mhurhangee/patent-ind-claim-en huggingface dataset:
A control device allocated to a charging station (CS) for charging a vehicle (EV), wherein the control device (CTR) comprises: - an interface (IFC) to the vehicle (EV), configured to receive a vehicle-side proof of authorization (JCRED1); - a near-field communication interface (IFM), configured for exchanging a terminal-side proof of authorization (JCRED2) with a mobile terminal device (MD); - an allocation unit (AS) for establishing a control link with the mobile terminal device (MD) via the near-field communication interface (IFM) after receiving the vehicle-side or the terminal-side proof of authorization (JCRED1; JCRED2) and for allocating the charging station (CS) to the vehicle (EV) after receipt and positive verification of both proofs of authorization (JCRED1;JCRED2) . - an interface (IFC) to the vehicle (EV), configured to receive a vehicle-side proof of authorization (JCRED1); - a near-field communication interface (IFM), configured for exchanging a terminal-side proof of authorization (JCRED2) with a mobile terminal device (MD); - an allocation unit (AS) for establishing a control link with the mobile terminal device (MD) via the near-field communication interface (IFM) after receiving the vehicle-side or the terminal-side proof of authorization (JCRED1; JCRED2) and for allocating the charging station (CS) to the vehicle (EV) after receipt and positive verification of both proofs of authorization (JCRED1;JCRED2) .
Method for controlling a technical system as plant with a Two Degree of Freedom controller having a feedforward controller providing an output (u FF ) and a feedback controller providing an output (u FB ) whereas the plant is modelled with a model with a chosen model structure having system parameters (K, τ) and the feedforward controller uses an inverse of the model of the plant and the Two Degree of Freedom controller is designed to calculate a control variable (u) of the plant from the output (u FF ) of the feedforward controller and the output (u FB ) of the feedback controller to achieve a setpoint value (y set ) of an output variable (y) of the plant in dependence from a state variable (x) of the plant , characterized in that the inverse of the model of the plant is constituted by a nonlinear dynamic part and a nonlinear static part, that a static map of the plant is provided that maps the control variable (u) and the state variable (x) onto the output variable (y) and the nonlinear static part is formed as inverted map of this static map , whereas the inverted map outputs the control variable (u) for a given state variable (x) and output variable (y), that a desired closed loop behaviour of the plant with a desired output variable (y des ) is chosen and the nonlinear dynamic part is formed as function of the system parameters (K, τ) of the model and of the desired output variable (y des ) of the desired closed loop behaviour of the plant and that the dynamic output (y dyn ) of the nonlinear dynamic part and the state variable (x) are fed into the inverted map of the nonlinear static part that outputs the output (u FF ) of the feedforward controller .
An aluminum alloy plate made of cast rolled material, wherein cast rolling comprises casting an ingot by DC casting, whereby during the DC casting molten metal inside of a casting mold is stirred, and then carrying out a homogenization process, a hot rolling process, and a cool rolling process to obtain a plate from the ingot, on which an anodically-oxidized coating is to be formed at least on a cross-sectional surface of the plate, which is a cross-sectional portion in a plate thickness direction, the plate comprising peritectic elements that show peritectic reaction with respect to aluminum, said peritectic elements comprising Ti and Cr, wherein the plate comprises 0.001%-0.1% of Ti, the percentage being by mass, and the same applies for percentages stated hereinafter, and 0.0001%-0.4% of Cr, the plate comprising 1.0%-6.0% of Mg that shows eutectic reaction with respect to aluminum, the plate further comprising one, two, or more kinds of elements selected from: Cu, in an amount of from more than 0% to equal to or less than 0.5%, Mn, in an amount of from more than 0% to equal to or less than 0.5%, Fe, in an amount of from more than 0% to equal to or less than 0.4%, and Si, in an amount of from more than 0% to equal to or less than 0.3%, in addition to the peritectic elements and Mg, and wherein the remainder of the aluminum alloy plate is made of Al and inevitable impurities; wherein the plate thickness is represented as t, as measured in mm, a range within ±0.01×t, as measured in mm from t/2 is represented as a central portion, a range within ±0.01×t, as measured in mm from t/4 is represented as a quarter portion, and a range within 0.02×t, as measured in mm from a top surface in the plate thickness direction is represented as a superficial portion, wherein the concentration of the peritectic elements in solid solution state in the plate thickness direction of the aluminum alloy plate is such that a concentration difference between in the central portion and in the quarter portion, and a concentration difference between in the central portion and in the superficial portion, are 0.04% or less, and wherein the concentration of Mg in solid solution state in the plate thickness direction of the aluminum alloy plate is such that a concentration difference between in the central portion and in the quarter portion, and a concentration difference between in the central portion and in the superficial portion, are 0.4% or less.
