mhurhangee/ep-ind-claims huggingface dataset:
A method performed by a terminal in a communication system, the method comprising: receiving, from a base station, a radio resource control, RRC, message comprising information on a normal resource pool; based on the terminal receiving information on an exceptional resource pool and a sensing result on the normal resource pool being not available, randomly selecting a resource from the exceptional resource pool, wherein the resource from the exceptional resource pool is for transmitting a scheduling assignment, SA, and data corresponding to the SA to another terminal; and transmitting the SA and the data based on the randomly selected resource from the exceptional resource pool. receiving, from a base station, a radio resource control, RRC, message comprising information on a normal resource pool; based on the terminal receiving information on an exceptional resource pool and a sensing result on the normal resource pool being not available, randomly selecting a resource from the exceptional resource pool, wherein the resource from the exceptional resource pool is for transmitting a scheduling assignment, SA, and data corresponding to the SA to another terminal; and transmitting the SA and the data based on the randomly selected resource from the exceptional resource pool.
A gasket comprising: a sheet-like base material; and a gasket portion which is made of a rubber-like elastic material and is integrally formed on at least one surface of said base material, wherein said gasket portion is constructed by a continuous projection portion which is provided with a fixed pattern, and a positioning projection which is lower than a height of said projection portion is formed on the surface of said base material, characterized in that said positioning projection exists separately from, in a non-integrated state with said projection portion. a sheet-like base material; and a gasket portion which is made of a rubber-like elastic material and is integrally formed on at least one surface of said base material, wherein said gasket portion is constructed by a continuous projection portion which is provided with a fixed pattern, and a positioning projection which is lower than a height of said projection portion is formed on the surface of said base material, characterized in that said positioning projection exists separately from, in a non-integrated state with said projection portion.
A thermoforming machine for containers, comprising a thermoforming station, equipped with a press that is fed by a sheet of previously heated thermoforming material; the sheet being pulled by a chain arranged on guides, and the press being equipped with a head, wherein a piston cap is provided, and a movable table configured to assemble at least one thermoforming mould for inverted conical containers, said thermoforming mould comprising two parts that can be separated when demoulding is carried out by lowering the movable table; characterised in that after the mould, the chain guides have a machining tilted in an upward direction, which creates a break in the sheet so that the previously formed containers tilt, moving them away from the mould and preventing the mould from contacting said previously formed containers when opened.
A vane comprising a wall with an integral longitudinal wall passage formed within the wall, wherein the vane is airfoil shaped, the integral longitudinal wall passage extends in a radial direction relative to the vane, the integral longitudinal wall passage includes an entrance aperture and a multiple of exit apertures, the multiple of exit apertures being transverse to the integral longitudinal wall passage, wherein the multiple of exit apertures are formed directly through the wall and are seal-less, wherein the integral longitudinal wall passage is a fuel passage, characterized in that the wall and the integral longitudinal wall passage are additively manufactured and the integral longitudinal wall passage extends for only a portion of a length of the wall.
A method for executing a smart contract, comprising: receiving, by a blockchain node, a request for creating a smart contract, wherein the request comprises code of the smart contract, and the code of the smart contract comprises hotspot code marked by using a hotspot identifier; identifying non-marked hotspot code other than the hotspot code marked by using the hotspot identifier, and compiling and storing the non-marked hotspot code, in a process of interpreting and executing the code of the smart contract; compiling, by the blockchain node, the code of the smart contract comprising the hotspot code into machine code through Just-In-Time, JIT, compilation after deploying the smart contract, and storing the compiled hotspot code marked by using the hotspot identifier; and executing, by the blockchain node when executing the deployed smart contract, the machine code if the machine code corresponding to the code of the smart contract is locally stored, wherein when executing the deployed smart contract, the blockchain node interprets and executes the code of the smart contract if the machine code of the smart contract is not locally stored, the interpreting and executing comprising: when the blockchain node executes the deployed smart contract, if the machine code of the smart contract is not locally stored, further querying, by the blockchain node, a current JIT compilation status of the code of the smart contract, and if JIT compilation has not been started, starting JIT compilation, and interpreting and executing the code of the smart contract. receiving, by a blockchain node, a request for creating a smart contract, wherein the request comprises code of the smart contract, and the code of the smart contract comprises hotspot code marked by using a hotspot identifier; identifying non-marked hotspot code other than the hotspot code marked by using the hotspot identifier, and compiling and storing the non-marked hotspot code, in a process of interpreting and executing the code of the smart contract; compiling, by the blockchain node, the code of the smart contract comprising the hotspot code into machine code through Just-In-Time, JIT, compilation after deploying the smart contract, and storing the compiled hotspot code marked by using the hotspot identifier; and executing, by the blockchain node when executing the deployed smart contract, the machine code if the machine code corresponding to the code of the smart contract is locally stored, wherein when executing the deployed smart contract, the blockchain node interprets and executes the code of the smart contract if the machine code of the smart contract is not locally stored, the interpreting and executing comprising: when the blockchain node executes the deployed smart contract, if the machine code of the smart contract is not locally stored, further querying, by the blockchain node, a current JIT compilation status of the code of the smart contract, and if JIT compilation has not been started, starting JIT compilation, and interpreting and executing the code of the smart contract.
