mhurhangee/ep-ind-claims huggingface dataset:
Method for producing a film composite (11, 43) for a security document, - in which a material core web and at least one material web (14, 16) are continuously laminated in a laminating device to form the film composite (11, 43), wherein - the material core web is fed preheated to an embossing station, - an embossing is introduced into at least one side of the material core web embossing is applied to at least one side, - the at least one material web is preheated and fed onto the material core web to cover the embossing, and - the material core web and the at least one material web are laminated in the lamination station to form the film composite. - in which a material core web and at least one material web (14, 16) are continuously laminated in a laminating device to form the film composite (11, 43), - the material core web is fed preheated to an embossing station, - an embossing is introduced into at least one side of the material core web embossing is applied to at least one side, - the at least one material web is preheated and fed onto the material core web to cover the embossing, and - the material core web and the at least one material web are laminated in the lamination station to form the film composite.
A wind turbine including a rotor, including a hub, a first rotor blade, a second rotor blade, a third rotor blade, and a load identification system comprising: a control system; and a plurality of acceleration sensors (400,402,404,406) mounted within the hub, wherein a first acceleration sensor is mounted adjacent to the first rotor blade, a second acceleration sensor is mounted adjacent to the second rotor blade, and a third acceleration sensor is mounted adjacent to the third rotor blade, the acceleration sensors being communicatively coupled with said control system, each of said acceleration sensors being configured to sense accelerations of the rotor in three dimensions and to transmit signals indicative of the sensed accelerations to said control system, said control system configured to receive the signals from said acceleration sensors and to identify a load on the wind turbine based on the received signals. a control system; and
A self-aligning piston configured to selectively engage and disengage a pipe segment, the self-aligning piston comprising: a piston body configured to rotate between a first position and a second position; at least one resilient, energy-storing member coupled to the piston body; and a roller assembly coupled to the piston body; wherein the self-aligning piston further comprises: a cam disposed between the at least one resilient, energy-storing member and the roller assembly, wherein the resilient, energy-storing member is configured to bias the piston body into the first position by rotating the roller assembly along the cam, wherein the first position corresponds to a predetermined, aligned orientation relative to the pipe segment and the second position corresponds to a variable, misaligned orientation relative to the pipe segment; and a splined shaft, wherein the piston body is configured to slide along the splined shaft as the self-aligning piston is actuated between an engaged position with the pipe segment and a disengaged position, wherein the piston body is configured to rotate around the splined shaft, and wherein the roller assembly is configured to rotate around the splined shaft. a piston body configured to rotate between a first position and a second position; at least one resilient, energy-storing member coupled to the piston body; and a roller assembly coupled to the piston body; wherein the self-aligning piston further comprises: a cam disposed between the at least one resilient, energy-storing member and the roller assembly, wherein the resilient, energy-storing member is configured to bias the piston body into the first position by rotating the roller assembly along the cam, wherein the first position corresponds to a predetermined, aligned orientation relative to the pipe segment and the second position corresponds to a variable, misaligned orientation relative to the pipe segment; and a splined shaft, a cam disposed between the at least one resilient, energy-storing member and the roller assembly, wherein the resilient, energy-storing member is configured to bias the piston body into the first position by rotating the roller assembly along the cam, wherein the first position corresponds to a predetermined, aligned orientation relative to the pipe segment and the second position corresponds to a variable, misaligned orientation relative to the pipe segment; and a splined shaft, wherein the piston body is configured to slide along the splined shaft as the self-aligning piston is actuated between an engaged position with the pipe segment and a disengaged position, wherein the piston body is configured to rotate around the splined shaft, and wherein the roller assembly is configured to rotate around the splined shaft.
Utility vehicle (1, 2), in particular an agricultural or municipal utility vehicle (1, 2), with an implement configured for exclusively working a ground area which runs parallel to a ground area to be travelled over by the utility vehicle (1, 2), wherein the ground area to be travelled over is a drivable surface which has essentially no vegetation, and the ground area to be cultivated is a surface which has vegetation which is to be cultivated by means of the implement, wherein the utility vehicle (1, 2) has a steering system, wherein the steering system comprises a control unit for generating steering signals for autonomous guidance of the utility vehicle (1, 2), a camera arrangement for recording images and a user interface connected to the control unit, wherein the control unit is configured for evaluating the image data generated by the camera arrangement in order to generate the steering signals as a function of the image data, wherein the at least one camera arrangement is positioned on the utility vehicle (1, 2) in such a way and is orientated with its gaze in such a way that the ground area to be travelled over and the ground area to be worked on laterally adjacent thereto can be detected simultaneously, and in that the control unit is configured to determine a boundary (20, 25) on the basis of the detected image data, along which the steering system guides the utility vehicle (1, 2) and/or the implement at a distance to be maintained.
