mhurhangee/ep-ind-claims huggingface dataset:
High temperature thermal barrier coating for the protection of thermally loaded components (10, 10') of a thermal machine, especially a gas turbine, said thermal barrier coating consists of a stabilized ZrO 2 composition, characterized in that said composition is stabilized with at least 15 mol% Y 1+ν Ta 1-ν O 4-ν, the ZrO 2 is partially substituted by at least 10 mol% HfO 2 and the composition is a stable tetragonal zirconia composition, which is established according to the formula Y 1 + v ⁢ Ta 1 - v ⁢ O 4 - v z ⁢ Zr 1 - x ⁢ Hf x ⁢ O 2 1 - z, with x ranging from 0.1 to 0.5, ν ranging from -0.1 to 0.2 and z ranging from 0,15 to 025.
Method for an automatic channel selection in a wireless network, the method comprising the steps of: A) building a list of available candidate communication channels; B) performing measurements for each candidate channel in the list, by calculating: ∘ adjacent channel interference; ∘ channel composite noise score, which aggregates all noise contributions of the channel, including background noise and channel interference; C) excluding candidate channels, for which either the adjacent channel interference or the channel composite noise score are off by a selected threshold from the reference values; the method being characterised in that it further comprises the steps of: D) selecting, among the remaining candidate channels, the channel where the least number of other operating devices is detected, E) iteratively performing at least one measurement on the operating channel, without breaking transmissions; F) updating a channel score, based on said measures, and storing the best score; G) comparing the current channel score and best channel score and if their difference is over a predefined threshold, executing the automatic channel selection according to steps A-D; H) if after the automatic channel selection process, the same channel is chosen preventing said iterative measurements; I) whereas in order to avoid an excessive number of automatic channel selection triggers a trigger-limiter is applied allowing for a maximum number of triggers in a given period. A) building a list of available candidate communication channels; B) performing measurements for each candidate channel in the list, by calculating: ∘ adjacent channel interference; ∘ channel composite noise score, which aggregates all noise contributions of the channel, including background noise and channel interference; ∘ adjacent channel interference; ∘ channel composite noise score, which aggregates all noise contributions of the channel, including background noise and channel interference; C) excluding candidate channels, for which either the adjacent channel interference or the channel composite noise score are off by a selected threshold from the reference values; D) selecting, among the remaining candidate channels, the channel where the least number of other operating devices is detected, E) iteratively performing at least one measurement on the operating channel, without breaking transmissions; F) updating a channel score, based on said measures, and storing the best score; G) comparing the current channel score and best channel score and if their difference is over a predefined threshold, executing the automatic channel selection according to steps A-D; H) if after the automatic channel selection process, the same channel is chosen preventing said iterative measurements; I) whereas in order to avoid an excessive number of automatic channel selection triggers a trigger-limiter is applied allowing for a maximum number of triggers in a given period.
Blade ring for an axial turbomachine, comprising a blade carrier having a number of retaining grooves - having support flanks - for blades and a corresponding number of blades, the blade roots of which, which are configured in a manner corresponding to the retaining grooves, are inserted into the retaining grooves, wherein at least one of the blades, preferably all of the blades, has or have, on the blade root underside thereof facing toward a groove base of the retaining groove, a recess, the base of which is at least partially obliquely inclined with respect to the groove base of the retaining groove and in which there is arranged in each case a wedge-shaped clamping element for pressing the blade root against the support flanks, characterized in that each recess is provided with a spring element, the spring force of which acts along the retaining groove on the respective wedge-shaped clamping element, in that the recess is delimited by a first side wall and a second side wall located opposite the first side wall, wherein the spring element is supported on the one hand on the first side wall and on the other hand on an obtuse end of the wedge-shaped clamping element, and in that provision is made of means with which, for mounting the blade in the retaining groove without prestress, the wedge-shaped clamping element can be displaced temporarily into a position in which the blade root sits in the retaining groove without prestress.
