mhurhangee/patent-ind-claim-en huggingface dataset:
A method for controlling communication in Internet of Vehicles, comprising: receiving (S202), by a Road Side Unit, RSU, first indication information, wherein the first indication information is used to indicate the RSU to start or stop sending a Vehicle-to-Everything communications, V2X, message; and starting or stopping sending the V2X message in response to the first indication information by the RSU (S204), wherein the receiving (S202), by the Road Side Unit, RSU, the first indication information, comprises receiving, by the RSU, the first indication information sent by a network device, wherein the network device comprises at least one of a base station, a Proximity Services, ProSe, function unit, a V2X function unit, and a network element that performs a Device-to-Device control function, and characterized by , before receiving (S202), by the RSU, the first indication information sent by the network device, the method further comprises sending, by the RSU, RSU signal coverage information of the RSU to the network device. receiving (S202), by a Road Side Unit, RSU, first indication information, wherein the first indication information is used to indicate the RSU to start or stop sending a Vehicle-to-Everything communications, V2X, message; and starting or stopping sending the V2X message in response to the first indication information by the RSU (S204), wherein the receiving (S202), by the Road Side Unit, RSU, the first indication information, comprises receiving, by the RSU, the first indication information sent by a network device, wherein the network device comprises at least one of a base station, a Proximity Services, ProSe, function unit, a V2X function unit, and a network element that performs a Device-to-Device control function, and characterized by , before receiving (S202), by the RSU, the first indication information sent by the network device, the method further comprises sending, by the RSU, RSU signal coverage information of the RSU to the network device.
A one-piece tool tip being integral with or being configured to be removably secured to a tool body, and configured to machine a metal object, the tool tip (16;16') having a tool tip diameter (D;D'), a rotational axis (A;A') and at least one coolant duct (44;78'), the tool tip (16;16') comprising at least one major cutting edge (28;28') formed at an intersection of a rake face (24;24') and a first major flank (26A;26A'), the rake face forming part of a chip flute (22;22B'), the at least one coolant duct being configured to be in flow communication with discharge orifices (46;46') exclusively in the tool tip (16;16'), wherein the tool tip (16;16') has an arrangement, such as a row, of two or more of the discharge orifices (46;46') exclusively in the rake face (24;24') of the at least one major cutting edge , wherein the arrangement extends at a non-zero angle (α) relative to the rotational axis (A;A'), characterized in that the tool tip has at least two major cutting edges (28;28'), each major cutting edge (28;28') having a rake face (24;24') with a respective arrangement of discharge orifices, wherein a majority of the discharge orifices (46;46') of each arrangement is located axially forwards of a line (Y;Y') intersecting radially outer ends of the major cutting edges. the tool tip (16;16') having a tool tip diameter (D;D'), a rotational axis (A;A') and at least one coolant duct (44;78'), the tool tip (16;16') comprising at least one major cutting edge (28;28') formed at an intersection of a rake face (24;24') and a first major flank (26A;26A'), the rake face forming part of a chip flute (22;22B'), the at least one coolant duct being configured to be in flow communication with discharge orifices (46;46') exclusively in the tool tip (16;16'), wherein the tool tip (16;16') has an arrangement, such as a row, of two or more of the discharge orifices (46;46') exclusively in the rake face (24;24') of the at least one major cutting edge , wherein the arrangement extends at a non-zero angle (α) relative to the rotational axis (A;A'), characterized in that the tool tip has at least two major cutting edges (28;28'), each major cutting edge (28;28') having a rake face (24;24') with a respective arrangement of discharge orifices, wherein a majority of the discharge orifices (46;46') of each arrangement is located axially forwards of a line (Y;Y') intersecting radially outer ends of the major cutting edges.
