mhurhangee/ep-ind-claims huggingface dataset:
A combine harvester including a first discharge apparatus having a variable discharge direction, a chopping assembly for cutting up straw and a second discharge apparatus which is arranged downstream of the chopping assembly and which can be moved into at least two different positions and which in the first position can be loaded with crop material by the chopping assembly and the first discharge apparatus and which in the second position permits the discharge of crop material with bypassing of the second discharge apparatus, characterised in that the discharge direction of the first discharge apparatus is dependent on the operating state of the chopping assembly, wherein upon a change in the operating state, that is to say when the chopping assembly is switched on or switched off, the discharge direction of the first discharge apparatus is automatically variable.
All-polymer fibrillar nanocomposites characterized in that they consist of a thermoplastic polymer from the group of polyolefins, and polystyrenes, eventually with known additives, and poly(tetrafluoroethylene) having crystallinity degree above 50 wt.% and melting temperature of 330°C or higher, in the form of individual nanofibers forming neither bundles nor agglomerates, with transversal sizes ranging from 10 to 500 nm, added in a content ranging from 3 wt.% to 15wt.%.
Aluminium alloy comprising the following composition, all values in weight %: Si 0.25 - 1.5 Cu 0.3 - 1.5 Fe up to 0.5 Mg <0.1 Mn up to 0.2 unavoidable impurities less than or equal to 0.05 each or less than or equal to 0.15 in total balance aluminium, wherein the aluminium alloy is an aluminium alloy clad layer. Si 0.25 - 1.5 Cu 0.3 - 1.5 Fe up to 0.5 Mg <0.1 Mn up to 0.2 unavoidable impurities less than or equal to 0.05 each or less than or equal to 0.15 in total balance aluminium, wherein the aluminium alloy is an aluminium alloy clad layer.
A battery charging apparatus comprising: a memory configured to store instructions; and a processor configured to execute the instructions wherein, when the instructions are executed, the processor is configured to: determine, in an initial charging step, a battery overpotential based on a battery voltage (S), the battery voltage (S) corresponding to a charging capacity of the battery, and a reference battery voltage (R), the reference battery voltage (R) being determined based on the charging capacity, wherein the battery overpotential is a difference between the battery voltage (S) and the reference battery voltage (R), determine whether a condition for changing a battery charging step is satisfied based on the battery overpotential, and change the battery charging step from the initial charging step to the adjusted charging step in response to the condition being satisfied, wherein the condition comprises a first condition defined as a case in which the battery overpotential is greater than or equal to a threshold voltage (A). a memory configured to store instructions; and a processor configured to execute the instructions wherein, when the instructions are executed, the processor is configured to: determine, in an initial charging step, a battery overpotential based on a battery voltage (S), the battery voltage (S) corresponding to a charging capacity of the battery, and a reference battery voltage (R), the reference battery voltage (R) being determined based on the charging capacity, wherein the battery overpotential is a difference between the battery voltage (S) and the reference battery voltage (R), determine whether a condition for changing a battery charging step is satisfied based on the battery overpotential, and change the battery charging step from the initial charging step to the adjusted charging step in response to the condition being satisfied, wherein the condition comprises a first condition defined as a case in which the battery overpotential is greater than or equal to a threshold voltage (A). determine, in an initial charging step, a battery overpotential based on a battery voltage (S), the battery voltage (S) corresponding to a charging capacity of the battery, and a reference battery voltage (R), the reference battery voltage (R) being determined based on the charging capacity, wherein the battery overpotential is a difference between the battery voltage (S) and the reference battery voltage (R), determine whether a condition for changing a battery charging step is satisfied based on the battery overpotential, and change the battery charging step from the initial charging step to the adjusted charging step in response to the condition being satisfied, wherein the condition comprises a first condition defined as a case in which the battery overpotential is greater than or equal to a threshold voltage (A).
A method for controlling power transmitted by a mobile device comprising: determining at the mobile device a resource utilization limitation of the mobile device; determining at the mobile device whether the resource utilization limitation exceeds a reporting threshold; in response to the resource utilization limitation exceeding the reporting threshold, sending a resource allocation request and the resource utilization limitation from the mobile device to a base station; and receiving a message indicating a dynamic resource allocation grant from the base station, wherein the message indicating a dynamic resource allocation grant includes a power control instruction for use during the duration of the dynamic resource allocation grant. determining at the mobile device a resource utilization limitation of the mobile device; determining at the mobile device whether the resource utilization limitation exceeds a reporting threshold; in response to the resource utilization limitation exceeding the reporting threshold, sending a resource allocation request and the resource utilization limitation from the mobile device to a base station; and receiving a message indicating a dynamic resource allocation grant from the base station, wherein the message indicating a dynamic resource allocation grant includes a power control instruction for use during the duration of the dynamic resource allocation grant.