A method for reducing SRAM (400, 500) leakage in an integrated circuit device (410, 510) that includes an SRAM module, the method comprising: receiving input data; encoding the received input data; storing the encoded input data in the SRAM module; the method characterised by: entering standby mode, wherein standby mode is entered by reducing supply voltage applied to the SRAM module to a lower voltage than a data retention voltage of the SRAM module and whereby the data retention voltage is the amount of voltage needed to be supplied to the SRAM module to retain the data stored in the SRAM module reliably and to compensate for SRAM leakage; scrubbing the data stored in the SRAM module while in standby mode; exiting standby mode; decoding the data stored in the SRAM module; performing error correction on the decoded data; outputting the error-corrected decoded data; and writing information regarding the error correction to the SRAM module. receiving input data; encoding the received input data; storing the encoded input data in the SRAM module; the method characterised by: entering standby mode, wherein standby mode is entered by reducing supply voltage applied to the SRAM module to a lower voltage than a data retention voltage of the SRAM module and whereby the data retention voltage is the amount of voltage needed to be supplied to the SRAM module to retain the data stored in the SRAM module reliably and to compensate for SRAM leakage; scrubbing the data stored in the SRAM module while in standby mode; exiting standby mode; decoding the data stored in the SRAM module; performing error correction on the decoded data; outputting the error-corrected decoded data; and writing information regarding the error correction to the SRAM module. entering standby mode, wherein standby mode is entered by reducing supply voltage applied to the SRAM module to a lower voltage than a data retention voltage of the SRAM module and whereby the data retention voltage is the amount of voltage needed to be supplied to the SRAM module to retain the data stored in the SRAM module reliably and to compensate for SRAM leakage; scrubbing the data stored in the SRAM module while in standby mode; exiting standby mode; decoding the data stored in the SRAM module; performing error correction on the decoded data; outputting the error-corrected decoded data; and writing information regarding the error correction to the SRAM module.
A shock absorbing grip assembly comprising: a) one or more slotted grip end clamps (16, 316, 416, 456); b) one or more cavities (20, 76, 86, 125, 133, 165, 181, 194, 216, 226, 319, 336, 418, 458) in said slotted grip end clamps; c) a grip sleeve (28, 70, 96, 106, 120, 142, 158, 174, 206, 306, 404), wherein said grip sleeve includes one or more protruding engagement members (24, 72, 100, 114, 156, 172, 204, 308), and further one or more elastomeric isolator inserts (22A, 22B, 22C, 64, 84, 124, 132, 164, 180, 192, 212, 220) housed within each of said one or more cavities in said grip end clamps and wherein said one or more protruding engagement members mates within said cavities in said slotted grip end clamps interacting with said one or more elastomeric isolator inserts; and d) an outer grip (36, 60, 94, 104, 116, 138, 154, 170, 202, 302, 402, 442); whereby said one or more grip end clamps suspends or suspend said grip sleeve (28, 70, 96, 106, 120, 142, 158, 174, 206, 306, 404, 444) from contact with a handle or handlebar, said grip sleeve having torsional, rotational, linear and axial shock absorbing capacity when mounted to a handle or handlebar. a) one or more slotted grip end clamps (16, 316, 416, 456); b) one or more cavities (20, 76, 86, 125, 133, 165, 181, 194, 216, 226, 319, 336, 418, 458) in said slotted grip end clamps; c) a grip sleeve (28, 70, 96, 106, 120, 142, 158, 174, 206, 306, 404), wherein said grip sleeve includes one or more protruding engagement members (24, 72, 100, 114, 156, 172, 204, 308), and further one or more elastomeric isolator inserts (22A, 22B, 22C, 64, 84, 124, 132, 164, 180, 192, 212, 220) housed within each of said one or more cavities in said grip end clamps and wherein said one or more protruding engagement members mates within said cavities in said slotted grip end clamps interacting with said one or more elastomeric isolator inserts; and d) an outer grip (36, 60, 94, 104, 116, 138, 154, 170, 202, 302, 402, 442); whereby said one or more grip end clamps suspends or suspend said grip sleeve (28, 70, 96, 106, 120, 142, 158, 174, 206, 306, 404, 444) from contact with a handle or handlebar, said grip sleeve having torsional, rotational, linear and axial shock absorbing capacity when mounted to a handle or handlebar.
