mhurhangee/ep-ind-claims huggingface dataset:
A device comprising: an input/output, IO, interface to couple the device to a processor over a link; a plurality of processing engines; a plurality of work queues (610, 612, 614, 616) to store descriptors of work to be executed by a processing engine of the device; and an arbiter comprising circuitry to dispatch descriptors in work queues (510, 512) to a processing engine; and configuration registers comprising group configuration registers to store data that controls mapping of the processing engines and work queues (610, 612, 614, 616) into groups (606, 608), each group (606; 608) comprising one or more work queues (610, 612; 614, 616) and one or more processing engines for processing descriptors in the work queues (610, 612; 614, 616) of the group (606; 608), wherein the device further comprises work submission registers to which descriptors are submitted to the device, wherein each work queue (610, 612; 614, 616) can be configured to run in one of two modes, dedicated or shared, and wherein work submission via a non-privileged work submission register is accepted until a number of descriptors in a shared work queue reaches a threshold configured for the shared work queue and work submission via a privileged work submission register is accepted until the shared work queue is full. an input/output, IO, interface to couple the device to a processor over a link; a plurality of processing engines; a plurality of work queues (610, 612, 614, 616) to store descriptors of work to be executed by a processing engine of the device; and an arbiter comprising circuitry to dispatch descriptors in work queues (510, 512) to a processing engine; and configuration registers comprising group configuration registers to store data that controls mapping of the processing engines and work queues (610, 612, 614, 616) into groups (606, 608), each group (606; 608) comprising one or more work queues (610, 612; 614, 616) and one or more processing engines for processing descriptors in the work queues (610, 612; 614, 616) of the group (606; 608), wherein the device further comprises work submission registers to which descriptors are submitted to the device, wherein each work queue (610, 612; 614, 616) can be configured to run in one of two modes, dedicated or shared, and wherein work submission via a non-privileged work submission register is accepted until a number of descriptors in a shared work queue reaches a threshold configured for the shared work queue and work submission via a privileged work submission register is accepted until the shared work queue is full.
A multi-patch threaded fastener comprising: a shank having a threaded portion; and two or more polymer patches disposed on the shank, the two or more polymer patches being formed from a thermoplastic or a thermoset material, the patches being disposed along a length of the shank and spaced along a circumference of a shank such that the threaded portion is exposed between adjacent patches of the two or more patches, wherein the two or more polymer patches are configured to wedge against a mating threaded component to promote contact between non-patched threaded portions of the shank and the mating threaded component to resist removal from the mating threaded component, and characterized in that one patch of the two or more patches has a different size or shape than another patch of the two or more patches. a shank having a threaded portion; and two or more polymer patches disposed on the shank, the two or more polymer patches being formed from a thermoplastic or a thermoset material, the patches being disposed along a length of the shank and spaced along a circumference of a shank such that the threaded portion is exposed between adjacent patches of the two or more patches, wherein the two or more polymer patches are configured to wedge against a mating threaded component to promote contact between non-patched threaded portions of the shank and the mating threaded component to resist removal from the mating threaded component, and characterized in that one patch of the two or more patches has a different size or shape than another patch of the two or more patches.
A punch, for removing hair follicles; the punch comprising: a generally tubular body formed about a generally central axis and extending from a generally tubular body proximal end to a generally tubular body distal end; a generally frustoconical portion, terminating in a generally frustoconical portion distal cutting end; wherein, an outer perimeter of the generally frustoconical portion distal cutting end is defined by a sharp cutting tip which extends and points away from the central axis in angles ranging from 30 degrees to 120 degrees to direct the cutting forces substantially away from hair follicle; wherein the cutting end creates a wound to remove hair follicles; wherein the generally frustoconical portion further comprises a generally frustoconical proximal end having a frustoconical proximal end radius from the generally central axis; wherein the generally frustoconical portion distal cutting end has a frustoconical distal end radius from the generally central axis; and wherein a frustoconical axis ratio between the frustoconical distal end radius and the frustoconical proximal end radius is between about 1:3 and about 1:1.10. a generally tubular body formed about a generally central axis and extending from a generally tubular body proximal end to a generally tubular body distal end; a generally frustoconical portion, terminating in a generally frustoconical portion distal cutting end; wherein, an outer perimeter of the generally frustoconical portion distal cutting end is defined by a sharp cutting tip which extends and points away from the central axis in angles ranging from 30 degrees to 120 degrees to direct the cutting forces substantially away from hair follicle; wherein the cutting end creates a wound to remove hair follicles; wherein the generally frustoconical portion further comprises a generally frustoconical proximal end having a frustoconical proximal end radius from the generally central axis; wherein the generally frustoconical portion distal cutting end has a frustoconical distal end radius from the generally central axis; and wherein a frustoconical axis ratio between the frustoconical distal end radius and the frustoconical proximal end radius is between about 1:3 and about 1:1.10.
