mhurhangee/ep-ind-claims huggingface dataset:
A process for heat transfer printing, the process comprising: electrostatically printing a transparent release composition onto a transfer material to form a release layer disposed on the transfer material; electrostatically printing an electrostatic ink composition on the release layer to form an image layer disposed on the release layer; contacting a thermoplastic film with the image layer, wherein the thermoplastic film is a bi-layer film in which the layers have different melting temperatures; contacting the thermoplastic film with a target substrate under conditions such that the thermoplastic film adheres to the target substrate and the release layer is softened; and separating the target substrate and the transfer material such that the thermoplastic film, image layer and release layer are transferred to the target substrate, wherein the bi-layer comprises a first layer having a first melting temperature and a second layer having a second melting temperature wherein the first melting temperature is lower than the second melting temperature and the second layer is contacted with the image layer and the first layer is contacted with the target substrate. electrostatically printing a transparent release composition onto a transfer material to form a release layer disposed on the transfer material; electrostatically printing an electrostatic ink composition on the release layer to form an image layer disposed on the release layer; contacting a thermoplastic film with the image layer, wherein the thermoplastic film is a bi-layer film in which the layers have different melting temperatures; contacting the thermoplastic film with a target substrate under conditions such that the thermoplastic film adheres to the target substrate and the release layer is softened; and separating the target substrate and the transfer material such that the thermoplastic film, image layer and release layer are transferred to the target substrate, wherein the bi-layer comprises a first layer having a first melting temperature and a second layer having a second melting temperature wherein the first melting temperature is lower than the second melting temperature and the second layer is contacted with the image layer and the first layer is contacted with the target substrate.
A load wrapping and transporting vehicle, comprising: a vehicle frame; a load support connected to said vehicle frame for supporting a palletized load; a spindle supporting a roll of wrapping film; characterized in that said load wrapping and transporting vehicle further comprises an endless track connected to said vehicle frame and extending about said load support; said spindle is guided by said endless track about said load support to wrap the palletized load with wrapping film dispensed by the roll of wrapping film; said load wrapping and transporting vehicle further comprises a carrier supported by said endless track and guided about said load support, said carrier movably supporting said spindle and the roll of wrapping film, wherein said carrier defines a linear path along which said spindle and the roll of wrapping film are movable; and said endless track defines an endless path along which said carrier is guided about said load support, said endless path being disposed in a horizontal plane and said linear path being disposed in a vertical plane substantially perpendicular to said horizontal plane such that said spindle and the roll of wrapping film are guided in a helical path about said load support to wrap the palletized load. a vehicle frame; a load support connected to said vehicle frame for supporting a palletized load; a spindle supporting a roll of wrapping film; characterized in that said load wrapping and transporting vehicle further comprises an endless track connected to said vehicle frame and extending about said load support; said spindle is guided by said endless track about said load support to wrap the palletized load with wrapping film dispensed by the roll of wrapping film; said load wrapping and transporting vehicle further comprises a carrier supported by said endless track and guided about said load support, said carrier movably supporting said spindle and the roll of wrapping film, wherein said carrier defines a linear path along which said spindle and the roll of wrapping film are movable; and said endless track defines an endless path along which said carrier is guided about said load support, said endless path being disposed in a horizontal plane and said linear path being disposed in a vertical plane substantially perpendicular to said horizontal plane such that said spindle and the roll of wrapping film are guided in a helical path about said load support to wrap the palletized load.
