mhurhangee/patent-ind-claim-en huggingface dataset:
A three-dimensional printing apparatus that receives or generates three-dimensional data representing a shape of a three-dimensional object to be formed, and generates cross-sectional image data from the three-dimensional data so as to form the three-dimensional object in accordance with the generated cross-sectional image data, the cross-sectional image data representing cross sections obtained by dividing the three-dimensional object, which is to be formed, into a plurality of layers continuous in a predetermined direction, the apparatus comprising: a display configured or programmed to present images; a layer image data generator configured or programmed to add thickness information, which is a predetermined interval corresponding to a layer pitch at which the three-dimensional object is to be actually formed, to the cross-sectional image data of each of the layers, thus generating layer image data three-dimensionally representing each of the layers to be actually formed on a one-by-one basis; a layer image data output configured or programmed to output the layer image data generated by the layer image data generator ; and a display controller configured or programmed to cause the display to present a first image upon actual formation of a predetermined layer of the three-dimensional object in accordance with the cross-sectional image data of the predetermined layer, the first image being based on the layer image data of the predetermined layer to be actually formed on a one-by-one basis, which is output from the layer image data output. a display configured or programmed to present images; a layer image data generator configured or programmed to add thickness information, which is a predetermined interval corresponding to a layer pitch at which the three-dimensional object is to be actually formed, to the cross-sectional image data of each of the layers, thus generating layer image data three-dimensionally representing each of the layers to be actually formed on a one-by-one basis; a layer image data output configured or programmed to output the layer image data generated by the layer image data generator ; and a display controller configured or programmed to cause the display to present a first image upon actual formation of a predetermined layer of the three-dimensional object in accordance with the cross-sectional image data of the predetermined layer, the first image being based on the layer image data of the predetermined layer to be actually formed on a one-by-one basis, which is output from the layer image data output.
A method of manufacturing a glass core preform for an optical fibre comprising: - providing a porous soot core preform having an outer surface and a central hole extending axially therethrough; - dehydrating the porous soot core preform at a first temperature by exposing the outer surface of the preform to an atmosphere containing chlorine, and - simultaneously consolidating the soot core preform and closing the central hole at a second temperature higher than the first temperature to form a glass core preform, wherein simultaneously consolidating and closing comprises sequentially alternating flowing chlorine containing gas into the central hole and reducing the internal pressure of the central hole , characterised in that a single sequence of alternated flowing of chlorine containing gas and reduction of pressure defines a cycle and the alternated flowing of chlorine containing gas and reducing the internal pressure in the central hole is for a plurality of cycles during simultaneous consolidation and closing of the central hole . - providing a porous soot core preform having an outer surface and a central hole extending axially therethrough; - dehydrating the porous soot core preform at a first temperature by exposing the outer surface of the preform to an atmosphere containing chlorine, and - simultaneously consolidating the soot core preform and closing the central hole at a second temperature higher than the first temperature to form a glass core preform,
Heating device for producing carbon fibers from a threadlike fiber starting material , wherein the heating device has a heating source for a central tubular induction heating element , through which the fiber starting material is moved, the tubular induction heating element is surrounded by a thermal insulation , the heating source is an induction coil outside the thermal insulation , and the central induction heating element receives a flow of inert gas in particular for the carbonization and/or graphitization of the fiber starting material , characterized in that the heating source is formed by at least one medium to high frequency induction coil , and in that on the outside of the thermal insulation there are provided a first and a second tube element of material transparent to the induction field of the induction coil , which are separated from each other by an annular gap , through which the inert gas flows, the inert gas is guided in counterflow through the annular gap between the first and the second tube element and through the central tubular induction heating element , wherein at the two axially opposite ends of the central tubular induction heating element and the first and second tube element there is provided a cover element each time, wherein the one cover element is provided for the diverting of the inert gas from the annular gap between the first and the second tube element to the central tubular induction heating element and the other cover element for the introducing of the inert gas into the annular gap between the first and the second tube element and for bringing the inert gas out from the central tubular induction heating element .