An apparatus comprising an unmanned aerial vehicle and a multi-tool module (6, 60a, 60b) coupled to the unmanned aerial vehicle, wherein: the unmanned aerial vehicle comprises a body frame, a plurality of rotor motors mounted to the body frame, a plurality of rotors operatively coupled to respective rotor motors of the plurality of rotor motors, and a controller; the multi-tool module (6, 60a, 60b) comprises a hub which is rotatable about an axis of rotation, a plurality of arms (64a-64d, 65) having respective first ends coupled to the hub, a plurality of tools (68, 70, 72, 74) mounted to respective second ends of respective arms of the plurality of arms, and a first motor operatively coupled to drive rotation of the hub, and wherein: the unmanned aerial vehicle further comprises a payload support frame (8, 3) pivotably coupled to the body frame; the multi-tool module (6, 60a, 60b) is attached to the payload support frame (8, 3); and the payload support frame (8, 3) comprises a plurality of surface attachment devices, the controller being configured to activate said surface attachment devices to maintain the UAV stationary on a surface of a structure to be repaired with said surface attachment devices abutting said surface. the unmanned aerial vehicle comprises a body frame, a plurality of rotor motors mounted to the body frame, a plurality of rotors operatively coupled to respective rotor motors of the plurality of rotor motors, and a controller; the multi-tool module (6, 60a, 60b) comprises a hub which is rotatable about an axis of rotation, a plurality of arms (64a-64d, 65) having respective first ends coupled to the hub, a plurality of tools (68, 70, 72, 74) mounted to respective second ends of respective arms of the plurality of arms, and a first motor operatively coupled to drive rotation of the hub, and wherein: the unmanned aerial vehicle further comprises a payload support frame (8, 3) pivotably coupled to the body frame; the multi-tool module (6, 60a, 60b) is attached to the payload support frame (8, 3); and the payload support frame (8, 3) comprises a plurality of surface attachment devices, the controller being configured to activate said surface attachment devices to maintain the UAV stationary on a surface of a structure to be repaired with said surface attachment devices abutting said surface. the unmanned aerial vehicle further comprises a payload support frame (8, 3) pivotably coupled to the body frame; the multi-tool module (6, 60a, 60b) is attached to the payload support frame (8, 3); and the payload support frame (8, 3) comprises a plurality of surface attachment devices, the controller being configured to activate said surface attachment devices to maintain the UAV stationary on a surface of a structure to be repaired with said surface attachment devices abutting said surface.
A method for preparing a multi-layer coating structure slow/controlled-release fertilizer, said multi-layer coating structure slow/controlled release fertilizer comprising a layer-by-layer coated fertilizer layer and a coating layer, wherein the fertilizer layer is separated from the coating layer, the fertilizer layer has at least two layers, the coating layer has at least two layers, and the innermost layer of the fertilizer layers is a fertilizer core; the fertilizer layer includes at least two of nitrogen fertilizer, phosphorus fertilizer and potassium fertilizer, the coating layer is polyurea formaldehyde, wherein the raw materials of the polyurea formaldehyde are urea and formaldehyde, the molar ratio of the urea to the formaldehyde is 1-2.5:1, and the polyurea formaldehyde includes at least a polyurea formaldehyde having two to five carbon atoms, wherein the method comprises steps of: applying the fertilizer layer and the fertilizer corresponding to the coating layer to the periphery of the fertilizer core according to a preset order, to form layer-by-layer coated fertilizer granules and wherein polyurea formaldehyde is prepared by the following steps: mixing urea and formaldehyde at a molar ratio of 1- 2.5:1, adjusting the pH of the reaction system to 7.5-11.5 and the temperature to 50°C-75°C, and then adjusting the pH to 2.5 ~ 5.5. wherein the method comprises steps of: applying the fertilizer layer and the fertilizer corresponding to the coating layer to the periphery of the fertilizer core according to a preset order, to form layer-by-layer coated fertilizer granules and wherein polyurea formaldehyde is prepared by the following steps: mixing urea and formaldehyde at a molar ratio of 1- 2.5:1, adjusting the pH of the reaction system to 7.5-11.5 and the temperature to 50°C-75°C, and then adjusting the pH to 2.5 ~ 5.5.
