mhurhangee/ep-ind-claims huggingface dataset:
An insect trap portion, comprising: an enclosure comprising a front housing portion having a first internal surface, and a rear housing portion having a second internal surface; an adhesive surface; and a first opening in the front housing portion, wherein the adhesive surface is at least partially contained within the enclosure and is configured to adhere to an insect; wherein the enclosure further comprises a divider portion disposed at least partially between the front housing portion and the rear housing portion, the divider portion having a front surface and a rear surface, wherein the front housing portion and rear housing portion are matingly engaged with each other to form the enclosure; and wherein the divider portion divides the enclosure into a front enclosure portion and a rear enclosure portion; and the divider portion comprises text or graphics configured to provide light and dark contrast areas for attracting insects characterised in that, the trap portion is configured to be removably engagable with a base portion and is configured to receive light from said base portion when engaged therewith wherein said base portion comprising: a lighting element configured to provide light to the trap portion; and a mounting portion configured to communicate with and receive power from a power source. an enclosure comprising a front housing portion having a first internal surface, and a rear housing portion having a second internal surface; an adhesive surface; and a first opening in the front housing portion, wherein the adhesive surface is at least partially contained within the enclosure and is configured to adhere to an insect; wherein the enclosure further comprises a divider portion disposed at least partially between the front housing portion and the rear housing portion, the divider portion having a front surface and a rear surface, wherein the front housing portion and rear housing portion are matingly engaged with each other to form the enclosure; and wherein the divider portion divides the enclosure into a front enclosure portion and a rear enclosure portion; and the divider portion comprises text or graphics configured to provide light and dark contrast areas for attracting insects characterised in that, the trap portion is configured to be removably engagable with a base portion and is configured to receive light from said base portion when engaged therewith wherein said base portion comprising: a lighting element configured to provide light to the trap portion; and a mounting portion configured to communicate with and receive power from a power source. a lighting element configured to provide light to the trap portion; and a mounting portion configured to communicate with and receive power from a power source.
A catheter system, which comprises: an elongate catheter defining a central longitudinal axis (k) and having a lumen (30, 142, 144, 170) extending at least partially therethrough, the catheter having a leading catheter end segment (28, 38, 154, 176, 180), wherein a longitudinal axis of the lumen is offset from the central longitudinal axis of the catheter; a guidewire positionable within the lumen of the catheter, the guidewire and the catheter being adapted for relative movement; and a fastening structure (36, 70, 146, 148, 174, 182) within the lumen of the elongate catheter and supported adjacent the leading catheter end segment, the guidewire extending through the fastening structure, wherein the fastening structure dimensioned to selectively engage the guidewire to secure the guidewire with respect to the leading catheter end segment, and wherein the fastening structure is positioned within the elongate catheter such that when the fastening structure is engaged with the guidewire, movement of the guidewire causes deflection of the leading catheter end segment with respect to the central longitudinal axis. an elongate catheter defining a central longitudinal axis (k) and having a lumen (30, 142, 144, 170) extending at least partially therethrough, the catheter having a leading catheter end segment (28, 38, 154, 176, 180), wherein a longitudinal axis of the lumen is offset from the central longitudinal axis of the catheter; a guidewire positionable within the lumen of the catheter, the guidewire and the catheter being adapted for relative movement; and a fastening structure (36, 70, 146, 148, 174, 182) within the lumen of the elongate catheter and supported adjacent the leading catheter end segment, the guidewire extending through the fastening structure, wherein the fastening structure dimensioned to selectively engage the guidewire to secure the guidewire with respect to the leading catheter end segment, and wherein the fastening structure is positioned within the elongate catheter such that when the fastening structure is engaged with the guidewire, movement of the guidewire causes deflection of the leading catheter end segment with respect to the central longitudinal axis.
