mhurhangee/patent-ind-claim-en huggingface dataset:
A processing system comprising: a processing unit ; a graphics display component comprising a layer selection module , the layer selection module being arranged to, for at least one pixel to be displayed: identify a set M of active layers for the at least one pixel; configure a display controller to generate composite pixel data for the at least one pixel based on a subset N of up to n layers from the set M ; determine whether a number m of active layers in the set M exceeds n ; output an indication of which active layers within the set M were excluded from the subset N , if it is determined that the number m of layers in the set M exceeds n ; a graphics management component arranged to receive the indication that active layers within the set M were excluded from the subset N , and to cause a number k of graphics layers within a set K from which the composite image as a whole is generated to be reduced to form a reduced set K '; wherein the layer selection module is arranged to generate an interrupt signal to the processing unit when the number m of active layers in the set M exceeds the display controller configuration limit n on at least one of a frame basis or a row basis. a processing unit ; a graphics display component comprising a layer selection module , the layer selection module being arranged to, for at least one pixel to be displayed: identify a set M of active layers for the at least one pixel; configure a display controller to generate composite pixel data for the at least one pixel based on a subset N of up to n layers from the set M ; determine whether a number m of active layers in the set M exceeds n ; output an indication of which active layers within the set M were excluded from the subset N , if it is determined that the number m of layers in the set M exceeds n ; identify a set M of active layers for the at least one pixel; configure a display controller to generate composite pixel data for the at least one pixel based on a subset N of up to n layers from the set M ; determine whether a number m of active layers in the set M exceeds n ; output an indication of which active layers within the set M were excluded from the subset N , if it is determined that the number m of layers in the set M exceeds n ; a graphics management component arranged to receive the indication that active layers within the set M were excluded from the subset N , and to cause a number k of graphics layers within a set K from which the composite image as a whole is generated to be reduced to form a reduced set K '; wherein the layer selection module is arranged to generate an interrupt signal to the processing unit when the number m of active layers in the set M exceeds the display controller configuration limit n on at least one of a frame basis or a row basis.
A method of wireless communication by a transmitter , the method comprising: generating , by the transmitter , a reference signal , the reference signal comprising two portions, wherein a first portion of the two portions comprises a preamble having a non-constant envelope for nonlinearity estimation by a receiver , and wherein a second portion of the two portions is separate from the first portion comprising the preamble and wherein the non-constant envelope is absent from the second portion of the reference signal; and wherein generating the reference signal comprises modulating the preamble to have a first dynamic range, the first dynamic range being higher than a second dynamic range of another signal generated by the transmitter having a constant envelope; and transmitting, by the transmitter, the reference signal. generating , by the transmitter , a reference signal , the reference signal comprising two portions, wherein a first portion of the two portions comprises a preamble having a non-constant envelope for nonlinearity estimation by a receiver , and wherein a second portion of the two portions is separate from the first portion comprising the preamble and wherein the non-constant envelope is absent from the second portion of the reference signal; and wherein generating the reference signal comprises modulating the preamble to have a first dynamic range, the first dynamic range being higher than a second dynamic range of another signal generated by the transmitter having a constant envelope; and transmitting, by the transmitter, the reference signal.
A case assembly for a gas turbine engine case, comprising: a flange ; a recess in the flange defined by a spot face ; a jacking insert comprising a back plate disposed in the recess; a threaded cylinder extending from the back plate into the flange ; wherein the recess is surrounded by a D-shaped wall ; the back plate of the jacking insert has a D-shaped geometry, wherein the D-shaped wall is configured to constrain the jacking insert from rotation; a bulkhead is pressed against the flange and covers the spot face ; wherein the back plate 205 of jacking insert 201 is disposed between the bulkhead 216 and the flange 206; and a bolt (202; 224) is configured to pass through the jacking insert and an opening defined by the bulkhead . a flange ; a recess in the flange defined by a spot face ; a jacking insert comprising a back plate disposed in the recess; a threaded cylinder extending from the back plate into the flange ; wherein the recess is surrounded by a D-shaped wall ; the back plate of the jacking insert has a D-shaped geometry, wherein the D-shaped wall is configured to constrain the jacking insert from rotation; a bulkhead is pressed against the flange and covers the spot face ; wherein the back plate 205 of jacking insert 201 is disposed between the bulkhead 216 and the flange 206; and a bolt (202; 224) is configured to pass through the jacking insert and an opening defined by the bulkhead .
