mhurhangee/patent-ind-claim-en huggingface dataset:
An airframe for a tiltrotor aircraft comprising: a wing airframe including a rib ; a fuselage airframe including a fore-aft overhead beam ; and a cradle support assembly including a forward wing support coupled to the fore-aft overhead beam and the wing airframe and an aft wing support coupled to the fore-aft overhead beam and the wing airframe ; wherein, the forward wing support includes a strut assembly coupled between the fore-aft overhead beam and the wing airframe and configured to provide pitch stiffness for the wing airframe ; and wherein, the rib , the fore-aft overhead beam , the forward wing support and the aft wing support are aligned in a vertical plane to form a wing-fuselage airframe beam assembly to support the wing airframe . a wing airframe including a rib ; a fuselage airframe including a fore-aft overhead beam ; and a cradle support assembly including a forward wing support coupled to the fore-aft overhead beam and the wing airframe and an aft wing support coupled to the fore-aft overhead beam and the wing airframe ; wherein, the forward wing support includes a strut assembly coupled between the fore-aft overhead beam and the wing airframe and configured to provide pitch stiffness for the wing airframe ; and wherein, the rib , the fore-aft overhead beam , the forward wing support and the aft wing support are aligned in a vertical plane to form a wing-fuselage airframe beam assembly to support the wing airframe .
Adhesive tape comprising a thermally vulcanizable, meltable, preferably pressure-sensitive adhesive which comprises a meltable polybutadiene-polyurethane as base elastomer and ground sulphur, where the meltable polybutadiene-polyurethane comprises the chemical reaction product of one or more polybutadiene-diols, one or more chain extenders having a hydroxyl functionality of two and a molar mass of less than or equal to 300 g/mol and optionally one or more polybutadiene-polyols having a number-averaged average functionality of between greater than 2.0 and less than or equal to 3, with one or more aliphatic or alicyclic diisocyanates, characterized in that no polyols or isocyanates other than those stated above are involved in the reaction to give the polybutadiene-polyurethane. one or more polybutadiene-diols, one or more chain extenders having a hydroxyl functionality of two and a molar mass of less than or equal to 300 g/mol and optionally one or more polybutadiene-polyols having a number-averaged average functionality of between greater than 2.0 and less than or equal to 3, with one or more aliphatic or alicyclic diisocyanates, characterized in that no polyols or isocyanates other than those stated above are involved in the reaction to give the polybutadiene-polyurethane.
A pharmaceutically acceptable solution comprising icodextrin and hydroxyalkyl starch (HAS), wherein said icodextrin is present at a concentration of from 1 to 7.5 % (w/v) and wherein said HAS is present at a concentration of from 1 to 15 % (w/v) for use in preventing metastasis formation and/or relapse by administration to a body cavity of a subject afflicted with cancer.
An electronic emulation component for actively emulating a passive component having capacitance or inductance of a desired value, the emulation component comprising: a pair of terminals for connection to an external circuit and across which said desired capacitance appears; a power convertor ; a controller connected to said power converter, said controller configured to provide a control signal (d) to said power converter which control signal has a value based at least in part on said desired value; and a passive component isolated from said pair of terminals by said convertor; characterized in that : the convertor is a DC - DC convertor, and in that said power convertor comprises an emulator for emulating said capacitance or said inductance, said emulator being configured to provide an emulation of a capacitance C B at said pair of terminals by providing a DC reference voltage v* DC to said power convertor at a control current ic, wherein said reference voltage is given by: v DC ∗ = 1 C B ∫ i C t dt . or in that said emulator is configured to provide an emulation of an inductance L B at said pair of terminals by providing a DC reference current i* DC to said power convertor at a control current vc, wherein said reference current is given by: i DC ∗ = 1 L B ∫ v C t dt . a pair of terminals for connection to an external circuit and across which said desired capacitance appears; a power convertor ; a controller connected to said power converter, said controller configured to provide a control signal (d) to said power converter which control signal has a value based at least in part on said desired value; and a passive component isolated from said pair of terminals by said convertor; characterized in that : the convertor is a DC - DC convertor, and in that said power convertor comprises an emulator for emulating said capacitance or said inductance, said emulator being configured to provide an emulation of a capacitance C B at said pair of terminals by providing a DC reference voltage v* DC to said power convertor at a control current ic, wherein said reference voltage is given by: v DC ∗ = 1 C B ∫ i C t dt . or in that said emulator is configured to provide an emulation of an inductance L B at said pair of terminals by providing a DC reference current i* DC to said power convertor at a control current vc, wherein said reference current is given by: i DC ∗ = 1 L B ∫ v C t dt .