Method for adjusting motor parameters in a variable speed drive intended to control an electric induction motor, wherein the method comprises: - a step for determining a first difference (ΔI Q) between a motor torque current reference (I Qref) and a motor torque current measurement (I Qm), and a second difference (ΔI D) between a motor flux current reference (I Dref) and a motor flux current measurement (I Dm), - a step for calculating a correction value (ΔR R) of the motor's rotor resistance and a correction value (ΔL R) of the motor's rotor inductance from the integral term of said first difference (ΔI Q) and from the integral term of said second difference (ΔI D), - a step for adjusting values of parameters of the motor model based on said correction values (ΔL R, ΔR R) of the rotor inductance and the rotor resistance, - a step for generating control voltages (U D, U Q) to be applied to the motor, using said adjusted motor parameter values. - a step for determining a first difference (ΔI Q) between a motor torque current reference (I Qref) and a motor torque current measurement (I Qm), and a second difference (ΔI D) between a motor flux current reference (I Dref) and a motor flux current measurement (I Dm), - a step for calculating a correction value (ΔR R) of the motor's rotor resistance and a correction value (ΔL R) of the motor's rotor inductance from the integral term of said first difference (ΔI Q) and from the integral term of said second difference (ΔI D), - a step for adjusting values of parameters of the motor model based on said correction values (ΔL R, ΔR R) of the rotor inductance and the rotor resistance, - a step for generating control voltages (U D, U Q) to be applied to the motor, using said adjusted motor parameter values.
A drug solution administration device comprising a main flow passage including a flow rate controller controlling a flow rate of the drug solution, and a bolus administration unit providing a drug solution, the bolus administration unit branching off the main flow passage characterized in that the bolus administration unit includes: an inflow passage connected to the main flow passage on a proximal end side of the flow rate controller; an outflow passage connected to the main flow passage on a distal end side of the flow rate controller; a reservoir connected between the inflow passage and the outflow passage, and reserving the drug solution; and a control portion controlling the reserve of the drug solution in the reservoir and dispensing of the drug solution from the reservoir, the inflow passage has a part in which the inflow passage branches into a first flow passage and a second flow passage smaller in flow passage cross-sectional area than the first flow passage, and the control portion includes: a first closer operable to close the first flow passage; and a second closer operable to close the outflow passage, linked with the first closer and operable to open and close the outflow passage when the first flow passage is closed.
A method, comprising: performing a first measurement of a position of an aircraft (102, 108, 402) relative to a first location based on an instrument landing system at a measurement time; performing a second measurement of the position of the aircraft (102, 108, 402) based on inertial measurements performed over a first time period starting prior to the first measurement at a first prior time and ending at the measurement time, the second measurement being further based on a measurement of the position of the aircraft at the first prior time based on the instrument landing system; performing a third measurement of the position of the aircraft (102, 108, 402) based on inertial measurements performed over a second time period greater than the first time period and starting prior to the first measurement at a second prior time and ending at the measurement time, the third measurement being further based on a measurement of the position of the aircraft at the second prior time based on the instrument landing system; and generating guidance information based on a selected one of the first, second, and third measurements of the position of the aircraft (102, 108, 402). performing a first measurement of a position of an aircraft (102, 108, 402) relative to a first location based on an instrument landing system at a measurement time; performing a second measurement of the position of the aircraft (102, 108, 402) based on inertial measurements performed over a first time period starting prior to the first measurement at a first prior time and ending at the measurement time, the second measurement being further based on a measurement of the position of the aircraft at the first prior time based on the instrument landing system; performing a third measurement of the position of the aircraft (102, 108, 402) based on inertial measurements performed over a second time period greater than the first time period and starting prior to the first measurement at a second prior time and ending at the measurement time, the third measurement being further based on a measurement of the position of the aircraft at the second prior time based on the instrument landing system; and generating guidance information based on a selected one of the first, second, and third measurements of the position of the aircraft (102, 108, 402).
An electronic oven with a set of reflective elements for controlling a distribution of heat in the electronic oven, comprising: a chamber; a microwave energy source coupled to an injection port in the chamber; a set of dielectric spindles that extend through a set of perforations in the chamber; a set of motors connected to the set of dielectric spindles; and a controller that controls the set of motors; wherein the set of reflective elements are held above a surface of the chamber by the set of dielectric spindles; wherein the set of motors rotate the set of reflective elements via the set of dielectric spindles; wherein the controller stores instructions that independently cause a rotation of each reflective element in the set of reflective elements using the set of motors; and wherein the set of motors, the set of reflective elements, and the set of dielectric spindles are each sets of at least three units. a chamber; a microwave energy source coupled to an injection port in the chamber; a set of dielectric spindles that extend through a set of perforations in the chamber; a set of motors connected to the set of dielectric spindles; and a controller that controls the set of motors; wherein the set of reflective elements are held above a surface of the chamber by the set of dielectric spindles; wherein the set of motors rotate the set of reflective elements via the set of dielectric spindles; wherein the controller stores instructions that independently cause a rotation of each reflective element in the set of reflective elements using the set of motors; and wherein the set of motors, the set of reflective elements, and the set of dielectric spindles are each sets of at least three units.
