a pedestal of the first row of pedestals or immediately upstream of a pedestal of the second row of pedestals; characterized in that, the first row of contour bumps extends a first distance from the first surface, the first row of pedestals extends a second distance from the first surface; the second row of pedestals extends a third distance from the first surface, and the first distance is less than 40% and more than 5% of the second distance and the third distance, and/or wherein the first row of contour bumps restricts the flow of cooling air between the first row of pedestals and the second row of pedestals to an extent less than the first row of pedestals and the second row of pedestals restrict the flow of cooling air.
Method for detecting a nucleic acid, comprising the steps of, a. amplifying the nucleic acid to be detected, b. during or after amplification, hybridizing to said nucleic acid to be detected a first probe that comprises an abasic site, additionally carrying a detectable label, wherein the position of the abasic site corresponds to a position known to have a polymorphism in said nucleic acid to be detected, c. and wherein said nucleic acid is detected if hybridization occurs, wherein the amplification method is real-time PCR and the melting temperature and/or point of said probe is determined during PCR or post PCR, wherein the method comprises at least one further probe which also comprises an abasic site but which carries the same label as said first hybridization probe and wherein the probes are distinguishable due to their difference in melting temperatures. a. amplifying the nucleic acid to be detected, b. during or after amplification, hybridizing to said nucleic acid to be detected a first probe that comprises an abasic site, additionally carrying a detectable label, wherein the position of the abasic site corresponds to a position known to have a polymorphism in said nucleic acid to be detected, c. and wherein said nucleic acid is detected if hybridization occurs,
A method for determining a susceptibility to myocardial infarction or coronary artery disease in a human individual from a Caucasian population, comprising determining the presence or absence of at least one allele of at least one polymorphic marker in a nucleic acid sample obtained from the individual wherein the at least one polymorphic marker is selected from the marker rs11751605, and markers in linkage disequilibrium therewith selected from the group consisting of the markers set forth in table 5, and wherein the presence of the at least one allele is indicative of a susceptibility to myocardial infarction or coronary artery disease in individuals from a Caucasian population.
Covering element for a floor covering comprising an upper surface having a relief structure, wherein the covering element comprises a support and a covering that covers an upper surface of the support, wherein the relief structure is provided in the support, wherein the covering comprises a glaze covering, wherein said relief structure comprises excavations having bottoms showing a deepness decreasing inclination towards at least an edge (4,4') of the covering element, wherein the relief structure represents a wood pattern, a stone pattern or a cement pattern, characterized in that the covering element is at least partially made of a ceramic material.
Method for controlling a combustion process, at least one substitute fuel in the form of a dispersible fraction being used, at least part of the substitute fuel undergoing a vibrational spectroscopic analysis in a first analysis device and the values determined in the analysis being used for controlling the combustion process, characterized in that the vibrational spectroscopic analysis is performed by means of terahertz spectroscopy, wherein, in dependence on the values determined in the vibrational spectroscopic analysis and/or at certain times, a part of the substitute fuel already analyzed in the first analysis device is discharged and sent for a second chemical analysis.
