mhurhangee/ep-ind-claims huggingface dataset:
A magnetic field sensor, comprising: a plurality of magnetic field sensing elements, wherein each one of the plurality of magnetic field sensing elements is configured to generate a respective x-y output signal responsive to a magnetic field in an x-y plane; an angle processing circuit coupled to receive the x-y output signals and configured to generate an uncorrected x-y angle value representative of an angle of the magnetic field in an x-y plane, wherein the uncorrected x-y angle value comprises a first angle error; a temperature sensor configured to generate a temperature signal representative of a temperature; an angle error correction module coupled to the angle processing circuit and the temperature sensor and configured to generate, in response to a measured magnetic field signal and the temperature signal, an x-y angle error value indicative of an error in the uncorrected x-y angle value and comprising a ratio of a nominal magnetic field strength to a measured magnetic field strength; a coefficient table configured to store a plurality of correction coefficients for use by the angle error correction module, wherein the plurality of correction coefficients comprises a plurality of magnitudes and phases of one or more harmonics of the first angle error; and a combining module configured to combine the uncorrected x-y angle value with the x-y angle error value to generate a corrected x-y angle value having a second angle error smaller than the first angle error. a plurality of magnetic field sensing elements, wherein each one of the plurality of magnetic field sensing elements is configured to generate a respective x-y output signal responsive to a magnetic field in an x-y plane; an angle processing circuit coupled to receive the x-y output signals and configured to generate an uncorrected x-y angle value representative of an angle of the magnetic field in an x-y plane, wherein the uncorrected x-y angle value comprises a first angle error; a temperature sensor configured to generate a temperature signal representative of a temperature; an angle error correction module coupled to the angle processing circuit and the temperature sensor and configured to generate, in response to a measured magnetic field signal and the temperature signal, an x-y angle error value indicative of an error in the uncorrected x-y angle value and comprising a ratio of a nominal magnetic field strength to a measured magnetic field strength; a coefficient table configured to store a plurality of correction coefficients for use by the angle error correction module, wherein the plurality of correction coefficients comprises a plurality of magnitudes and phases of one or more harmonics of the first angle error; and a combining module configured to combine the uncorrected x-y angle value with the x-y angle error value to generate a corrected x-y angle value having a second angle error smaller than the first angle error.
Transmission (101, 201, 301) with a first shaft, a second shaft, a third shaft, a fourth shaft, a fifth shaft, a sixth shaft, a first shifting element, a second shifting element, a third shifting element, a fourth shifting element, a fifth shifting element, a sixth shifting element, a seventh shifting element, an eighth shifting element, a ninth shifting element and an output; wherein the first shaft and the third shaft are connectable to each other for conjoint rotation via the first shifting element; wherein the first shaft and the second shaft are connectable to each other for conjoint rotation via the second shifting element; wherein the second shaft and the fourth shaft are connectable to each other for a rotational action via the third shifting element; wherein the third shaft and the fourth shaft are in each case connectable to each other for conjoint rotation via the fourth shifting element and the fifth shifting element; wherein the second shaft and the fifth shaft are connectable to each other for a rotational action via the sixth shifting element; wherein the fourth shaft and the fifth shaft are connectable to each other for a rotational action via the seventh shifting element; wherein the third shaft and the fifth shaft are connectable to each other for a rotational action via the eighth shifting element; wherein a fixed gear of the fourth shaft and a fixed gear of the fifth shaft are each connected to the output for a rotational action; wherein a first gearwheel of the sixth shaft and a fixed gear of the second shaft intermesh; wherein a second gearwheel of the sixth shaft and a fixed gear of the third shaft intermesh; wherein the first gearwheel is a free gear of the sixth shaft and the second gearwheel is a fixed gear of the sixth shaft, or the first gearwheel is the fixed gear of the sixth shaft and the second gearwheel is the free gear of the sixth shaft; and wherein the free gear of the sixth shaft and the sixth shaft are connectable to each other for conjoint rotation via the ninth shifting element, characterized in that a fixed gear of the second shaft and the first gearwheel of the sixth shaft intermesh; the fixed gear of the second shaft is connected for a rotational action to a first free gear (L4.1) of the fourth shaft and to a first free gear (L5.1) of the fifth shaft; the first free gear (L4.1) of the fourth shaft and the fourth shaft are connectable to each other for conjoint rotation via the third shifting element; and the first free gear (L5.1) of the fifth shaft and the fifth shaft are connectable to each other for conjoint rotation via the sixth shifting element.