A method for preliminary treatment of molten iron by conducting desiliconization and dephosphorization of molten iron with a converter type container wherein molten iron tapped from a blast furnace is first charged into the converter type container to conduct desiliconization and then the molten iron and a part of a slag after the desiliconization are retained in the container to conduct intermediate slag removal and subsequently the molten iron and slag retained in the container after the desiliconization is added with a lime-based flux solvent while blowing oxygen to conduct dephosphorization of the molten iron, wherein not less than 30 mass% of a slag having a slag basicity of not less than 1.2 after the dephosphorization is retained in the converter type container, and then at least untreated molten iron is charged into the container containing the slag after the dephosphorization to conduct desiliconization, and silicon concentration of molten iron at the end of the desiliconization is made to not more than 0.2 mass% and a basicity of the slag after the desiliconization is made to not less than 0.5 but not more than 1.5 and a temperature of the molten iron is made to not lower than 1240°C but not higher than 1400°C, and wherein subsequently dephosphorization is conducted in the same container, wherein an intermediate slag removal of discharging not less than 40 mass% of the slag after the desiliconization from the container is conducted before the dephosphorization.
A flow-restricted compound spray generating device for a faucet having a spout with a spout orifice diameter, comprising: (a) a housing having a water inlet and outlet aligned along a central or spray axis, said housing defining an interior terminating distally at said outlet in a spray face member (120A, 120B) having an interior surface in fluid communication with said housing's inlet and interior and an exterior surface having a central area surrounded by a periphery defining a spray face member peripheral edge; (b) said spray face member including at least a first fluidic circuit oscillator defining geometry (132, 142, 152) including an outlet orifice (138, 148, 158) wherein said first fluidic circuit oscillator defining geometry is molded in-situ into the interior surface of said spray face member's central area and is configured to aim an oscillating spray having a selected oscillating spray thickness distally along the spray axis; and (c) said spray face member also including a plurality of non-oscillating laminar or jet spray generating orifices (160A, 160B) arrayed evenly around said spray face member's periphery to aim a plurality of non-oscillating laminar or jet sprays distally along an axis which is either parallel to or slightly diverging from the spray axis, wherein the plurality of non-oscillating laminar or jet sprays distally along said axes which are either parallel to or slightly diverging from the spray axis define a plurality of high velocity streams arrayed along the axes which define a ring of spray with a diameter which is substantially equal to the spout orifice diameter, and wherein the oscillating spray's oscillating spray thickness is substantially equal to the spout orifice diameter when viewed from a user's perspective, so that a compound flow is generated having an apparent outflow which has a pleasing spray density with an apparent outflow thickness which is substantially equal to or larger than the spout orifice's diameter. (a) a housing having a water inlet and outlet aligned along a central or spray axis, said housing defining an interior terminating distally at said outlet in a spray face member (120A, 120B) having an interior surface in fluid communication with said housing's inlet and interior and an exterior surface having a central area surrounded by a periphery defining a spray face member peripheral edge; (b) said spray face member including at least a first fluidic circuit oscillator defining geometry (132, 142, 152) including an outlet orifice (138, 148, 158) wherein said first fluidic circuit oscillator defining geometry is molded in-situ into the interior surface of said spray face member's central area and is configured to aim an oscillating spray having a selected oscillating spray thickness distally along the spray axis; and (c) said spray face member also including a plurality of non-oscillating laminar or jet spray generating orifices (160A, 160B) arrayed evenly around said spray face member's periphery to aim a plurality of non-oscillating laminar or jet sprays distally along an axis which is either parallel to or slightly diverging from the spray axis,
Method for manufacturing insulation panels that comprise a foam core with a rigid complete or partial shell, wherein an extrusion of panel material, that comprises the said core and the said shell, is first manufactured, from which insulation panels are then separated, whereby the extrusion is manufactured in a continuous way by the shell being formed by an extrusion process, whereby this shell is provided with an opening during or after extrusion, whereby a liquid foam-forming substance is then introduced into the shell via this opening, after which the shell with the foam-forming substance is exposed to conditions that enable the foam to form and harden, so as to form the core, and is calibrated, whereby after the liquid foam-forming substance has been introduced into the shell through the opening, the opening in the shell provided with the foam-forming substance or foam is closed, whereby the opening in the shell is obtained by a closed shell being extruded, and an opening is made in the shell after extrusion, whereby the shell is extruded in a size that is larger than necessary for the shell of the insulation panel, whereby the size of the shell is reduced because the opening is made by cutting open the extruded shell, whereby a quantity of material is removed from the shell.
