mhurhangee/ep-ind-claims huggingface dataset:
Spindle-head system, comprising a spindle head and a spindle-head-adjusting device, wherein the spindle head has a spindle-head housing, extending along a spindle-head axis of rotation, and has a cross slide, mounted so as to be perpendicularly adjustable in relation to the spindle-head axis of rotation from the spindle-head housing, and the spindle-head-adjusting device is configured for cross-slide adjustment of the cross slide, wherein the spindle-head-adjusting device has a spindle-head frame for being placed onto the spindle head, has a first adjustment element (12, 13) and a second adjustment element (12, 13), which is arranged opposite the first adjustment element (12, 13), wherein the first adjustment element (12, 13) and the second adjustment element (12, 13) are each mounted on the spindle-head frame so as to be extendable into a frame inner region of the spindle-head frame and retractable out of the frame inner region, wherein the spindle-head frame is configured to be placeable onto a housing outer side of the spindle-head housing in a reversibly releasable manner, characterized in that the cross slide has a first indentation (4c, 4d) for lateral guidance of the first adjustment element (12, 13), the first indentation (4c, 4d) extends parallel to an adjustment direction, which is oriented perpendicularly to the spindle-head axis of rotation, of the cross slide, and the first adjustment element (12, 13) is mounted on the spindle-head frame so as to be extendable into the first indentation (4c, 4d).
A method of providing an annular rotor for a flywheel comprising: winding a tow comprising a matrix of fibres about an axis, the tow being arranged in layers comprising a gap between adjacent tow windings, characterised in that the winding angle between a normal to the axis and the tow is less than 3.5°; and magnetic particles are provided within the matrix of a size less than the critical flaw size of the tow, wherein the critical flaw size is calculated based on a maximum amount of stress that the annular rotor is to be exposed to during operation of the flywheel, wherein the critical flaw size is determined according to Griffith's crack theory. winding a tow comprising a matrix of fibres about an axis, the tow being arranged in layers comprising a gap between adjacent tow windings, characterised in that the winding angle between a normal to the axis and the tow is less than 3.5°; and magnetic particles are provided within the matrix of a size less than the critical flaw size of the tow, wherein the critical flaw size is calculated based on a maximum amount of stress that the annular rotor is to be exposed to during operation of the flywheel, wherein the critical flaw size is determined according to Griffith's crack theory.
A mounting device for a sanitary item for mounting on a rod (9, 29) protruding from a wall, wherein the mounting device comprises the following: a positive locking element (12, 13, 30, 40) for creating a positive locking arrangement which fixes the sanitary item in place by installing the positive locking element (12, 13, 30, 40) on the rod (9, 29, 39); a wedge-shaped clamping mechanism for clamping the sanitary item against the positive locking arrangement and therefore for pressing the sanitary item on to the wall; characterised in that the positive locking element (12, 13, 30, 40) is attached to the mounting device and the positive locking arrangement can be created by sliding on and then lowering the mounting device and therefore the positive locking element (12, 13, 30, 40) on to the rod (9, 29) and by an engagement between a ribbed surface of the positive locking element (12, 13, 30, 40) and a male thread provided on the rod (9, 29, 39). a positive locking element (12, 13, 30, 40) for creating a positive locking arrangement which fixes the sanitary item in place by installing the positive locking element (12, 13, 30, 40) on the rod (9, 29, 39); a wedge-shaped clamping mechanism for clamping the sanitary item against the positive locking arrangement and therefore for pressing the sanitary item on to the wall; characterised in that the positive locking element (12, 13, 30, 40) is attached to the mounting device and the positive locking arrangement can be created by sliding on and then lowering the mounting device and therefore the positive locking element (12, 13, 30, 40) on to the rod (9, 29) and by an engagement between a ribbed surface of the positive locking element (12, 13, 30, 40) and a male thread provided on the rod (9, 29, 39).
A mixing apparatus for a high viscosity material comprising: a first supply unit for supplying a first raw material to a first channel; a second supply unit for supplying a second raw material to a second channel; a mixing pipe with which the first channel and the second channel merge and through which the first raw material and the second raw material pass; a static mixer and a dynamic mixer provided in the mixing pipe for mixing the first raw material and the second raw material; a discharge pipe through which a mixed material obtained through the static mixer and the dynamic mixer is discharged; and an in-system decompressor for setting the inside of the static mixer and the dynamic mixer in a decompressed atmosphere, wherein in the mixing apparatus, the in-system decompressor is connected through a decompression pipe with the discharge pipe to set the insides of the static mixer and the dynamic mixer in the decompressed atmosphere before the first raw material and the second raw material are led to the static mixer and the dynamic mixer and mixing work for the first and second raw materials (MI,HA) is started. a first supply unit for supplying a first raw material to a first channel; a second supply unit for supplying a second raw material to a second channel; a mixing pipe with which the first channel and the second channel merge and through which the first raw material and the second raw material pass; a static mixer and a dynamic mixer provided in the mixing pipe for mixing the first raw material and the second raw material; a discharge pipe through which a mixed material obtained through the static mixer and the dynamic mixer is discharged; and an in-system decompressor for setting the inside of the static mixer and the dynamic mixer in a decompressed atmosphere, wherein in the mixing apparatus, the in-system decompressor is connected through a decompression pipe with the discharge pipe to set the insides of the static mixer and the dynamic mixer in the decompressed atmosphere before the first raw material and the second raw material are led to the static mixer and the dynamic mixer and mixing work for the first and second raw materials (MI,HA) is started.