An aircraft landing gear assembly comprising: a sliding tube; a support beam pivotally connected to the sliding tube; at least one caterpillar track assembly including: a pair of track end wheels pivotally mounted to the support beam; a caterpillar track extending between and around the pair of track end wheels; and characterized in that the at least one caterpillar track assembly further includes a first air cushion device located between the track end wheels and arranged to provide an air cushion adjacent to a portion of an inner surface of the load bearing section of the caterpillar track section, wherein the caterpillar track assembly further comprises a second air cushion device located between the track end wheels and arranged to provide an air cushion adjacent to a portion of the inner surface of the non-load bearing/return section of the caterpillar track assembly. a sliding tube; a support beam pivotally connected to the sliding tube; at least one caterpillar track assembly including: a pair of track end wheels pivotally mounted to the support beam; a caterpillar track extending between and around the pair of track end wheels; and characterized in that the at least one caterpillar track assembly further includes a first air cushion device located between the track end wheels a pair of track end wheels pivotally mounted to the support beam; a caterpillar track extending between and around the pair of track end wheels; and characterized in that the at least one caterpillar track assembly further includes a first air cushion device located between the track end wheels and arranged to provide an air cushion adjacent to a portion of an inner surface of the load bearing section of the caterpillar track section,
A rotatable grate device for a solid fuel heating boiler, comprising a lamella grate mounted rotatably in a frame and a cleaning device which engages between individual lamellae (2.1) of the lamella grate, characterized in that the frame is produced by casting technology, that the lamella grate is produced by casting technology in one piece and that parts of the cleaning device are configured to be horizontally movable between adjacent lamellae (2.1).
Sealing system with a window frame and a wall of a building, which wall is made of timber, natural or artificial stone blocks, concrete or the like and comprises an external side, an internal side and a wall opening for insertion of the window frame, which has lower and upper substantially horizontal opening boundaries and upright opening boundaries which are arranged a distance from one another, wherein the external side, the lower opening boundary and each upright opening boundary include three planes, wherein the sealing system also comprises sealing elements (20; 21) which with sealing sections (22, 23, 24; 25, 26, 27) adjoin a first plane of the external side, a second plane of the respective upright opening boundaries (17; 18) and a third plane of the lower horizontal opening boundary, and upright frame sections (31, 32) and a horizontal frame section of the window frame cooperate with the sealing sections (23, 24; 26, 27), running along the second and the third plane (29, 30), and wherein the sealing sections (23, 24; 26, 27) of the sealing element (20; 21) of the second and the third plane (29, 30) protrude over the sealing section (22; 25) of the first plane with a defined first projection, characterised in that plaster base (46; 47) is attached at least to the sealing sections (22; 25) which run along the first plane.
A heat reservoir comprising: a plate-shaped porous substrate having 2 main surfaces; a heat storage material composition impregnating into the porous substrate; and a coat layer covering at least one of the 2 main surfaces of the porous substrate, wherein the heat storage material composition comprises a latent heat storage material and a thermoplastic elastomer, wherein the coat layer has a property such that a configuration can be maintained after it is exposed to a temperature of 200°C to 600°C in the air for 10 to 60 minutes, wherein the coat layer can reflect an infrared radiation at a wavelength of 0.3 to 100 μm by 80% or more, and wherein the porous substrate is a wooden molded article. a plate-shaped porous substrate having 2 main surfaces; a heat storage material composition impregnating into the porous substrate; and a coat layer covering at least one of the 2 main surfaces of the porous substrate, wherein the heat storage material composition comprises a latent heat storage material and a thermoplastic elastomer, wherein the coat layer has a property such that a configuration can be maintained after it is exposed to a temperature of 200°C to 600°C in the air for 10 to 60 minutes, wherein the coat layer can reflect an infrared radiation at a wavelength of 0.3 to 100 μm by 80% or more, and wherein the porous substrate is a wooden molded article.