A fluid-filled chamber comprising: a first barrier sheet formed from a first thermoplastic material; a second barrier sheet attached to the first barrier sheet and formed from a second thermoplastic material, the first barrier sheet and the second barrier sheet cooperating to define an internal cavity; and a tensile member disposed within the internal cavity and formed from a third thermoplastic material, the tensile member including a plurality of tensile elements each having a longitudinal axis that extends in a direction from the first barrier sheet to the second barrier sheet ; said fluid-filled chamber characterized in that it further comprises a first weld that attaches the first barrier sheet , the second barrier sheet , and the tensile member together by melding the first thermoplastic material of the first barrier sheet , the second thermoplastic material of second barrier sheet , and the third thermoplastic material of the tensile member . a first barrier sheet formed from a first thermoplastic material; a second barrier sheet attached to the first barrier sheet and formed from a second thermoplastic material, the first barrier sheet and the second barrier sheet cooperating to define an internal cavity; and a tensile member disposed within the internal cavity and formed from a third thermoplastic material, the tensile member including a plurality of tensile elements each having a longitudinal axis that extends in a direction from the first barrier sheet to the second barrier sheet ; said fluid-filled chamber characterized in that it further comprises a first weld that attaches the first barrier sheet , the second barrier sheet , and the tensile member together by melding the first thermoplastic material of the first barrier sheet , the second thermoplastic material of second barrier sheet , and the third thermoplastic material of the tensile member .
A summation rocker system for acting on the end of a stem of a poppet valve of an engine in dependence upon the combined lifts of a first and a second cam profile defined by different cam lobes of a concentric camshaft , the system comprising: a first rocker mounted on a pivot shaft and having a first follower to contact the first cam profile and an end acting on the valve to displace the valve by an amount dependent upon the lift of the first cam profile, a rocker shaft to be fixedly mounted on the engine, and a second rocker pivotable about the rocker shaft , the second rocker having a second follower to contact the second cam profile and acting to displace the pivot shaft of the first rocker in dependence of the lift of second cam profile, the rocker shaft intersecting a plane containing the axis of the pivot shaft and the end of the first rocker acting on the valve stem, characterized in that the first rocker includes a cut-out for receiving the rocker shaft , which cut-out is configured and dimensioned to prevent the rocker shaft from interfering with movement of the first rocker . a first rocker mounted on a pivot shaft and having a first follower to contact the first cam profile and an end acting on the valve to displace the valve by an amount dependent upon the lift of the first cam profile, a rocker shaft to be fixedly mounted on the engine, and a second rocker pivotable about the rocker shaft , the second rocker having a second follower to contact the second cam profile and acting to displace the pivot shaft of the first rocker in dependence of the lift of second cam profile, the rocker shaft intersecting a plane containing the axis of the pivot shaft and the end of the first rocker acting on the valve stem, characterized in that the first rocker includes a cut-out for receiving the rocker shaft , which cut-out is configured and dimensioned to prevent the rocker shaft from interfering with movement of the first rocker .
A hydrazide functional material represented by the following Formula (I), wherein for Formula (I), n is 2, x is 0 and y is 1 for a first n unit and x is 0 or 1, y is 0 or 1, provided that the sum of x and y is 1 for a second n unit, L 1 , independently for each n, is selected from a divalent hydrocarbyl group optionally interrupted with at least one of -O- and -S-, L 2 , independently for each n, is selected from a divalent hydrocarbyl group, and R 1 , independently for each n, is selected from hydrogen and hydrocarbyl. n is 2, x is 0 and y is 1 for a first n unit and x is 0 or 1, y is 0 or 1, provided that the sum of x and y is 1 for a second n unit, L 1 , independently for each n, is selected from a divalent hydrocarbyl group optionally interrupted with at least one of -O- and -S-, L 2 , independently for each n, is selected from a divalent hydrocarbyl group, and R 1 , independently for each n, is selected from hydrogen and hydrocarbyl.