A system for laying a flexible product from a storage area below a deck of a vessel, the system comprising: an inline quadrant above the deck for guiding flexible product to a portside or starboard side of the vessel, the inline quadrant with a portside entrance and a starboard side entrance; a highway with a highway portside guide and a highway starboard side guide for guiding the flexible product from a below deck position to an above deck position on either the portside or the starboard side, the highway extending to the portside entrance and the starboard side entrance of the inline quadrant; and a smart spooling system to guide flexible product between the storage area and to either the portside guide or the starboard side guide of the highway, wherein the smart spooling system comprises: a lower bend for guiding flexible product to and from the storage area, wherein the lower bend is able to tilt and/or move laterally with respect to the vessel; and a guide for guiding flexible product between the lower bend to either the starboard side entrance or the portside entrance of the highway. an inline quadrant above the deck for guiding flexible product to a portside or starboard side of the vessel, the inline quadrant with a portside entrance and a starboard side entrance; a highway with a highway portside guide and a highway starboard side guide for guiding the flexible product from a below deck position to an above deck position on either the portside or the starboard side, the highway extending to the portside entrance and the starboard side entrance of the inline quadrant; and a smart spooling system to guide flexible product between the storage area and to either the portside guide or the starboard side guide of the highway, wherein the smart spooling system comprises: a lower bend for guiding flexible product to and from the storage area, wherein the lower bend is able to tilt and/or move laterally with respect to the vessel; and a guide for guiding flexible product between the lower bend to either the starboard side entrance or the portside entrance of the highway. a lower bend for guiding flexible product to and from the storage area, wherein the lower bend is able to tilt and/or move laterally with respect to the vessel; and a guide for guiding flexible product between the lower bend to either the starboard side entrance or the portside entrance of the highway.
An installation for production of multiple Glycerol Tert-Butyl Ethers (GTBE) blends, comprising: a reaction vessel comprising: a reaction chamber for accommodating the production of GTBE; at least one reactant inlet in fluid communication with the reaction chamber for supplying glycerol and isobutene therein; a product outlet in fluid communication with the reaction chamber for withdrawing the GTBE blend; and a regulator configured for regulating conditions of the reaction vessel in alternating fashion between a first mode and a second mode, the first mode causing production of a mono-shifted GTBE blend and the second mode causing production of a di- and/or tri-shifted GTBE blend, wherein the regulator is configured to modify a residence time of reactants in the reaction chamber, and wherein the regulator is coupled to the product outlet to regulate withdrawal of the GTBE blend. a reaction vessel comprising: a reaction chamber for accommodating the production of GTBE; at least one reactant inlet in fluid communication with the reaction chamber for supplying glycerol and isobutene therein; a product outlet in fluid communication with the reaction chamber for withdrawing the GTBE blend; and a reaction chamber for accommodating the production of GTBE; at least one reactant inlet in fluid communication with the reaction chamber for supplying glycerol and isobutene therein; a product outlet in fluid communication with the reaction chamber for withdrawing the GTBE blend; and a regulator configured for regulating conditions of the reaction vessel in alternating fashion between a first mode and a second mode, the first mode causing production of a mono-shifted GTBE blend and the second mode causing production of a di- and/or tri-shifted GTBE blend, wherein the regulator is configured to modify a residence time of reactants in the reaction chamber, and wherein the regulator is coupled to the product outlet to regulate withdrawal of the GTBE blend.
A method for determining an operating parameter of a pressing tool in a joining press, in particular of a crimp tool in a crimp press, comprising the steps that an operating time is determined by an operating duration timer of a controller of the joining press, and that a tool service status of the pressing tool is determined by an analysis and evaluation module of the controller, and that the tool service status of the pressing tool is transmitted to a memory chip, in particular an RFID chip, arranged on the pressing tool by the analysis and evaluation module of the controller, and that a force action is determined by a force measuring device arranged on the joining press during the performance of pressing, characterized in that the tool service status of the pressing tool is determined from the operating time and the acting force. comprising the steps that an operating time is determined by an operating duration timer of a controller of the joining press, and that a tool service status of the pressing tool is determined by an analysis and evaluation module of the controller, and that the tool service status of the pressing tool is transmitted to a memory chip, in particular an RFID chip, arranged on the pressing tool by the analysis and evaluation module of the controller, and that a force action is determined by a force measuring device arranged on the joining press during the performance of pressing, characterized in that the tool service status of the pressing tool is determined from the operating time and the acting force.