A laser sensor module for particle size detection for determining an air quality, the laser sensor module comprising at least one first laser, at least one first detector, at least one electrical driver and at least one evaluator, wherein the first laser is adapted to emit first laser light in reaction to signals provided by the at least one driver, wherein the at least one first detector is adapted to determine a first self-mixing interference signal of an optical wave within a first laser cavity of the first laser, wherein the first self-mixing interference signal is caused by first reflected laser light reentering the first laser cavity, the first reflected laser light being reflected by a particle receiving at least a part of the first laser light, characterized in that the evaluator is adapted to determine a size of the particle by determining a first relative distance between the particle and the first laser by means of the first self-mixing interference signal and by determining a first amplitude information by means of the first self-mixing interference signal, wherein the laser module further comprises at least one first focus region, wherein the first relative distance is related to a distance between the first focus region and the particle, and wherein the evaluator is adapted to determine the first relative distance based on at least one characteristic of the first self-mixing interference signal being related to the distance between the first focus region and the particle, and wherein the first amplitude information comprises a maximum or minimum amplitude of the first self-mixing interference signal, and wherein the at least one characteristic of the first self-mixing interference signal being related to the distance between the first focus region and the particle comprises at least one of phase information, number of oscillations, number of relative maxima or minima, ratio of amplitudes of relative maxima minima, number of zero crossings within a defined interval of the first self-mixing interference signal, one or more distances between the zero crossings and shape of an envelope of the first self-mixing interference signal.
An output assembly for an accessory system of a gas turbine engine, the gas turbine engine comprising an accessory gearbox, the output assembly defining an axis and comprising: a first rotating member extending along the axis and comprising a mechanical connector for coupling the output assembly to the accessory system; a second rotating member extending along the axis and comprising opposed first end and second end, the first end comprising an opening, the second rotating member coupled to the first rotating member at a first axial position at the opening of the first end and at a second axial position at the second end; a one-way clutch, the second rotating member coupled to the first rotating member at the second axial position through the one-way clutch; wherein the first rotating member further comprises an extension member extending at least partially between the first axial position and the second axial position and through the opening of the first end at the first axial position, the extension member including a designed fail point, the output further comprising; a spring member attached to the extension member and pressing together the one-way clutch, wherein the one-way clutch is formed at least in part by the first rotating member and at least in part by the second rotating member, the spring member is attached to the extension member at a third axial position along an axial direction A2 extending along an axis of the output assembly, and the spring member extends to the second rotating member at the first end. a first rotating member extending along the axis and comprising a mechanical connector for coupling the output assembly to the accessory system; a second rotating member extending along the axis and comprising opposed first end and second end, the first end comprising an opening, the second rotating member coupled to the first rotating member at a first axial position at the opening of the first end and at a second axial position at the second end; a one-way clutch, the second rotating member coupled to the first rotating member at the second axial position through the one-way clutch; wherein the first rotating member further comprises an extension member extending at least partially between the first axial position and the second axial position and through the opening of the first end at the first axial position, the extension member including a designed fail point, the output further comprising; a spring member attached to the extension member and pressing together the one-way clutch, wherein the one-way clutch is formed at least in part by the first rotating member and at least in part by the second rotating member, the spring member is attached to the extension member at a third axial position along an axial direction A2 extending along an axis of the output assembly, and the spring member extends to the second rotating member at the first end.
A middle stanchion for a semi-trailer, which is placed in a pocket formed on a side wall, wherein in the lower part of the middle stanchion there is a safety lock consisting of a lower lever and an arm, characterized in that it comprises a safety hook module which can be locked to a pin, the arm being attached to the hook module in a hinged manner - thus, that in this way a rotational movement of the hook module is possible, and on the other side for the modular hook mounting the arm is rotatably mounted on the lower lever, and the lower lever is attached to the middle stanchion by means of a which determines the axis of rotation of the lever, thereby the axis is displaced relative to the attachment of the arm to the lever, whereby after operation and lifting of the lower lever, it performs an oscillating movement according to a pitch circle, which centre is determined by the axis of rotation of the lower lever, i.e. the pin, and the axis of rotation of the oscillating arm located in an opening at the point of connection of the arm to the hook module, and the hook module, the arm and the lower lever - forming an eccentric mechanism - together form the safety lock.
