mhurhangee/ep-ind-claims huggingface dataset:
A motorcycle, rear-brake adaptor unit comprising: a rear-brake lever in communication with a rear brake hydraulic master cylinder; a step-plate connected directly to the rear-brake lever; one foot peg; and a lower step-plate in operative communication with the rear-brake lever, the lower step-plate disposed in a position behind the step-plate in a plane lower than the step-plate, the position providing simultaneous foot access to both the step-plate and the lower step-plate when a rider foot is resting on the one-foot peg. a rear-brake lever in communication with a rear brake hydraulic master cylinder; a step-plate connected directly to the rear-brake lever; one foot peg; and a lower step-plate in operative communication with the rear-brake lever, the lower step-plate disposed in a position behind the step-plate in a plane lower than the step-plate, the position providing simultaneous foot access to both the step-plate and the lower step-plate when a rider foot is resting on the one-foot peg.
A glazing comprising: a first glass substrate; a second glass substrate; and a viewing area of an information acquisition system, wherein the viewing area is formed to provide an optical power pattern in which the optical power varies across the viewing area, based on distance from which information is to be collected, and wherein the optical power is transmitted optical power, wherein the optical power pattern is determined by a difference in refractive index of at least one of the first and second glass substrates (121, 124). a first glass substrate; a second glass substrate; and a viewing area of an information acquisition system, wherein the viewing area is formed to provide an optical power pattern in which the optical power varies across the viewing area, based on distance from which information is to be collected, and wherein the optical power is transmitted optical power, wherein the optical power pattern is determined by a difference in refractive index of at least one of the first and second glass substrates (121, 124).
Suction unit, in particular for medical and dental purposes, with a suction machine and with an electric motor driving the latter, wherein the suction machine has a radial impeller element (132, 134), and the electric motor is a highspeed motor, in particular an electrically commutated electric motor, and the suction machine comprises sound insulation (110, 68, 38) which surrounds a work chamber in which a radial impeller element (132, 134) is arranged, characterized in that the sound insulation comprises a liquid volume (110; 90).
A method for shaping a material film or sheet for making three-dimensional shapes, in which method the film or sheet is heated and a pressure difference is applied by means of a pressure medium to one side of the film or sheet; the heating being performed along an outline of the three-dimensional shape to be formed to a temperature which will permit a change in the shape of the film or sheet in the area of the heated outline and will create stretching along the heated outline in order to cause the unheated part of the film or sheet inside the outline to deviate from its initial plane, the targeted three-dimensional structure being divided into two-dimensional slices, the outlines of which in the film or sheet are sequentially heated and subjected to a pressure difference to generate the desired structure, characterized in comprising the following steps: - providing a countersurface to limit the stretching of the heated material during a stretching stage - allowing the material to cool and harden - moving the countersurface to a new position - heating a next outline - applying a pressure difference to stretch the material along said next heated outline until the material again meets the countersurface - repeating the process until the desired shape is obtained. - providing a countersurface to limit the stretching of the heated material during a stretching stage - allowing the material to cool and harden - moving the countersurface to a new position - heating a next outline - applying a pressure difference to stretch the material along said next heated outline until the material again meets the countersurface - repeating the process until the desired shape is obtained.
A water vapor permeable membrane comprising a dense layer and a support layer that are adjacent to each other, wherein said dense layer contains voids with a length of 0.1 μm or less and said layer has a thickness of 0.1 μm or more and 2 μm or less; wherein in said support layer, void (a), being the void with the largest length in the 2 μm thick region measured from the boundary between the dense layer and the support layer into the support layer, has a length of 0.3 μm or more and void (b), being the void with the largest length in the region ranging between 2 μm and 4 μm measured from said boundary into the support layer, has a length of 0.5 μm or more, the length of said void (b) being larger than that of said void (a) and said support layer contains voids that have an internal dimension in the thickness direction of the water vapor permeable membrane equivalent to 30% or more of the thickness of the water vapor permeable membrane, such voids being referred to as voids (c); wherein the void lengths are defined as the maximum internal dimension of a void observed in the cross section of the membrane when measured as described in the Examples in the specification; wherein the membrane comprises polysulfone; and wherein the water vapor permeable membrane is obtained by using, as a core liquid, a solution that can aggregate or coagulate the raw material solution for membrane production and discharging a raw material solution for membrane production which has a viscosity of 5 to 30 poise and contains polysulfone resin at a concentration of 10 mass % or more and 25 mass % or less from a nozzle and bringing a poor solvent into contact with the raw material solution for membrane production immediately after the raw material solution for membrane production is discharged from the nozzle and coagulating the raw material solution to form the water vapor permeable membrane.