A floating wind turbine assembly for generating electricity, comprising: a turbine wheel support including a floatable support, a turbine wheel mounted on said turbine wheel support, said turbine wheel including an axle structure and being rotatable about said axle structure about a central axis, an electrical generator mounted in registration with said turbine wheel for generating electricity in response to the rotation of said turbine wheel, and an anchor line for holding said turbine wheel against the on-coming atmospheric wind, characterized by said anchor line being connected to said axle structure, said turbine wheel including a circular rim concentric with and rotatable about said central axis, sail wings mounted to said circular rim and extending radially toward said central axis, said sail wings including a pitch that induces said sail wings to rotate about said central axis in response to atmospheric wind moving about said sail wings, and said electrical generator being mounted in engagement with said circular perimeter rim for generating electricity in response to the rotation of said circular perimeter rim. a turbine wheel support including a floatable support, a turbine wheel mounted on said turbine wheel support, said turbine wheel including an axle structure and being rotatable about said axle structure about a central axis, an electrical generator mounted in registration with said turbine wheel for generating electricity in response to the rotation of said turbine wheel, and an anchor line for holding said turbine wheel against the on-coming atmospheric wind, characterized by said anchor line being connected to said axle structure, said turbine wheel including a circular rim concentric with and rotatable about said central axis, sail wings mounted to said circular rim and extending radially toward said central axis, said sail wings including a pitch that induces said sail wings to rotate about said central axis in response to atmospheric wind moving about said sail wings, and said electrical generator being mounted in engagement with said circular perimeter rim for generating electricity in response to the rotation of said circular perimeter rim.
A device for fixing a cable in place on a cable outlet connector, consisting of a clamping sleeve, a spring element, and a locking ring, characterized in that • the spring element comprises at least one locking hook • which can be inserted into a peripheral groove of the cable outlet connector by a relative movement of the locking ring in relation to the clamping sleeve, • and in that upon rotation of the locking ring into an end position of a first direction, the locking hooks of the spring element are fully inserted into the peripheral groove of the cable outlet connector, so that the clamping sleeve is captively held on the cable outlet connector. • the spring element comprises at least one locking hook • which can be inserted into a peripheral groove of the cable outlet connector by a relative movement of the locking ring in relation to the clamping sleeve, • and in that upon rotation of the locking ring into an end position of a first direction, the locking hooks of the spring element are fully inserted into the peripheral groove of the cable outlet connector, so that the clamping sleeve is captively held on the cable outlet connector.
A block piece for holding an optical workpiece, in particular a spectacle lens, for processing thereof, comprising: a basic body having a central axis, a workpiece mounting face portion against which the workpiece can be blocked by means of a blocking material, and a clamping portion via which the workpiece blocked on said basic body can be fixed in a machine or apparatus for processing of the workpiece; characterized in that said clamping portion of said basic body comprises at least one radially extending clamping protrusion that has two opposed side faces each facing in the circumferential direction, for application of clamping forces that are directed essentially in a circumferential direction with respect to the central axis of said basic body. a basic body having a central axis, a workpiece mounting face portion against which the workpiece can be blocked by means of a blocking material, and a clamping portion via which the workpiece blocked on said basic body can be fixed in a machine or apparatus for processing of the workpiece; a central axis, a workpiece mounting face portion against which the workpiece can be blocked by means of a blocking material, and a clamping portion via which the workpiece blocked on said basic body can be fixed in a machine or apparatus for processing of the workpiece; characterized in that said clamping portion of said basic body comprises at least one radially extending clamping protrusion that has two opposed side faces each facing in the circumferential direction, for application of clamping forces that are directed essentially in a circumferential direction with respect to the central axis of said basic body.
A system for inserting a needle into a subject, said insertion system comprising: a capture unit comprising a capture unit mechanism configured for alternately releasing and gripping either said needle or a holder configured for holding said needle; a controllable drive mechanism adapted to insert said needle into the subject in a series of separate insertion steps, said controllable drive mechanism being synchronized with said capture unit mechanism such that said capture unit grips said needle or said holder during an insertion step, and releases said needle or said holder between insertion steps; and a breathing monitoring system configured to monitor the subject's breathing cycles, said breathing monitoring system comprising either a breathing tracking sensor or a signal obtained from a ventilator; wherein: said insertion system comprises a tracking system configured to determine the position of said needle or said holder relative to said capture unit, and said insertion system is configured to correlate the position of said capture unit mechanism to the position of said needle or said holder, using said tracking system, and to synchronize the releasing and gripping of said needle or said holder with the subject's breathing cycle, such that the insertion steps are performed in the same part of each breathing cycle of the subject. a capture unit comprising a capture unit mechanism configured for alternately releasing and gripping either said needle or a holder configured for holding said needle; a controllable drive mechanism adapted to insert said needle into the subject in a series of separate insertion steps, said controllable drive mechanism being synchronized with said capture unit mechanism such that said capture unit grips said needle or said holder during an insertion step, and releases said needle or said holder between insertion steps; and a breathing monitoring system configured to monitor the subject's breathing cycles, said breathing monitoring system comprising either a breathing tracking sensor or a signal obtained from a ventilator; wherein: said insertion system comprises a tracking system configured to determine the position of said needle or said holder relative to said capture unit, and said insertion system is configured to correlate the position of said capture unit mechanism to the position of said needle or said holder, using said tracking system, and to synchronize the releasing and gripping of said needle or said holder with the subject's breathing cycle, such that the insertion steps are performed in the same part of each breathing cycle of the subject. said insertion system comprises a tracking system configured to determine the position of said needle or said holder relative to said capture unit, and said insertion system is configured to correlate the position of said capture unit mechanism to the position of said needle or said holder, using said tracking system, and to synchronize the releasing and gripping of said needle or said holder with the subject's breathing cycle, such that the insertion steps are performed in the same part of each breathing cycle of the subject.