Agricultural machine with a device, which is rollable over soil or over a crop, for soil cultivation or for picking up crop, in particular a soil roller for soil cultivation or a crop picking-up device, with a supporting body which is supported rotatably on a supporting frame via rolling bearings, and with tools which are arranged next to one another in the axial direction on the supporting body and are rollable over the soil, wherein the rolling bearings having a bearing housing are fastened to supporting body walls provided substantially on the end sides of the supporting body, and are each connected to a supporting arm of the supporting body via a bearing bolt, wherein the rolling bearing is fastened releasably to a supporting body wall via the bearing housing, and the bearing pin is fastened releasably to the associated supporting arm, the bearing bolt is connected to the supporting body wall via the rolling bearing and the bearing housing, the rolling bearing has a bearing inner ring (13.1) into which the bearing bolt is introducible, and in that the bearing inner ring (13.1) of the rolling bearing is lockable to the bearing bolt via a securing element which is introducible into the bearing inner ring (13.1) of the rolling bearing; the bearing bolt is of spherical-segment-shaped design at least in regions, in that the spherical-segment-shaped region (12.2) of the bearing bolt has a flat end surface facing the supporting body wall and a cylindrical bearing bolt head (12.1) which faces away from the supporting body wall and in which receptacles for fastening means of the supporting frame are provided; and the securing element, at its region facing the bearing bolt, is formed in a complementary manner to the spherical design of the spherical segment (12.2) of the bearing bolt.
Method for testing or verifying the indirect pressure monitoring system of the wheels of a vehicle, which monitoring system detects a tire pressure variation using the Anti-lock Braking System - Electronic Stability Program sensors system, comprising the following steps: - checking the inflation pressure of at least two wheels of a vehicle and, if they are deflated, inflating them to a predetermined pressure, - controlling the advancement of the vehicle so as to bring said at least two wheels above or at dragging into rotation means (2a, 2b), - activating said dragging means (2a, 2b) so as to simultaneously drag into rotation said at least two wheels with speeds different one with respect to the other, - verifying whether the indirect pressure monitoring system signals or not an anomaly, such as a rotation speed or pressure different among said at least two wheels dragged into rotation and, if the indirect pressure monitoring system does not signal an anomaly, then the indirect pressure monitoring system does not work properly and must be serviced. - checking the inflation pressure of at least two wheels of a vehicle and, if they are deflated, inflating them to a predetermined pressure, - controlling the advancement of the vehicle so as to bring said at least two wheels above or at dragging into rotation means (2a, 2b), - activating said dragging means (2a, 2b) so as to simultaneously drag into rotation said at least two wheels with speeds different one with respect to the other, - verifying whether the indirect pressure monitoring system signals or not an anomaly, such as a rotation speed or pressure different among said at least two wheels dragged into rotation and, if the indirect pressure monitoring system does not signal an anomaly, then the indirect pressure monitoring system does not work properly and must be serviced.
A process for producing a component, comprising the sintering of a composition comprising: a) hard material particles comprising an inner core comprising fused tungsten carbide and an outer shell comprising tungsten carbide, and b) binder metals selected from the group consisting of Co, Ni, Fe and alloys, comprising at least one metal selected from Co, Ni and Fe; wherein the sintering is effected in a sintering temperature range of from 1250 °C to 1400 °C for a period of from 3 to 15 minutes, and is effected at a gas pressure of less than 100 Pa (10 -3 bar), wherein the cooling after the sintering process within the temperature range of from the sintering temperature to 500°C is effected at a cooling rate of below 100 K/min, and wherein the sintering is carried out while applying a pressure of from 20 to 80 MPa to the composition. a) hard material particles comprising an inner core comprising fused tungsten carbide and an outer shell comprising tungsten carbide, and b) binder metals selected from the group consisting of Co, Ni, Fe and alloys, comprising at least one metal selected from Co, Ni and Fe;
A doctor blade holder system, comprising: a) a doctor blade support structure that includes an elongated slot for receiving a doctor blade (2, 56) and a separate elongated slot (10, 68) to house mounting hardware (14, 75) for attaching the doctor blade support structure to a holder mounting plate (13, 74); b) an adjustable profiling plate (4, 52) adapted to cause pressure to be applied to the doctor blade (2, 56) in a continuous manner along the length of the doctor blade (2, 56), wherein the profiling plate (4, 52) is mounted to the holder mounting plate (13, 74) with a series of mounting structures allowing flexure or localized rotation of the profiling plate (4, 52) with respect to holder mounting plate (13, 74) around one or two axes; c) a series of adjustment mechanisms (29, 84) attached to the holder mounting plate (13, 74) and acting on the profiling plate (4, 52), wherein the adjustment mechanisms (29, 84) are capable of displacing the profiling plate (4, 52) in a bidirectional manner; and d) a back-up blade (5, 106) to transfer force from the profiling plate (4, 52) to the doctor blade (2, 56). a) a doctor blade support structure that includes an elongated slot for receiving a doctor blade (2, 56) and a separate elongated slot (10, 68) to house mounting hardware (14, 75) for attaching the doctor blade support structure to a holder mounting plate (13, 74); b) an adjustable profiling plate (4, 52) adapted to cause pressure to be applied to the doctor blade (2, 56) in a continuous manner along the length of the doctor blade (2, 56), wherein the profiling plate (4, 52) is mounted to the holder mounting plate (13, 74) with a series of mounting structures allowing flexure or localized rotation of the profiling plate (4, 52) with respect to holder mounting plate (13, 74) around one or two axes; c) a series of adjustment mechanisms (29, 84) attached to the holder mounting plate (13, 74) and acting on the profiling plate (4, 52), wherein the adjustment mechanisms (29, 84) are capable of displacing the profiling plate (4, 52) in a bidirectional manner; and d) a back-up blade (5, 106) to transfer force from the profiling plate (4, 52) to the doctor blade (2, 56).