A rotary machine with pistons and a barrel, comprising: - a housing through which there passes a shaft, of geometric axis x-x', mounted fixedly with respect to the housing, - a thrust plate rotatably mounted on the shaft, - a wobble plate pressing against the thrust plate, - a reaction rod a first end of which is articulated to the housing and a second end of which is articulated to the wobble plate, - a female spherical bearing bushing secured to the wobble plate, articulated about a male spherical ball centered on the shaft, characterized in that the ball comprises a male spherical bearing bushing rotatably mounted with respect to the shaft, and in that the rotary machine comprises a means of driving the rotation of the male spherical bearing bushing about the geometric axis x-x'. - a housing through which there passes a shaft, of geometric axis x-x', mounted fixedly with respect to the housing, - a thrust plate rotatably mounted on the shaft, - a wobble plate pressing against the thrust plate, - a reaction rod a first end of which is articulated to the housing and a second end of which is articulated to the wobble plate, - a female spherical bearing bushing secured to the wobble plate, articulated about a male spherical ball centered on the shaft,
A method for providing visibility alerts by transmitting information related to a fog covered area in which visibility is affected, said method comprising: monitoring a geographical area by each of a plurality of visibility detectors; receiving, at each of a plurality of lighting units of at least one Outdoor Lighting Network, monitoring data from at least one of said visibility detectors, wherein at least two of said lighting units are in communication with each other; deriving a consolidated estimate of visibility conditions pertaining to a combined geographical area defined by the monitored geographical areas associated with two or more of said visibility detectors; the method characterised by determining a position, direction and speed of said fog covered area from the consolidated estimate of visibility conditions; and transmitting information comprising the position, direction and speed of said fog covered area. monitoring a geographical area by each of a plurality of visibility detectors; receiving, at each of a plurality of lighting units of at least one Outdoor Lighting Network, monitoring data from at least one of said visibility detectors, wherein at least two of said lighting units are in communication with each other; deriving a consolidated estimate of visibility conditions pertaining to a combined geographical area defined by the monitored geographical areas associated with two or more of said visibility detectors; the method characterised by determining a position, direction and speed of said fog covered area from the consolidated estimate of visibility conditions; and transmitting information comprising the position, direction and speed of said fog covered area.
Wind deflector device for a wiper blade, with at least one wind deflector unit, which is provided to deflect an incident air flow, wherein the wind deflector unit comprises an actuating unit, which is provided to passively increase a wind deflector height at least in regions when an incident air flow velocity increases, characterized in that, as an incident air flow velocity increases, at least one end edge of the wind deflector unit at least partially moves in an opposed manner to the incident air flow.
A tower of a wind turbine with at least one wall part, wherein the one wall part is connected to a second, bordering wall part, or the one wall part is arranged on a main body, wherein the wall part is connected to the main body, wherein the one wall part has at least one transverse borehole during or for forming the tower, wherein the transverse borehole is a radial borehole, and the transverse borehole is penetrated by a transverse bolt, characterized in that: the one wall part borders and/or is arranged at the face or to abut the second wall part, and the wall part is clamped to the bordering second wall part by means of a clamping element engaging with the transverse bolt and/or the one wall part borders and/or is arranged at the face or to abut the main body, and the one wall part is clamped to the main body by means of a clamping element engaging with the transverse bolt. the one wall part borders and/or is arranged at the face or to abut the second wall part, and the wall part is clamped to the bordering second wall part by means of a clamping element engaging with the transverse bolt and/or the one wall part borders and/or is arranged at the face or to abut the main body, and the one wall part is clamped to the main body by means of a clamping element engaging with the transverse bolt.
A computer implemented method to detect an anomalous change to a web application, the web application executing with a web server, the method comprising: receiving a first set of records for the web application operating in a training mode of operation, each record including characteristics of a content of a web page for the web application and the characteristics including features of a response message generated by the web server; generating a sparse distributed representation of the set of records to form a training set for a hierarchical temporal memory "HTM"; training the HTM based on the training set in order that the trained HTM provides a model of the operation of the web application in the training mode of operation; receiving a second set of records for the web application, each record including characteristics of content of the web page and the characteristics including features of a response message generated by the web server; generating a sparse distributed representation of the second set of records to form an input set for the trained HTM; executing the trained HTM based on the input set to determine a degree of recognition of the records of the input set; and responsive to a determination that a degree of recognition of one or more records of the input set is below a threshold degree, identifying an anomalous change to the web page. receiving a first set of records for the web application operating in a training mode of operation, each record including characteristics of a content of a web page for the web application and the characteristics including features of a response message generated by the web server; generating a sparse distributed representation of the set of records to form a training set for a hierarchical temporal memory "HTM"; training the HTM based on the training set in order that the trained HTM provides a model of the operation of the web application in the training mode of operation; receiving a second set of records for the web application, each record including characteristics of content of the web page and the characteristics including features of a response message generated by the web server; generating a sparse distributed representation of the second set of records to form an input set for the trained HTM; executing the trained HTM based on the input set to determine a degree of recognition of the records of the input set; and responsive to a determination that a degree of recognition of one or more records of the input set is below a threshold degree, identifying an anomalous change to the web page.