An antenna system providing radio communications to a plurality of moving aerial vehicles, said system comprising an array of fixed antennas ; at least one or a plurality of transceivers selectively connected to the array of fixed antennas; and a control unit configured to switch individual antennas from said array to connect with at least one transceiver; wherein the control unit is configured with a switch matrix to control the connections from the antennas to the plurality of transceivers to implement a desired communications protocol, characterised in that the system is further configurable to supply exclusion policies to the control unit which identify which antennas are not to be connected to the switch matrix , wherein an exclusion policy identifies antennas determined to have a primary user located within their beamwidth , the primary user being a high priority user of the radio spectrum who has legal protection against interference, and which does not belong to the plurality of moving aerial vehicles which are serviced by the antenna system, wherein the determination is made from a dynamically generated database comprised in the antenna system containing information associated with each primary user and the locations and pointing angles of each of the antennas.
A method of manufacturing a capsule for containing a substance from which a beverage can be produced, the method comprising: - using an in-mould labelling technique to unite a label with a capsule body of synthetic plastics material so that the label covers at least part of a base wall of the capsule body and at least part of a side wall of the capsule body , wherein the label comprises a disc and one or more sections joined to a periphery of the disc, characterized in that , the label is inserted into a mould and the one or more sections are folded up relative to the disc and manipulated to a curved form of the side wall , such that the disc covers at least said part of the base wall and the one or more sections cover at least said part of the side wall , wherein the layer of synthetic plastics material is moulded onto the label bonding the label to the injection moulded capsule body , and wherein the disc is dimensioned larger than the base wall , and wherein a peripheral edge of the disc is folded up and manipulated to the curved form of the side wall such that the peripheral edge of the disc comes to extend beyond an inner edge of the one or more sections creating an overlap between them. - using an in-mould labelling technique to unite a label with a capsule body of synthetic plastics material so that the label covers at least part of a base wall of the capsule body and at least part of a side wall of the capsule body , wherein the label comprises a disc and one or more sections joined to a periphery of the disc, characterized in that , the label is inserted into a mould and the one or more sections are folded up relative to the disc and manipulated to a curved form of the side wall , such that the disc covers at least said part of the base wall and the one or more sections cover at least said part of the side wall , wherein the layer of synthetic plastics material is moulded onto the label bonding the label to the injection moulded capsule body , and wherein the disc is dimensioned larger than the base wall , and wherein a peripheral edge of the disc is folded up and manipulated to the curved form of the side wall such that the peripheral edge of the disc comes to extend beyond an inner edge of the one or more sections creating an overlap between them.
A method for acquiring a traffic state, the method comprising: acquiring monitoring data from a plurality of cameras in a camera group, wherein the plurality of cameras are capable of monitoring a target intersection; determining , based on the monitoring data acquired from each camera in the plurality of cameras, a moving trajectory of a reference object recorded by the each camera in the plurality of cameras, wherein the reference object is an object moving according to an indication of a signal light to pass through the target intersection, and the monitoring data comprises a plurality of image frames about the target interaction collected by the cameras and a time point when the cameras collect each of the image frames; fusing moving trajectories of the reference object to obtain a completed trajectory; and determining an indication state of the signal light on a corresponding road based on a travel direction of the corresponding road, the completed trajectory being located on the corresponding road. acquiring monitoring data from a plurality of cameras in a camera group, wherein the plurality of cameras are capable of monitoring a target intersection; determining , based on the monitoring data acquired from each camera in the plurality of cameras, a moving trajectory of a reference object recorded by the each camera in the plurality of cameras, wherein the reference object is an object moving according to an indication of a signal light to pass through the target intersection, and the monitoring data comprises a plurality of image frames about the target interaction collected by the cameras and a time point when the cameras collect each of the image frames; fusing moving trajectories of the reference object to obtain a completed trajectory; and determining an indication state of the signal light on a corresponding road based on a travel direction of the corresponding road, the completed trajectory being located on the corresponding road.
A door and suspension mechanism assembly for use at or near an end of an elongated housing , said door and suspension mechanism assembly comprising a door , an elongated housing and a suspension mechanism allowing a linear movement of said door relative to said elongated housing and said suspension mechanism allowing a pivoting movement of said door relative to said elongated housing , wherein said suspension mechanism comprises a pivot hinge and a support arm , the support arm having a variable length, the pivot hinge connecting said door pivotally to a first end of the support arm , the assembly being characterized in that said door comprises a part of one or more openings that allow one or more cables to extend from the outside into said elongated housing , said part of the openings of the door being configured to form, in a closed position of the door , a complete opening with another part of the openings provided at an edge of an opening around a cavity in the elongated housing wherein said one or more openings extend in the longtudinal direction of the elongated housing .