An inspection fixture for a top guide of a boiling water reactor comprising: a frame sized to rest and be supported on a top edge of a fuel assembly opening within the top guide; a central shaft rotatably supported from the frame extends down below the fuel assembly opening, substantially along an axis of a fuel assembly to be positioned below the opening, when the frame is supported on the top edge of the fuel assembly opening; characterized by: a linkage assembly fixedly connected to the central shaft extends laterally therefrom with a hinged distal linkage block having a hinge line substantially parallel to and spaced from the central shaft; a wheel track supported from said frame in a manner to extend around a periphery of the fuel assembly opening, substantially proximate a border thereof when the frame is supported on the top edge of the fuel assembly opening; a cam follower that rides on the wheel track and is supported from the distal linkage block; and a camera support bracket connected to the central shaft and rotationally connected to the distal linkage block of the linkage assembly. a frame sized to rest and be supported on a top edge of a fuel assembly opening within the top guide; a central shaft rotatably supported from the frame extends down below the fuel assembly opening, substantially along an axis of a fuel assembly to be positioned below the opening, when the frame is supported on the top edge of the fuel assembly opening; characterized by: a linkage assembly fixedly connected to the central shaft extends laterally therefrom with a hinged distal linkage block having a hinge line substantially parallel to and spaced from the central shaft; a wheel track supported from said frame in a manner to extend around a periphery of the fuel assembly opening, substantially proximate a border thereof when the frame is supported on the top edge of the fuel assembly opening; a cam follower that rides on the wheel track and is supported from the distal linkage block; and a camera support bracket connected to the central shaft and rotationally connected to the distal linkage block of the linkage assembly. a linkage assembly fixedly connected to the central shaft extends laterally therefrom with a hinged distal linkage block having a hinge line substantially parallel to and spaced from the central shaft; a wheel track supported from said frame in a manner to extend around a periphery of the fuel assembly opening, substantially proximate a border thereof when the frame is supported on the top edge of the fuel assembly opening; a cam follower that rides on the wheel track and is supported from the distal linkage block; and a camera support bracket connected to the central shaft and rotationally connected to the distal linkage block of the linkage assembly.
An apparatus, comprising: a valve controller operatively coupled to a first valve and a second valve, the second valve operatively positioned downstream from and in series, in a flow direction, with the first valve, the valve controller to control a position of the first valve and a position of the second valve based on a coordinated control signal received by the valve controller; wherein the first valve is an isolation valve and the second valve is a control valve. a valve controller operatively coupled to a first valve and a second valve, the second valve operatively positioned downstream from and in series, in a flow direction, with the first valve, the valve controller to control a position of the first valve and a position of the second valve based on a coordinated control signal received by the valve controller; wherein the first valve is an isolation valve and the second valve is a control valve.
A method for washing automobiles, two-wheeled vehicles, bicycles, construction equipment, farm equipment, aircraft, railroad cars, ships, and/or various other types of car/vehicle/transportation means, the method comprising spraying onto automobiles, two-wheeled vehicles, bicycles, construction equipment, farm equipment, aircraft, railroad cars, ships, and/or the various other types of car/vehicle/transportation means an aerosol composition, thereby washing the automobiles, two-wheeled vehicles, bicycles, construction equipment, farm equipment, aircraft, railroad cars, ships, and/or the various other types of car/vehicle/transportation means, wherein the aerosol composition contains a gas propellant and a detergent composition, which detergent composition contains -1-chloro-3,3,3-trifluoropropene and hydrofluoroether type (HFE-type) nonflammable fluorinated-type solvent, wherein the mass% ratio thereof ( -1-chloro-3,3,3-trifluoropropene/HFE-type nonflammable fluorinated-type solvent) is within a range that is 30/70 to 99/1, and wherein the HFE-type nonflammable fluorinated-type solvent is one or more species selected from among C 4 F 9 OCH 3 and C 3 F 7 OCH 3. the method comprising spraying onto automobiles, two-wheeled vehicles, bicycles, construction equipment, farm equipment, aircraft, railroad cars, ships, and/or the various other types of car/vehicle/transportation means an aerosol composition, thereby washing the automobiles, two-wheeled vehicles, bicycles, construction equipment, farm equipment, aircraft, railroad cars, ships, and/or the various other types of car/vehicle/transportation means, wherein the aerosol composition contains a gas propellant and a detergent composition, which detergent composition contains -1-chloro-3,3,3-trifluoropropene and hydrofluoroether type (HFE-type) nonflammable fluorinated-type solvent, wherein the mass% ratio thereof ( -1-chloro-3,3,3-trifluoropropene/HFE-type nonflammable fluorinated-type solvent) is within a range that is 30/70 to 99/1, and wherein the HFE-type nonflammable fluorinated-type solvent is one or more species selected from among C 4 F 9 OCH 3 and C 3 F 7 OCH 3.