A chimeric polypeptide comprising (i) a muralytic domain having at least 90% identity to amino acids 669-808 of SEQ ID NO:1; and (ii) a heterologous cell binding domain that binds to a target bacterium, said chimeric polypeptide having bactericidal activity. (i) a muralytic domain having at least 90% identity to amino acids 669-808 of SEQ ID NO:1; and (ii) a heterologous cell binding domain that binds to a target bacterium, said chimeric polypeptide having bactericidal activity.
A mobile terminal comprising: a base body wearable on a user's body; a module body detachably coupled to the base body; a rotary unit coupled to a rear surface of the module body or an upper surface of the base body, the rotary unit comprising a rotary hinge portion provided in a center of the rotary unit; a first coupling portion and a second coupling portion provided in a rear surface of the rotary unit and a front surface of the base body or a front surface of the rotary unit and a rear surface of the module body, respectively, the second coupling portion detachably coupled to the first coupling portion; a bezel provided in an edge portion of a display; and a function display unit output to the bezel, wherein a position of the function display unit is changed to be displayed at the relatively same position in the module body when the module body is rotated. a base body wearable on a user's body; a module body detachably coupled to the base body; a rotary unit coupled to a rear surface of the module body or an upper surface of the base body, the rotary unit comprising a rotary hinge portion provided in a center of the rotary unit; a first coupling portion and a second coupling portion provided in a rear surface of the rotary unit and a front surface of the base body or a front surface of the rotary unit and a rear surface of the module body, respectively, the second coupling portion detachably coupled to the first coupling portion; a bezel provided in an edge portion of a display; and a function display unit output to the bezel,
A reduction gearbox for an aircraft engine, the gearbox comprising: an input pinion configured to be driven by the aircraft engine; an input gear meshed with the input pinion; a drive gear meshed with the input gear; an output pinion characterized by that the reduction gearbox being selectively configurable between an engaged configuration and a disengaged configuration, the input gear and output pinion being drivingly engaged in the engaged configuration, the input gear being rotatable independently of the output pinion in the disengaged configuration; and an output gear meshed with the output pinion, the output gear configured to drive an output shaft of the aircraft engine. an input pinion configured to be driven by the aircraft engine; an input gear meshed with the input pinion; a drive gear meshed with the input gear; an output pinion characterized by that the reduction gearbox being selectively configurable between an engaged configuration and a disengaged configuration, the input gear and output pinion being drivingly engaged in the engaged configuration, the input gear being rotatable independently of the output pinion in the disengaged configuration; and an output gear meshed with the output pinion, the output gear configured to drive an output shaft of the aircraft engine.
A downhole closed loop method for controlling a drilling toolface when drilling a subterranean borehole, the method comprising: (a) drilling the subterranean borehole; (b) receiving a reference attitude of a bottom hole assembly in the subterranean borehole, the reference attitude measured at an upper survey station in the subterranean borehole at a first time; (c) receiving a measured attitude of the bottom hole assembly in the subterranean borehole; the measured attitude measured at a lower survey station in the subterranean borehole at a second time, the second time being later than the first time; (d) processing downhole the reference attitude and the measured attitude to compute an angle change of the subterranean borehole between the upper and lower survey stations; (e) comparing the angle change of the subterranean borehole with a predetermined threshold; (f) repeating (c), (d), and (e) when the angle change of the subterranean borehole is less than the predetermined threshold; (g) processing downhole the reference attitude and the measured attitude to compute a toolface angle when the angle change of the subterranean borehole is greater than or equal to the predetermined threshold; and (h) processing downhole the toolface angle computed in (g) to control a direction of drilling of the subterranean borehole. (a) drilling the subterranean borehole; (b) receiving a reference attitude of a bottom hole assembly in the subterranean borehole, the reference attitude measured at an upper survey station in the subterranean borehole at a first time; (c) receiving a measured attitude of the bottom hole assembly in the subterranean borehole; the measured attitude measured at a lower survey station in the subterranean borehole at a second time, the second time being later than the first time; (d) processing downhole the reference attitude and the measured attitude to compute an angle change of the subterranean borehole between the upper and lower survey stations; (e) comparing the angle change of the subterranean borehole with a predetermined threshold; (f) repeating (c), (d), and (e) when the angle change of the subterranean borehole is less than the predetermined threshold; (g) processing downhole the reference attitude and the measured attitude to compute a toolface angle when the angle change of the subterranean borehole is greater than or equal to the predetermined threshold; and (h) processing downhole the toolface angle computed in (g) to control a direction of drilling of the subterranean borehole.