A tool system for handling a dry tube in a nuclear reactor including a plurality of fuel assemblies arranged under a top guide having a grid shape inside the nuclear reactor, the system comprising: a body; and a moveable retainer shaped to selectively secure to the dry tube from the single opening so as to move the dry tube without intersecting one of the fuel assemblies in other openings directly adjacent to the dry tube; wherein the body comprises: a transverse cross-section shaped to the top guide such that the body fits in a single quadrant of an opening in the top guide; and a plurality of wings attached to the body; characterized in that the plurality of wings are shaped to fit around two separate sides of the grid at a top end of the top guide. a body; and a moveable retainer shaped to selectively secure to the dry tube from the single opening so as to move the dry tube without intersecting one of the fuel assemblies in other openings directly adjacent to the dry tube; wherein the body comprises: a transverse cross-section shaped to the top guide such that the body fits in a single quadrant of an opening in the top guide; and a plurality of wings attached to the body; characterized in that the plurality of wings are shaped to fit around two separate sides of the grid at a top end of the top guide. a transverse cross-section shaped to the top guide such that the body fits in a single quadrant of an opening in the top guide; and a plurality of wings attached to the body; characterized in that the plurality of wings are shaped to fit around two separate sides of the grid at a top end of the top guide.
A dynamic support apparatus comprising: a cushion; at least one actuator wherein the at least one actuator defines an interior volume and wherein the interior volume may be configured to be at least partially filled with a fluid; a support disposed in the interior volume wherein the support configured to support an occupant when the interior volume is not filled with fluid sufficient to support the occupant; and wherein the at least one actuator comprises pleated walls and includes a first side and opposing second side connected by a side wall, wherein the first side is thicker than the side wall. a cushion; at least one actuator wherein the at least one actuator defines an interior volume and wherein the interior volume may be configured to be at least partially filled with a fluid; a support disposed in the interior volume wherein the support configured to support an occupant when the interior volume is not filled with fluid sufficient to support the occupant; and wherein the at least one actuator comprises pleated walls and includes a first side and opposing second side connected by a side wall, wherein the first side is thicker than the side wall.
A confectionery comprising a sweetener composition, the sweetener composition comprising at least one encapsulated compound wherein the at least one encapsulated compound is selected from the group consisting of rebaudioside A, rebaudioside D, rebaudioside M, and combinations thereof, and wherein the encapsulating material of the at least one encapsulated compound is selected from the group consisting of hydroxyl methyl cellulose, hydroxypropyl methylcellulose (HPMC), microcrystalline cellulose, carboxymethyl cellulose, ethylcellulose, and combinations thereof, wherein the confectionery is a chewing gum or a chewy confection, and wherein the sweetener composition is added to provide an amount from 0.2 to 0.4 wt% of rebaudioside A, rebaudioside D, rebaudioside M and combinations thereof in the chewing gum or chewy confection.
A probe head (12; 112; 312) of an air data probe, the probe head comprising: a unitary body (22; 122; 322) extending from a first end (18; 118; 318) to a second end (20; 120; 320) of the probe head, the body comprising: an inlet (28; 128; 328) adjacent the first end of the probe head; an air passageway (30; 130; 330) extending through the body from the inlet to the second end of the probe head; characterized by a water dam (32; 132; 332) extending radially through the body such that the air passageway is redirected around the water dam; and a plurality of heater bores (34; 134A, 134B; 334A, 334B) extending within the body; and a plurality of rod heaters (24; 124A, 124B; 324A, 324B),, each heater rod being positioned in a heater bore. a unitary body (22; 122; 322) extending from a first end (18; 118; 318) to a second end (20; 120; 320) of the probe head, the body comprising: an inlet (28; 128; 328) adjacent the first end of the probe head; an air passageway (30; 130; 330) extending through the body from the inlet to the second end of the probe head; characterized by a water dam (32; 132; 332) extending radially through the body such that the air passageway is redirected around the water dam; and a plurality of heater bores (34; 134A, 134B; 334A, 334B) extending within the body; and an inlet (28; 128; 328) adjacent the first end of the probe head; an air passageway (30; 130; 330) extending through the body from the inlet to the second end of the probe head; characterized by a water dam (32; 132; 332) extending radially through the body such that the air passageway is redirected around the water dam; and a plurality of heater bores (34; 134A, 134B; 334A, 334B) extending within the body; and a plurality of rod heaters (24; 124A, 124B; 324A, 324B),, each heater rod being positioned in a heater bore.