A computer implemented method for detecting vehicle collisions, the method comprising: receiving, by one or more computing devices, acceleration data of a vehicle over a period of time; receiving, by the one or more computing devices, expected acceleration data of the vehicle over the period of time; determining, by the one or more computing devices, a change in the vehicle's acceleration over the period of time, where the change in the vehicle's acceleration over the period of time is a difference between the expected acceleration data and the acceleration data; detecting an occurrence, by the one or more computing devices, when the change in the vehicle's acceleration is greater than a threshold value; assigning, by the one or more computing devices, the occurrence into a collision category; and performing, by the one or more computing devices, a responsive action based on the assigned collision category. receiving, by one or more computing devices, acceleration data of a vehicle over a period of time; receiving, by the one or more computing devices, expected acceleration data of the vehicle over the period of time; determining, by the one or more computing devices, a change in the vehicle's acceleration over the period of time, where the change in the vehicle's acceleration over the period of time is a difference between the expected acceleration data and the acceleration data; detecting an occurrence, by the one or more computing devices, when the change in the vehicle's acceleration is greater than a threshold value; assigning, by the one or more computing devices, the occurrence into a collision category; and performing, by the one or more computing devices, a responsive action based on the assigned collision category.
A method of controlling an idling wind turbine comprising at least a hub configured to rotate relative to a nacelle and at least one rotor blade coupled to the hub by means of at least one pitching system, wherein said method comprising at least the steps of: - collecting wind condition data from at least one wind sensor (101, 102) which measures the wind condition data in the vicinity and preferably up-wind of the wind turbine; - collecting wind turbine position data from a sensor system; - processing said wind condition data and wind turbine position data in a control system comprising at least one computer by executing a control algorithm to compute an optimal pitch angle value for each of the rotor blade s in which the forces from aerodynamic lift and drag on that rotor blade are reduced to a minimum; - pitching said rotor blades by means of said pitch system to the computed optimal pitch angle value characterised in that - the rotor blades are continuously pitched in the same direction in any multiple of 360 degrees for continuously adjusting to the wind direction, and - wherein the rotor blades are pitched past 360 degrees from a first pitch angle to the computed optimal pitch angle. - collecting wind condition data from at least one wind sensor (101, 102) which measures the wind condition data in the vicinity and preferably up-wind of the wind turbine; - collecting wind turbine position data from a sensor system; - processing said wind condition data and wind turbine position data in a control system comprising at least one computer by executing a control algorithm to compute an optimal pitch angle value for each of the rotor blade s in which the forces from aerodynamic lift and drag on that rotor blade are reduced to a minimum; - pitching said rotor blades by means of said pitch system to the computed optimal pitch angle value - the rotor blades are continuously pitched in the same direction in any multiple of 360 degrees for continuously adjusting to the wind direction, and - wherein the rotor blades are pitched past 360 degrees from a first pitch angle to the computed optimal pitch angle.
Method for producing a film comprising a non-magnetic matrix and a plurality of three-dimensional magnetic microstructures organised within said matrix in a predetermined pattern, comprising the steps of: - providing a substrate, called the master substrate, comprising a face, called the magnetically structured face, composed of a plurality of magnetic field micro-sources (10a, 10b), having a magnetic field gradient of between 10 2 and 10 6 T/m, - providing magnetic micro- or nano-particles on the magnetically structured face of said master substrate, said particles agglomerating into organised three-dimensional microstructures under the effect of the attractive magnetophoretic force exerted by the magnetic field gradient at the surface of the master substrate, - depositing a matrix of a non-magnetic material on the magnetically structured face of the master substrate and on the organised three-dimensional microstructures, so as to enclose said organised microstructures and form said film, - delaminating said film from the master substrate. - providing a substrate, called the master substrate, comprising a face, called the magnetically structured face, composed of a plurality of magnetic field micro-sources (10a, 10b), having a magnetic field gradient of between 10 2 and 10 6 T/m, - providing magnetic micro- or nano-particles on the magnetically structured face of said master substrate, said particles agglomerating into organised three-dimensional microstructures under the effect of the attractive magnetophoretic force exerted by the magnetic field gradient at the surface of the master substrate, - depositing a matrix of a non-magnetic material on the magnetically structured face of the master substrate and on the organised three-dimensional microstructures, so as to enclose said organised microstructures and form said film, - delaminating said film from the master substrate.
