mhurhangee/ep-ind-claims huggingface dataset:
A cutter body assembly (20, 20') comprising: a disk-shaped cutter body and a plurality of support pads (24, 24') removably retained therein, the cutter body having an axis of rotation, a direction of rotation (D R) about the axis of rotation, two opposing end surfaces (26a, 26b) and a body peripheral surface extending therebetween, and each of the plurality of support pads (24, 24') protruding from one of the two opposing end surfaces (26a, 26b), wherein a median plane perpendicular to the axis of rotation intersects the body peripheral surface, and two annular-shaped planes are equidistantly offset from opposite sides of the median plane by a first distance, and wherein each of the plurality of support pads (24, 24') intersects one of the two annular-shaped planes, and the cutter body intersects neither of the two annular-shaped planes, wherein the cutter body has a plurality of pad pockets for mounting and indexing the plurality of support pads (24, 24'), characterized in that each support pad (24, 24') has an axially outermost point (No) located a second distance from the median plane, and in that each support pad (24, 24') is indexable in its associated pad pocket to increase or decrease the second distance. a disk-shaped cutter body and a plurality of support pads (24, 24') removably retained therein, the cutter body having an axis of rotation, a direction of rotation (D R) about the axis of rotation, two opposing end surfaces (26a, 26b) and a body peripheral surface extending therebetween, and each of the plurality of support pads (24, 24') protruding from one of the two opposing end surfaces (26a, 26b), wherein a median plane perpendicular to the axis of rotation intersects the body peripheral surface, and two annular-shaped planes are equidistantly offset from opposite sides of the median plane by a first distance, and wherein each of the plurality of support pads (24, 24') intersects one of the two annular-shaped planes, and the cutter body intersects neither of the two annular-shaped planes, wherein the cutter body has a plurality of pad pockets for mounting and indexing the plurality of support pads (24, 24'), characterized in that each support pad (24, 24') has an axially outermost point (No) located a second distance from the median plane, and in that each support pad (24, 24') is indexable in its associated pad pocket to increase or decrease the second distance.
A method of synchronizing multi-level output controllable devices (10, 11, 12) in a network, the method comprising: determining, by a processor in a controllable device, that a received data packet is a retransmission of an initial control command data packet, wherein the retransmitted data packet includes an operation command that cause the controllable device to perform an operation that was requested to be performed by a plurality of controllable devices operating in cooperation; obtaining from the retransmitted data packet, information related to performance of the operation, the information including a time indicator that indicates the time when the initial command was given, or that indicates a duration of the operation; determining a time when the initial command was transmitted; obtaining a ramp rate related to the operation to be performed, the ramp rate indicating to the controllable device how quickly to transition from an expected start value to a commanded value; calculating an adjusted ramp rate, the adjusted ramp rate for controlling the controllable device to synchronize operation with others of the controllable devices; setting an output value for the controllable device based on the adjusted ramp rate; and completing the operation using the set output value. determining, by a processor in a controllable device, that a received data packet is a retransmission of an initial control command data packet, wherein the retransmitted data packet includes an operation command that cause the controllable device to perform an operation that was requested to be performed by a plurality of controllable devices operating in cooperation; obtaining from the retransmitted data packet, information related to performance of the operation, the information including a time indicator that indicates the time when the initial command was given, or that indicates a duration of the operation; determining a time when the initial command was transmitted; obtaining a ramp rate related to the operation to be performed, the ramp rate indicating to the controllable device how quickly to transition from an expected start value to a commanded value; calculating an adjusted ramp rate, the adjusted ramp rate for controlling the controllable device to synchronize operation with others of the controllable devices; setting an output value for the controllable device based on the adjusted ramp rate; and completing the operation using the set output value.
A seabed supported unit for drilling and production of hydrocarbons, comprising a seabed supported base structure positioned and fixed with respect to a sea bed, forming a support for a floatable drilling unit and/or a floatable production unit, wherein the base structure is provided with buoyancy devices, with an upwards extending wall structure extending around the base structure along three sides and also intended to extend up above a sea level when installed at a site, while the fourth side is provided with an opening in the upwards extending wall structure for introducing the floatable drilling and/or production unit (30, 50), the floatable drilling and/or production unit (30, 50) being retractably arrangeable on top of the base structure and within the upwards extending wall structure, and where an exterior side of the upwards extending wall structure is provided with preinstalled sections comprising prepared well points intended to be used for drilling wells through, wherein the prepared well points are arranged on a cantilever unit extending laterally out from the exterior side of the upwards extending wall structure and terminated above the sea level, forming a structurally integrated part with the upwards extending wall structure.
