mhurhangee/ep-ind-claims huggingface dataset:
A method to determine a hot cargo load condition of a cargo load in a refrigerated container, the method comprising: providing a plurality of sensors disposed within the refrigerated container; operating a refrigeration unit with a set of desired operational parameters corresponding to the cargo load; analyzing a plurality of sensor readings corresponding to the plurality of sensors via a processor, and characterized in that the method further comprises creating a temperature distribution profile of the refrigerated container corresponding to the plurality of sensor readings via the processor; retrieving a historical temperature distribution profile corresponding to the cargo load via a historical database; comparing the temperature distribution profile to the historical temperature distribution profile via the processor; and identifying the hot cargo load condition in response to the temperature distribution profile exceeding the historical temperature distribution profile via the processor; wherein the historical temperature distribution profile is a temperature distribution profile corresponding to a similar cargo load which was transported in a similar refrigerated container under similar conditions. providing a plurality of sensors disposed within the refrigerated container; operating a refrigeration unit with a set of desired operational parameters corresponding to the cargo load; analyzing a plurality of sensor readings corresponding to the plurality of sensors via a processor, and characterized in that the method further comprises creating a temperature distribution profile of the refrigerated container corresponding to the plurality of sensor readings via the processor; retrieving a historical temperature distribution profile corresponding to the cargo load via a historical database; comparing the temperature distribution profile to the historical temperature distribution profile via the processor; and identifying the hot cargo load condition in response to the temperature distribution profile exceeding the historical temperature distribution profile via the processor; wherein the historical temperature distribution profile is a temperature distribution profile corresponding to a similar cargo load which was transported in a similar refrigerated container under similar conditions.
A device for drying a plurality of different plastic parts, in particular small sized material, such as crushed plastic waste, comprising a drum with an inlet opening for introducing humid plastic parts into the drum, and an outlet opening for discharging dehumidified plastic parts from the drum, means for transportation of the plastic parts, with the plastic parts being transportable from the inlet opening through the drum to the outlet opening, and means for dehumidifying the plastic parts, with the plastic parts being dehumidifiable inside of the drum, preferably by an air flow, characterised in that on the inner wall of the drum several baffle plates are substantially arranged one above the other, which have an angle of attack with respect to the inner wall of the drum, and each form sectionwise a flow and/or guiding channel for the plastic parts on the inner wall of the drum so that the plastic parts are transported by the means for transportation of the plastic parts through the drum alongside the flow and/or guiding channel formed by the baffle plates
Turret, particularly for an armoured military vehicle, comprising a support structure and a firearm carried by the support structure, the support structure including a base fixed to the turret and a connection beam articulated at its front end to the base so as to be able to rotate around a first horizontal axis of rotation, wherein the support structure also includes a firearm-carrying beam articulated at its rear end to the rear end of the connection beam so as to be able to rotate around a second horizontal axis of rotation parallel to the first, and in that the firearm is received in the firearm-carrying beam substantially so as to not project out from the back thereof.
A method for producing a heater comprising a co-sintered multi-layer structure for a system for providing an inhalable aerosol, having the steps: providing at least one first substrate layer; arranging at least one first insulating layer at least in regions on the first substrate layer; arranging at least one heating element at least in regions on the first insulating layer; arranging at least one second substrate layer and at least one second insulating layer at least in regions on the heating element, wherein the second insulating layer is arranged at least in regions on the second substrate layer, and wherein the second insulating layer is connected at least in regions to the heating element and/or the first insulating layer; pressing the layers and the heating element; and firing the pressed layers in order to co-sinter the layers of the multi-layer structure. providing at least one first substrate layer; arranging at least one first insulating layer at least in regions on the first substrate layer; arranging at least one heating element at least in regions on the first insulating layer; arranging at least one second substrate layer and at least one second insulating layer at least in regions on the heating element, wherein the second insulating layer is arranged at least in regions on the second substrate layer, and wherein the second insulating layer is connected at least in regions to the heating element and/or the first insulating layer; pressing the layers and the heating element; and firing the pressed layers in order to co-sinter the layers of the multi-layer structure.
Device for fastening ballistic protective elements and additional mounting parts on an object that is in particular to be protected from the effects of weapons or the effects of mines, said device comprising a welded cam (2-2") that can be fastened to the object that is to be protected and the base region of said welded cam that is facing the object can be connected via a welded connection to the object, and said welded cam comprises a threaded hole and it is possible to screw a screw into said threaded hole from the outside, wherein the welded cam (2-2") is provided with an outer thread, and wherein the device comprises a clamping nut (7; 7') having a through-going hole having an inner thread and said inner thread can be screwed onto the welded cam (2-2"), characterised in that a band (9;9') is provided on the side of the clamping nut (7;7') that is remote from the object that is to be protected and the dimensions of said band are selected in such a manner that when the device is in the assembled state the respective ballistic protective element can be fastened between the band (9; 9') of the clamping nut (7; 7') and the object that is to be protected, and also the corresponding attachment component can be fastened in a non-positive locking manner between the screw head of the screw and the band (9; 9') of the clamping nut (7; 7').
