mhurhangee/ep-ind-claims huggingface dataset:
A device comprising a trap chamber for collecting flying insects, an inlet communicating with the trap chamber, an airflow generator constructed to draw air into the trap chamber via the inlet so that insects proximate to the inlet are drawn in the trap chamber, and a lure for attracting flying insects to the device; the lure including: a solution of lactic acid as a first chemical attractant; and, a source of ammonia as a second chemical attractant; wherein the lure is capable of providing effective amounts of lactic acid and ammonia continuously for at least a period of one week; characterised in that the first and second attractants are contained in separate first and second chambers, respectively, said first and second chambers being housed in a common housing and are physically isolated from each other prior to use of the lure. a solution of lactic acid as a first chemical attractant; and, a source of ammonia as a second chemical attractant; wherein the lure is capable of providing effective amounts of lactic acid and ammonia continuously for at least a period of one week; characterised in that the first and second attractants are contained in separate first and second chambers, respectively, said first and second chambers being housed in a common housing and are physically isolated from each other prior to use of the lure.
Method for setting a filling height in a container (25, 32) of at least one agricultural transport vehicle or towed transport wagon, into which crop picked up by at least one self-propelled harvesting machine is overloaded by means of an overloading system until a predetermined filling height is reached and is transported by the transport vehicle or the transport wagon to a remote unloading point, wherein a quantity of crop overloaded by the harvesting machine into the container (25, 32) is determined by at least one measuring device arranged on the harvesting machine and transmitted to a control unit, characterised in that a quantity of crop material transferred by the transport vehicle or the transport wagon at the unloading point is determined by a further measuring device and transmitted to the control unit to determine a quantity difference between the quantity of crop material received and the quantity of crop material transferred, and in that at least one control signal is generated as a function of the determined quantity difference, by means of which the filling level realised by the overloading system is adjusted.
A cart for medical instruments, comprising: a housing having a longitudinal axis; a first motor configured to rotate the housing about the longitudinal axis; and one or more trays removably disposed within the housing, each tray having one or more retainers, each of the one or more retainers configured to hold a medical instrument, and wherein each tray includes a door; an actuator configured to open the door; and a processor operably connected to the first motor, the processor having a storage medium, wherein the processor is programmed to: receive a request for a medical instrument; cause the first motor to rotate the housing until a tray containing the requested medical instrument is at a working position where the door may be opened for retrieval of the instrument; and record a use of the requested medical instrument on the storage medium. a housing having a longitudinal axis; a first motor configured to rotate the housing about the longitudinal axis; and one or more trays removably disposed within the housing, each tray having one or more retainers, each of the one or more retainers configured to hold a medical instrument, and wherein each tray includes a door; an actuator configured to open the door; and a processor operably connected to the first motor, the processor having a storage medium, wherein the processor is programmed to: receive a request for a medical instrument; cause the first motor to rotate the housing until a tray containing the requested medical instrument is at a working position where the door may be opened for retrieval of the instrument; and record a use of the requested medical instrument on the storage medium. receive a request for a medical instrument; cause the first motor to rotate the housing until a tray containing the requested medical instrument is at a working position where the door may be opened for retrieval of the instrument; and record a use of the requested medical instrument on the storage medium.
Device for detecting electromagnetic radiation, comprising: - a substrate; - a matrix-array of thermal detectors, said matrix-array being placed on the substrate; and - an encapsulating structure encapsulating the matrix-array of thermal detectors and comprising an encapsulating layer that extends in a continuous manner around and above the matrix-array of thermal detectors so as to define, with the substrate, a cavity in which the matrix-array of thermal detectors is located, the encapsulating layer comprising at least one section, called the internal bearing section, located between two adjacent thermal detectors, said section bearing directly against the substrate, said internal bearing section comprising a sidewall that is separate, in a plane parallel to the plane of the substrate, from a peripheral wall of the encapsulating layer that encircles the matrix-array of thermal detectors; characterized in that the thermal detectors each comprise an absorbing membrane suitable for absorbing the radiation to be detected, said membrane being suspended above the substrate and thermally insulated therefrom by anchoring pins and thermally insulating arms, and in that at least one internal bearing section extends along absorbing membranes of two adjacent thermal detectors, along a longitudinal axis (Δ) passing through two adjacent anchoring pins, each of said anchoring pins participating in holding, above the substrate, the absorbing membranes of said two adjacent thermal detectors. - a substrate; - a matrix-array of thermal detectors, said matrix-array being placed on the substrate; and - an encapsulating structure encapsulating the matrix-array of thermal detectors and comprising an encapsulating layer that extends in a continuous manner around and above the matrix-array of thermal detectors so as to define, with the substrate, a cavity in which the matrix-array of thermal detectors is located, the encapsulating layer comprising at least one section, called the internal bearing section, located between two adjacent thermal detectors, said section bearing directly against the substrate, said internal bearing section comprising a sidewall that is separate, in a plane parallel to the plane of the substrate, from a peripheral wall of the encapsulating layer that encircles the matrix-array of thermal detectors;
Wood-drying method in a drying kiln comprising the steps of placing the wood on spacers inside the drying kiln, thereafter providing steam to the interior of kiln and heating it until said steam has displaced the atmospheric air in the kiln, continue the heating until the steam Is superheated, characterised by,during a first stage of the drying process, stopping the increase in the temperature when the inside temperature In the drying kiln has reached 70°C, and keeping the temperature in the kiln in the range of 70-80°C during a period of at least 2 hours with a maximum of 3 hours to relax the wood, thereafter,in a second stage of the drying process, carrying out a drying phase at a temperature of 120°C maximum, preferably at a temperature in the range of 105-110°C, while measuring moisture content of the wood and stopping the drying phase when the wood has reached a desired final moisture content, thereafter, in a final stage of the drying process, letting the wood cool spontaneously, where the entire process is carried out in conditions of atmospheric pressure.