A dental imaging element comprising: a substrate having four chamfered corners; and a two-dimensional array of pixel sensors located on said substrate, said array being organized as a plurality of rows and columns, a layer of scintillation material overlying said two-dimensional array of pixel sensors, characterised by the provision of the array as an array of CMOS pixel sensors, the pixel sensors in each column being connected to a corresponding bit bus by a row select switch that connects said pixel sensor in said row to that bit bus in response to a row select signal on a corresponding row select line; a row decoder that generates said row select signal on a selected one of said row select lines in response to a row address being coupled thereto; a column decoder that connects a selected one of said bit buses to an interface connecting said dental imaging element_to a circuit that is external to said dental imaging element; and wherein the two-dimensional array of CMOS pixel sensors has four chamfered corners with the rows or columns that extend into the chamfered corners having lengths that are less than the rows or columns, respectively, that do not extend into said chamfered corners, the two-dimensional array of CMOS pixel sensors extends into the chamfered corners of said substrate, and said row decoder and said column decoder are located between two of said columns and two of said rows, respectively, such that said row decoder and said column decoder do not extend into any one of said chamfered corners. a substrate having four chamfered corners; and a two-dimensional array of pixel sensors located on said substrate, said array being organized as a plurality of rows and columns, a layer of scintillation material overlying said two-dimensional array of pixel sensors, characterised by the provision of the array as an array of CMOS pixel sensors, the pixel sensors in each column being connected to a corresponding bit bus by a row select switch that connects said pixel sensor in said row to that bit bus in response to a row select signal on a corresponding row select line; a row decoder that generates said row select signal on a selected one of said row select lines in response to a row address being coupled thereto; a column decoder that connects a selected one of said bit buses to an interface connecting said dental imaging element_to a circuit that is external to said dental imaging element; and wherein the two-dimensional array of CMOS pixel sensors has four chamfered corners with the rows or columns that extend into the chamfered corners having lengths that are less than the rows or columns, respectively, that do not extend into said chamfered corners, the two-dimensional array of CMOS pixel sensors extends into the chamfered corners of said substrate, and said row decoder and said column decoder are located between two of said columns and two of said rows, respectively, such that said row decoder and said column decoder do not extend into any one of said chamfered corners.
A variable geometry turbocharger in which exhaust gas from an engine acts on a turbine rotor through inside of a scroll chamber formed in a turbine casing and a plurality of variable nozzle vanes (45, 80), the variable geometry turbocharger comprising: a nozzle vane accommodating unit in which the plurality of variable nozzle vanes (45, 80) are arranged in a circumferential direction between the scroll chamber and the turbine rotor, the nozzle vane accommodating unit including parallel walls formed to be substantially parallel to both end surfaces of each of the nozzle vanes (45, 80) with a gap in between; a nozzle shaft (49, 72, 87) which protrudes on one of the both end surfaces of the nozzle vane (45, 80) and rotatably supports the nozzle vane; a shaft hole (53, 61, 74, 89) in which the nozzle shaft (49, 72, 87) fits with a gap in between, the shaft hole (53, 61, 74, 89) being formed in one of the parallel walls; a distal end surface of the nozzle vane (45, 80) with which a clearance is reduced when the nozzle vane (45, 80) which has received exhaust-gas pressure is inclined toward an inner diameter side due to a fitting gap formed between the shaft hole (53, 61, 74, 89) and the nozzle shaft (49, 72, 87) fit to each other, the clearance being formed between the distal end surface and a wall surface of another one of the parallel walls; and a clearance reduction promotion portion (60, 65, 70, 82) which promotes reduction of the clearance, achieved by the inclination of the distal end surface of the nozzle vane (45, 80), with an increased inclination angle of the distal end surface or an increased exhaust-gas-affected surface of the nozzle vane (45, 80). a nozzle vane accommodating unit in which the plurality of variable nozzle vanes (45, 80) are arranged in a circumferential direction between the scroll chamber and the turbine rotor, the nozzle vane accommodating unit including parallel walls formed to be substantially parallel to both end surfaces of each of the nozzle vanes (45, 80) with a gap in between; a nozzle shaft (49, 72, 87) which protrudes on one of the both end surfaces of the nozzle vane (45, 80) and rotatably supports the nozzle vane; a shaft hole (53, 61, 74, 89) in which the nozzle shaft (49, 72, 87) fits with a gap in between, the shaft hole (53, 61, 74, 89) being formed in one of the parallel walls; a distal end surface of the nozzle vane (45, 80) with which a clearance is reduced when the nozzle vane (45, 80) which has received exhaust-gas pressure is inclined toward an inner diameter side due to a fitting gap formed between the shaft hole (53, 61, 74, 89) and the nozzle shaft (49, 72, 87) fit to each other, the clearance being formed between the distal end surface and a wall surface of another one of the parallel walls; and a clearance reduction promotion portion (60, 65, 70, 82) which promotes reduction of the clearance, achieved by the inclination of the distal end surface of the nozzle vane (45, 80), with an increased inclination angle of the distal end surface or an increased exhaust-gas-affected surface of the nozzle vane (45, 80).