A method of degrading cannabinoid by a photocatalytic reaction on a solution containing cannabinoid using a photocatalyst, wherein the cannabinoid comprises one or a combination or two or more of tetrahydrocannabinol THC, cannabinol CBD, cannabigerol CBG, cannabichromene CBC, cannabinol CBN, and propyl homologues Δ9-tetrahydrocannabivarin THCV and cannabidivarin CBDV; wherein the method comprises the following steps: placing the liquid containing cannabinoid in a container equipped with illuminance equipment, adding a photocatalyst and stirring at room temperature; and standing the liquid in step , and filtering to obtain a filtrate and a filter cake; wherein the illumination equipment in step has an illuminance of 2000~20000 Lx; wherein a mass-volume ratio of an amount of the photocatalyst to the solution containing cannabinoid in step is 5% to 50% in mg/mL; wherein the solution containing cannabinoid is a waste liquid produced in a process of extraction and purification of hemp, wherein the photocatalyst in step is selected from one or a combination of two or more of bismuth vanadate, bismuth oxychloride, bismuth vanadate/titanium dioxide composite, bismuth vanadate/bismuth oxychloride composite, bismuth oxychloride/titanium dioxide composite in any proportion. wherein the method comprises the following steps: placing the liquid containing cannabinoid in a container equipped with illuminance equipment, adding a photocatalyst and stirring at room temperature; and standing the liquid in step , and filtering to obtain a filtrate and a filter cake; placing the liquid containing cannabinoid in a container equipped with illuminance equipment, adding a photocatalyst and stirring at room temperature; and standing the liquid in step , and filtering to obtain a filtrate and a filter cake; wherein the illumination equipment in step has an illuminance of 2000~20000 Lx; wherein a mass-volume ratio of an amount of the photocatalyst to the solution containing cannabinoid in step is 5% to 50% in mg/mL; wherein the solution containing cannabinoid is a waste liquid produced in a process of extraction and purification of hemp, wherein the photocatalyst in step is selected from one or a combination of two or more of bismuth vanadate, bismuth oxychloride, bismuth vanadate/titanium dioxide composite, bismuth vanadate/bismuth oxychloride composite, bismuth oxychloride/titanium dioxide composite in any proportion.
A torque tube assembly comprising: a torque tube comprising a barrel portion disposed between a flange and a back leg , the flange extending radially inward towards an axis of rotation and the back leg extending radially outward from the barrel portion ; a channel defined by a channel wall and disposed in the flange and in the inner diameter of the barrel portion , the channel being configured to receive a sacrificial member ; and a sacrificial member disposed in the channel . a torque tube comprising a barrel portion disposed between a flange and a back leg , the flange extending radially inward towards an axis of rotation and the back leg extending radially outward from the barrel portion ; a channel defined by a channel wall and disposed in the flange and in the inner diameter of the barrel portion , the channel being configured to receive a sacrificial member ; and a sacrificial member disposed in the channel .
A method of forming a flexible annular seal for a moveable thrust assembly of a rocket motor assembly comprising: selecting a first silicone material; selecting a second silicone material; combining the first silicone material and the second silicone material with at least one curing/crosslinking agent to form a polysiloxane composition including the first silicone material, the second silicone material, and the at least one curing/crosslinking agent, the at least one curing/crosslinking agent being selected from dicumyl peroxide and bis (2,4-dischlorobenzoyl)-peroxide; forming a preliminary structure having an annular shape from the polysiloxane composition; and curing the preliminary structure to form a cured structure comprising a cured polysiloxane composition, wherein the curing comprises subjecting the preliminary structure to a temperature within a range of from about 50°C to 300°C for a period of time within a range of from 5 minutes to 10 hours; the method characterized by ; forming the polysiloxane composition to be homogeneous, including a uniform dispersion of the first silicone material, the second silicone material, and the at least one curing/crosslinking agent; and forming the cured structure, the cured polysiloxane composition comprising crosslinked polysiloxane chains of the first silicone material and the second silicone material. selecting a first silicone material; selecting a second silicone material; combining the first silicone material and the second silicone material with at least one curing/crosslinking agent to form a polysiloxane composition including the first silicone material, the second silicone material, and the at least one curing/crosslinking agent, the at least one curing/crosslinking agent being selected from dicumyl peroxide and bis (2,4-dischlorobenzoyl)-peroxide; forming a preliminary structure having an annular shape from the polysiloxane composition; and curing the preliminary structure to form a cured structure comprising a cured polysiloxane composition, wherein the curing comprises subjecting the preliminary structure to a temperature within a range of from about 50°C to 300°C for a period of time within a range of from 5 minutes to 10 hours; the method characterized by ; forming the polysiloxane composition to be homogeneous, including a uniform dispersion of the first silicone material, the second silicone material, and the at least one curing/crosslinking agent; and forming the cured structure, the cured polysiloxane composition comprising crosslinked polysiloxane chains of the first silicone material and the second silicone material.
An article carrying apparatus comprising: a plurality of carrier lanes each for receiving and conveying a number of articles ; one or more diverters arranged to control the distribution of received articles into each of the plurality of carrier lanes , characterised in that the one or more diverters being positioned at a receiving end of the carrier lanes and between adjacent carrier lanes, the diverters being individually controllable to rotate so that an input channel for a carrier lane can be enlarged or restricted by adjusting adjacent diverters in order to increase or reduce a flow of articles to the carrier lane; a sensor arranged to determine a capacity use parameter for each carrier lane ; and a controller arranged to control the position of the one or more diverters dependent on the determined capacity use parameters. a plurality of carrier lanes each for receiving and conveying a number of articles ; one or more diverters arranged to control the distribution of received articles into each of the plurality of carrier lanes , characterised in that the one or more diverters being positioned at a receiving end of the carrier lanes and between adjacent carrier lanes, the diverters being individually controllable to rotate so that an input channel for a carrier lane can be enlarged or restricted by adjusting adjacent diverters in order to increase or reduce a flow of articles to the carrier lane; a sensor arranged to determine a capacity use parameter for each carrier lane ; and a controller arranged to control the position of the one or more diverters dependent on the determined capacity use parameters.