A tire comprising a tread portion having a tread surface, wherein at least a part of the tread surface of the tread portion has a surface roughness at which the maximum profile peak height Rp specified by JIS B 0601 is 5μm or more and 70μm or less, wherein protrusions each having a hemispherical shape are formed on at least the part of the tread surface, and wherein the protrusions are formed with a height H of more than 20μm in a number density of 80/mm 2 or more on at least the part of the tread surface of the tread portion.
System for providing drilling fluid for earth drilling, wherein the drilling fluid comprises a fluid and at least one mineral, comprising a recycling unit for processing drilling fluid that has been supplied, a mixing unit for mixing drilling fluid processed by the recycling unit with fluid and/or mineral, wherein the mixing unit is coupled with a drilling fluid state meter (4, 5, 6), in order to mix based on the state of the drilling fluid, and a conduit connecting the bore or borehole to the recycling unit, wherein at least one drilling fluid state meter (4, 5, 6) is arranged in the conduit to determine the state of drilling fluid coming from the bore, wherein the system is configured to select the desired state of the drilling fluid depending on the soil and/or the earth drilling device being used, wherein a control is coupled with the drilling fluid state meter (4, 5, 6), with which the mixing unit for providing the desired state of the drilling fluid can be controlled, wherein a conduit is provided which connects the recycling unit and the mixing unit, and a sensor of a drilling fluid state meter is arranged in the conduit, characterized in that the drilling fluid state meter (4, 5, 6) is configured to determine the nature of the soil in which the bore is being made and the control is configured to set the desired state of the drilling fluid based on the soil that has been determined.
A cold formed steel brake piston for a vehicle partial lining disk brake, with a structure in the form of a cup open on one side, comprising a base and a wall, with a groove embossed radially on the outside in the wall, and with a wall bracket embossed radially on the inside on the wall, the wall being profiled at a distance next to the wall bracket with at least one groove and with at least one land in such a way that the wall comprises wall surface areas which have different thicknesses and are spaced apart from one another with an offset in the circumferential direction, characterized in that the grooves and/or lands are provided so as to be spaced apart from one another with an irregular offset on an inner wall of the wall.
An antenna (100, 804), comprising: an enclosure including a front wall and a back wall opposite to the front wall, and a front face and a back face opposite to the front face, wherein both the front face and the back face extend between the front wall and the back wall to form a cavity within the enclosure and wherein the enclosure further includes a slot formed in the front face to form a cavity backed slot; a radio frequency "RF" connector (120, 300) mounted in the front wall; a shaped feed line (122, 600) mounted within the cavity, the shaped feed line (122, 600) being electrically coupled to the RF connector (120, 300) to transmit and receive RF energy, and wherein the shaped feed line (122, 600) extends across the slot to couple the RF energy between the slot and the shaped feed line (122, 600), and wherein the shaped feed line (122, 600) has a predetermined structure to substantially reduce an electric field strength to improve power handling of the antenna (100, 804); characterized in that the antenna comprises a tee section electrically connected to the shaped feed line; and a shunt tuning stub electrically connected to the tee section and to the front wall of the enclosure to short circuit the shunt stub to the front wall, wherein the tee section and the shunt tuning stub include a selected length and diameter to tune the antenna (100, 804) to a desired antenna bandwidth. an enclosure including a front wall and a back wall opposite to the front wall, and a front face and a back face opposite to the front face, wherein both the front face and the back face extend between the front wall and the back wall to form a cavity within the enclosure and wherein the enclosure further includes a slot formed in the front face to form a cavity backed slot; a radio frequency "RF" connector (120, 300) mounted in the front wall; a shaped feed line (122, 600) mounted within the cavity, the shaped feed line (122, 600) being electrically coupled to the RF connector (120, 300) to transmit and receive RF energy, and wherein the shaped feed line (122, 600) extends across the slot to couple the RF energy between the slot and the shaped feed line (122, 600), and wherein the shaped feed line (122, 600) has a predetermined structure to substantially reduce an electric field strength to improve power handling of the antenna (100, 804); characterized in that the antenna comprises a tee section electrically connected to the shaped feed line; and a shunt tuning stub electrically connected to the tee section and to the front wall of the enclosure to short circuit the shunt stub to the front wall, wherein the tee section and the shunt tuning stub include a selected length and diameter to tune the antenna (100, 804) to a desired antenna bandwidth.