A storage system comprising: a host system; and a plurality of storage sets configured to interface through two different protocols with the host system, and wherein at least one of the plurality of storage sets comprises: a first memory region comprising a volatile memory; a second memory region comprising a volatile memory; and a third memory region comprising a nonvolatile memory, and wherein: the at least one of the plurality of storage sets is configured to move data stored in the third memory region to a selected memory region among the first memory region and the second memory region based on a data access feature; and the at least one of the plurality of storage sets is further configured to adjust an execution order of pre-fetching commands received from the host system to pre-fetch data stored in the third memory region based on an operation state affecting the latency of of the third memory region. a host system; and a plurality of storage sets configured to interface through two different protocols with the host system, and wherein at least one of the plurality of storage sets comprises: a first memory region comprising a volatile memory; a second memory region comprising a volatile memory; and a third memory region comprising a nonvolatile memory, and a first memory region comprising a volatile memory; a second memory region comprising a volatile memory; and a third memory region comprising a nonvolatile memory, and wherein: the at least one of the plurality of storage sets is configured to move data stored in the third memory region to a selected memory region among the first memory region and the second memory region based on a data access feature; and the at least one of the plurality of storage sets is further configured to adjust an execution order of pre-fetching commands received from the host system to pre-fetch data stored in the third memory region based on an operation state affecting the latency of of the third memory region. the at least one of the plurality of storage sets is configured to move data stored in the third memory region to a selected memory region among the first memory region and the second memory region based on a data access feature; and the at least one of the plurality of storage sets is further configured to adjust an execution order of pre-fetching commands received from the host system to pre-fetch data stored in the third memory region based on an operation state affecting the latency of of the third memory region.
A shroud segment for a turbine stage of a gas turbine engine wherein the gas turbine engine comprises an engine axis, the segment forming an endwall for the working gas annulus of the stage, and providing a close clearance to the tips of a row of turbine blades which sweep across the segment, in use a leakage flow of the working gas passing through the clearance gap between the blade tips and the segment, wherein: the segment has a plurality of cooling holes (51, 81) and respective air feed passages (52, 53) for the cooling holes (51, 81) wherein an axial line of each feed passage is defined, relative to the engine axis, by a swirl angle angled in a circumferential direction away from a radial line which is perpendicular to the engine axis, and a radial angle angled away from the radial line towards the engine axis, such that the axial line of each feed passage defines a delivered air swirl direction, the cooling holes (51, 81) being distributed over that part of the gas-washed surface of the segment which is swept by the blade tips, the cooling holes (51, 81) delivering, in use, cooling air which spreads over the gas-washed surface, and the feed passages being configured such that the delivered air opposes the leakage flow of the working gas; and the feed passages are configured such that the delivered-air swirl directions of those cooling holes (51, 81) swept by axially downstream trailing edges of the blade tips are rotated towards an axially upstream direction of the engine, relative to the delivered-air swirl directions of those cooling holes (51, 81) swept by axially upstream leading edges of the blade tips. the segment has a plurality of cooling holes (51, 81) and respective air feed passages (52, 53) for the cooling holes (51, 81) wherein an axial line of each feed passage is defined, relative to the engine axis, by a swirl angle angled in a circumferential direction away from a radial line which is perpendicular to the engine axis, and a radial angle angled away from the radial line towards the engine axis, such that the axial line of each feed passage defines a delivered air swirl direction, the cooling holes (51, 81) being distributed over that part of the gas-washed surface of the segment which is swept by the blade tips, the cooling holes (51, 81) delivering, in use, cooling air which spreads over the gas-washed surface, and the feed passages being configured such that the delivered air opposes the leakage flow of the working gas; and the feed passages are configured such that the delivered-air swirl directions of those cooling holes (51, 81) swept by axially downstream trailing edges of the blade tips are rotated towards an axially upstream direction of the engine, relative to the delivered-air swirl directions of those cooling holes (51, 81) swept by axially upstream leading edges of the blade tips.