A process for treating thick fine tailings having a solids content of between 10 wt% and 45 wt%, and a fines content of at least 50 wt% of the total solids content, the process comprising: pre-shear thinning the thick fine tailings to produce a shear thinned thick fine tailings fluid with reduced yield stress or viscosity compared to the thick fine tailings; mixing a flocculant into the shear thinned thick fine tailings fluid to produce a mixture comprising water and flocs; and dewatering the mixture to allow water to separate from the flocs. pre-shear thinning the thick fine tailings to produce a shear thinned thick fine tailings fluid with reduced yield stress or viscosity compared to the thick fine tailings; mixing a flocculant into the shear thinned thick fine tailings fluid to produce a mixture comprising water and flocs; and dewatering the mixture to allow water to separate from the flocs.
A nacelle comprising: a nacelle outer wall and a nacelle inner wall spaced radially inwardly of said nacelle outer wall; a scoop inlet (102; 116; 122) for delivering air from a bypass duct defined between said nacelle inner and outer walls (82; 80), and for communicating the air radially inwardly of said inner wall to a downstream user; and said inner wall being provided with at least one opening at a location upstream of said scoop inlet (102; 116; 122); characterised by comprising: a tab (99; 115) extending upstream of said scoop inlet, wherein said opening is formed in said tab. a nacelle outer wall and a nacelle inner wall spaced radially inwardly of said nacelle outer wall; a scoop inlet (102; 116; 122) for delivering air from a bypass duct defined between said nacelle inner and outer walls (82; 80), and for communicating the air radially inwardly of said inner wall to a downstream user; and said inner wall being provided with at least one opening at a location upstream of said scoop inlet (102; 116; 122); characterised by comprising: a tab (99; 115) extending upstream of said scoop inlet, wherein said opening is formed in said tab.
A wing folding mechanism for a pair of wings, comprising a lower wing and a co-operative upper wing extending opposite to each other in a deployment position and approach each other when rotated from respective remote ends to a resting position characterized in that a spherical rolling element slot, adapted to receive a number of uniform spherical rolling elements, is provided at a corresponding lower wing root and a corresponding upper wing root, so that the lower wing and the upper wing are allowed to extend symmetrical to each other; a plurality of spherical rolling elements are disposed at the spherical rolling element slots; an alignment element is positioned coaxially with a wing pin hole and a linear energy storage element is arranged in a such manner that release of the stored energy accrued during the folding of the wings deploys the wings by actuation of the spherical rolling element slots and is disposed around the alignment element to exert a pressing force to the upper wing, and the rolling elements in the slots climb by rolling inside the slots 10) of the corresponding wings when the lower wing and the upper wing rotate relative to each other during the folding of the wings.
A nacelle assembly for a turbofan aircraft engine having an engine centerline, the nacelle assembly comprising: (a) a stationary forward nacelle portion having an outer fairing and a trailing edge; (b) a translatable variable area fan nozzle comprising two or more nozzle segments, each nozzle segment having first and second opposed ends and a leading edge that outwardly and rearwardly slopes at a first angle with respect to the engine centerline, the fan nozzle being selectively movable between a stowed position and one or more deployed positions, wherein in the deployed position, an upstream bypass flow exit is formed between the trailing edge and the leading edge; and (c) a split beavertail fairing comprising an upstream fairing portion on the outer fairing and a downstream fairing portion on at least one end of at least one nozzle segment; (d) wherein when the at least one nozzle segment is in the stowed position, the upstream fairing portion and the downstream fairing portion combine to form a substantially continuous outer surface extending between the outer fairing and the at least one nozzle segment; and (e) wherein when the at least one nozzle segment is in the deployed position, the upstream fairing portion and the downstream fairing portion define a substantially rearwardly extending elongated gap therebetween, characterized by the elongated gap being inclined with respect to the engine centerline (C 1) at a second angle (β 1), which is different to the first angle (θ 1). (a) a stationary forward nacelle portion having an outer fairing and a trailing edge; (b) a translatable variable area fan nozzle comprising two or more nozzle segments, each nozzle segment having first and second opposed ends and a leading edge that outwardly and rearwardly slopes at a first angle with respect to the engine centerline, the fan nozzle being selectively movable between a stowed position and one or more deployed positions, wherein in the deployed position, an upstream bypass flow exit is formed between the trailing edge and the leading edge; and (c) a split beavertail fairing comprising an upstream fairing portion on the outer fairing and a downstream fairing portion on at least one end of at least one nozzle segment; (d) wherein when the at least one nozzle segment is in the stowed position, the upstream fairing portion and the downstream fairing portion combine to form a substantially continuous outer surface extending between the outer fairing and the at least one nozzle segment; and (e) wherein when the at least one nozzle segment is in the deployed position, the upstream fairing portion and the downstream fairing portion define a substantially rearwardly extending elongated gap therebetween, characterized by the elongated gap being inclined with respect to the engine centerline (C 1) at a second angle (β 1), which is different to the first angle (θ 1).