Method for generating signals for influencing the movement of a vehicle body, whose movement sequences can be open-loop or closed-loop controlled, of a motor vehicle, wherein the movement of the vehicle body is determined by sensor, the sensor signals corresponding to the determined sensor values are fed to a damper regulator, and the damper regulator supplies at least one control signal for actuating actuators, in particular semi-active or active dampers, by means of which the movement of the vehicle body can be influenced, wherein the at least one control signal for actuating the actuators is determined from the sensor signals taking into account instantaneous and expected driving states and/or load states and/or energy states and/or driver activities as a function of selectable requests with respect to the movement of the vehicle body and driving safety requirements by means of state-dependent regulating algorithms, characterized in that the state-dependent regulating algorithms take into account superordinate messages, wherein diagnostic signals and/or equivalent value signals and/or emergency operation signals are taken into account as superordinate messages.
A winged injection needle comprising an injection needle main body, a base that supports the base end of the injection needle main body, and wings protruding from the base toward the left and right sides, functioning as handles, Comprising the wings constructed with plate members that are freely foldable through hinge sections, so that in the folded state, the wings protrude from the base toward the left and right sides to function as handles, while in the expanded state, the wings extend along the injection needle main body from the base toward the leading edge of the injection needle to function as a safety cover covering the injection needle main body, and injection needle retraction means which causes the injection needle main body to retract from the wings during the procedure of expanding the wings, the wings each comprising a cylinder that fits around the base, a first plate section connected to a front end of the cylinder in a freely foldable manner through a first hinge section, a second plate section connected to a tip of the first plate section in a freely foldable manner through a second hinge section, and a tip plate section connected to a tip of the second plate section in a freely foldable manner through a third hinge section, and by valley folding the first hinge sections, mountain folding the second hinge sections and valley folding the third hinge sections, the wings protrude from the base toward the left and right sides with the first plate sections and the second plate sections in a front/back overlapping folded state, to function as handles, while in the expanded state with all of the hinge sections expanded in a linear manner, the first plate sections and second plate sections extend along the injection needle main body from the base toward the leading edge of the injection needle to function as the safety cover covering the injection needle main body, the injection needle retraction means comprising a slide supporting member that supports the base in a freely slidable manner in the direction of retraction by the cylinder of the wings, a spring that energizes the base in the direction of retraction, and an engagement section that engages with and holds the base in a non-rear position, the base and the injection needle main body being forced to retract with respect to the cylinder of the wings in response to release of engagement by the engagement section.
A paddle assembly (1; 11; 31; 51; 71; 91) comprising a paddle (2; 12; 32; 52; 72; 92), said paddle (2; 12; 32; 52; 72; 92) comprising a handle (4; 14; 34; 54; 74; 94), at one end of which a fixed blade (5; 15; 95) is attached and at the opposite end of which a grip member is attached, wherein the paddle assembly (1; 11; 31; 51; 71; 91) further comprises a removable blade (3; 13; 53; 85; 93) and attachment means configured to removably attach the removable blade (3; 13; 53; 85; 93) to the paddle (2; 12; 32; 52; 72; 92) on the end of the handle (4; 14; 34; 54; 74; 94) on the grip member side, such that the paddle assembly (1; 11; 31; 51; 71; 91) is able to adopt a first double-paddle configuration when the removable blade (3; 13; 53; 85; 93) is attached to the end of the handle (4; 14; 34; 54; 74; 94) on the grip member side, characterized in that the attachment means are also configured to removably attach the removable blade (3; 13; 53; 85; 93) to the end of the handle (4; 14; 34; 54; 74; 94) on the fixed blade (5; 15; 95) side, such that the paddle assembly (1; 11; 31; 51; 71; 91) is able to adopt a second single-paddle configuration when the removable blade (3; 13; 53; 85; 93) is attached to the end of the handle (4; 14; 34; 54; 74) on the fixed blade (5; 15; 95) side against the fixed blade (5; 15; 95), and in that, in the second configuration, the lower surface of the removable blade (3; 13; 53; 85; 93) is located against the upper surface of the fixed blade (5; 15; 95) whose shape matches therewith or the upper surface of the removable blade (3; 13; 53; 85; 93) is located against the lower surface of the fixed blade (5; 15; 95) whose shape matches therewith.