Crystalline methylthioninium chloride dihydrate as Form C, having the following characteristic peaks in a powder X-ray diffraction pattern using CuKa radiation: Peak 2θ values (± 0.1°) 1 8.1 2 11.1 3 17.6 4 25.9 5 27.2
Wheel suspension for a motor vehicle, having a multi-link assembly made from links, which has the side member and cross member on an auxiliary frame of the vehicle body, and are hinged on a wheel carrier, and having a rotary actuator for an active chassis control, which has an engine-transmission unit with which the torques are transferable to the multi-link assembly via a torsion bar as positioning forces, characterised in that links (14, 16) of the multi-link assembly delimit a clearance to the front and to the rear in the vehicle longitudinal direction (x), in which clearance the engine-transmission unit of the rotary actuator is partially arranged, in that the engine-transmission unit of the rotary actuator has a transmission gear unit which is coaxial to the torsion bar and an engine which is arranged with a radial axial spacing (r) relative to the torsion bar and drives the transmission gear unit with an intermediate gear, in that the transmission gear unit of the engine-transmission unit is arranged beneath one of the side members, wherein the torsion rod of the rotary actuator is oriented to align with the course of the side member and in that the engine of the engine-transmission unit is arranged in the clearance.
Well tool device for melting and thereafter hardening of casing, and cement and formation outside of the casing, for forming a permanent barrier in a well, comprising: - a housing in which a compartment is provided; - a pyrotechnic mixture provided within the compartment; - an ignition device adapted to heating at least a part of the pyrotechnic mixture to its ignition temperature; thereby starting a pyrotechnic heat generating process resulting in that casing, and cement and formation outside of the casing, will start to melt, resulting in a permanent barrier when the pyrotechnic heat generating process ends; wherein the pyrotechnic mixture comprises a first metal; wherein the housing comprises a lower housing section, an intermediate housing section and an upper housing section; wherein the first metal is aluminum or an aluminum alloy; characterized in that - at least a section of the housing is made of the first metal; - the section of the housing made of the first metal is the intermediate section. - a housing in which a compartment is provided; - a pyrotechnic mixture provided within the compartment; - an ignition device adapted to heating at least a part of the pyrotechnic mixture to its ignition temperature; thereby starting a pyrotechnic heat generating process resulting in that casing, and cement and formation outside of the casing, will start to melt, resulting in a permanent barrier when the pyrotechnic heat generating process ends; wherein the pyrotechnic mixture comprises a first metal; wherein the housing comprises a lower housing section, an intermediate housing section and an upper housing section; wherein the first metal is aluminum or an aluminum alloy; characterized in that wherein the pyrotechnic mixture comprises a first metal; wherein the housing comprises a lower housing section, an intermediate housing section and an upper housing section; wherein the first metal is aluminum or an aluminum alloy; characterized in that - at least a section of the housing is made of the first metal; - the section of the housing made of the first metal is the intermediate section.
A bone fixation plate, comprising: a main body formed of a first material, the main body having a main body first end, a main body second end, a main body first side, a main body second side, a first surface, and a second surface opposite the first surface, the main body defining a first set of openings extending through the main body between the first and second surfaces (815, 817) and the main body further defining a recess for each opening of the first set of openings, the recess having a recess length and extending to a main body circumferential surface for each respective opening of the first set of openings; and a support member formed of a second, different material and attached to the main body, the support member defining a second set of openings aligned with the first set of openings and a support member circumferential surface for each opening of the second set of openings; wherein each main body circumferential surface is disposed adjacent and continuous with a support member circumferential surface to define an opening circumferential surface that bounds an opening of the first set of openings and an opening of the second set of openings. a main body formed of a first material, the main body having a main body first end, a main body second end, a main body first side, a main body second side, a first surface, and a second surface opposite the first surface, the main body defining a first set of openings extending through the main body between the first and second surfaces (815, 817) and the main body further defining a recess for each opening of the first set of openings, the recess having a recess length and extending to a main body circumferential surface for each respective opening of the first set of openings; and a support member formed of a second, different material and attached to the main body, the support member defining a second set of openings aligned with the first set of openings and a support member circumferential surface for each opening of the second set of openings; wherein each main body circumferential surface is disposed adjacent and continuous with a support member circumferential surface to define an opening circumferential surface that bounds an opening of the first set of openings and an opening of the second set of openings.