An aircraft comprising: a left fixed wing; a right fixed wing; a fuselage coupled to the left and the right fixed wings; at least one tail coupled to the fuselage; a lifting propeller ; a connector or a gear or a link; and a motor that drives the lifting propeller using the connector or the gear or the link, wherein each of the at least one tail has a vertical stabilizer and the vertical stabilizer has a top distal end ; the lifting propeller is disposed on the top distal end of the vertical stabilizer ; the motor has a rotary axis, and the rotary axis is substantially parallel to a longitudinal axis of the aircraft , and the lifting propeller has a rotary axis at an angle between 75 degrees to 135 degrees relative to the rotary axis of the motor that drives the lifting propeller ; and wherein the motor is either disposed within the top distal end of the vertical stabilizer or the vertical stabilizer is fixed to a structure and the motor is disposed within the structure directly below the vertical stabilizer . a left fixed wing; a right fixed wing; a fuselage coupled to the left and the right fixed wings; at least one tail coupled to the fuselage; a lifting propeller ; a connector or a gear or a link; and a motor that drives the lifting propeller using the connector or the gear or the link, wherein each of the at least one tail has a vertical stabilizer and the vertical stabilizer has a top distal end ; the lifting propeller is disposed on the top distal end of the vertical stabilizer ; the motor has a rotary axis, and the rotary axis is substantially parallel to a longitudinal axis of the aircraft , and the lifting propeller has a rotary axis at an angle between 75 degrees to 135 degrees relative to the rotary axis of the motor that drives the lifting propeller ; and wherein the motor is either disposed within the top distal end of the vertical stabilizer or the vertical stabilizer is fixed to a structure and the motor is disposed within the structure directly below the vertical stabilizer .
A humanized anti-OX40 agonist antibody comprising a humanized heavy chain variable region (VH) and a humanized light chain variable region (VL), wherein the VL comprises the amino acid sequence SEQ ID NO: 29 and the VH comprises the amino acid sequence SEQ ID NO: 59, and wherein the antibody further comprises a human IgG1 constant region.
Motor system comprising: - an electrical machine with a plurality of sub-machines , each having a separate stator winding , which windings serve to drive a common rotor with a particular torque contribution; - a control branch for each of the stator windings , each control branch being designed to operate the particular sub-machine with phase voltages (Uu, Uv, Uw) in order to provide a desired torque contribution; - one or more cascaded controls in each of the control branches , which are designed to specify the phase voltages (Uu, Uv, Uw) for controlling the associated stator winding depending on a predetermined target value, the plurality of separate stator windings being galvanically separated from the other stator windings , characterized in that the control branches are electrically separated from one another and provide asynchronous control of the sub-machines, and in that at least one of the one or more controls is designed exclusively with a proportional component or without dynamic components, a position control being provided which is designed only with a proportional component. - an electrical machine with a plurality of sub-machines , each having a separate stator winding , which windings serve to drive a common rotor with a particular torque contribution; - a control branch for each of the stator windings , each control branch being designed to operate the particular sub-machine with phase voltages (Uu, Uv, Uw) in order to provide a desired torque contribution; - one or more cascaded controls in each of the control branches , which are designed to specify the phase voltages (Uu, Uv, Uw) for controlling the associated stator winding depending on a predetermined target value,
Motorcycle assembly with a fuel tank fastening assembly for a motorcycle, with a fuel tank , a retaining bracket , fastened to the fuel tank , and a battery carrier , the retaining bracket being fastened to the battery carrier , and with a motorcycle frame , characterized in that the battery carrier of the fuel tank fastening assembly is fastened to the motorcycle frame , with the result that the fuel tank is fastened via the battery carrier to the motorcycle frame , and the battery is accommodated and fastened in the battery carrier .
A digital flatbed cutter comprising: a flatbed on which a workpiece (W) can be positioned; a head unit movable laterally along an x-axis direction and a perpendicular y-axis direction in a parallel plane above the flatbed ; a tape applicator head mounted to the head unit and including an applicator roller adapted to apply a strip of double-sided adhesive tape to the workpiece (W), the applicator roller being rotatable about a z-axis that is normal to the plane and perpendicular to the x- and y-axes, and the applicator roller being movable along the z-axis; a cutter head mounted to the head unit and including a knife or blade adapted to cut the workpiece (W), the knife or blade being movable along the z-axis; a creaser head mounted to the head unit and including a creaser wheel adapted to crease the workpiece (W), the creaser wheel being movable along the z-axis; and a control unit adapted to control the movement of the head unit using a digital file with tape application information which specifies where each tape strip should be applied to the workpiece (W) by the applicator roller of the tape applicator head , and cutting and creasing information which specifies where the workpiece (W) should be cut by the knife or blade of the cutter head and creased by the creaser wheel of the creaser head . a flatbed on which a workpiece (W) can be positioned; a head unit movable laterally along an x-axis direction and a perpendicular y-axis direction in a parallel plane above the flatbed ; a tape applicator head mounted to the head unit and including an applicator roller adapted to apply a strip of double-sided adhesive tape to the workpiece (W), the applicator roller being rotatable about a z-axis that is normal to the plane and perpendicular to the x- and y-axes, and the applicator roller being movable along the z-axis; a cutter head mounted to the head unit and including a knife or blade adapted to cut the workpiece (W), the knife or blade being movable along the z-axis; a creaser head mounted to the head unit and including a creaser wheel adapted to crease the workpiece (W), the creaser wheel being movable along the z-axis; and a control unit adapted to control the movement of the head unit using a digital file with tape application information which specifies where each tape strip should be applied to the workpiece (W) by the applicator roller of the tape applicator head , and cutting and creasing information which specifies where the workpiece (W) should be cut by the knife or blade of the cutter head and creased by the creaser wheel of the creaser head .