A system comprising: a training reinforcement assistance device having a frame supporting an optical system, wherein the optical system is configured to display virtual content on a display, and to enable viewing of at least a portion of a surrounding environment; an imager operably coupled with the frame and configured to produce an image of an environment of the imager; an accelerometer operably coupled with the frame and configured to detect an orientation of the frame; an eye-tracking system operably coupled with the frame and configured to detect a viewing direction of an operator; and a controller operably coupled with the imager and the display, wherein the controller is configured to receive environmental information from at least one of the imager, the accelerometer, or the eye-tracking system, and to overlay the image of the environment to assist an operator in maneuvering a material handling vehicle based on vehicle kinematics of the material handling vehicle within a line of sight of the operator through the optical system, and the image is positioned on at least one fork of the material handling vehicle as perceived through the optical system, preferably the system comprises the material handling vehicle. a training reinforcement assistance device having a frame supporting an optical system, wherein the optical system is configured to display virtual content on a display, and to enable viewing of at least a portion of a surrounding environment; an imager operably coupled with the frame and configured to produce an image of an environment of the imager; an accelerometer operably coupled with the frame and configured to detect an orientation of the frame; an eye-tracking system operably coupled with the frame and configured to detect a viewing direction of an operator; and a controller operably coupled with the imager and the display, wherein the controller is configured to receive environmental information from at least one of the imager, the accelerometer, or the eye-tracking system, and to overlay the image of the environment to assist an operator in maneuvering a material handling vehicle based on vehicle kinematics of the material handling vehicle within a line of sight of the operator through the optical system, and the image is positioned on at least one fork of the material handling vehicle as perceived through the optical system,
An apparatus comprising: at least one transceiver (130; 131; 132) configured to simultaneously maintain a plurality of simultaneous Media-Access-Control, MAC, layer connections with a plurality of location origin beacon transceivers, LOBTs (104; 106; 108), the plurality of LOBTs (104; 106; 108) each configured to communicate location information, the location information representing a location of said LOBT, with said apparatus, and said at least one transceiver (130; 131; 132) configured to communicate wireless communication signals, said wireless communication signals including said location information, with said plurality of LOBTs (104; 106; 108) via said plurality of simultaneous MAC-layer connections; wherein said transceiver (130; 131; 132) is further configured to transmit to a server a simultaneous connectivity request identifying said plurality of LOBTs (104; 106; 108), to receive from said server a connectivity request acknowledgement acknowledging establishment of said plurality of MAC-layer connections with said plurality of LOBTs (104; 106; 108), and to communicate with said plurality of LOBTs (104; 106; 108) via said plurality of simultaneous MAC-layer connections. at least one transceiver (130; 131; 132) configured to simultaneously maintain a plurality of simultaneous Media-Access-Control, MAC, layer connections with a plurality of location origin beacon transceivers, LOBTs (104; 106; 108), the plurality of LOBTs (104; 106; 108) each configured to communicate location information, the location information representing a location of said LOBT, with said apparatus, and said at least one transceiver (130; 131; 132) configured to communicate wireless communication signals, said wireless communication signals including said location information, with said plurality of LOBTs (104; 106; 108) via said plurality of simultaneous MAC-layer connections; wherein said transceiver (130; 131; 132) is further configured to transmit to a server a simultaneous connectivity request identifying said plurality of LOBTs (104; 106; 108), to receive from said server a connectivity request acknowledgement acknowledging establishment of said plurality of MAC-layer connections with said plurality of LOBTs (104; 106; 108), and to communicate with said plurality of LOBTs (104; 106; 108) via said plurality of simultaneous MAC-layer connections.
Tobacco dosing system for providing doses of tobacco, wherein the dosing system comprises; - a tobacco supply constructed and arranged to supply tobacco, - a dosing device comprising at least one dosing cup (11, 12) for receiving the tobacco to be dosed, - a gas flow device constructed and arranged to in use provide a gas flow through the tobacco received by the at least one dosing cup (11, 12), and characterised in that the tobacco dosing system further comprises; - a gas flow measuring device constructed and arranged to measure a property of the gas flow, and - a controlling device operably connected to the dosing device and the gas flow measuring device to control the operation of the tobacco dosing system on basis of the measured property. - a tobacco supply constructed and arranged to supply tobacco, - a dosing device comprising at least one dosing cup (11, 12) for receiving the tobacco to be dosed, - a gas flow device constructed and arranged to in use provide a gas flow through the tobacco received by the at least one dosing cup (11, 12), and characterised in that the tobacco dosing system further comprises; - a gas flow measuring device constructed and arranged to measure a property of the gas flow, and - a controlling device operably connected to the dosing device and the gas flow measuring device to control the operation of the tobacco dosing system on basis of the measured property.