A method for making a controlled release material, comprising the steps of:- (a) forming granules comprising one or more wax and one or more disintegrant, wherein granules are formed by mixing of one or more disintegrant and one or more molten wax, whilst retaining the wax in molten form, and subsequently solidifying the mixture on cooling to below melting point whilst mixing to form granules; (b) spheronisation of the granules and (c) compaction of the spheronised granules of step (b) so as to form the controlled release material, wherein the disintegrant is low-substituted hydroxypropyl cellulose (L-HPC). (a) forming granules comprising one or more wax and one or more disintegrant, wherein granules are formed by mixing of one or more disintegrant and one or more molten wax, whilst retaining the wax in molten form, and subsequently solidifying the mixture on cooling to below melting point whilst mixing to form granules; (b) spheronisation of the granules and (c) compaction of the spheronised granules of step (b) so as to form the controlled release material, wherein the disintegrant is low-substituted hydroxypropyl cellulose (L-HPC).
A jarring tool for releasing equipment lodged in a well comprising: a) a housing ; b) an axially movable mandrel positioned within the housing ; c) a dog clutch surrounding the mandrel ; d) a trigger sleeve surrounding the dog clutch ; e) the dog clutch and trigger sleeve having complementary surfaces which when in alignment will cause the dog clutch to release the mandrel ; f) a spring positioned within the housing to resist the travel of the mandrel within the housing ; and g) a hydraulic chamber and a piston located in the hydraulic chamber and surrounding the mandrel and, the piston being positioned between the spring and dog clutch CHARACTERISED IN THAT the jarring tool further comprises h) means for adjusting the axial position of the trigger sleeve with respect to a stop shoulder formed on an inner surface of the housing by applying a rotational force to the trigger sleeve via a tool inserted into a slot provided in the housing . a) a housing ; b) an axially movable mandrel positioned within the housing ; c) a dog clutch surrounding the mandrel ; d) a trigger sleeve surrounding the dog clutch ; e) the dog clutch and trigger sleeve having complementary surfaces which when in alignment will cause the dog clutch to release the mandrel ; f) a spring positioned within the housing to resist the travel of the mandrel within the housing ; and g) a hydraulic chamber and a piston located in the hydraulic chamber and surrounding the mandrel and, the piston being positioned between the spring and dog clutch CHARACTERISED IN THAT the jarring tool further comprises h) means for adjusting the axial position of the trigger sleeve with respect to a stop shoulder formed on an inner surface of the housing by applying a rotational force to the trigger sleeve via a tool inserted into a slot provided in the housing .
A method for detecting at least one disease selected from the group consisting of visceral fat accumulation, hyperglycemia, dyslipidemia, hypertension and atherosclerosis or a combination of two or more of diseases or detecting onset risk of these diseases, which comprises (a) a step of measuring a ganglioside GM3 in a blood sample derived from a subject, wherein the ganglioside GM3 has a structure represented by the following formula : wherein in the formula , R 1 represents a glycan constituting the ganglioside GM3, and R 2 -C(=O)- represents a fatty acid residue having 16 or more and 24 or less carbon atoms which may have a double bond, and having an OH group as a substituent. (a) a step of measuring a ganglioside GM3 in a blood sample derived from a subject, wherein the ganglioside GM3 has a structure represented by the following formula : wherein in the formula , R 1 represents a glycan constituting the ganglioside GM3, and R 2 -C(=O)- represents a fatty acid residue having 16 or more and 24 or less carbon atoms which may have a double bond, and having an OH group as a substituent.
A method of maintaining and regulating the frequency of a timepiece resonator mechanism about the natural frequency (ω0) thereof, the mechanism including at least one elastic return means that includes at least one balance spring or torsion wire or flexible guide member, where at least one regulator device is implemented, acting on said resonator mechanism with a periodic motion, said periodic motion imposing a periodic modulation of the resonant frequency of said resonator mechanism , which is a parametric resonator, with a regulation frequency (ωR) that is comprised between 0.9 times and 1.1 times the value of an integer multiple of said natural frequency (ω0), said integer being greater than or equal to 2 and less than or equal to 10, characterized in that said at least one regulator device is made to act by controlling a periodic variation in the real part of the rigidity of at least one said elastic return means , said real part of the rigidity defining the frequency of said resonator mechanism .