A mold for thermally bending automotive glass, comprising a fixed frame and two movable frames , the two movable frames are respectively hinged to the left and the right ends of the fixed frame , the two movable frames can be rotated about the respective hinged connection points, so as to form a bending surface with the fixed frame , and the bending surface has a curvature equal to the curvature of the resultant shape of the thermally bent automotive glass, wherein a curvature adjusting device is correspondingly additionally provided at the bottom of each movable frame , each curvature adjusting device comprises two sidings , two hooks and an adjusting lever , the adjusting lever is hinged to the bottom surface of the movable frame on the same side, the adjusting lever is in parallel to the connection line of the two hinged connection points of the movable frame on the same side and the fixed frame , the bottom ends of the two hooks are respectively fixed to the two ends of the adjusting lever , and the top ends of the two hooks are respectively hung on the two corresponding sidings at adjustable positions.
Cleaning and disinfection device for medical and/or dental instruments, comprising a filter device for filtering rinsing liquid, wherein the filter device comprises a filter element having a raw side and a clean side , an inlet for selectively supplying rinsing liquid or drying air into the filter device , a first outlet , and a second outlet , wherein the inlet and the second outlet are in flow communication with the raw side of the filter element and wherein the first outlet is in flow communication with the clean side of the filter element , wherein the first outlet is is in flow communication with a device for flushing out inner lumens of medical and/or dental instruments, wherein the second outlet can be brought into flow communication with a device for cleaning outer sides of medical and/or dental instruments and wherein a valve device is arranged in a flow path leading through the second outlet , which valve device can prevent or allow a flow of rinsing liquid through the second outlet .
A print apparatus comprising: conveying means configured to convey a sheet in a first direction; a first print head having a plurality of ejection orifices for ejecting ink, wherein the ejection orifices are arranged in a second direction intersecting the first direction; a second print head provided adjacently to the first print head downstream of the first print head in the first direction and having a plurality of ejection orifices for ejecting ink, wherein the ejection orifices are arranged in the second direction; humidifying means configured to generate a humidified gas, characterized by a supply port provided on one side in the second direction with respect to a space formed between the first print head and the second print head and configured to supply the humidified gas generated by the humidifying means to the space, and a discharge port provided on the other side in the second direction with respect to the space and configured to discharge the humidified gas supplied from the supply port. conveying means configured to convey a sheet in a first direction; a first print head having a plurality of ejection orifices for ejecting ink, wherein the ejection orifices are arranged in a second direction intersecting the first direction; a second print head provided adjacently to the first print head downstream of the first print head in the first direction and having a plurality of ejection orifices for ejecting ink, wherein the ejection orifices are arranged in the second direction; humidifying means configured to generate a humidified gas, characterized by a supply port provided on one side in the second direction with respect to a space formed between the first print head and the second print head and configured to supply the humidified gas generated by the humidifying means to the space, and a discharge port provided on the other side in the second direction with respect to the space and configured to discharge the humidified gas supplied from the supply port.
A method for calibrating a magnetic resonance imaging (MRI) phantom which deviates from an expected geometry due to geometric inaccuracies caused by manufacturing imprecision, the phantom comprising at least one MRI detectable part with a position within the expected geometry which is known with a geometric inaccuracy, wherein the method comprises the following steps: - step 1: placing the phantom at a predetermined location in a magnetic resonance imaging system such that the MRI detectable part is within a symmetry plane , i.e. along one of the x=0, y=0 or z=0 planes of a gradient coil system of the magnetic resonance imaging system and; - step 2: acquiring an MRI image of the MRI detectable part of the phantom by means of a first sequence, wherein the MRI image comprises multiple slices, wherein each of the slices is oriented along the symmetry plane; - step 3: causing a computer to determine the geometric inaccuracy, i.e. the deviation from the expected geometry of the MRI detectable part of the MRI phantom based on the position and the representation of the part in the MRI image using the assumption that a gradient field generated by the gradient coil system has zero x-distortion in an x=0 plane, zero y-distortion in a y=0 plane and zero z-distortion in a z=0 plane such that, if the part deviates from the symmetry plane in the MRI image, this deviation is caused by said mechanical inaccuracy, and not caused by the first sequence used. - step 1: placing the phantom at a predetermined location in a magnetic resonance imaging system such that the MRI detectable part is within a symmetry plane , i.e. along one of the x=0, y=0 or z=0 planes of a gradient coil system of the magnetic resonance imaging system and; - step 2: acquiring an MRI image of the MRI detectable part of the phantom by means of a first sequence, wherein the MRI image comprises multiple slices, wherein each of the slices is oriented along the symmetry plane; - step 3: causing a computer to determine the geometric inaccuracy, i.e. the deviation from the expected geometry of the MRI detectable part of the MRI phantom based on the position and the representation of the part in the MRI image using the assumption that a gradient field generated by the gradient coil system has zero x-distortion in an x=0 plane, zero y-distortion in a y=0 plane and zero z-distortion in a z=0 plane such that, if the part deviates from the symmetry plane in the MRI image, this deviation is caused by said mechanical inaccuracy, and not caused by the first sequence used.