A cutting tool, comprising: a substrate; a flank face; a rake face; and a coating layer on the substrate, the coating layer having an outer surface and a substrate side, the coating layer being located at the flank face, wherein the coating layer consists of nitride or carbonitride containing Ti and Al and has a thickness of 3 to 9 μm at the flank face, wherein a first intensity ratio I / I (p s) of a diffraction intensity I of a crystal plane to a diffraction intensity I of a crystal plane measured by a thin film X-ray diffraction method using Cu-Kα rays of the coating layer on the outer surface at the flank face is 0.2 - 1 and is higher than the first intensity ratio (p b) of the coating layer on the substrate side at the flank face. a substrate; a flank face; a rake face; and a coating layer on the substrate, the coating layer having an outer surface and a substrate side, the coating layer being located at the flank face, wherein the coating layer consists of nitride or carbonitride containing Ti and Al and has a thickness of 3 to 9 μm at the flank face, wherein a first intensity ratio I / I (p s) of a diffraction intensity I of a crystal plane to a diffraction intensity I of a crystal plane measured by a thin film X-ray diffraction method using Cu-Kα rays of the coating layer on the outer surface at the flank face is 0.2 - 1 and is higher than the first intensity ratio (p b) of the coating layer on the substrate side at the flank face.
An apparatus (270; 370; 470; 570) for detecting particles of hadron radiation that have passed through a subject, the apparatus comprising: a plurality of detector devices, the plurality of detector devices comprising at least a first set of detector devices (272An; 372An; 472An; 572An), the first set of detector devices comprising a plurality of solid-state semiconductor detector devices provided at spaced-apart locations along a beam axis, the detector devices each being configured to generate an electrical signal indicative of passage of a particle through or absorption of a hadron particle by the device; and at least one absorber portion (274An; 374An; 474An; 574An) configured to absorb at least a portion of an energy of a particle, wherein one said at least one absorber portion is provided in a particle path between at least one pair of adjacent detector devices, the apparatus being configured to generate a signal indicative of the energy of a particle, the signal being dependent at least in part on the electrical signals indicative of passage of a particle through or absorption of a particle by one of the detector devices. a plurality of detector devices, the plurality of detector devices comprising at least a first set of detector devices (272An; 372An; 472An; 572An), the first set of detector devices comprising a plurality of solid-state semiconductor detector devices provided at spaced-apart locations along a beam axis, the detector devices each being configured to generate an electrical signal indicative of passage of a particle through or absorption of a hadron particle by the device; and at least one absorber portion (274An; 374An; 474An; 574An) configured to absorb at least a portion of an energy of a particle, wherein one said at least one absorber portion is provided in a particle path between at least one pair of adjacent detector devices, the apparatus being configured to generate a signal indicative of the energy of a particle, the signal being dependent at least in part on the electrical signals indicative of passage of a particle through or absorption of a particle by one of the detector devices.