A turbine blade or turbine vane for a gas turbine, comprising successively along a radial direction of said gas turbine, a root for attaching the turbine blade or turbine vane to a carrier, a platform , an aerodynamically shaped hollow airfoil comprising a suction side wall and a pressure side wall extending with respect to the direction of a hot gas flow from a common leading edge to common a trailing edge and extending transversely thereof from said platform to an airfoil tip , wherein the airfoil comprises at least one cooling cavity extending in accordance to a cooling fluid flow direction from a platform level to said airfoil tip, said at least one cooling cavity being in fluid connection with a number of cooling fluid outlets distributed along the trailing edge through an array of impingement cooling features located there between, characterized in that said array extends into a region which is located radially outside the airfoil within the platform comprising also impingement cooling feature.
A turbomachine part , comprising: a body having a first side and a second side ; and an overhung section extending in an overhung manner, such that the overhung section lacks structural support in a portion thereof, from at least one of the first side and the second side of the body , wherein at least a portion of the overhung section includes a first plurality of material layers extending in a first direction, and a second plurality of material layers extending in a second direction at a non-coplanar direction relative to the first direction of the first plurality of material layers . a body having a first side and a second side ; and an overhung section extending in an overhung manner, such that the overhung section lacks structural support in a portion thereof, from at least one of the first side and the second side of the body , wherein at least a portion of the overhung section includes a first plurality of material layers extending in a first direction, and a second plurality of material layers extending in a second direction at a non-coplanar direction relative to the first direction of the first plurality of material layers .
An additive manufacturing apparatus for forming a three-dimensional article layer by layer from a powder, the apparatus comprising: an outer casing forming a build chamber , a build tank arranged inside the casing in the build chamber, and a temperature control arrangement comprising at least a first circuit for a first working fluid, the first circuit being positioned at a wall portion (40; 50) of the apparatus for transferring heat between the build chamber and the first working fluid; characterized in that the temperature control arrangement comprises a heat exchanger for transferring heat between the first working fluid of the first circuit and a second working fluid. an outer casing forming a build chamber , a build tank arranged inside the casing in the build chamber, and a temperature control arrangement comprising at least a first circuit for a first working fluid, the first circuit being positioned at a wall portion (40; 50) of the apparatus for transferring heat between the build chamber and the first working fluid; characterized in that the temperature control arrangement comprises a heat exchanger for transferring heat between the first working fluid of the first circuit and a second working fluid.
An air-ground communication control method, wherein the method is applied to a hierarchical network that comprises a ground network and at least one aerial network, and the method comprises: receiving (S110), by a ground device, location information of a high-altitude device sent by the high-altitude device, wherein the ground device is located in the ground network, the high-altitude device is located in the aerial network, and a beam of the high-altitude device covers the ground device; determining (S120) a beam direction from the ground device to the high-altitude device and beam width information according to location information of the ground device and the location information of the high-altitude device; and sending (S130) the beam width information to the high-altitude device in the beam direction, wherein the beam width information is used to adjust an interval of sending the location information of the high-altitude device. receiving (S110), by a ground device, location information of a high-altitude device sent by the high-altitude device, wherein the ground device is located in the ground network, the high-altitude device is located in the aerial network, and a beam of the high-altitude device covers the ground device; determining (S120) a beam direction from the ground device to the high-altitude device and beam width information according to location information of the ground device and the location information of the high-altitude device; and sending (S130) the beam width information to the high-altitude device in the beam direction, wherein the beam width information is used to adjust an interval of sending the location information of the high-altitude device.