A system for processing solid materials, the system comprising: a solid material feeder; a reactor having a chamber, a solid material inlet, a gas inlet, and an outlet, the reactor being configured to facilitate chemical reactions and/or comminution of solid feed material using tensive forces of shockwaves created in a supersonic gaseous vortex within the chamber, the solid material feeder being configured to provide solid material into the chamber of the reactor through the solid material inlet, the solid material being processed within the chamber by nonabrasive mechanisms facilitated by the shockwaves within the chamber, the outlet being configured to effectuate a rapid cooling of the processed solid material exiting the reactor to reduce occurrences of back reactions; a gas source configured to introduce a high-velocity stream of gas into the chamber of the reactor through the gas inlet to effectuate the supersonic gaseous vortex within the chamber, wherein the gas inlet includes an inlet nozzle disposed within the gas inlet, the inlet nozzle being configured to emit shock waves in the high-velocity stream of gas introduced by the gas source whereby the high-velocity stream of gas is emitted into the chamber at a supersonic speed; and storage configured to collect processed material that is communicated through the outlet of the reactor. a solid material feeder; a reactor having a chamber, a solid material inlet, a gas inlet, and an outlet, the reactor being configured to facilitate chemical reactions and/or comminution of solid feed material using tensive forces of shockwaves created in a supersonic gaseous vortex within the chamber, the solid material feeder being configured to provide solid material into the chamber of the reactor through the solid material inlet, the solid material being processed within the chamber by nonabrasive mechanisms facilitated by the shockwaves within the chamber, the outlet being configured to effectuate a rapid cooling of the processed solid material exiting the reactor to reduce occurrences of back reactions; a gas source configured to introduce a high-velocity stream of gas into the chamber of the reactor through the gas inlet to effectuate the supersonic gaseous vortex within the chamber, wherein the gas inlet includes an inlet nozzle disposed within the gas inlet, the inlet nozzle being configured to emit shock waves in the high-velocity stream of gas introduced by the gas source whereby the high-velocity stream of gas is emitted into the chamber at a supersonic speed; and storage configured to collect processed material that is communicated through the outlet of the reactor.
A method of operating a filtration system for separating particulate solid matter from a liquid and having a housing having a surface of revolution shaped cavity therein defined around an axis, the cavity housing a filter element and also having a filtrate outlet, an inlet and at least one purge outlet (16, 25), characterized in that the filter element includes a filtration membrane and a support membrane mounted concentrically around the axis with the filtration membrane being rotatably mounted to the housing externally to the support membrane, the filtrate outlet is located inside the filter element, the inlet and the at least one purge outlet (16, 25) are both located outside the filter element; and in that the method comprises: operating the filtration system in a regular filtration mode including simultaneously: feeding an inlet flow rate into the cavity through the inlet; rotating the filtration membrane about the axis, at a rotation speed relative to the support membrane; extracting a filtrate flow rate sequentially across the filter element and the filtrate outlet; and, subsequently temporarily operating the filtration system in a declogging mode including: extracting a greater purge flow rate through the at least one purge outlet (16, 25) than during the regular filtration mode. operating the filtration system in a regular filtration mode including simultaneously: feeding an inlet flow rate into the cavity through the inlet; rotating the filtration membrane about the axis, at a rotation speed relative to the support membrane; extracting a filtrate flow rate sequentially across the filter element and the filtrate outlet; and, subsequently feeding an inlet flow rate into the cavity through the inlet; rotating the filtration membrane about the axis, at a rotation speed relative to the support membrane; extracting a filtrate flow rate sequentially across the filter element and the filtrate outlet; and, subsequently temporarily operating the filtration system in a declogging mode including: extracting a greater purge flow rate through the at least one purge outlet (16, 25) than during the regular filtration mode.