A method for operating a power station of fluctuating electrical capacity that, besides a voltage-setting system former outputting active power and reactive power and at least one load, is connected to a limited AC grid, - wherein a desired self-contained operating range of the system former is defined on the PQ level, in which operating range the system former is able to efficiently correct fluctuations arising in a mains voltage of the AC grid, - characterized in that a present operating point of the system former on the PQ level is ascertained, and - wherein an output of active power and reactive power by the power station is controlled such that the operating point of the system former is kept in the desired operating range. - wherein a desired self-contained operating range of the system former is defined on the PQ level, in which operating range the system former is able to efficiently correct fluctuations arising in a mains voltage of the AC grid, - characterized in that a present operating point of the system former on the PQ level is ascertained, and - wherein an output of active power and reactive power by the power station is controlled such that the operating point of the system former is kept in the desired operating range.
A vertical flow reactor comprising: a casing; an outer wall contained within the casing, the outer wall being partially above and partially below ground level of a bore hole in which the vertical flow reactor is contained; an annular space defined between the outer wall and the casing; a flow partition contained within the outer wall; a further annular space defined between the outer wall and the flow partition; a transport apparatus that directs pre-mixed waste and water feed components into the flow partition, the waste and water feed components flowing downward in the flow partition and exiting in the annular space outside of the flow partition, where the waste and water feed components flow upward; a compressor that introduces oxygen into the waste and water feed components at or near the top of the vertical flow reactor as small bubbles, the waste, water, and oxygen combination flowing downward within the flow partition such that, the waste, water, and oxygen is heated by heat transfer from liquid flowing upward in the annular space outside the flow partition, said flow partition being insulated at a lower portion thereof to reduce heat transfer between down flowing and up flowing, thus causing more heat transfer to occur in the upper portion and providing more time for reaction at high temperature in the lower portion. a casing; an outer wall contained within the casing, the outer wall being partially above and partially below ground level of a bore hole in which the vertical flow reactor is contained; an annular space defined between the outer wall and the casing; a flow partition contained within the outer wall; a further annular space defined between the outer wall and the flow partition; a transport apparatus that directs pre-mixed waste and water feed components into the flow partition, the waste and water feed components flowing downward in the flow partition and exiting in the annular space outside of the flow partition, where the waste and water feed components flow upward; a compressor that introduces oxygen into the waste and water feed components at or near the top of the vertical flow reactor as small bubbles, the waste, water, and oxygen combination flowing downward within the flow partition such that, the waste, water, and oxygen is heated by heat transfer from liquid flowing upward in the annular space outside the flow partition, said flow partition being insulated at a lower portion thereof to reduce heat transfer between down flowing and up flowing, thus causing more heat transfer to occur in the upper portion and providing more time for reaction at high temperature in the lower portion.
A method of operating aircraft for flight in a close formation, comprising: establishing a communication link between a first aircraft (310, 710, 810, 910, 1410, 2910, 5810) and a second aircraft (320, 750, 850, 860, 920, 930, 940, 950, 1450, 2930, 5820), wherein the first aircraft leads the second aircraft in the close formation; assigning to at least one of the first aircraft or the second aircraft, via the communication link, initial positions relative to one another in the close formation; providing flight control input for aligning the first and second aircraft in their respective initial positions; tracking, by at least one aircraft in the close formation, at least one vortex generated by at least one other aircraft in the close formation, wherein the tracking includes collecting airflow measurements, at the second aircraft, for sensing a first vortex (620, 720, 820, 1020, 1030, 1420, 2920) generated by a wingtip of the first aircraft and analyzing the received data to create computer vortex models for mapping the vortex field and subdividing the mapped vortex field into different vortex regions, identifying locations of respective vortex cores, and updating the positions of the vortex cores with respect to the second aircraft; and based on the tracking, providing flight control input to adjust a relative position between the first aircraft and the second aircraft based on the positions of the vortex cores. establishing a communication link between a first aircraft (310, 710, 810, 910, 1410, 2910, 5810) and a second aircraft (320, 750, 850, 860, 920, 930, 940, 950, 1450, 2930, 5820), wherein the first aircraft leads the second aircraft in the close formation; assigning to at least one of the first aircraft or the second aircraft, via the communication link, initial positions relative to one another in the close formation; providing flight control input for aligning the first and second aircraft in their respective initial positions; tracking, by at least one aircraft in the close formation, at least one vortex generated by at least one other aircraft in the close formation, wherein the tracking includes collecting airflow measurements, at the second aircraft, for sensing a first vortex (620, 720, 820, 1020, 1030, 1420, 2920) generated by a wingtip of the first aircraft and analyzing the received data to create computer vortex models for mapping the vortex field and subdividing the mapped vortex field into different vortex regions, identifying locations of respective vortex cores, and updating the positions of the vortex cores with respect to the second aircraft; and based on the tracking, providing flight control input to adjust a relative position between the first aircraft and the second aircraft based on the positions of the vortex cores.
