mhurhangee/ep-ind-claims huggingface dataset:
Tractor front hitch comprising:- - a support structure for attachment to a chassis of the tractor: - a linkage pivotally attached to the support structure for pivoting in a vertical sense about a generally horizontal axis; - actuator means mounted on the support structure for pivoting the linkage relative to the support structure, wherein which the or each actuator means is a main hydraulic cylinder; - characterised in that the or each hydraulic cylinder is mounted at its upper end on the support structure and at its lower end about an axis on a link which is pivotally mounted about an axis on the linkage and can be secured in first and second pivotal positions relative to the linkage, with the link secured in said first pivotal position (18,20) a first working range of movement of the linkage relative to the support structure is provided by the actuator means and with the link secured in said second pivotal position (19,21) a second more raised working range of movement of the linkage relative to the support structure is provided by the actuator means. - a support structure for attachment to a chassis of the tractor: - a linkage pivotally attached to the support structure for pivoting in a vertical sense about a generally horizontal axis; - actuator means mounted on the support structure for pivoting the linkage relative to the support structure, wherein which the or each actuator means is a main hydraulic cylinder; - characterised in that the or each hydraulic cylinder is mounted at its upper end on the support structure and at its lower end about an axis on a link which is pivotally mounted about an axis on the linkage and can be secured in first and second pivotal positions relative to the linkage, with the link secured in said first pivotal position (18,20) a first working range of movement of the linkage relative to the support structure is provided by the actuator means and with the link secured in said second pivotal position (19,21) a second more raised working range of movement of the linkage relative to the support structure is provided by the actuator means.
A housing assembled on one surface of a base to be mounted on a vehicle, comprising: a circumferential wall member enclosing parts provided to the base; and a lid member mounted on an opening (21 a) in the circumferential wall member on a side of the one surface of the base, wherein the lid member comprises a contour inscribed on a quadrilateral formed with two pairs of two sides facing each other, wherein the contour of the lid member is formed in a point-symmetrical shape with respect to a center of the opening, characterized in that the lid member further comprises first cut-out parts formed by cutting out one of the pair of diagonal corners of the quadrilateral, the first cut-out parts having the same size, and second cut-out parts formed by cutting out the other of the pair of diagonal corners, the second cut-out parts having the same size, wherein an area of the first cut-out parts is greater than an area of the second cut-out parts, and wherein one of the pairs of the first cut-out parts is arranged at a part which is front in the front direction of the vehicle and low in the vertical direction when the base is mounted on the vehicle. a circumferential wall member enclosing parts provided to the base; and a lid member mounted on an opening (21 a) in the circumferential wall member on a side of the one surface of the base, wherein the lid member comprises a contour inscribed on a quadrilateral formed with two pairs of two sides facing each other, wherein the contour of the lid member is formed in a point-symmetrical shape with respect to a center of the opening, characterized in that the lid member further comprises first cut-out parts formed by cutting out one of the pair of diagonal corners of the quadrilateral, the first cut-out parts having the same size, and second cut-out parts formed by cutting out the other of the pair of diagonal corners, the second cut-out parts having the same size, wherein an area of the first cut-out parts is greater than an area of the second cut-out parts, and wherein one of the pairs of the first cut-out parts is arranged at a part which is front in the front direction of the vehicle and low in the vertical direction when the base is mounted on the vehicle.
A rigid package for tobacco articles with a hinged lid and comprising: at least one group of tobacco articles; at least one wrap, which encloses the group of tobacco articles; an outer container, which has a front wall and a rear wall; a lid having a rear wall, which is hinged to the rear wall of the outer container so as to allow the lid to rotate relative to the outer container; an inner container, which has a rear wall, houses the wrap and is arranged inside the outer container in a sliding manner; and a lifting mechanism, which connects the inner container to the lid so as to move the inner container relative to the outer container, using the rotation movement of the lid, between a lowered position, in which the inner container is completely inserted into the outer container, and an extracted position, in which the inner container is partially extracted from the outer container; the cigarette package is characterized in that: the wrap has a tobacco article extraction opening closed by a re-stick sealing flap; and the lifting mechanism comprises a rigid connection tab, which, on one side, is directly hinged to the rear wall of the inner container and is glued to the rear wall of the lid. at least one group of tobacco articles; at least one wrap, which encloses the group of tobacco articles; an outer container, which has a front wall and a rear wall; a lid having a rear wall, which is hinged to the rear wall of the outer container so as to allow the lid to rotate relative to the outer container; an inner container, which has a rear wall, houses the wrap and is arranged inside the outer container in a sliding manner; and a lifting mechanism, which connects the inner container to the lid so as to move the inner container relative to the outer container, using the rotation movement of the lid, between a lowered position, in which the inner container is completely inserted into the outer container, and an extracted position, in which the inner container is partially extracted from the outer container; the cigarette package is characterized in that: the wrap has a tobacco article extraction opening closed by a re-stick sealing flap; and the lifting mechanism comprises a rigid connection tab, which, on one side, is directly hinged to the rear wall of the inner container and is glued to the rear wall of the lid. the wrap has a tobacco article extraction opening closed by a re-stick sealing flap; and the lifting mechanism comprises a rigid connection tab, which, on one side, is directly hinged to the rear wall of the inner container and is glued to the rear wall of the lid.