A method for controlling flight control surfaces of an aircraft wing having a first flight control surface and a second flight control surface, the first flight control surface having a first leading edge and a first trailing edge, the second flight control surface having a contact surface extending between a second leading edge and a second trailing edge, the first flight control surface being movable to contact the first trailing edge with the contact surface and make a seal therewith, the method comprising: displacing the first trailing edge of the first flight control surface towards the contact surface of the second flight control surface; characterised in that the method further comprises: determining a mechanical stiffness of the first flight control surface as defined by a ratio of ΔF/ΔX as the first flight control surface is displaced, where ΔF is a difference in force F applied to at least two different positions X1 and X2 of the first flight control surface at times T1 and T2, and ΔX is a difference in position X2-X1; and achieving full contact between the first trailing edge and the second leading edge when a known full contact mechanical stiffness is reached. displacing the first trailing edge of the first flight control surface towards the contact surface of the second flight control surface; characterised in that the method further comprises: determining a mechanical stiffness of the first flight control surface as defined by a ratio of ΔF/ΔX as the first flight control surface is displaced, where ΔF is a difference in force F applied to at least two different positions X1 and X2 of the first flight control surface at times T1 and T2, and ΔX is a difference in position X2-X1; and achieving full contact between the first trailing edge and the second leading edge when a known full contact mechanical stiffness is reached. determining a mechanical stiffness of the first flight control surface as defined by a ratio of ΔF/ΔX as the first flight control surface is displaced, where ΔF is a difference in force F applied to at least two different positions X1 and X2 of the first flight control surface at times T1 and T2, and ΔX is a difference in position X2-X1; and achieving full contact between the first trailing edge and the second leading edge when a known full contact mechanical stiffness is reached.
Method for providing a head mounted optical system adapted to a wearer, the method comprising: - an optical system providing step, during which an optical system is provided, - a wearer data providing step, during which wearer data comprising at least the wearer's prescription is provided, - an encapsulating step, during which the optical system is at least partly encapsulated in a transparent capsule, - a mounting step, during which the encapsulated optical system or the optical system is mounted in a spectacle frame, - a customizing step, during which, respectively, at least one face of the optical system or one face (32, 34) of the transparent capsule is customized according to the wearer data, wherein the optical system is at least partly encapsulated in a transparent capsule by stacking in close contact the optical system with at least one substrate of the transparent capsule and made integral with an adhesive, characterized in that the customizing step is implemented after the mounting step, and during the customizing step an optical patch is added to the face to be customized of the capsule or of the optical system. - an optical system providing step, during which an optical system is provided, - a wearer data providing step, during which wearer data comprising at least the wearer's prescription is provided, - an encapsulating step, during which the optical system is at least partly encapsulated in a transparent capsule, - a mounting step, during which the encapsulated optical system or the optical system is mounted in a spectacle frame, - a customizing step, during which, respectively, at least one face of the optical system or one face (32, 34) of the transparent capsule is customized according to the wearer data,