Use of an epoxy resin composition comprising at least one reaction product from the reaction of at least one amine of the formula (I) with at least one carbonyl compound of the formula (II) and hydrogen, NH 2 -CH 2 -A-CH 2 -NH 2 (I) where A is a phenylene radical or cyclohexylene radical, R is a hydrogen radical or alkyl radical having 1 to 8 carbon atoms, m is 0 or 1, and X is a hydroxyl radical or methyl radical or methoxy radical, where the molar ratio between the amine of the formula (I) and the carbonyl compound of the formula (II) is in the range from 1/0.7 to 1/1.2, as a cold-curing primer or adhesive, characterized in that the reaction product contains an amount of amine of the formula (III) in the range from 30 to 80 weight%. A is a phenylene radical or cyclohexylene radical, R is a hydrogen radical or alkyl radical having 1 to 8 carbon atoms, m is 0 or 1, and X is a hydroxyl radical or methyl radical or methoxy radical, where the molar ratio between the amine of the formula (I) and the carbonyl compound of the formula (II) is in the range from 1/0.7 to 1/1.2, as a cold-curing primer or adhesive,
An air conditioner in which refrigerant circulates, the air conditioner comprising: a compressor ; a first heat exchanger ; a first expansion valve ; a second heat exchanger ; and a controller configured to change an opening degree (LP) of the first expansion valve by a first operation amount (ΔLP op , ΔLP1 op ) according to a temperature difference between a target temperature (Td m ) and a temperature (Td) of the refrigerant discharged by the compressor , the refrigerant circulating through the compressor , the first heat exchanger , the first expansion valve , and the second heat exchanger , characterized in that the controller is configured to set a first ratio of the first operation amount to the temperature difference when a specific condition is satisfied to be larger than a second ratio of the first operation amount to the temperature difference when the specific condition is not satisfied, the specific condition indicating that a degree of subcooling of the refrigerant flowing between the first heat exchanger and the first expansion valve is smaller than zero. a compressor ; a first heat exchanger ; a first expansion valve ; a second heat exchanger ; and a controller configured to change an opening degree (LP) of the first expansion valve by a first operation amount (ΔLP op , ΔLP1 op ) according to a temperature difference between a target temperature (Td m ) and a temperature (Td) of the refrigerant discharged by the compressor , the refrigerant circulating through the compressor , the first heat exchanger , the first expansion valve , and the second heat exchanger , characterized in that the controller is configured to set a first ratio of the first operation amount to the temperature difference when a specific condition is satisfied to be larger than a second ratio of the first operation amount to the temperature difference when the specific condition is not satisfied, the specific condition indicating that a degree of subcooling of the refrigerant flowing between the first heat exchanger and the first expansion valve is smaller than zero.
A file storage method, characterized in that the method comprises: receiving (S101) a storage request for a to-be-stored file; determining (SI02) an idle key for storing the to-be-stored file as a target key consisting of a name and a value; obtaining (S103) to-be-stored metadata of the to-be-stored file according to the determined target key, wherein the to-be-stored metadata comprises: fixed sub-metadata comprising sub-metadata corresponding to file information of the to-be-stored file and variable sub-metadata comprising sub-metadata corresponding to stripe information corresponding to the determined target key, wherein each stripe corresponds to multiple keys and to one or more IP hard disks; and storing (S104) the to-be-stored metadata in a metadata database, storing the fixed sub-metadata in the name of the determined target key, storing the variable sub-metadata in a preset storage area which has a one-to-one correspondence with the determined target key, and storing the to-be-stored file in the value of the determined target key, wherein the variable sub-metadata stored in the preset storage area is used to recover metadata lost in the metadata database. receiving (S101) a storage request for a to-be-stored file; determining (SI02) an idle key for storing the to-be-stored file as a target key consisting of a name and a value; obtaining (S103) to-be-stored metadata of the to-be-stored file according to the determined target key, wherein the to-be-stored metadata comprises: fixed sub-metadata comprising sub-metadata corresponding to file information of the to-be-stored file and variable sub-metadata comprising sub-metadata corresponding to stripe information corresponding to the determined target key, wherein each stripe corresponds to multiple keys and to one or more IP hard disks; and storing (S104) the to-be-stored metadata in a metadata database, storing the fixed sub-metadata in the name of the determined target key, storing the variable sub-metadata in a preset storage area which has a one-to-one correspondence with the determined target key, and storing the to-be-stored file in the value of the determined target key, wherein the variable sub-metadata stored in the preset storage area is used to recover metadata lost in the metadata database.