A method for supporting the ends of a composite pressurized storage vessel, the method comprising: supporting two ends of a cylindrical composite pressurized storage vessel with an axial rod/tube fixed axially inside the storage vessel at each end, the supporting step comprising connecting the axial rod/tube to a rod adapter having a threaded interface that engages with a rod anchor disposed on the storage vessel; and, providing a fluid pathway (170, 175) into the vessel from at least one of the two ends which is not obstructed by the axial rod/tube. supporting two ends of a cylindrical composite pressurized storage vessel with an axial rod/tube fixed axially inside the storage vessel at each end, the supporting step comprising connecting the axial rod/tube to a rod adapter having a threaded interface that engages with a rod anchor disposed on the storage vessel; and, providing a fluid pathway (170, 175) into the vessel from at least one of the two ends which is not obstructed by the axial rod/tube.
A ride vehicle system, comprising: a ride vehicle comprising a seat configured to accommodate a passenger; a restraint system of the ride vehicle, wherein the restraint system comprises a restraint configured to secure the passenger within the seat; and a forced air system of the ride vehicle, wherein the forced air system is configured to generate an air flow, direct the air flow internally through the restraint, and discharge the air flow toward the passenger via a discharge port of the restraint. a ride vehicle comprising a seat configured to accommodate a passenger; a restraint system of the ride vehicle, wherein the restraint system comprises a restraint configured to secure the passenger within the seat; and a forced air system of the ride vehicle, wherein the forced air system is configured to generate an air flow, direct the air flow internally through the restraint, and discharge the air flow toward the passenger via a discharge port of the restraint.
A crew seat to be installed in an aircraft, comprising: - a seat structure which can be fixed to a fixed part of the aircraft, - a seat bottom, - a seat bottom slide provided with two arms positioned on either side of the seat bottom, and - the seat bottom being mounted so as to slide relative to the seat bottom slide between a retracted position and a deployed position, - one of the elements among the seat bottom and the seat bottom slide comprising rollers able to slide along corresponding rails provided in the other of the elements among the seat bottom and the seat bottom slide, - the rails having a curved shape so that the seat bottom can form in the deployed position an angle greater than 10 degrees, preferably of the order of 14 degrees, relative to a horizontal plane parallel to the aircraft floor, characterized in that said seat further comprises a backrest having a first end rotatably mounted relative to the seat bottom and a second end rotatably mounted relative to a headrest of said seat, said headrest being slidably mounted relative to the seat structure so as to follow a movement of said backrest. - a seat structure which can be fixed to a fixed part of the aircraft, - a seat bottom, - a seat bottom slide provided with two arms positioned on either side of the seat bottom, and - the seat bottom being mounted so as to slide relative to the seat bottom slide between a retracted position and a deployed position, - one of the elements among the seat bottom and the seat bottom slide comprising rollers able to slide along corresponding rails provided in the other of the elements among the seat bottom and the seat bottom slide, - the rails having a curved shape so that the seat bottom can form in the deployed position an angle greater than 10 degrees, preferably of the order of 14 degrees, relative to a horizontal plane parallel to the aircraft floor,
A bag checking machine with a sorting module, installed before the bag can enter the checking machine, and which comprises driving means that activate the module characterized in that said module comprises: - a pressure roller that puts pressure on the bags as they pass through under said pressure roller, which has an ascending and a descending motion - a first input roller connected to conveyance means of the checking machine and to the pressure roller, and - at least one automatic or manually-operated diverter element positioned below said pressure roller, which has at least two positions, a first upward position that blocks the passing of the bags towards the conveyance means and guides the bags towards another predetermined destination, and a second downward position that defines a passage formed by the conveyance means while said diverter element blocks the passing of the bags towards the other predetermined destination and guides the bags towards the passage. - a pressure roller that puts pressure on the bags as they pass through under said pressure roller, which has an ascending and a descending motion - a first input roller connected to conveyance means of the checking machine and to the pressure roller, and - at least one automatic or manually-operated diverter element positioned below said pressure roller, which has at least two positions, a first upward position that blocks the passing of the bags towards the conveyance means and guides the bags towards another predetermined destination, and a second downward position that defines a passage formed by the conveyance means while said diverter element blocks the passing of the bags towards the other predetermined destination and guides the bags towards the passage.