A solar cell, comprising: a semiconductor substrate, the semiconductor substrate including a first surface and a second surface arranged opposite to each other; an emitter and a first passivation layer formed over the first surface of the semiconductor substrate; a tunneling layer formed over the second surface of the semiconductor substrate; a first doped conductive layer and a retardation layer formed on a surface of the tunneling layer, wherein the first doped conductive layer is located between the tunneling layer and the retardation layer, and the first doped conductive layer and the retardation layer correspond to a metallization region; a second doped conductive layer formed over the surface of the tunneling layer, the second doped conductive layer covering the tunneling layer in a non-metallization region and the retardation layer, wherein a doping concentration of the second doped conductive layer is greater than a doping concentration of the first doped conductive layer, and the retardation layer is configured to retard migration of a doped element in the second doped conductive layer to the first doped conductive layer; a second passivation layer formed over a surface of the second doped conductive layer; and a second electrode penetrating through the second passivation layer to form contact with the second doped conductive layer and a first electrode penetrating through the first passivation layer to form contact with the emitter. a semiconductor substrate, the semiconductor substrate including a first surface and a second surface arranged opposite to each other; an emitter and a first passivation layer formed over the first surface of the semiconductor substrate; a tunneling layer formed over the second surface of the semiconductor substrate; a first doped conductive layer and a retardation layer formed on a surface of the tunneling layer, wherein the first doped conductive layer is located between the tunneling layer and the retardation layer, and the first doped conductive layer and the retardation layer correspond to a metallization region; a second doped conductive layer formed over the surface of the tunneling layer, the second doped conductive layer covering the tunneling layer in a non-metallization region and the retardation layer, wherein a doping concentration of the second doped conductive layer is greater than a doping concentration of the first doped conductive layer, and the retardation layer is configured to retard migration of a doped element in the second doped conductive layer to the first doped conductive layer; a second passivation layer formed over a surface of the second doped conductive layer; and a second electrode penetrating through the second passivation layer to form contact with the second doped conductive layer and a first electrode penetrating through the first passivation layer to form contact with the emitter.
A civil aviation component having a fibre-reinforced composite structure, the component comprising: a plurality of structural fibres embedded in a cured matrix material; and a plurality of nanostructures extending from one or more of the structural fibres, a density of the nanostructures being at least about 10 7 nanostructures per cm 2 of area of a surface of the one or more structural fibres, wherein the density of nanostructures is determined by the method set out in the description with reference to example 3; characterized in that the matrix material comprises a polyester, vinyl-ester, epoxy, benzoxazine and/or bismaleimide resin system, and wherein the matrix material is doped with graphene. a plurality of structural fibres embedded in a cured matrix material; and a plurality of nanostructures extending from one or more of the structural fibres, a density of the nanostructures being at least about 10 7 nanostructures per cm 2 of area of a surface of the one or more structural fibres, wherein the density of nanostructures is determined by the method set out in the description with reference to example 3;
Direct current rotating electric machine, such as a motor vehicle starter, comprising: - a stator with salient poles comprising at least four poles distributed uniformly on the circumference of the stator, - a rotor arranged inside the rotor, - a group of brushes (13, 14) arranged to allow the rotor to be electrically powered, - at least two geometrically opposite salient poles each comprising at least one slit parallel to the axis of rotation of the rotor characterized in that a slit is arranged in the middle of the salient pole concerned. - a stator with salient poles comprising at least four poles distributed uniformly on the circumference of the stator, - a rotor arranged inside the rotor, - a group of brushes (13, 14) arranged to allow the rotor to be electrically powered, - at least two geometrically opposite salient poles each comprising at least one slit parallel to the axis of rotation of the rotor
A dress cover for an extendable cushion, comprising: a first section and at least a second section, the first section being fabricated from a first, expandable material and the at least a second section being fabricated from at least a second material, the second material being at least one non-expandable material, the first section including a compressed top surface length when the extendable cushion is in a retracted state, the first section including an expanded top surface length when the extendable cushion is in an extended state, the expanded top surface length being greater than the compressed top surface length, the dress cover configured to have a smooth side profile when the extendable cushion is in either of the retracted state or the extended state, the side profile of the dress cover being viewable when an aircraft seat including the extendable cushion with the dress cover is in a lie-flat or bed position, characterised in that the at least a second section includes a second section and a third section, the first section being positioned between the second section and the third section. a first section and at least a second section, the first section being fabricated from a first, expandable material and the at least a second section being fabricated from at least a second material, the second material being at least one non-expandable material, the first section including a compressed top surface length when the extendable cushion is in a retracted state, the first section including an expanded top surface length when the extendable cushion is in an extended state, the expanded top surface length being greater than the compressed top surface length, the dress cover configured to have a smooth side profile when the extendable cushion is in either of the retracted state or the extended state, the side profile of the dress cover being viewable when an aircraft seat including the extendable cushion with the dress cover is in a lie-flat or bed position, characterised in that the at least a second section includes a second section and a third section, the first section being positioned between the second section and the third section.