A redundant coupling arrangement , comprising: a first member defining a first axis ; a second member defining a second axis being in operable communication with the first member ; a first torque transmitting arrangement configured to transfer torque between the first member and the second member while allowing at least one of axial displacement between the first member and the second member and angular misalignment of the first axis relative to the second axis ; a second torque transmitting arrangement configured to transfer torque between the first member and the second member while allowing at least one of axial displacement between the first member and the second member and angular misalignment of the first axis relative to the second axis ; characterized in that the second torque transmitting arrangement includes a spherical body disposed within a collar, wherein the collar is fixed in rotation relative to one of the first member and the second member, wherein the spherical body is fixed relative to the other of the first member and the second member; and wherein the spherical body has a plurality of external splines distributed circumferentially about a radially outer surface of the spherical body. a first member defining a first axis ; a second member defining a second axis being in operable communication with the first member ; a first torque transmitting arrangement configured to transfer torque between the first member and the second member while allowing at least one of axial displacement between the first member and the second member and angular misalignment of the first axis relative to the second axis ; a second torque transmitting arrangement configured to transfer torque between the first member and the second member while allowing at least one of axial displacement between the first member and the second member and angular misalignment of the first axis relative to the second axis ; characterized in that the second torque transmitting arrangement includes a spherical body disposed within a collar, wherein the collar is fixed in rotation relative to one of the first member and the second member, wherein the spherical body is fixed relative to the other of the first member and the second member; and wherein the spherical body has a plurality of external splines distributed circumferentially about a radially outer surface of the spherical body.
A gas turbine engine comprising: an engine core and a fan driven by the engine core ; a nacelle radially surrounding the engine core and the fan , the nacelle comprising: a ring shaped body defining a center axis and having a radially outward surface and a radially inward surface; an aft portion of the radially inward surface including an axially extending convergent-divergent exit nozzle ; and an axially extending secondary circumferential ring duct (180;280;380;480;580) passing through said nacelle in said convergent-divergent exit nozzle radially outward of the radially inward surface, the axially extending secondary duct (180;280;380;480;580) including an inlet (281;381;481;581) at a convergent portion (136;236;336;436;536) of the convergent-divergent exit nozzle and an outlet (190;290;390;490;590) at a divergent portion (138;238;338;438;538) of the convergent-divergent exit nozzle ; wherein the nacelle defines a bypass passage having the convergent-divergent exit nozzle , wherein the convergent-divergent exit nozzle further includes a primary passage. an engine core and a fan driven by the engine core ; a nacelle radially surrounding the engine core and the fan , the nacelle comprising: a ring shaped body defining a center axis and having a radially outward surface and a radially inward surface; an aft portion of the radially inward surface including an axially extending convergent-divergent exit nozzle ; and an axially extending secondary circumferential ring duct (180;280;380;480;580) passing through said nacelle in said convergent-divergent exit nozzle radially outward of the radially inward surface, the axially extending secondary duct (180;280;380;480;580) including an inlet (281;381;481;581) at a convergent portion (136;236;336;436;536) of the convergent-divergent exit nozzle and an outlet (190;290;390;490;590) at a divergent portion (138;238;338;438;538) of the convergent-divergent exit nozzle ; wherein the nacelle defines a bypass passage having the convergent-divergent exit nozzle , wherein the convergent-divergent exit nozzle further includes a primary passage. a ring shaped body defining a center axis and having a radially outward surface and a radially inward surface; an aft portion of the radially inward surface including an axially extending convergent-divergent exit nozzle ; and an axially extending secondary circumferential ring duct (180;280;380;480;580) passing through said nacelle in said convergent-divergent exit nozzle radially outward of the radially inward surface, the axially extending secondary duct (180;280;380;480;580) including an inlet (281;381;481;581) at a convergent portion (136;236;336;436;536) of the convergent-divergent exit nozzle and an outlet (190;290;390;490;590) at a divergent portion (138;238;338;438;538) of the convergent-divergent exit nozzle ; wherein the nacelle defines a bypass passage having the convergent-divergent exit nozzle , wherein the convergent-divergent exit nozzle further includes a primary passage.