A terminal plate member on which a terminal of a coil component is adapted to be mounted, the terminal plate member comprising: an annular frame having an inner peripheral edge; a pair of extension members extending from the inner peripheral edge of the annular frame toward an inner space of the annular frame member in a first direction; characterized in that a throughhole section is provided in the annular frame at proximal end of at least one of the pair of extension members to form a deformable section of the annular frame, wherein the throughhole section is provided along a second direction with a length bigger than the width of the one of the pair of extension members in such a manner as to form a deformable section of the annular frame, and the second direction is perpendicular to the first direction. an annular frame having an inner peripheral edge; a pair of extension members extending from the inner peripheral edge of the annular frame toward an inner space of the annular frame member in a first direction; characterized in that a throughhole section is provided in the annular frame at proximal end of at least one of the pair of extension members to form a deformable section of the annular frame, wherein the throughhole section is provided along a second direction with a length bigger than the width of the one of the pair of extension members in such a manner as to form a deformable section of the annular frame, and the second direction is perpendicular to the first direction.
A photographing parameter adjustment method, applied to a mobile terminal, wherein the mobile terminal comprises a camera module and a foldable display, and the method comprises: receiving a touch operation performed on the foldable display; in a process of receiving the touch operation, receiving a folding operation performed on the foldable display; wherein the method is characterized by further comprising: determining a shortest distance between the touch position of the touch operation and a first side of the foldable display; determining an adjustment step size corresponding to the shortest distance as an adjustment step size of a photographing parameter; determining a weight coefficient of the adjustment step size based on a change value of the folding angle of the foldable display; and adjusting the photographing parameter of the camera module based on the adjustment step size and the weight coefficient. receiving a touch operation performed on the foldable display; in a process of receiving the touch operation, receiving a folding operation performed on the foldable display; wherein the method is characterized by further comprising: determining a shortest distance between the touch position of the touch operation and a first side of the foldable display; determining an adjustment step size corresponding to the shortest distance as an adjustment step size of a photographing parameter; determining a weight coefficient of the adjustment step size based on a change value of the folding angle of the foldable display; and adjusting the photographing parameter of the camera module based on the adjustment step size and the weight coefficient. determining a shortest distance between the touch position of the touch operation and a first side of the foldable display; determining an adjustment step size corresponding to the shortest distance as an adjustment step size of a photographing parameter; determining a weight coefficient of the adjustment step size based on a change value of the folding angle of the foldable display; and adjusting the photographing parameter of the camera module based on the adjustment step size and the weight coefficient.
A method for holding a panel for a fuselage assembly , the method comprising: providing a cradle fixture comprising a base and an adjustable retaining structure having a curved shape ; and engaging the adjustable retaining structure with the panel by: moving the adjustable retaining structure relative to the base towards the panel such that the adjustable retaining structure impinges on the panel ; and wherein moving the adjustable retaining structure towards the panel comprises using at least one scissor lift mechanism . providing a cradle fixture comprising a base and an adjustable retaining structure having a curved shape ; and engaging the adjustable retaining structure with the panel by: moving the adjustable retaining structure relative to the base towards the panel such that the adjustable retaining structure impinges on the panel ; and wherein moving the adjustable retaining structure towards the panel comprises using at least one scissor lift mechanism . moving the adjustable retaining structure relative to the base towards the panel such that the adjustable retaining structure impinges on the panel ; and wherein moving the adjustable retaining structure towards the panel comprises using at least one scissor lift mechanism .