Planar electrically floating qubit circuit structure comprising: a Josephson junction region including first and second weakly coupled superconductors; first and second electrode regions galvanically coupled to said first and second superconductors, respectively; and a ground electrode region ; characterised in that the series capacitance of said first and second electrode regions to said ground electrode region is greater than the self-capacitance of said Josephson junction region . a Josephson junction region including first and second weakly coupled superconductors; first and second electrode regions galvanically coupled to said first and second superconductors, respectively; and a ground electrode region ; characterised in that the series capacitance of said first and second electrode regions to said ground electrode region is greater than the self-capacitance of said Josephson junction region .
A ski boot, comprising a ski boot shell and a ski boot sole , wherein the ski boot sole comprises a front end of the ski boot sole, a rear end of the ski boot sole, a lower side of the sole and a free upper side of the sole via which the ski boot sole protrudes forwards, backwards and/or laterally beyond the ski boot shell, wherein the lower side of the sole comprises a first bearing region for placing upright on a bearing plate of a ski binding, and a second bearing region for walking without skis, and a width of the ski boot sole in the second bearing region is larger than a width of the ski boot sole in the first bearing region , characterised in that the ski boot is a children's ski boot, wherein when a ski boot is placed on a level plane, a distance between the front end of the free upper side of the sole and the plane is 23 mm ± 3 mm, wherein the second bearing region is curved convexly, at least in the longitudinal direction (X) of the boot, and an apical point of the second bearing region - which comprises a contact point or contact line or contact area of the ski boot sole of the ski boot which is placed on a level plane and exhibits a length (L) of the sole - has a distance (a) from the front end of the sole, wherein a ratio a/L has a value of 0.3 ± 0.05 and preferably 0.3 ± 0.03, and wherein the first bearing region comprises a hard component which exhibits a Shore D hardness of preferably more than 45, and the second bearing region preferably comprises a soft component which exhibits a Shore A hardness of preferably 65 to 85.
A combined flue ozone distribution system, comprising a first ozone distributor and a second ozone distributor that are disposed in a flue , wherein the first ozone distributor and the second ozone distributor each comprises: a plurality of main distribution pipes , a plurality of branch distribution pipes , and connecting pipes configured to supply ozone, wherein both sides of each of the plurality of main distribution pipes are each provided with a branch distribution pipe , a first end of one of the plurality of main distribution pipes is communicated with a connecting pipe , and a second end of the one of the plurality of main distribution pipes is communicated with a branch distribution pipe , characterized in that the first ozone distributor further comprises hemispherical distributors , and one of the hemispherical distributors is disposed at an end of the one of the plurality of branch distribution pipes of the first ozone distributor ; the second ozone distributor further comprises rhombic guide plates , and one of the rhombic guide plates is disposed at an end of the one of the plurality of branch distribution pipes of the second ozone distributor . a plurality of main distribution pipes , a plurality of branch distribution pipes , and connecting pipes configured to supply ozone, wherein both sides of each of the plurality of main distribution pipes are each provided with a branch distribution pipe , a first end of one of the plurality of main distribution pipes is communicated with a connecting pipe , and a second end of the one of the plurality of main distribution pipes is communicated with a branch distribution pipe , characterized in that the first ozone distributor further comprises hemispherical distributors , and one of the hemispherical distributors is disposed at an end of the one of the plurality of branch distribution pipes of the first ozone distributor ; the second ozone distributor further comprises rhombic guide plates , and one of the rhombic guide plates is disposed at an end of the one of the plurality of branch distribution pipes of the second ozone distributor .