A process for the recovery of a purified C 4 -C 12 (meth)acrylic ester, from a crude reaction mixture obtained by transesterification of a light (meth)acrylic ester by the corresponding alcohol, said reaction mixture comprising a catalyst for the transesterification reaction, said process being characterized in that it is carried out using a purification system comprising a divided wall column equipped with a separating wall creating separation zones in the column, the wall not being joined to the upper dome of the column in the top part and being joined to the bottom of the column in the bottom part, said divided wall column combined at the top with a single condenser and at the bottom with two boilers, comprising a common rectification section above the wall, a prefractionation section comprising the feeding of the column, a withdrawal section separated from the prefractionation section by the wall comprising the withdrawal of the purified ester, and characterized in that i) a gas stream is extracted at the top of the rectification section and recycled after condensation at least in part in the reactor, ii) a stream is withdrawn at the bottom of the prefractionation section and recycled at least in part in the reactor, iii) a stream is withdrawn at the bottom of the withdrawal section and recycled at least in part in the prefractionation section of the column, and iv) a stream of purified (meth)acrylic ester is drawn off as a sidestream from the withdrawal section at a point located above the bottom withdrawal of said withdrawal section. said process being characterized in that it is carried out using a purification system comprising a divided wall column equipped with a separating wall creating separation zones in the column, the wall not being joined to the upper dome of the column in the top part and being joined to the bottom of the column in the bottom part, said divided wall column combined at the top with a single condenser and at the bottom with two boilers, comprising a common rectification section above the wall, a prefractionation section comprising the feeding of the column, a withdrawal section separated from the prefractionation section by the wall comprising the withdrawal of the purified ester, and characterized in that i) a gas stream is extracted at the top of the rectification section and recycled after condensation at least in part in the reactor, ii) a stream is withdrawn at the bottom of the prefractionation section and recycled at least in part in the reactor, iii) a stream is withdrawn at the bottom of the withdrawal section and recycled at least in part in the prefractionation section of the column, and iv) a stream of purified (meth)acrylic ester is drawn off as a sidestream from the withdrawal section at a point located above the bottom withdrawal of said withdrawal section.
A hydroelectric turbine comprising: - a rotor assembly having a rotation axis x and comprising a number m of modules adjacent to each other and aligned to each other, each module comprising a number n of blades parallel to said rotation axis x and arranged about said rotation axis x with a predetermined angular range θ, said rotor assembly arranged to rotate, in use, about said rotation axis x when said blades are immersed in a water flow; - a support structure arranged to support said rotor assembly; - an electric power generator operatively connected to said rotor assembly, said electric power generator arranged to generate electric power by the rotation of said rotor assembly about said rotation axis x; said blades having, in cross-section, an aerodynamic profile, in order to increase the fluid dynamic efficiency of said blades when they are immersed in said water flow, said support structure being configured to keep said rotation axis x, in use, in a position substantially horizontal and orthogonal to said water flow, said support structure comprising two arms arranged to move said rotor assembly relatively respect to said support structure for placing said rotor assembly between a position completely immersed in said water flow and a position emerged from said water flow, said hydroelectric turbine characterized in that the n -th blade of a first module is arranged with a predetermined angular offset φ with respect to the respective n -th blade (115") of a second module (111") next to said first module, in that said rotor assembly comprises a central shaft arranged to increase the structural stiffness of said rotor assembly, said central shaft being aligned to said rotation axis x, and in that said blades are connected to said central shaft through a plurality of dividing elements, each dividing element comprising at least one blade having an aerodynamic profile and arranged in order to offer the minimum resistance against said water flow. - a rotor assembly having a rotation axis x and comprising a number m of modules adjacent to each other and aligned to each other, each module comprising a number n of blades parallel to said rotation axis x and arranged about said rotation axis x with a predetermined angular range θ, said rotor assembly arranged to rotate, in use, about said rotation axis x when said blades are immersed in a water flow; - a support structure arranged to support said rotor assembly; - an electric power generator operatively connected to said rotor assembly, said electric power generator arranged to generate electric power by the rotation of said rotor assembly about said rotation axis x;