Wheel hub with improved sealing system for being associated with an axle shaft having an outer end intended to be associated with a wheel and an inner end, opposite the outer end, in particular for a commercial or industrial vehicle, comprising: - a flange of an axle bridge, - a bearing support intended to be axially associated with the flange, - a bearing press fitted inside the bearing support, having a fixed and externally complementary part with respect to the bearing support and a rotating part adapted to rotatingly support said axle shaft, -, - a sealing system formed by a gasket and a related seat, the wheel hub being characterized in that said seat is arranged • for direct interaction between said fixed part and said flange and • to preload said gasket radially. - a flange of an axle bridge, - a bearing support intended to be axially associated with the flange, - a bearing press fitted inside the bearing support, having a fixed and externally complementary part with respect to the bearing support and a rotating part adapted to rotatingly support said axle shaft, -, - a sealing system formed by a gasket and a related seat, the wheel hub being characterized in that said seat is arranged • for direct interaction between said fixed part and said flange and • to preload said gasket radially. • for direct interaction between said fixed part and said flange and • to preload said gasket radially.
A food container including a screw lid, the screw lid comprising: a centre panel, a series of radially extending asymmetric protrusions arranged around a peripheral edge region in a continuous sequence, wherein the asymmetric protrusions facilitate enhanced gripping when the lid is turned in an opening direction as compared to the gripping facilitated when the lid is turned in a closing direction, characterized in that each asymmetric protrusion has a maximum radial extent that is curved to smooth an outer surface of the screw lid, and wherein each asymmetric protrusion further comprises a minimum radial extent defining an interior corner filleted to smooth the outer surface of the screw lid, and in that the peripheral edge region has an upper lip that curls radially inward towards the centre panel. a centre panel, a series of radially extending asymmetric protrusions arranged around a peripheral edge region in a continuous sequence, wherein the asymmetric protrusions facilitate enhanced gripping when the lid is turned in an opening direction as compared to the gripping facilitated when the lid is turned in a closing direction, characterized in that each asymmetric protrusion has a maximum radial extent that is curved to smooth an outer surface of the screw lid, and wherein each asymmetric protrusion further comprises a minimum radial extent defining an interior corner filleted to smooth the outer surface of the screw lid, and in that the peripheral edge region has an upper lip that curls radially inward towards the centre panel.
A method, implemented in a computing device, the method comprising: identifying, in a host operating system of the computing device, a physical device to be made accessible to a guest partition of the computing device; virtualizing, by the host operating system of the computing device, a first portion of the physical device for access to the physical device by the guest partition, the first portion including at least part of a control plane for the physical device, the virtualizing making an exposed physical device control plane accessible to the guest partition by the host operating system; managing, by the host operating system of the computing device, accesses to the first portion of the physical device by the guest partition; and allowing the guest partition to directly access a non-virtualized second portion of the physical device, the non-virtualized second portion including at least part of a data plane for the physical device. identifying, in a host operating system of the computing device, a physical device to be made accessible to a guest partition of the computing device; virtualizing, by the host operating system of the computing device, a first portion of the physical device for access to the physical device by the guest partition, the first portion including at least part of a control plane for the physical device, the virtualizing making an exposed physical device control plane accessible to the guest partition by the host operating system; managing, by the host operating system of the computing device, accesses to the first portion of the physical device by the guest partition; and allowing the guest partition to directly access a non-virtualized second portion of the physical device, the non-virtualized second portion including at least part of a data plane for the physical device.