Corrector for chromatic and spherical aberration in an electron microscope with six multipole elements (1, 2, 3, 4, 5, 6) arranged successively in the beam path symmetrically to a plane of symmetry, all of which are used for the production of quadrupole fields (1', 2', 3', 4', 5', 6') and the third and fourth also for the production of octupole fields (3", 4"), wherein said fields are commutated and the quadrupole fields (1', 2', 3', 4', 5', 6') of all six multipole elements (1, 2, 3, 4, 5, 6) are rotated through 90° from one to the next and, in relation to their field strengths, are point symmetrical to the intersection of the optical axis with the plane of symmetry, wherein the following exchange symmetries result, an exchange symmetry of the axial fundamental paths (xα, yβ) with the plane of symmetry as the plane of symmetry for the exchange of the profile of the axial fundamental paths xα and yβ and also an exchange symmetry of the off-axial fundamental paths (xγ, yδ) with the intersection of the optical axis with the plane of symmetry as the point for a point symmetrical exchange of the profile of the off-axial fundamental paths xγ and yδ and wherein thereafter all fundamental paths (xα, yβ, xγ, yδ) are brought together again at the end of the corrector, wherein through the interaction of the quadrupole fields (3', 4') of the third and fourth multipole element configured as magnetic and electrical fields (3', 4'), a chromatic aberration correction is possible and also by means of the quadrupole fields (1', 2', 3', 4', 5', 6') and the octupole fields (3", 4") a spherical aberration correction is possible characterized in that in the quadrupole field of the first quadrupole element a stigmatic intermediate image of the axial fundamental paths (xγ, yδ) is produced and this quadrupole field is adjusted in such a manner that astigmatic intermediate images (12, 13) of the off-axial fundamental paths (xγ, yδ) in the region of the middle of the quadrupole fields (3', 4') of the third and fourth multipole element are generated and there too, the adjustment of the quadrupole field of the second quadrupole element means that the axial fundamental paths (xα, yβ) of the same section (x, y), in which the intermediate images (12, 13) of the off-axial fundamental paths (xγ, yδ) lie, are at a maximum in each case.
A photovoltaic device being an interdigitated back contact photovoltaic device comprising: - a silicon-based substrate being of p-type or n-type doping and having a first face defining a X-Y plane; - an intrinsic amorphous silicon layer a-Si:H(i) situated on said first face; - a first patterned silicon layer situated on said intrinsic layer, said first silicon layer being of p-type or n-type doping, said first patterned silicon layer comprising interstices (2") between charge collection portions, said charge collection portions comprising each second portions of an at least partially nano-crystalline silicon layer at their side away from said silicon-based substrate; - a second nano-crystalline silicon layer being situated on said charge collection portions, and on said interstices (2"), and having another type of doping than the doping type of said patterned silicon layer, wherein - said charge collection portions comprise each an amorphous layer portion situated between said intrinsic layer and said second portions, said amorphous layer portions having, in at least one of its cross sections parallel to said X-Y plane, and in any radial direction, a largest width (L2a) that is greater than any width (L2b) of said second portions, said amorphous layer portions and said second portions being basically centered to each other, - a silicon-based substrate being of p-type or n-type doping and having a first face defining a X-Y plane; - an intrinsic amorphous silicon layer a-Si:H(i) situated on said first face; - a first patterned silicon layer situated on said intrinsic layer, said first silicon layer being of p-type or n-type doping, - a second nano-crystalline silicon layer being situated on said charge collection portions, and on said interstices (2"), and having another type of doping than the doping type of said patterned silicon layer, - said charge collection portions comprise each an amorphous layer portion situated between said intrinsic layer and said second portions, said amorphous layer portions having, in at least one of its cross sections parallel to said X-Y plane, and in any radial direction, a largest width (L2a) that is greater than any width (L2b) of said second portions, said amorphous layer portions and said second portions being basically centered to each other,
A composition comprising a stable aqueous dispersion of a copolymer containing acrylic polymer blocks and urethane polymer blocks wherein a) each acrylic block and each urethane block are linked to each other through a sulfur atom; b) the dispersion contains from 30% to 85% water by weight of the total dispersion; and c) the dispersion contains a substantial absence of an organic solvent.