A method of measuring an index (Ira) of local stiffness of the wall of a conducting artery, transmitting the blood of a subject, characterised in that the said method includes at least: - one measuring step, in one single measuring point, of electrical impedance variation (ΔZ) of a volume of blood circulating in a segment of the said artery; - one step for determining a first intermediary index (RP %, RP), representative of a resistive characteristic brought into play in the stiffening of the said wall, and a second intermediary index (PCPA %, ID), representative of a capacitive characteristic brought into play in the stiffening of the said wall, the said first (RP %, RP) and second (PCPA %, ID) intermediary indexes being obtained from the said measuring step of electrical impedance variation (ΔZ); - one step for determining the said index (Ira) of the local stiffness in accordance with the said first (RP %, RP) and second (PCPA %, ID) intermediary indexes. - one measuring step, in one single measuring point, of electrical impedance variation (ΔZ) of a volume of blood circulating in a segment of the said artery; - one step for determining a first intermediary index (RP %, RP), representative of a resistive characteristic brought into play in the stiffening of the said wall, and a second intermediary index (PCPA %, ID), representative of a capacitive characteristic brought into play in the stiffening of the said wall, the said first (RP %, RP) and second (PCPA %, ID) intermediary indexes being obtained from the said measuring step of electrical impedance variation (ΔZ); - one step for determining the said index (Ira) of the local stiffness in accordance with the said first (RP %, RP) and second (PCPA %, ID) intermediary indexes.
Device for controlling the angular velocity of an out-of-service spacecraft making it possible to facilitate the operations of active removal of the spacecraft as space debris, comprising a stator and a rotor able to move on a rotation axis with respect to the stator, the stator being intended to be driven by the spacecraft to be stabilized, the rotor being intended to orient itself along the terrestrial magnetic field, where the stator comprises an electrically conductive non-ferromagnetic body while the rotor comprises a magnetized system configured to induce, in the stator, eddy currents for braking a relative movement of the rotor with respect to the stator.
A polymeric material and an antigen for use in the treatment of an infection, wherein said polymeric material has a molecular weight greater than 1,000 Daltons and is obtainable by reacting 6 to 8 molar equivalents of oxygen or an equivalent amount of oxygen from another oxidizing agent with a carotenoid.
A wireless power transmission method of a wireless power transmitter, the method comprising: setting a first waiting time after completing booting upon receiving power, wherein the first waiting time refers to a waiting period to transition of the state of the wireless power transmitter from a configuration state to a power save state; transmitting a first signal for detection or identification of at least one of wireless power receivers, wherein the first signal includes a first pattern code corresponding to the wireless power transmitter; receiving a second signal from the at least one of wireless power receivers, wherein the wireless power receiver generates the second signal in response to the first signal, wherein the second signal includes a second pattern code; comparing the first pattern code and the second pattern code to identify the first wireless power receiver; and transmitting power only to the first identified wireless power receiver at one time point, wherein the first waiting time is randomly set not to exceed a predefined maximum waiting time; and the transmitting of the first signal is initiated at a time point in which the first waiting time elapses from a first specific time point, wherein the first signal and the second signal are transmitted by performing bi-directional communication with a different frequency band from a frequency for wireless power transmission, wherein the bi-directional communication between the wireless power transmitter and the wireless power receiver is performed by using a half-duplex Bluetooth low energy communication protocol. setting a first waiting time after completing booting upon receiving power, wherein the first waiting time refers to a waiting period to transition of the state of the wireless power transmitter from a configuration state to a power save state; transmitting a first signal for detection or identification of at least one of wireless power receivers, wherein the first signal includes a first pattern code corresponding to the wireless power transmitter; receiving a second signal from the at least one of wireless power receivers, wherein the wireless power receiver generates the second signal in response to the first signal, wherein the second signal includes a second pattern code; comparing the first pattern code and the second pattern code to identify the first wireless power receiver; and transmitting power only to the first identified wireless power receiver at one time point, wherein the first waiting time is randomly set not to exceed a predefined maximum waiting time; and the transmitting of the first signal is initiated at a time point in which the first waiting time elapses from a first specific time point, wherein the first signal and the second signal are transmitted by performing bi-directional communication with a different frequency band from a frequency for wireless power transmission, wherein the bi-directional communication between the wireless power transmitter and the wireless power receiver is performed by using a half-duplex Bluetooth low energy communication protocol.