An aircraft, comprising: a fixed wall structure ; and a seat with self-stowage capability, the seat comprising: a seat pan comprising a lever which is rotatable between stowed and open positions; a fixed seat structure fixed to the fixed wall structure and comprising an annulus; and an elastic assembly comprising a damper and an arc-spring disposable within the annulus to permit first rotations of the seat pan lever from the stowed position to the open positions and to urge second rotations of the seat pan lever from the open positions to the stowed position, and characterized in that the aircraft further comprises a boss coupled with the lever and defining an axis about which the lever is rotatable relative to the fixed wall structure between the stowed and open positions and a fully open position is 90° from the stowed position. a fixed wall structure ; and a seat with self-stowage capability, the seat comprising: a seat pan comprising a lever which is rotatable between stowed and open positions; a fixed seat structure fixed to the fixed wall structure and comprising an annulus; and an elastic assembly comprising a damper and an arc-spring disposable within the annulus to permit first rotations of the seat pan lever from the stowed position to the open positions and to urge second rotations of the seat pan lever from the open positions to the stowed position, and characterized in that the aircraft further comprises a boss coupled with the lever and defining an axis about which the lever is rotatable relative to the fixed wall structure between the stowed and open positions and a fully open position is 90° from the stowed position. a seat pan comprising a lever which is rotatable between stowed and open positions; a fixed seat structure fixed to the fixed wall structure and comprising an annulus; and an elastic assembly comprising a damper and an arc-spring disposable within the annulus to permit first rotations of the seat pan lever from the stowed position to the open positions and to urge second rotations of the seat pan lever from the open positions to the stowed position, and characterized in that the aircraft further comprises a boss coupled with the lever and defining an axis about which the lever is rotatable relative to the fixed wall structure between the stowed and open positions and a fully open position is 90° from the stowed position.
A chain link for an energy guiding chain for guiding cables, lines and the like, wherein the chain link has hinge members for hinged connection to further chain links of the same structure for providing the energy guiding chain, wherein the chain link has two laterally mutually spaced chain plates having narrow sides delimiting same and extending in the longitudinal direction of the chain link, and at least one transverse bar connecting the chain plates together, wherein at least one transverse bar is adapted to be pivotable forming a hinge connection in relation to at least one chain plate and can be transferred by pivotal movement into a closed position of connecting the chain plates together and into an open position at least partially opening the intermediate space between the chain plates , wherein at least one pivotable end region of the transverse bar can be latchingly fixed to the chain plate hingedly connected to the transverse bar, and wherein the hinge connection between the transverse bar and the chain plate has a substantially cylindrical hinge pin of the radius R1 over at least a part of the periphery of the pin at one of the corresponding components of the transverse bar and the chain link and a substantially cylindrical pin receiving means at the other of the two corresponding components , and wherein the hinge pin has at least one recess over a portion of its length at the pin side that is remote from the narrow sides, which recess is set back from the cylindrical surface of the pin , and the pin receiving means has at least one latching nose which projects from the cylindrical region of the pin receiving means of the radius R1 and engages into the recess , characterised in that the hinge pin is provided with the at least one recess only over a portion of its length at the pin side that is remote from the narrow sides , which recess is set back from the cylindrical surface of the pin , and that the hinge pin is of a cylindrical configuration in another portion which cooperates with the pin receiving means .