A coating system on an article having a substrate formed of a silicon-containing material, the coating system comprising an inner layer overlying the substrate, an intermediate layer overlying the inner layer, and a top coat overlying the intermediate layer and formed of a thermal-insulating material, characterized in that: the intermediate layer consists essentially of an yttria-stabilized hafnia and at least one material selected from the group consisting of mullite, alumina, and aluminosilicates, and the intermediate layer has a coefficient of thermal expansion between that of the thermal-insulating material and that of the inner layer; and further comprising at least one bond coat layer between the substrate and the inner layer, the at least one bond coat layer formed of mullite or a mixture of mullite and barium strontium aluminosilicate.
Domestic appliance, preferably an extractor hood, comprising a lamp fixture (1, 2) which is designed to receive a lamp in the domestic appliance in an installation direction, the lamp fixture (1, 2) comprising a supporting body which is designed to be rigidly connected to the domestic appliance, and a socket body which is designed to receive the lamp, it being possible to variably position the socket body in the installation direction of the lamp with respect to the supporting body such that different lamps having different dimensions in the installation direction can be arranged so as to be flush with the supporting body and/or with the domestic appliance, the domestic appliance having an object opening through which to guide the lamp fixture (1, 2) in an installation direction and a stop for blocking the passing of the lamp fixture (1, 2) through the object opening in the installation direction, so that the lamp fixture (1, 2) can fit, preferably flush, in the object opening, the stop preferably being designed as an edge of the object opening that points radially inwards, characterised in that the supporting body has a latching structure which is oriented radially inwards, the socket body having a corresponding latching structure which is oriented radially outwards, and it being possible for the latching structures (19, 21) of the supporting body and of the socket body to form a force-locking and/or form-locking connection with one another in or counter to the installation direction, which connection can automatically hold the socket body, together with the received lamp, counter to the installation direction of the lamp, and the latching structure of the supporting body being arranged on a tongue which is elastically yielding in the radial direction, so that the tongue can yield radially such that the socket body can be moved relative to the supporting body in the installation direction and counter to the installation direction of the lamp after overcoming a threshold force and can simultaneously be automatically held by the threshold force counter to the installation direction of the lamp, the threshold force being preferably at least slightly greater than the combined weight of the socket body and of the lamp.
A recombinant adeno-associated virus vector of pseudotype 2/7 or 2/8 encoding insulin growth factor-1 (IGF-1), for use in treating a motor neuron disorder in a mammal, wherein the vector is to be injected into the spinal cord of the mammal.
A fuel supply system that supplies fuel gas, comprising: a fuel gas tank in which the fuel gas is stored at high pressure; a temperature detecting portion that detects a temperature inside the fuel gas tank; a fuel gas discharge flow path that is connected to the fuel gas tank; a main stop valve that is provided in the fuel gas discharge flow path; and a control portion that is adapted to control opening and closing of the main stop valve, the fuel supply system characterized in that the main stop valve includes an inlet portion through which the fuel gas flows in and an outlet portion through which the fuel gas flows out, a main valve that is arranged between the inlet portion and the outlet portion and that is adapted to open and close the fuel gas discharge flow path, a pilot flow path that is provided so as to communicate the inlet portion with the outlet portion, a pilot valve that is adapted to open and close the pilot flow path, and an actuator capable of opening and closing the main valve and the pilot valve at different timings, and wherein the pilot flow path and the pilot valve are formed inside the main valve, and wherein the control portion is adapted to open the pilot valve and close the main valve when a detected temperature detected by the temperature detecting portion is equal to or lower than a first reference temperature. a fuel gas tank in which the fuel gas is stored at high pressure; a temperature detecting portion that detects a temperature inside the fuel gas tank; a fuel gas discharge flow path that is connected to the fuel gas tank; a main stop valve that is provided in the fuel gas discharge flow path; and a control portion that is adapted to control opening and closing of the main stop valve, the fuel supply system characterized in that the main stop valve includes an inlet portion through which the fuel gas flows in and an outlet portion through which the fuel gas flows out, a main valve that is arranged between the inlet portion and the outlet portion and that is adapted to open and close the fuel gas discharge flow path, a pilot flow path that is provided so as to communicate the inlet portion with the outlet portion, a pilot valve that is adapted to open and close the pilot flow path, and an actuator capable of opening and closing the main valve and the pilot valve at different timings, and wherein the pilot flow path and the pilot valve are formed inside the main valve, and wherein the control portion is adapted to open the pilot valve and close the main valve when a detected temperature detected by the temperature detecting portion is equal to or lower than a first reference temperature.