Inflatable transport box having a bottom, a rear wall, a right side wall and a left side wall, the bottom, rear wall and the side walls (2a, 2b) consisting of a dropstitch material, wherein the rear wall is connected to the bottom at one fold edge and forms an integral dropstitch component with the bottom, the left side wall and the right side wall are connected to the rear wall at fold edges on both sides and the side walls (2a, 2b) are dropstitch components, wherein, by folding an inner dropstitch wall, partial areas arranged on both sides of the fold come to rest on one another, and wherein bond areas (9, 10) of the surface of the dropstitch material are glued or welded to one another in the fold edges.
Chemical compounds for use as an agent for regeneration of a neurological injury and/or treatment of neurological injury such as: H 2 N-RGD-amide (referred to as RGD1), H 2 N-RGDRGD-amide (referred to as RGD2), H 2 N-RGDRGDRGD-amide (referred to as RGD3), acetyl-RGDRGDRGD-amide (referred to as Ac-RGD3) H 2 N-RGDRGDRGDRGD-amide (referred to as RGD4)
An aircraft comprising a winglet system and a wing, the winglet system comprising: an upper winglet and a lower winglet mounted to the wing; the lower winglet having a static position when the wing is subject to a ground static loading; and the lower winglet being configured such that upward deflection of the wing under 1-g flight loading causes the lower winglet to move from the static position to an in-flight position and resulting in an absolute span increase of the wing. an upper winglet and a lower winglet mounted to the wing; the lower winglet having a static position when the wing is subject to a ground static loading; and the lower winglet being configured such that upward deflection of the wing under 1-g flight loading causes the lower winglet to move from the static position to an in-flight position and resulting in an absolute span increase of the wing.
A battery controlling apparatus for a vehicle for carrying out constant current control for charging a battery incorporated in a vehicle to a predetermined voltage with fixed current and thereafter carrying out constant voltage control for charging the battery while maintaining the predetermined voltage and reducing the current, comprising: an SOC calculation section adapted to detect a charging rate of the battery upon starting of the constant current control; an elapsed time measurement section, adapted to measure elapsed time from starting time of the constant current control; a timeout setting section adapted to set a timeout period of the constant current control based on the charging rate detected by said SOC calculation section; and a current cutoff section adapted to cut off the current to be supplied to the battery when the elapsed time measured by said elapsed time measurement section upon the constant current control exceeds the timeout period set by said timeout setting section, characterized in that said timeout setting section calculates a period by subtracting offset time set based on a current value in the constant current control from maximum charging time set based on the charging rate, and sets the period as the timeout period. an SOC calculation section adapted to detect a charging rate of the battery upon starting of the constant current control; an elapsed time measurement section, adapted to measure elapsed time from starting time of the constant current control; a timeout setting section adapted to set a timeout period of the constant current control based on the charging rate detected by said SOC calculation section; and a current cutoff section adapted to cut off the current to be supplied to the battery when the elapsed time measured by said elapsed time measurement section upon the constant current control exceeds the timeout period set by said timeout setting section, characterized in that said timeout setting section calculates a period by subtracting offset time set based on a current value in the constant current control from maximum charging time set based on the charging rate, and sets the period as the timeout period.
Downstream pressure compensator, consisting of at least one valve housing having at least three fluid connection points in the form of a work port, a return port and a control port, in which valve housing, counter to the action of an energy accumulator, a valve piston, guided so as to be longitudinally movable, starting from a respective opening or control position, is moved towards a valve seat into a closing position in which the work port and return port are separated from each other, wherein, by means of a pressure equalisation device, the fluid pressure present at the work port is guided in such a manner to a pressure-active area (A 1 *) of the valve piston that the latter reaches its respective opening or control position in a pressure-equalised manner due to the force of the energy accumulator, wherein the pressure equalisation device comprises a pressure equalisation channel, characterised in that the pressure equalisation channel, guided in the valve piston, opens with its one free end towards the work port in the valve housing and with its other free end into an annular groove in the valve piston, and in that the pressure equalisation channel is guided in the form of at least one centrally or eccentrically arranged longitudinal bore in the valve piston and in the form of at least one transverse bore between this longitudinal bore and the annular groove, and in that a non-return valve opening towards the annular groove is arranged in the respective transverse bore.