A negative electrode active material containing a negative electrode active material particle; the negative electrode active material particle comprising a silicon compound particle containing a silicon compound that contains oxygen, wherein the silicon compound particle contains a Li compound, and at least part of Si constituting the silicon compound particle is present in at least one state selected from oxide of Si 2+ to Si 3+ containing no Li, and compound containing Li and Si 2+ to Si 3+, wherein the silicon compound particle has a peak or shoulder peak in an energy range from 1844 eV to 1846.5 eV in a XANES region of a Si K-edge in an X-ray absorption spectrum obtained when an X-ray absorption fine structure analysis is performed according to the method indicated in the description, wherein as the silicon compound particle is charged with electricity in a larger amount in an electricity charging process, the peak or shoulder peak appearing in the energy range from 1844 eV to 1846.5 eV in the XANES region of the Si K-edge has a higher intensity. the negative electrode active material particle comprising a silicon compound particle containing a silicon compound that contains oxygen, wherein the silicon compound particle contains a Li compound, and at least part of Si constituting the silicon compound particle is present in at least one state selected from oxide of Si 2+ to Si 3+ containing no Li, and compound containing Li and Si 2+ to Si 3+, wherein the silicon compound particle has a peak or shoulder peak in an energy range from 1844 eV to 1846.5 eV in a XANES region of a Si K-edge in an X-ray absorption spectrum obtained when an X-ray absorption fine structure analysis is performed according to the method indicated in the description, wherein as the silicon compound particle is charged with electricity in a larger amount in an electricity charging process, the peak or shoulder peak appearing in the energy range from 1844 eV to 1846.5 eV in the XANES region of the Si K-edge has a higher intensity.
A method for controlling receive diversity of an antenna system of a computer device, the antenna system including two or more antenna elements (218a, 218b), the method comprising: establishing a session with a remote transmitting system; determining whether a predetermined criteria detected by the computer device is satisfied within the session, and if so: activating at least two of the antenna elements (218a, 218b) for receiving transmissions, enabling performance of receive diversity on the received transmissions, and performing receive diversity on the received transmissions; if the predetermined criteria is not satisfied within the session: activating at least one of the antenna elements, disabling performance of receive diversity on the received transmissions, and performing a default signal processing on the received transmissions; and displaying an interface on the computer device, the interface including a sliding scale for setting of a threshold during the session, wherein the predetermined criteria includes the threshold, and wherein the interface includes a second sliding scale and the predetermined criteria is detected within a time period, the time period being second adjustable by a user through the interface using the second sliding scale. establishing a session with a remote transmitting system; determining whether a predetermined criteria detected by the computer device is satisfied within the session, and if so: activating at least two of the antenna elements (218a, 218b) for receiving transmissions, enabling performance of receive diversity on the received transmissions, and performing receive diversity on the received transmissions; if the predetermined criteria is not satisfied within the session: activating at least one of the antenna elements, disabling performance of receive diversity on the received transmissions, and performing a default signal processing on the received transmissions; and displaying an interface on the computer device, the interface including a sliding scale for setting of a threshold during the session, wherein the predetermined criteria includes the threshold, and wherein the interface includes a second sliding scale and the predetermined criteria is detected within a time period, the time period being second adjustable by a user through the interface using the second sliding scale.
A shaving system comprising: a handle having a distal end and a proximal end, and a shaving assembly comprising an interface element configured to removably interface with the handle and a blade unit pivotably mounted on the interface element, characterized in that the handle includes a protrusion at its distal end having a pair of walls extending perpendicular to the longitudinal axis of the handle, and the interface element of the shaving assembly includes a cavity, wherein the cavity is an asymmetrical cavity configured to receive the protrusion in a predetermined manner such that only one orientation is possible, and wherein complementary keyed structures (130, 120, 20, 22) are provided, comprising channels on both of the walls of the pair of walls of the protrusion and complementary ribs on surfaces of the cavity which oppose the walls. a handle having a distal end and a proximal end, and a shaving assembly comprising an interface element configured to removably interface with the handle and a blade unit pivotably mounted on the interface element, characterized in that the handle includes a protrusion at its distal end having a pair of walls extending perpendicular to the longitudinal axis of the handle, and the interface element of the shaving assembly includes a cavity, wherein the cavity is an asymmetrical cavity configured to receive the protrusion in a predetermined manner such that only one orientation is possible, and wherein complementary keyed structures (130, 120, 20, 22) are provided, comprising channels on both of the walls of the pair of walls of the protrusion and complementary ribs on surfaces of the cavity which oppose the walls.