A method for anti-ice performance analysis to determine a heating air cycle profile, comprising: cycling a flow of heating air through an aircraft structure; measuring a temperature of the aircraft structure to generate an oscillatory signal; measuring a minimum temperature value of the aircraft structure based on the oscillatory signal; and calculating, by a controller, anti-ice conditions of the aircraft structure based on the minimum temperature value, and characterized by calculating, by the controller, a runback ice thickness on the aircraft structure based on the minimum temperature value; determining, by the controller, whether the calculated runback ice thickness is greater than or equal to a threshold value; wherein the minimum temperature value is the temperature measured at a location corresponding to a coldest location of an aircraft structure, wherein the location corresponds to an exhaust port of heating air within the aircraft structure; and characterized in that calculating the runback ice thickness includes using the minimum temperature value as a constant value signal for simplifying the calculation as a steady state calculation. cycling a flow of heating air through an aircraft structure; measuring a temperature of the aircraft structure to generate an oscillatory signal; measuring a minimum temperature value of the aircraft structure based on the oscillatory signal; and calculating, by a controller, anti-ice conditions of the aircraft structure based on the minimum temperature value, and characterized by calculating, by the controller, a runback ice thickness on the aircraft structure based on the minimum temperature value; determining, by the controller, whether the calculated runback ice thickness is greater than or equal to a threshold value; wherein the minimum temperature value is the temperature measured at a location corresponding to a coldest location of an aircraft structure, wherein the location corresponds to an exhaust port of heating air within the aircraft structure; and characterized in that calculating the runback ice thickness includes using the minimum temperature value as a constant value signal for simplifying the calculation as a steady state calculation.
Measuring insert for determining and/or monitoring a temperature of a medium in a vessel or pipe for insertion into a protective tube which protective tube at least partially protrudes into an inner volume of the vessel or pipe, the measuring insert comprising an elongated tube, and a temperature sensor arranged inside an end region of the elongated tube; characterized in that, the measuring insert further comprises a coupling element fastened to the elongated tube, in the end region in which the temperature sensor is arranged, wherein the coupling element is embodied and/or dimensioned so as to serve for fixing the measuring insert inside the protective tube in a state in which the measuring insert is introduced into the protective tube, wherein the coupling element comprises: - a spring element as a first at least partially elastic and/or deformable element, wherein the spring element comprises a plurality of outward curved bars and at least one ring-shaped connection element, to which the plurality of bars is connected; and fastening means, for fastening the coupling element to the elongated tube, wherein the fastening means comprise at least one ring-shaped element, with an inner diameter corresponding to an outer diameter of the elongated tube. an elongated tube, and a temperature sensor arranged inside an end region of the elongated tube; the measuring insert further comprises a coupling element fastened to the elongated tube, in the end region in which the temperature sensor is arranged, wherein the coupling element is embodied and/or dimensioned so as to serve for fixing the measuring insert inside the protective tube in a state in which the measuring insert is introduced into the protective tube, wherein the coupling element comprises: - a spring element as a first at least partially elastic and/or deformable element, wherein the spring element comprises a plurality of outward curved bars and at least one ring-shaped connection element, to which the plurality of bars is connected; and fastening means, for fastening the coupling element to the elongated tube, wherein the fastening means comprise at least one ring-shaped element, with an inner diameter corresponding to an outer diameter of the elongated tube. - a spring element as a first at least partially elastic and/or deformable element, wherein the spring element comprises a plurality of outward curved bars and at least one ring-shaped connection element, to which the plurality of bars is connected;
A vortex flow type water surface control device for a draining device that includes an inflow pipe, an outflow pipe, an intercepting pipe, and a separating weir that is disposed to block said intercepting pipe and said inflow pipe from said outflow pipe, comprising a control plate that is disposed between an opening of said inflow pipe and an opening of said intercepting pipe, the height of the control plate being higher than at least the height of said separating weir, characterized in that said control plate is located between said inflow pipe and said intercepting pipe and positioned such that when a flow passes from said inflow pipe to said intercepting pipe, said flow passes between said control plate and said weir, thereby generating a vortex flow on a rear surface of said control plate.
A microfluidic cell culture device comprising: a medium inlet structure comprising a fluidic medium inlet and a plurality of fluidically connected microfluidic medium channels; and a cell culture inlet structure comprising a fluidic medium output and a plurality of fluidically connected microfluidic cell culture channels; wherein an artificial sinusoid channel wall has been formed, which separates the microfluidic medium channels from the microfluidic cell culture channels, the channel wall having a plurality of narrow fluidic passages allowing fluidic flow between the microfluidic medium channels and the microfluidic cell culture channels; wherein the fluidic medium output also functions as a fluidic cellular inlet. a medium inlet structure comprising a fluidic medium inlet and a plurality of fluidically connected microfluidic medium channels; and a cell culture inlet structure comprising a fluidic medium output and a plurality of fluidically connected microfluidic cell culture channels; wherein an artificial sinusoid channel wall has been formed, which separates the microfluidic medium channels from the microfluidic cell culture channels, the channel wall having a plurality of narrow fluidic passages allowing fluidic flow between the microfluidic medium channels and the microfluidic cell culture channels; wherein the fluidic medium output also functions as a fluidic cellular inlet.