A spacecraft comprising: a plurality of sub-systems for controlling operations of the spacecraft; and a deployable spacecraft body comprising a plurality of panels and a plurality of hinges each connecting adjacent ones of the plurality of panels, the hinges being arranged to permit the plurality of panels to be folded into a stowed configuration and unfolded into a deployed configuration, wherein the plurality of sub-systems are fixed to and supported by one or more of the plurality of panels, characterised in that the plurality of panels comprises a plurality of interior panels and a plurality of peripheral panels, wherein the plurality of peripheral panels are arranged around a circumference of the body in the deployed configuration, wherein the plurality of interior panels have shapes such that in the deployed configuration the plurality of interior panels substantially fill available space between the plurality of peripheral panels, thereby providing a flat, planar structure that has a substantially continuous surface in the deployed configuration. a plurality of sub-systems for controlling operations of the spacecraft; and a deployable spacecraft body comprising a plurality of panels and a plurality of hinges each connecting adjacent ones of the plurality of panels, the hinges being arranged to permit the plurality of panels to be folded into a stowed configuration and unfolded into a deployed configuration, wherein the plurality of sub-systems are fixed to and supported by one or more of the plurality of panels, characterised in that the plurality of panels comprises a plurality of interior panels and a plurality of peripheral panels, wherein the plurality of peripheral panels are arranged around a circumference of the body in the deployed configuration, wherein the plurality of interior panels have shapes such that in the deployed configuration the plurality of interior panels substantially fill available space between the plurality of peripheral panels, thereby providing a flat, planar structure that has a substantially continuous surface in the deployed configuration.
An ultrasound imaging device comprising: a pair of imaging probes arranged to be disposed at side-by-side, spaced apart acoustic windows, respectively facing opposite sides of a central region to be imaged, and adapted to dynamically scan jointly in an interleaved manner and in a single lateral direction in imaging said region, said scan being along a synchronization line extending laterally across said region, monotonically progressive in said direction, said direction being substantially a direction between said pair; an image acquiring circuitry in communication with the pair of imaging probes, wherein the image acquiring circuitry is adapted to operate said probes for said scan through a pair of said windows, the image acquiring circuitry including a receive beamformer for beamforming data obtained by the image acquiring circuitry in said scan to yield beamformed samples; and scan conversion circuitry in communication with the pair of imaging probes and the image acquiring circuitry, wherein the scan conversion circuitry is configured for, based on said samples, dynamically reconstructing spatially intermediate pixels, said samples being correspondingly derived from the scan acquisition through said acoustic windows, said reconstructing being further based on temporal weighting of said samples. a pair of imaging probes arranged to be disposed at side-by-side, spaced apart acoustic windows, respectively facing opposite sides of a central region to be imaged, and adapted to dynamically scan jointly in an interleaved manner and in a single lateral direction in imaging said region, said scan being along a synchronization line extending laterally across said region, monotonically progressive in said direction, said direction being substantially a direction between said pair; an image acquiring circuitry in communication with the pair of imaging probes, wherein the image acquiring circuitry is adapted to operate said probes for said scan through a pair of said windows, the image acquiring circuitry including a receive beamformer for beamforming data obtained by the image acquiring circuitry in said scan to yield beamformed samples; and scan conversion circuitry in communication with the pair of imaging probes and the image acquiring circuitry, wherein the scan conversion circuitry is configured for, based on said samples, dynamically reconstructing spatially intermediate pixels, said samples being correspondingly derived from the scan acquisition through said acoustic windows, said reconstructing being further based on temporal weighting of said samples.