Tyre for vehicles which are intended to bear heavy loads, the tread of which comprises a composition based on at least: - an elastomer matrix comprising: ∘ a thermoplastic styrene elastomer which represents from 10 to 45% by weight of the elastomer matrix, which thermoplastic styrene elastomer comprises at least one rigid styrene segment and at least one flexible diene segment, which at least one flexible diene segment comprises at least 20% by weight of conjugated diene units, it being possible for the conjugated diene units to be all or in part hydrogenated, ∘ a diene elastomer selected from the group consisting of polybutadienes, butadiene copolymers and mixtures thereof, which represents more than 50% of the difference between the weight of the elastomer matrix and the weight of the thermoplastic styrene elastomer, - a reinforcing filler comprising ∘ silica, between 50% and 99% by weight of the reinforcing filler, ∘ carbon black, between 1% and 50% by weight of the reinforcing filler, ∘ the content of reinforcing filler varying within a range extending from 20 to 60 phr, - a coupling agent, - a crosslinking system. - an elastomer matrix comprising: ∘ a thermoplastic styrene elastomer which represents from 10 to 45% by weight of the elastomer matrix, which thermoplastic styrene elastomer comprises at least one rigid styrene segment and at least one flexible diene segment, which at least one flexible diene segment comprises at least 20% by weight of conjugated diene units, it being possible for the conjugated diene units to be all or in part hydrogenated, ∘ a diene elastomer selected from the group consisting of polybutadienes, butadiene copolymers and mixtures thereof, which represents more than 50% of the difference between the weight of the elastomer matrix and the weight of the thermoplastic styrene elastomer, ∘ a thermoplastic styrene elastomer which represents from 10 to 45% by weight of the elastomer matrix, which thermoplastic styrene elastomer comprises at least one rigid styrene segment and at least one flexible diene segment, which at least one flexible diene segment comprises at least 20% by weight of conjugated diene units, it being possible for the conjugated diene units to be all or in part hydrogenated, ∘ a diene elastomer selected from the group consisting of polybutadienes, butadiene copolymers and mixtures thereof, which represents more than 50% of the difference between the weight of the elastomer matrix and the weight of the thermoplastic styrene elastomer, - a reinforcing filler comprising ∘ silica, between 50% and 99% by weight of the reinforcing filler, ∘ carbon black, between 1% and 50% by weight of the reinforcing filler, ∘ the content of reinforcing filler varying within a range extending from 20 to 60 phr, ∘ silica, between 50% and 99% by weight of the reinforcing filler, ∘ carbon black, between 1% and 50% by weight of the reinforcing filler, ∘ the content of reinforcing filler varying within a range extending from 20 to 60 phr, - a coupling agent, - a crosslinking system.
A tubular cracking furnace, for example an ethylene cracking furnace, comprising a convection section and a radiant section or dual radiant sections, at least one pass radiant tube of metal arranged in said radiant section having at least one member for intensifying heat transfer through the wall of the at least one radiant tube to fluid flowing through that tube in a fluid flow direction, by changing plug flow of the fluid in the at least one radiant tube to turbulence flow, said at least one member comprising a first such member, which is arranged at a location between 10D and 25D upstream, relative to the fluid flow direction, of an extreme point of said at least one pass radiant tube metal temperature, at which extreme point the tube metal temperature is a maximum, wherein D is the inner diameter of said at least one pass radiant tube.
A compound helicopter with a fuselage and at least one main rotor that is operably coupled to an associated main gear box and at least adapted for generating lift in operation, the fuselage comprising a lower region and an upper region that is opposed to the lower region , the at least one main rotor and the associated main gear box being arranged in the upper region , wherein at least one propeller is provided that is at least adapted for generating forward and/or backward thrust in operation, the at least one propeller being mounted to a fixed wing arrangement that is laterally attached to the fuselage , the fixed wing arrangement comprising at least one upper wing and at least one lower wing which are at least interconnected at an interconnection region and which are respectively connected to the fuselage , and wherein each propeller is mounted to an associated interconnection region , characterized in that an upper stub wing arrangement is provided in the upper region of the fuselage , wherein the upper stub wing arrangement comprises at least one upper stub wing , and wherein the at least one upper wing of the fixed wing arrangement is mounted to the upper stub wing of the upper stub wing arrangement .
A joining head for fastening a fastening element by means of a die to the surface (20.1) of a component with a gripper that can be linearly displaced in a first displacement direction R G and a magazine for containing a plurality of fastening elements that can be linearly displaced in a second displacement direction R M , wherein the first displacement direction R G runs transversely to the second displacement direction R M , characterized in that the gripper is designed as at least one die and the component can be fastenend by clinching.
A turbine wheel for a turbocharger comprising: a hub ; a plurality of blades extending from said hub ; and a backwall extending from said hub and having an outer diameter (D1), wherein said backwall includes a first backwall surface and an opposing second backwall surface ; characterized in that said first backwall surface includes a datum ring having a diameter in a range between 50% and 85% of said outer diameter (D1), and in that said turbine wheel is integrally cast. a hub ; a plurality of blades extending from said hub ; and a backwall extending from said hub and having an outer diameter (D1), wherein said backwall includes a first backwall surface and an opposing second backwall surface ; characterized in that said first backwall surface includes a datum ring having a diameter in a range between 50% and 85% of said outer diameter (D1), and in that said turbine wheel is integrally cast.