Method of coding of an input data, characterised in that it comprises: - mapping (21, 192) of input data on an input constellation associated with a determined modulation to get input constellation symbols; then - mapping (60, 710, 193-194) said input constellation symbols on multiple carriers to generate a frequency domain symbol per transmit antenna, such that a multicarrier signal, in the frequency domain, is generated for each transmit antenna; then - generation (611, 61Ntx, 196) of the multicarrier signal for each antenna in the time domain; then - clipping (621, 198) said time domain multicarrier signal for each antenna with a fixed threshold to get modified time domain symbols; then - generation (631, 63Ntx, 199) of frequency domain modified symbols from said modified time domain symbols; then - de-mapping (64, 720) the frequency domain modified symbols to generate symbols modified with regard to said input constellation symbols; then - amplification (65, 66, 1911) of the difference between the modified symbols and the input constellation symbols with a fixed non null value for each carrier, wherein said fixed non null value is independent of input data, to get resulting frequency domain symbols; then - adding the result of said amplification to the input constellation symbols; then - projection (68, 1912) of the result of said adding onto an extended constellation that comprises extended regions associated with symbols of the input constellation; then - generation (271, 27NTx, 1913) of a resulting time domain signal from the result of said projection (68, 1912). - mapping (21, 192) of input data on an input constellation associated with a determined modulation to get input constellation symbols; then - mapping (60, 710, 193-194) said input constellation symbols on multiple carriers to generate a frequency domain symbol per transmit antenna, such that a multicarrier signal, in the frequency domain, is generated for each transmit antenna; then - generation (611, 61Ntx, 196) of the multicarrier signal for each antenna in the time domain; then - clipping (621, 198) said time domain multicarrier signal for each antenna with a fixed threshold to get modified time domain symbols; then - generation (631, 63Ntx, 199) of frequency domain modified symbols from said modified time domain symbols; then - de-mapping (64, 720) the frequency domain modified symbols to generate symbols modified with regard to said input constellation symbols; then - amplification (65, 66, 1911) of the difference between the modified symbols and the input constellation symbols with a fixed non null value for each carrier, wherein said fixed non null value is independent of input data, to get resulting frequency domain symbols; then - adding the result of said amplification to the input constellation symbols; then - projection (68, 1912) of the result of said adding onto an extended constellation that comprises extended regions associated with symbols of the input constellation; then - generation (271, 27NTx, 1913) of a resulting time domain signal from the result of said projection (68, 1912).
An inrun track machining system for a ski jumping hill inrun track of a ski jumping hill and for preparation of an icy inrun track with a right single track and a left single track having the following characteristics: - a track machining carriage comprising: • at least one left track machining device for thermal removing of ice and / or snow in the left single track, • at least one right track machining device for thermal removing of ice and / or snow in the right single track, and • a guidance device for the forced guidance of the movement of the track machining carriage along the inrun track, - drive means for moving the track machining carriage with a movement speed along the inrun track of the ski jumping hill, and - a control device for controlling the movement speed of the track machining carriage and for controlling the removal of ice and / or snow in the right single track and the left single track by means of two track machining devices (10,11), wherein the track machining devices (10,11) comprise electric heating shoes (100,110) for removing of ice and / or snow from the single tracks by means of mechanical contact between the ice and / or snow and the electrical heating shoes (100,110). - a track machining carriage comprising: • at least one left track machining device for thermal removing of ice and / or snow in the left single track, • at least one right track machining device for thermal removing of ice and / or snow in the right single track, and • a guidance device for the forced guidance of the movement of the track machining carriage along the inrun track, • at least one left track machining device for thermal removing of ice and / or snow in the left single track, • at least one right track machining device for thermal removing of ice and / or snow in the right single track, and • a guidance device for the forced guidance of the movement of the track machining carriage along the inrun track, - drive means for moving the track machining carriage with a movement speed along the inrun track of the ski jumping hill, and - a control device for controlling the movement speed of the track machining carriage and for controlling the removal of ice and / or snow in the right single track and the left single track by means of two track machining devices (10,11), wherein
Method for controlling fuel metering in a carburetor or a low pressure injection system of a two stroke crank case scavenged internal combustion engine when the engine is operating at idle speed, the method comprising the steps of: a) monitoring the engine speed; b) determining a first variable based on a first moving average algorithm using the monitored engine speed as input data; c) determining a second variable based on a second moving average algorithm using the monitored engine speed as input data, where the first moving average algorithm is arranged to react faster to an engine speed change than the second moving average algorithm; d) comparing the second variable to the first variable, where if 1) the second variable is higher than the first variable: the fuel metering is set in a first leaner setting, and where if 2) the second variable is lower than the first variable: the fuel metering is set in a second richer setting. a) monitoring the engine speed; b) determining a first variable based on a first moving average algorithm using the monitored engine speed as input data; c) determining a second variable based on a second moving average algorithm using the monitored engine speed as input data, where the first moving average algorithm is arranged to react faster to an engine speed change than the second moving average algorithm; d) comparing the second variable to the first variable, where if 1) the second variable is higher than the first variable: the fuel metering is set in a first leaner setting, and where if 2) the second variable is lower than the first variable: the fuel metering is set in a second richer setting.