A propulsion system , comprising: an engine comprising a combustion chamber ; a solid fuel storage system comprising one or more metal hydride compound segments ; a heating system operable to apply heat to the one or more metal hydride compound segments to desorb gaseous hydrogen fuel from the one or more metal hydride compound segments; and a piping system configured to direct the gaseous hydrogen fuel to the combustion chamber of the engine, wherein the combustion chamber is receptive of the gaseous hydrogen fuel and configured to combust the gaseous hydrogen fuel to drive an operation of the engine; wherein the solid fuel storage system comprises canisters in which the one or more metal hydride compound segments are storable, and the heating system comprises heating elements disposed in the canisters to heat the one or more metal hydride compound segments; the propulsion system being characterised in that each canister comprises: an outer casing ; heating element films supported on an interior surface of the outer casing; and perforated heating element films defining a central gas channel , wherein the one or more metal hydride compound segments are radially interposable between the heating element films and the perforated heating element films. an engine comprising a combustion chamber ; a solid fuel storage system comprising one or more metal hydride compound segments ; a heating system operable to apply heat to the one or more metal hydride compound segments to desorb gaseous hydrogen fuel from the one or more metal hydride compound segments; and a piping system configured to direct the gaseous hydrogen fuel to the combustion chamber of the engine, wherein the combustion chamber is receptive of the gaseous hydrogen fuel and configured to combust the gaseous hydrogen fuel to drive an operation of the engine; wherein the solid fuel storage system comprises canisters in which the one or more metal hydride compound segments are storable, and the heating system comprises heating elements disposed in the canisters to heat the one or more metal hydride compound segments; the propulsion system being characterised in that each canister comprises: an outer casing ; heating element films supported on an interior surface of the outer casing; and perforated heating element films defining a central gas channel , wherein the one or more metal hydride compound segments are radially interposable between the heating element films and the perforated heating element films. an outer casing ; heating element films supported on an interior surface of the outer casing; and perforated heating element films defining a central gas channel , wherein the one or more metal hydride compound segments are radially interposable between the heating element films and the perforated heating element films.
A method , comprising: applying an arbitrary transformation to a plurality of vectors to produce a plurality of transformed vectors, the arbitrary transformation including one of a unitary transformation, an equiangular tight frame, ETF, transformation, or a nearly equiangular tight frame, NETF, transformation, the arbitrary transformation based on a matrix that is not an identity matrix or a discrete Fourier matrix; producing , using the arbitrary transformation, a first transformed signal based on at least a first transformed vector from the plurality of transformed vectors; producing , using the arbitrary transformation, a second transformed signal based on at least a second transformed vector from the plurality of transformed vectors; transmitting the first transformed signal, via a first communications channel, to a first signal receiver that is configured to detect the first transformed signal; transmitting the second transformed signal, via a second communications channel, to a second signal receiver that is configured to detect the second transformed signal; and providing a signal representing the arbitrary transformation to the first signal receiver and the second signal receiver, for recovery of the plurality of vectors at the first signal receiver and the second signal receiver based on the arbitrary transformation. applying an arbitrary transformation to a plurality of vectors to produce a plurality of transformed vectors, the arbitrary transformation including one of a unitary transformation, an equiangular tight frame, ETF, transformation, or a nearly equiangular tight frame, NETF, transformation, the arbitrary transformation based on a matrix that is not an identity matrix or a discrete Fourier matrix; producing , using the arbitrary transformation, a first transformed signal based on at least a first transformed vector from the plurality of transformed vectors; producing , using the arbitrary transformation, a second transformed signal based on at least a second transformed vector from the plurality of transformed vectors; transmitting the first transformed signal, via a first communications channel, to a first signal receiver that is configured to detect the first transformed signal; transmitting the second transformed signal, via a second communications channel, to a second signal receiver that is configured to detect the second transformed signal; and providing a signal representing the arbitrary transformation to the first signal receiver and the second signal receiver, for recovery of the plurality of vectors at the first signal receiver and the second signal receiver based on the arbitrary transformation.
A curable composition comprising: oxidized boron nitride particles, each comprising a hydrated boron oxide surface layer disposed on a boron nitride base; and a polyaziridine. oxidized boron nitride particles, each comprising a hydrated boron oxide surface layer disposed on a boron nitride base; and a polyaziridine.
An integrated access and backhaul, IAB, node for performing a communication, the IAB node comprising: a transceiver ; and a processor coupled with the transceiver and configured to: transmit, to an IAB donor , a radio resource control, RRC, message including information indicating a relay capability of the IAB node, and wherein the IAB donor comprises a distribution unit, DU, and a central unit, CU , establish a F1 interface between a DU of the IAB node and the CU of the IAB donor, after the IAB node is authenticated with a core network entity based on the information indicating the relay capability, and provide a service to a user equipment, UE, based on a result of the establishment. a transceiver ; and a processor coupled with the transceiver and configured to: transmit, to an IAB donor , a radio resource control, RRC, message including information indicating a relay capability of the IAB node, and wherein the IAB donor comprises a distribution unit, DU, and a central unit, CU , establish a F1 interface between a DU of the IAB node and the CU of the IAB donor, after the IAB node is authenticated with a core network entity based on the information indicating the relay capability, and provide a service to a user equipment, UE, based on a result of the establishment.