A container-handling vehicle for picking up storage containers from a three-dimensional grid of an underlying storage system, comprising a vehicle body and at least one lifting device, wherein the lifting device comprises a lifting shaft assembly (47,47') comprising a lifting shaft (22,22') and at least one motor (23,76, 76') for rotating the lifting shaft (22,22'), a lifting frame (17,17') for releasably connecting a storage container, and a first pair of lifting bands and a second pair of lifting bands connecting the lifting shaft to the lifting frame, wherein - the lifting shaft (22,22') comprises a first end section and a second end section; - each lifting band (16a, 16b) has a first end and a second end connected to the lifting shaft and a corresponding lifting band connector (32,32') on the lifting frame, respectively; - each pair of lifting bands (16a,16b) has a first lifting band connected at the first end section of the lifting shaft and a second lifting band connected at the second end section of the lifting shaft; - the first pair of lifting bands extends in a substantially horizontal direction from the lifting shaft towards a band guiding assembly (31,53), the band guiding assembly is arranged to change the direction of the first pair of lifting bands to extend in a vertical direction; characterized in that, the second pair of lifting bands extends in a vertical direction from the lifting shaft (22,22') at the side of the lifting shaft facing away from the band guiding assembly (31,53), and the connections between the first ends of the first pair of lifting bands and the lifting shaft is staggered by 75-105 degrees relative the connections between the first ends of the second pair of lifting bands and the lifting shaft. - the lifting shaft (22,22') comprises a first end section and a second end section; - each lifting band (16a, 16b) has a first end and a second end connected to the lifting shaft and a corresponding lifting band connector (32,32') on the lifting frame, respectively; - each pair of lifting bands (16a,16b) has a first lifting band connected at the first end section of the lifting shaft and a second lifting band connected at the second end section of the lifting shaft; - the first pair of lifting bands extends in a substantially horizontal direction from the lifting shaft towards a band guiding assembly (31,53), the band guiding assembly is arranged to change the direction of the first pair of lifting bands to extend in a vertical direction;
A blower system for a gas turbine engine, the blower system comprising: a rotor assembly configured to be mechanically coupled to a spool of the gas turbine engine; an airframe port configured to receive and discharge air to an airframe system; wherein the blower system is configured to operate in an engine drive mode in which air received from the airframe port drives a rotor of the rotor assembly to rotate the spool, and in a blower mode in which the spool drives the rotor to discharge air to the airframe port; and a routing-control valve comprising: a primary channel for bidirectional flow between the rotor assembly and the airframe port; a primary valve member configured to open and close the primary channel; an auxiliary channel (461, 462) branched from the primary channel and configured to bypass the primary valve member for: a first auxiliary flow from the airframe port to the rotor assembly; or a second auxiliary flow for purging air from the rotor assembly to a discharge port. a rotor assembly configured to be mechanically coupled to a spool of the gas turbine engine; an airframe port configured to receive and discharge air to an airframe system; wherein the blower system is configured to operate in an engine drive mode in which air received from the airframe port drives a rotor of the rotor assembly to rotate the spool, and in a blower mode in which the spool drives the rotor to discharge air to the airframe port; and a routing-control valve comprising: a primary channel for bidirectional flow between the rotor assembly and the airframe port; a primary valve member configured to open and close the primary channel; an auxiliary channel (461, 462) branched from the primary channel and configured to bypass the primary valve member for: a first auxiliary flow from the airframe port to the rotor assembly; or a second auxiliary flow for purging air from the rotor assembly to a discharge port. a primary channel for bidirectional flow between the rotor assembly and the airframe port; a primary valve member configured to open and close the primary channel; an auxiliary channel (461, 462) branched from the primary channel and configured to bypass the primary valve member for: a first auxiliary flow from the airframe port to the rotor assembly; or a second auxiliary flow for purging air from the rotor assembly to a discharge port. a first auxiliary flow from the airframe port to the rotor assembly; or a second auxiliary flow for purging air from the rotor assembly to a discharge port.
Steel support profile for support structures for facades or conservatories, in which a receiving channel is formed for receiving fastening screws for fastening retaining profiles by an outwardly facing side wall of the steel support profile, wherein the side wall is inserted between two longitudinal walls of a base profile which are parallel to one another and spaced apart from one another and the side wall comprises two ends which are bent over and come to bear on the inside of the two longitudinal walls of the base profile, characterised in that the side wall is welded to the base profile by means of weld seams and grooves are formed at the junctions between the side wall and the inside of the two longitudinal walls of the base profile, into which grooves the weld seams are secured.