A chroman derivative that is a compound represented by the following Formula (Ia): wherein, in Formula (Ia), each of Y 1 and Y 2 independently represents a hydrogen atom, a hydroxy group, an alkoxy group, an aryloxy group, or a halogen atom; each of R 1 and R 2 independently represents a hydrogen atom, an alkyl group, an aryl group, an acyl group, an alkoxycarbonyl group, an aryloxycarbonyl group, or a carbamoyl group.
Transmission arrangement for a hybrid vehicle having an internal combustion engine and an electric machine, wherein a first drive torque of the internal combustion engine and a second drive torque of the electric machine are transmissible to at least one drive shaft of the hybrid vehicle by means of the transmission arrangement, wherein the transmission arrangement comprises a first planetary transmission with the first components first sun gear, first ring gear and first planet carrier, characterized in that a third drive torque is transmissible to a second planet carrier of a second planetary transmission by means of the first planet carrier, wherein the second planetary transmission has the second components second planet carrier, second sun gear and third sun gear, wherein the second sun gear meshes with a first toothing of a second planet gear and the third sun gear meshes with a second toothing of the second planet gear, wherein the drive shaft of the hybrid vehicle is driveable by means of the third sun gear.
A fan assembly for a gas turbine engine, comprising: a spinner, a fan hub aft of the spinner, and a joint therebetween; a support ring for internally supporting the spinner including a first portion facing the fan hub and a second portion connected to the spinner at the joint, wherein the connection between the second portion and the joint is a bonded connection; characterized in that the fan assembly further comprises bonding rails at the joint. a spinner, a fan hub aft of the spinner, and a joint therebetween; a support ring for internally supporting the spinner including a first portion facing the fan hub and a second portion connected to the spinner at the joint, wherein the connection between the second portion and the joint is a bonded connection; characterized in that the fan assembly further comprises bonding rails at the joint.
A dishwasher comprising: a tub having a washing space therein; a base disposed below the tub and configured to define a predetermined installation space; a sorption drying device accommodated in the installation space and configured to absorb moisture from air discharged from the tub and resupply the air into the tub; and a sump configured to store washing water to be provided to the washing space, wherein the sorption drying device comprises: a blowing part configured to generate an airflow by accelerating the air discharged from the tub; a heater part configured to heat the air having passed through the blowing part; and an absorbent configured to absorb water vapor contained in the air having passed through the heater part, characterized in that the blowing part, the heater part, and the absorbent are disposed in the installation space based on a forward/rearward direction so as to be arranged between the sump and a rear surface of the base in a leftward/rightward direction. a tub having a washing space therein; a base disposed below the tub and configured to define a predetermined installation space; a sorption drying device accommodated in the installation space and configured to absorb moisture from air discharged from the tub and resupply the air into the tub; and a sump configured to store washing water to be provided to the washing space, wherein the sorption drying device comprises: a blowing part configured to generate an airflow by accelerating the air discharged from the tub; a heater part configured to heat the air having passed through the blowing part; and an absorbent configured to absorb water vapor contained in the air having passed through the heater part, characterized in that the blowing part, the heater part, and the absorbent are disposed in the installation space based on a forward/rearward direction so as to be arranged between the sump and a rear surface of the base in a leftward/rightward direction. a blowing part configured to generate an airflow by accelerating the air discharged from the tub; a heater part configured to heat the air having passed through the blowing part; and an absorbent configured to absorb water vapor contained in the air having passed through the heater part, characterized in that the blowing part, the heater part, and the absorbent are disposed in the installation space based on a forward/rearward direction so as to be arranged between the sump and a rear surface of the base in a leftward/rightward direction.