System consisting of a spray gun and a paint reservoir, it being possible, by forming a compressed-air chamber in the paint reservoir, to pressurise, by means of compressed air, paint located in the paint reservoir in order to feed said paint into the spray gun and to spray the paint using the spray gun, the spray gun also comprising a gun body and a nozzle, a nozzle needle being mounted in the pistol body in order to actuatably close the nozzle by means of the nozzle needle, the nozzle needle also penetrating a membrane which is rigidly connected to the nozzle needle and which seals, in a fluid-tight manner, a chamber which is remote from the nozzle and through which the nozzle needle passes, the membrane simultaneously allowing a movement which is necessary for opening and closing the spray gun, characterised in that, in order to use the chamber through which nozzle needle passes as a pressure chamber, the compressed-air chamber is connected thereto.
A tetradentate cyclometalated platinum complex based on oxygen atom linkage and containing phenyl acridine, wherein the tetradentate cyclometalated platinum complex has a structure of general formula: wherein R 1, R 2, R 3, R 4 and R 5 each independently represent a mono-substitution, a di-substitution, a tri-substitution, a tetra-substitution or a non-substitution, and R 1, R 2, R 3, R 4 and R 5 are each independently hydrogen, deuterium, alkyl, aryl, cycloalkyl, heterocyclyl, heteroaryl or a combination thereof; and two or more adjacent ones of R 1, R 2, R 3, R 4 and R 5 are each independently or selectively linked to form a fused ring.
An energy absorbing assembly, comprising: a support structure having a first wall and an outer wall (20, 22) that extend in a first direction (x) from a first end to a second end, the first direction (x) being perpendicular to a second direction (z) defined between the first end and the second end; energy absorber that extends across the first wall of the support structure, the energy absorber comprising a plurality of crushable members configured to crush and absorb energy upon impact, first crash can; and second crash can, wherein the first and second crash cans extend from the first and second ends of the support structure; wherein the energy absorbing assembly is a single element which can be formed in situ; and wherein the first and second crash cans comprise a back face with a cavity open from the back face, wherein the cavity converges toward a front face. a support structure having a first wall and an outer wall (20, 22) that extend in a first direction (x) from a first end to a second end, the first direction (x) being perpendicular to a second direction (z) defined between the first end and the second end; energy absorber that extends across the first wall of the support structure, the energy absorber comprising a plurality of crushable members configured to crush and absorb energy upon impact, first crash can; and second crash can, wherein the first and second crash cans extend from the first and second ends of the support structure; wherein the energy absorbing assembly is a single element which can be formed in situ; and wherein the first and second crash cans comprise a back face with a cavity open from the back face, wherein the cavity converges toward a front face.
Transport platform for loading, conveying and storing elongate cut-to-length loads, in particular timber logs, said transport platform being implemented as a beam construction having a base assembly which is constructed from longitudinal beams and cross beams, wherein a base-proximal corner casting by way of which the transport platform is able to be locked to a semitrailer contour of a truck semitrailer or any other mode of transport is provided at each of the four corner regions of the base assembly, and wherein the base assembly at each of the four corner regions has a vertical beam which terminates by way of a corner casting on the upper side to which a further transport platform stacked thereon is able to be locked, or in which a container stacker engages for loading the transport platform, characterized in that the transport platform in the platform longitudinal direction (x) by way of at least one rearward protrusion is extended beyond the base-proximal corner castings; in that the rearward protrusion in the case of a transport platform loaded on the truck semitrailer is disposed on the rear side of the semitrailer; in that the transport platform has a cab-proximal protrusion which in a state loaded on the truck semitrailer protrudes in the direction of a truck cab; and in that the cab-proximal protrusion, while forming a base-proximal void, is offset from the platform lower side by a height offset (Δz) such that, when positioning the transport platform on the truck semitrailer, semitrailer components are disposed in the region of the base-proximal void.