A method of forming a device, the method comprising: growing a p-type layer (12, 36, 100); forming a mask layer on a surface of the p-type layer (12, 36, 100); growing a light emitting layer (14, 34) and an n-type layer (16, 32) on the mask layer and the p-type layer (12, 36, 100), the light emitting layer (14, 34) being sandwiched between the p-type layer (12, 36, 100) and the n-type layer (16, 32); forming at least one embedded trench by removing the mask layer, the at least one embedded trench exposing at least one portion of the p-type layer (12, 36, 100) to an ambient environment; and then annealing the device. growing a p-type layer (12, 36, 100); forming a mask layer on a surface of the p-type layer (12, 36, 100); growing a light emitting layer (14, 34) and an n-type layer (16, 32) on the mask layer and the p-type layer (12, 36, 100), the light emitting layer (14, 34) being sandwiched between the p-type layer (12, 36, 100) and the n-type layer (16, 32); forming at least one embedded trench by removing the mask layer, the at least one embedded trench exposing at least one portion of the p-type layer (12, 36, 100) to an ambient environment; and then annealing the device.
Component of a surface coating plant, in particular a painting plant or powder coating plant, wherein the component itself has a coating upon whose surface particles are freely deposited during operation of the plant, characterized in that the coating is formed as the sacrificial layer, which may be detached in layers from the component together with the particles, wherein several layers may be peeled off one by one without a new coating being required in between, and wherein the sacrificial layer comprises a mixture of lime, a water-based liquid and a binding agent, preferably an adhesion promoter on a resin base.
A method in a steering fault detection system adapted to detect a steering fault of a vehicle, the vehicle comprises an active steering support system adapted to assist steering the vehicle at least in dependence of one environmental signal and to generate a steering assist control signal to a steering servo system of the vehicle, wherein said steering assist control signal includes one or many steering assist control values, wherein the method comprises: B - applying said steering assist control signal to said steering fault detection system; C - analysing said steering assist control values in relation to predetermined ideal steering assist control values, and D - generating an indication signal in dependence of said analysis, wherein said indication signal includes steering fault information, characterized in that said steering fault information includes type of fault and/or magnitude of fault which is used to identify incorrectly set wheel geometries and plays in steered axles or wheel suspensions. B - applying said steering assist control signal to said steering fault detection system; C - analysing said steering assist control values in relation to predetermined ideal steering assist control values, and D - generating an indication signal in dependence of said analysis, wherein said indication signal includes steering fault information, characterized in that said steering fault information
Method for producing a foam of poly(meth)acrylimide, characterized in that a mixture comprising (meth)acrylonitrile, (meth)acrylic acid, a polyol, at least one initiator and at least one blowing agent is polymerized to form a slab or a powder, is optionally temperature-conditioned, and then is foamed at a temperature between 120 and 300°C, wherein the polyol is a diol and the diol is ethylene glycol, 1,10-decanediol, beta-hydroxyalkylamides, OH-telechelic polytetrahydrofuran having an average molar mass between 500 and 8000 g/mol, or comprises OH-telechelic polyolefins, polycarbonates, polyoxymethylenes, polyethylene glycols, polypropylene glycols, polyglycerols or polyesters each having a molar mass between 200 and 10 000 g/mol and the mixture consists of - 20 to 60 wt% of (meth)acrylonitrile, - 40 to 78 wt% of (meth)acrylic acid, - 0 to 20 wt% of further monofunctional, vinylically unsaturated monomers, - one or more polyols in an amount such that the hydroxyl number of the mixture is between 0.0008 and 0.2 mol of OH groups/100 g of polymer, preferably between 0.001 and 0.1 mol of OH groups/100 g of polymer, - 1 to 15 wt% of a blowing agent, of a copolymerizable blowing agent or of a blowing agent mixture, - optionally 0 to 5 wt% of further crosslinkers, - an initiator system and - customary additional substances. - 20 to 60 wt% of (meth)acrylonitrile, - 40 to 78 wt% of (meth)acrylic acid, - 0 to 20 wt% of further monofunctional, vinylically unsaturated monomers, - one or more polyols in an amount such that the hydroxyl number of the mixture is between 0.0008 and 0.2 mol of OH groups/100 g of polymer, preferably between 0.001 and 0.1 mol of OH groups/100 g of polymer, - 1 to 15 wt% of a blowing agent, of a copolymerizable blowing agent or of a blowing agent mixture, - optionally 0 to 5 wt% of further crosslinkers, - an initiator system and - customary additional substances.