Battery charger (C) for electric vehicles, comprising: - at least a voltage converter (DC/DC CONV); - at least a power factor correction circuit (PFC) connected upstream of said voltage converter (DC/DC CONV); - at least a controller circuit (PFC CNTR) operatively connected to said correction circuit (PFC) and adapted to drive said correction circuit (PFC) for the correction of the power factor in said battery charger (C); - at least a feedback line (L) connected to the output of said voltage converter (DC/DC CONV) and to at least an input of said controller circuit (PFC CNTR), characterized by the fact that said controller circuit (PFC CNTR) comprises at least a first input connected to the output of said voltage converter (DC/DC CONV) through said feedback line (L) and at least a second input connected to the input of said correction circuit (PFC), wherein said controller circuit (PFC CNTR) is configured to vary the output voltage (V PFC ) of said correction circuit (PFC) within a predefined voltage interval and according to the output voltage (V DCOUT ) of said voltage converter (DC/DC CONV) and compatibly with the mains input voltage (VMAINS), wherein said feedback line (L) comprises at least a first adder (SUM1) having a first input connected to the output of said correction circuit (PFC), a second input connected to the output of said voltage converter (DC/DC CONV) and an output connected to said first input of the controller circuit (PFC CNTR), and wherein said feedback line (L) comprises at least a second adder (SUM2) having a first input connected to the input of said correction circuit (PFC), a second input connected to the output of said voltage converter (DC/DC CONV) and an output connected to said second input of the controller circuit (PFC CNTR). - at least a voltage converter (DC/DC CONV); - at least a power factor correction circuit (PFC) connected upstream of said voltage converter (DC/DC CONV); - at least a controller circuit (PFC CNTR) operatively connected to said correction circuit (PFC) and adapted to drive said correction circuit (PFC) for the correction of the power factor in said battery charger (C); - at least a feedback line (L) connected to the output of said voltage converter (DC/DC CONV) and to at least an input of said controller circuit (PFC CNTR),
A pump arrangement , configured to be used with a double breast pump device comprising two expression kits , each expression kit being designed to subject a breast of a user of the device to a pressure profile and to receive milk expressed from the breast, the pump arrangement comprising: - a pump configured to create the pressure profile in the expression kits , and - a first air conduit and a second air conduit , each air conduit being designed to allow for air connection of an expression kit to the pump arrangement , - wherein the first air conduit is connectable to and disconnectable from a suction side of the pump through a first suction switching mechanism , - wherein the first air conduit is connectable to and disconnectable from a discharge side of the pump through a first discharge switching mechanism , - wherein the second air conduit is connectable to and disconnectable from the suction side of the pump through a second suction switching mechanism , - wherein the second air conduit is connectable to and disconnectable from the discharge side of the pump through a second discharge switching mechanism , and - wherein the first air conduit and the second air conduit are connectable to and disconnectable from each other directly through an intermediate switching mechanism arranged between the air conduits at a bypass position with respect to the pump . - a pump configured to create the pressure profile in the expression kits , and - a first air conduit and a second air conduit , each air conduit being designed to allow for air connection of an expression kit to the pump arrangement , - wherein the first air conduit is connectable to and disconnectable from a suction side of the pump through a first suction switching mechanism , - wherein the first air conduit is connectable to and disconnectable from a discharge side of the pump through a first discharge switching mechanism , - wherein the second air conduit is connectable to and disconnectable from the suction side of the pump through a second suction switching mechanism , - wherein the second air conduit is connectable to and disconnectable from the discharge side of the pump through a second discharge switching mechanism , and - wherein the first air conduit and the second air conduit are connectable to and disconnectable from each other directly through an intermediate switching mechanism arranged between the air conduits at a bypass position with respect to the pump .
A wing for use with an aircraft , the wing comprising: a fixed portion ; a folding portion proximate a distal end of the wing , the folding portion including: a raked surface; and a winglet ; the wing further comprising a hinge operatively coupled between the fixed and folding portions to enable the folding portion to fold relative to the fixed portion ; wherein the wing includes a bottom surface and a top surface , and wherein the winglet extends past the bottom surface and past the top surface of the wing ; wherein the folding portion is configured to rotate about the hinge relative to the fixed portion ; and wherein the folding portion rotates to an angular displacement greater than 90 degrees from the fixed portion so that the part of the winglet that extends past the bottom surface remains within a span limit . a fixed portion ; a folding portion proximate a distal end of the wing , the folding portion including: a raked surface; and a winglet ; a raked surface; and a winglet ; the wing further comprising a hinge operatively coupled between the fixed and folding portions to enable the folding portion to fold relative to the fixed portion ; wherein the wing includes a bottom surface and a top surface , and wherein the winglet extends past the bottom surface and past the top surface of the wing ; wherein the folding portion is configured to rotate about the hinge relative to the fixed portion ; and wherein the folding portion rotates to an angular displacement greater than 90 degrees from the fixed portion so that the part of the winglet that extends past the bottom surface remains within a span limit .