A method for improving fuel efficiency of an aircraft, the method comprising: calculating a current aircraft fuel weight in fuel tanks (28, 30, 32, 34, 36) of the aircraft during a flight of the aircraft, wherein calculating is based on sensing a quantity and calculating a density based on a sensed temperature of the aircraft fuel; reading the current aircraft fuel weight by a flight management system; calculating a current center of gravity position of the aircraft from the current aircraft fuel weight by the flight management system; calculating a longitudinal trim drag factor for the aircraft from the current center of gravity position by the flight management system; calculating an adjusted fuel burn prediction for the aircraft utilizing the longitudinal trim drag factor by the flight management system; and when an autopilot system of the aircraft is engaged in response to the changing center of gravity position, automatically adjusting, by the flight management system, the pitch or pitch trim of the aircraft in response to the adjusted fuel burn prediction, and when the autopilot system of the aircraft is not engaged in response to the changing center of gravity position, prompting, by the flight management system, a pilot to manually adjust the pitch trim of the aircraft in response to the adjusted fuel burn prediction. calculating a current aircraft fuel weight in fuel tanks (28, 30, 32, 34, 36) of the aircraft during a flight of the aircraft, wherein calculating is based on sensing a quantity and calculating a density based on a sensed temperature of the aircraft fuel; reading the current aircraft fuel weight by a flight management system; calculating a current center of gravity position of the aircraft from the current aircraft fuel weight by the flight management system; calculating a longitudinal trim drag factor for the aircraft from the current center of gravity position by the flight management system; calculating an adjusted fuel burn prediction for the aircraft utilizing the longitudinal trim drag factor by the flight management system; and when an autopilot system of the aircraft is engaged in response to the changing center of gravity position, automatically adjusting, by the flight management system, the pitch or pitch trim of the aircraft in response to the adjusted fuel burn prediction, and when the autopilot system of the aircraft is not engaged in response to the changing center of gravity position, prompting, by the flight management system, a pilot to manually adjust the pitch trim of the aircraft in response to the adjusted fuel burn prediction.
Mechanical drive system comprising a frame, at least one rotating electrical machine (22, 22a, 22b) having a rotor with a non-through shaft (25, 25a, 25b) disposed on the frame, and at least one transfer box (23, 47, 48, 67, 68, 85, 93) comprising at least one driving gearwheel (37, 45, 46, 65, 66, 86, 87, 94, 95), the driving gearwheel being secured to a rotor shaft of the rotating electrical machine, the transfer box being disposed on the frame, characterised in that the rotor with a non-through shaft comprises a cylindrical magnetic mass sandwiched between two half-shafts (27, 27a, 27b, 28, 28a, 28b), the half-shafts forming the rotor shaft.
Pressure measurement device, having a first pressure measurement apparatus which is designed as a gas friction vacuum meter and which is configured to provide first pressure measurement values, a second pressure measurement apparatus which is designed as a faster and/or continuous pressure measurement apparatus compared to the first pressure measurement apparatus and which is configured to provide second pressure measurement values, and having a controller provided such that it is capable of relating the first pressure measurement values provided by the first pressure measurement apparatus and the second pressure measurement values provided by the second pressure measurement apparatus to one another, characterised in that the controller has a calibration apparatus provided such that it is able to calibrate and optionally adjust, in particular continuously, using the first pressure measurement values provided by the first pressure measurement apparatus, the second pressure measurement values provided by the second pressure measurement apparatus, and/or to calibrate and optionally adjust, in particular continuously, using the second pressure measurement values provided by the second pressure measurement apparatus, the first pressure measurement values provided by the first pressure measurement apparatus.
A method comprising: applying a first process to identify a region of interest in encoded video data if information to assist ROI identification is available; and applying a second process to identify the ROI in the encoded video data if the information to assist ROI identification is not available, wherein the second process comprises analyzing one or more characteristics of the encoded video data to determine whether to identify the ROI using bitstream domain analysis of the encoded video data or to identify the ROI using pixel domain analysis of the encoded video data. applying a first process to identify a region of interest in encoded video data if information to assist ROI identification is available; and applying a second process to identify the ROI in the encoded video data if the information to assist ROI identification is not available, wherein the second process comprises analyzing one or more characteristics of the encoded video data to determine whether to identify the ROI using bitstream domain analysis of the encoded video data or to identify the ROI using pixel domain analysis of the encoded video data.