A boundary layer ingestion fan system for location aft of the fuselage of an aircraft, comprising: a nacelle defining a duct; a fan located within the duct, the fan comprising a hub arranged to rotate around a rotational axis (A-A) and a plurality of blades attached to the hub, each of which has: a span from a root at the hub defining a 0 percent span position (r hub) to a tip defining a 100 percent span position (r tip) and a plurality of span positions therebetween (r ∈ [r hub, r tip]), and a leading edge and a trailing edge defining, for each span position, a chord therebetween having a chord length (c); characterized in that for each one of said plurality of blades, the ratio of chord length at the 0 percent span position (c hub) to chord length at the 100 percent span position (c tip) is 1 or greater; and in that the ratio of chord lengths (c) between the 75 and 100 percent span positions to chord length at the 100 percent span position (c tip) is 1 or less. a nacelle defining a duct; a fan located within the duct, the fan comprising a hub arranged to rotate around a rotational axis (A-A) and a plurality of blades attached to the hub, each of which has: a span from a root at the hub defining a 0 percent span position (r hub) to a tip defining a 100 percent span position (r tip) and a plurality of span positions therebetween (r ∈ [r hub, r tip]), and a leading edge and a trailing edge defining, for each span position, a chord therebetween having a chord length (c); characterized in that for each one of said plurality of blades, the ratio of chord length at the 0 percent span position (c hub) to chord length at the 100 percent span position (c tip) is 1 or greater; and in that the ratio of chord lengths (c) between the 75 and 100 percent span positions to chord length at the 100 percent span position (c tip) is 1 or less. a span from a root at the hub defining a 0 percent span position (r hub) to a tip defining a 100 percent span position (r tip) and a plurality of span positions therebetween (r ∈ [r hub, r tip]), and a leading edge and a trailing edge defining, for each span position, a chord therebetween having a chord length (c); characterized in that for each one of said plurality of blades, the ratio of chord length at the 0 percent span position (c hub) to chord length at the 100 percent span position (c tip) is 1 or greater; and in that the ratio of chord lengths (c) between the 75 and 100 percent span positions to chord length at the 100 percent span position (c tip) is 1 or less.
An air vent for a motor vehicle, comprising a housing which defines an air guiding channel and a plurality of lamellae which are provided at their ends with bearing pins (12, 14), the lamellae being pivotably attached thereby to the housing, wherein the lamellae are mounted on opposing sides with one respective radial bearing (28, 40) and on just one side with one respective axial bearing, characterized in that the axial bearing comprises a fork which encompasses the bearing pin assigned thereto with radial clearance, wherein the bearing pin is provided with at least one axial bearing surface (22, 24) which is arranged on one side of the fork, wherein the fork preferably comprises an insertion chamfer.
Braking system for a vehicle, comprising - two meterable metering brake circuits; and comprising - a non-meterable parking brake circuit; wherein - the parking brake circuit has two parking brake devices which can each be allocated to a wheel of the vehicle; and wherein - the parking brake circuit has a parking operating device, with which the two parking brake devices can be operated simultaneously; characterised in that - each of the two metering brake circuits has precisely one metering brake device which can be allocated to a wheel of the vehicle; - the two metering brake circuits have a common metering operating device (25, 26), with which the two metering brake devices can be operated simultaneously; and in that - the metering operating device has a tandem brake cylinder, with two chambers which are each part of one of the metering brake circuits. - two meterable metering brake circuits; and comprising - a non-meterable parking brake circuit; wherein - the parking brake circuit has two parking brake devices which can each be allocated to a wheel of the vehicle; and wherein - the parking brake circuit has a parking operating device, with which the two parking brake devices can be operated simultaneously; characterised in that - each of the two metering brake circuits has precisely one metering brake device which can be allocated to a wheel of the vehicle; - the two metering brake circuits have a common metering operating device (25, 26), with which the two metering brake devices can be operated simultaneously; and in that - the metering operating device has a tandem brake cylinder, with two chambers which are each part of one of the metering brake circuits.