Aircraft which comprises at least two electrical devices and for each electrical device a fault current circuit for said electrical device passing by a current return network of said aircraft, said current return network consisting of metallic parts of the aircraft, each fault current circuit comprising at least one part made of composite material forming an electrical connection between said electrical device and said current return network, the aircraft being characterised in that each fault current circuit comprises at least one contact metallic member connected electrically to one of the electrical devices and assembled to said at least one part made of composite material by tight adjustment of the member with said part made of composite material, the contact member extending in a hole of the part made of composite material, a diameter v of the member and a diameter e of the hole satisfying: ( v - e)/ v ≥ 0.0025, the aircraft comprises a metallic structure connected to the parts made of composite material such that the fault current circuit of each electrical device passes by the part made of composite material associated with this electrical device and the metallic structure without passing by the part made of composite material associated with each other electrical device, and each fault current circuit mostly comprises, with reference to a length of said fault current circuit, metallic parts of the aircraft.
A support assembly for supporting a moveable member (22,202) of an agricultural combine comprising: the moveable member (22,202) operatively connected to the combine and moveable relative to the combine, the moveable member having a lower portion; a support member (24,204) connected to the combine, the support member having an upper portion; and a pliable resilient member (26,206) having a first end connected to the support member (24,204) and a second end connected to the lower portion of the moveable member (22,202), the pliable resilient member (26,206) being configured to allow movement of the moveable member (22,202) relative to the support member (24,204) in six degrees of freedom and to support the moveable member in a spaced apart relation to the support member, characterized in that: the first end of the pliable resilient member (26,206) is connected to the upper portion of the support member (24,204) and the support member (24,204) is pivotably connected to the combine to support the moveable member (22,202) in at least a first position and a second position. the moveable member (22,202) operatively connected to the combine and moveable relative to the combine, the moveable member having a lower portion; a support member (24,204) connected to the combine, the support member having an upper portion; and a pliable resilient member (26,206) having a first end connected to the support member (24,204) and a second end connected to the lower portion of the moveable member (22,202), the pliable resilient member (26,206) being configured to allow movement of the moveable member (22,202) relative to the support member (24,204) in six degrees of freedom and to support the moveable member in a spaced apart relation to the support member, characterized in that: the first end of the pliable resilient member (26,206) is connected to the upper portion of the support member (24,204) and the support member (24,204) is pivotably connected to the combine to support the moveable member (22,202) in at least a first position and a second position. the first end of the pliable resilient member (26,206) is connected to the upper portion of the support member (24,204) and the support member (24,204) is pivotably connected to the combine to support the moveable member (22,202) in at least a first position and a second position.
A catalyst for hydrosilylation, said catalyst comprising a complex having the following formula: wherein each R is an independently selected hydrocarbyl group, each R 1 is an independently selected aryl group, and X is a halogen atom.
A catheter pump comprising a pump head for introducing into the arterial vasculature, an outer catheter, an inner catheter arranged in said outer catheter, and a rotor shaft rotatably arranged in said inner catheter for driving an expandable conveying element provided at said pump head, wherein said conveying element is rotatably mounted between a distal bearing point and a proximal bearing point, wherein said outer catheter has a sleeve portion surrounding said proximal bearing point on the distal end thereof, and wherein said proximal bearing point is movable in the axial direction relative to said sleeve portion in order to expand said conveying element, characterized in that said proximal bearing point comprises a bearing receptacle having a rotational bearing point for a rotary head connected to the distal end of said rotor shaft in a rotationally fixed manner and a force application point axially spaced therefrom for a force application portion provided at the distal end of said inner catheter for axially moving said proximal bearing points relative to said sleeve portion.
An occlusal stent delivery catheter for delivering an implant through a viewing scope into a lung passageway, said catheter comprising: an elongate tubular shaft having a proximal end and a distal end, wherein the distal end is extendable beyond the distal end of the viewing scope and is configured to releasably hold the implant therein; a handle; a positioning rod disposed within the elongate tubular shaft and fixedly attached to the handle; wherein the outer surface of the distal end comprises a plurality of markings which are visible from the viewing scope when the delivery catheter is extended therefrom to assist in positioning the distal end of the catheter in the lung passageway, and wherein the markings are located on the distal end such that the elongate shaft can be manipulated to align at least one marking with an anatomical feature to align the implant prior to being released. an elongate tubular shaft having a proximal end and a distal end, wherein the distal end is extendable beyond the distal end of the viewing scope and is configured to releasably hold the implant therein; a handle; a positioning rod disposed within the elongate tubular shaft and fixedly attached to the handle; wherein the outer surface of the distal end comprises a plurality of markings which are visible from the viewing scope when the delivery catheter is extended therefrom to assist in positioning the distal end of the catheter in the lung passageway, and wherein the markings are located on the distal end such that the elongate shaft can be manipulated to align at least one marking with an anatomical feature to align the implant prior to being released.