A device for the protection of LED street lighting against overvoltage which comprises an overvoltage protection, a driver and a LED street lighting, wherein the overvoltage protection is connectable to individual L, N, PE conductors of the electrical power supply network in front of the points of connection of the driver to the individual L, N, PE conductors of the electrical power supply network, whereby at least one LED panel is connected to the driver, while driver and LED panel are situated in a housing of the LED lighting, characterized in that the housing is conductively connectable to the ground or to the local ground, and in the housing, between the connection of the overvoltage protection to the individual L, N, PE conductors of the electrical power supply network and the connection of the driver to the individual L, N, PE conductors of the electrical power supply network, a choke for asymmetric distribution of the energy of a current wave between the overvoltage protection and the driver is connected in the phase conductor L and/or in the neutral conductor N.
A device for maneuvering an aerodynamic flap arranged on a motor vehicle, wherein it comprises mechanical means for causing the flap to pass from a retracted position to a deployed position, by performing movements in a given order: - extending the flap while keeping the plane of the flap parallel to the direction of an air flow circulating around the flap when the vehicle is moving, such that the aerodynamic pressure exerted on the flap when the vehicle is moving is substantially zero, then - pivoting the flap about a pivot axis (AA') situated in a plane of the flap and passing substantially through a center of aerodynamic thrust of the flap, such that the torque applied on the pivot axis (AA')and resulting from the aerodynamic forces exerted on the flap when the vehicle is moving is substantially zero, and, conversely, from a deployed position to a retracted position by performing said movements in reverse order. - extending the flap while keeping the plane of the flap parallel to the direction of an air flow circulating around the flap when the vehicle is moving, such that the aerodynamic pressure exerted on the flap when the vehicle is moving is substantially zero, then - pivoting the flap about a pivot axis (AA') situated in a plane of the flap and passing substantially through a center of aerodynamic thrust of the flap, such that the torque applied on the pivot axis (AA')and resulting from the aerodynamic forces exerted on the flap when the vehicle is moving is substantially zero,
Component comprising an adhesion-reducing coating which has at least one top layer that provides the adhesion-reducing surface, wherein the top layer • has a metallic matrix • in which particles of a plastic which form at least part of the surface are incorporated, characterized in that the component consists of a plastic and a starting layer for electroless coating with metal is applied thereto, wherein the starting layer • has a matrix made of a synthetic resin • in which metallic particles are incorporated as nuclei for the electroless coating. • has a metallic matrix • in which particles of a plastic which form at least part of the surface are incorporated, • has a matrix made of a synthetic resin • in which metallic particles are incorporated as nuclei for the electroless coating.
A medical system, comprising: a compressible device; a covering over the compressible device, wherein the covering includes a delivery configuration and a deployed configuration, wherein, in the delivery configuration, the covering at least partially covers the compressible device to maintain the compressible device in a compressed state, and wherein, in the deployed configuration, the covering is releasable from the device to transition the compressible device from the compressed state to an expanded state, wherein the covering is a netting; and a thread or a wire coupled to the netting, wherein the thread or the wire is configured to remove the netting via a force applied to the thread or the wire. a compressible device; a covering over the compressible device, wherein the covering includes a delivery configuration and a deployed configuration, wherein, in the delivery configuration, the covering at least partially covers the compressible device to maintain the compressible device in a compressed state, and wherein, in the deployed configuration, the covering is releasable from the device to transition the compressible device from the compressed state to an expanded state, wherein the covering is a netting; and a thread or a wire coupled to the netting, wherein the thread or the wire is configured to remove the netting via a force applied to the thread or the wire.
A method of relaying device to device, D2D, data, which is relayed by a relay user equipment, UE, in a wireless access system supporting D2D communication, the method comprising: receiving, from a D2D UE, a demodulation reference signal, DM-RS, comprising a base sequence defined for transmitting D2D data; receiving, from the D2D UE, the D2D data through a resource region; detecting the D2D data based on the DM-RS, wherein when the base sequence is configured based on an identification of the D2D UE and a predetermined offset value, the D2D UE is determined to be out-of-coverage UE, and wherein when the base sequence is configured based on only the identification of the D2D UE, the D2D UE is determined to be in-coverage UE; and relaying the D2D data received from the D2D UE when the D2D UE is determined to be out-of-coverage UE. receiving, from a D2D UE, a demodulation reference signal, DM-RS, comprising a base sequence defined for transmitting D2D data; receiving, from the D2D UE, the D2D data through a resource region; detecting the D2D data based on the DM-RS, wherein when the base sequence is configured based on an identification of the D2D UE and a predetermined offset value, the D2D UE is determined to be out-of-coverage UE, and wherein when the base sequence is configured based on only the identification of the D2D UE, the D2D UE is determined to be in-coverage UE; and relaying the D2D data received from the D2D UE when the D2D UE is determined to be out-of-coverage UE.