mhurhangee/ep-ind-claims huggingface dataset:
An aircraft defining a longitudinal direction, a vertical direction, and a lateral direction, the aircraft comprising: a fuselage extending between a forward end and an aft end along the longitudinal direction; a boundary layer ingestion fan mounted to the fuselage at the aft end of the fuselage, the boundary layer ingestion fan defining a centerline and comprising a plurality of fan blades rotatable about the centerline; characterized in that the aircraft further comprises: an air injection assembly comprising: a plurality of injection ports defined on a surface of the fuselage at a location upstream of the boundary layer ingestion fan; and a fluid passageway, the fluid passageway extending through at least a portion of the fuselage and being in fluid communication with the plurality of injection ports for directing a supplemental airflow through the plurality of injection ports; wherein the air injection assembly further comprises; a plurality of inlet ports defined on a bottom surface of the fuselage, and wherein the fluid passageway extends between the plurality of inlet ports and the plurality of injection ports. a fuselage extending between a forward end and an aft end along the longitudinal direction; a boundary layer ingestion fan mounted to the fuselage at the aft end of the fuselage, the boundary layer ingestion fan defining a centerline and comprising a plurality of fan blades rotatable about the centerline; characterized in that the aircraft further comprises: an air injection assembly comprising: a plurality of injection ports defined on a surface of the fuselage at a location upstream of the boundary layer ingestion fan; and a fluid passageway, the fluid passageway extending through at least a portion of the fuselage and being in fluid communication with the plurality of injection ports for directing a supplemental airflow through the plurality of injection ports; wherein the air injection assembly further comprises; a plurality of inlet ports defined on a bottom surface of the fuselage, and wherein the fluid passageway extends between the plurality of inlet ports and the plurality of injection ports. a plurality of injection ports defined on a surface of the fuselage at a location upstream of the boundary layer ingestion fan; and a fluid passageway, the fluid passageway extending through at least a portion of the fuselage and being in fluid communication with the plurality of injection ports for directing a supplemental airflow through the plurality of injection ports; wherein the air injection assembly further comprises; a plurality of inlet ports defined on a bottom surface of the fuselage, and wherein the fluid passageway extends between the plurality of inlet ports and the plurality of injection ports.
A disinfection system for a continuous positive air pressure (CPAP) device, said CPAP device comprising a water reservoir tank, a hose, and a mask connected to the water reservoir tank by the hose, characterized in that the disinfection system comprises: an ozone device comprising an ozone compartment and a mask compartment, the ozone compartment comprising an ozone operating system configured to pull in ambient air into an air pump to create ozone; an ozone distribution line connected to the ozone device; and a CPAP connector unit connected to the ozone distribution line, the CPAP connector unit further configured to connect to the water reservoir tank to provide ozone into the water reservoir tank and to the hose to provide ozone into the hose, wherein the hose is configured to carry the ozone into the mask compartment an ozone device comprising an ozone compartment and a mask compartment, the ozone compartment comprising an ozone operating system configured to pull in ambient air into an air pump to create ozone; an ozone distribution line connected to the ozone device; and a CPAP connector unit connected to the ozone distribution line, the CPAP connector unit further configured to connect to the water reservoir tank to provide ozone into the water reservoir tank and to the hose to provide ozone into the hose, wherein the hose is configured to carry the ozone into the mask compartment
Rectifier of a bladed stator of an axial turbomachine, comprising blades and an inner ferrule held in place by the blades and configured for mating with a rotor of the turbomachine, the inner ferrule consisting of at least two segments (8a, 8b) having the general form of an arc of a circle and intended to be arranged end to end so as to form the ferrule, each segment (8a, 8b) including on the outside a plurality of openings arranged at regular distances along the general arc of the circle of the segment, into each of which the end of one of the blades of the stator is fitted; characterized in that each end of a segment (8a, 8b) possesses a section (11a, 11b) of which the profile essentially corresponds with that of the end of the corresponding blade, so that the joint between two adjacent segments (8a, 8b) corresponds with the profile of the corresponding blade; and the joint between the blades and the segments (8a, 8b) is provided by an elastomer.
A system for network coverage modelling for unmanned aerial vehicles (UAVs), comprising: one or more processors; and memory having instructions stored therein, the instructions, when executed by the one or more processors, cause the one or more processors to perform acts comprising: receiving network configuration data for multiple base stations of a wireless communication network that are located in an area; receiving environmental data that includes information on natural and manmade features in the area; segregating an airspace above the area into a plurality of vertically layered 3-dimensional sections; and generating a coverage model for predicting network coverage of the wireless communication network in the 3-dimensional sections in the airspace above the area, wherein generating the coverage model includes applying a machine learning algorithm to training data that includes the network configuration data, the environmental data and boundary locations of the plurality of vertically layered 3-dimensional sections. one or more processors; and memory having instructions stored therein, the instructions, when executed by the one or more processors, cause the one or more processors to perform acts comprising: receiving network configuration data for multiple base stations of a wireless communication network that are located in an area; receiving environmental data that includes information on natural and manmade features in the area; segregating an airspace above the area into a plurality of vertically layered 3-dimensional sections; and generating a coverage model for predicting network coverage of the wireless communication network in the 3-dimensional sections in the airspace above the area, wherein generating the coverage model includes applying a machine learning algorithm to training data that includes the network configuration data, the environmental data and boundary locations of the plurality of vertically layered 3-dimensional sections. receiving network configuration data for multiple base stations of a wireless communication network that are located in an area; receiving environmental data that includes information on natural and manmade features in the area; segregating an airspace above the area into a plurality of vertically layered 3-dimensional sections; and generating a coverage model for predicting network coverage of the wireless communication network in the 3-dimensional sections in the airspace above the area, wherein generating the coverage model includes applying a machine learning algorithm to training data that includes the network configuration data, the environmental data and boundary locations of the plurality of vertically layered 3-dimensional sections.
Articulation for deploying and locking a solar generator or a reflector or other deployable aerospace components, comprising two articulation halves (4, 10), an articulation spindle and a drive, characterized in that a drive spring of the drive, over the angle of deployment of the two articulation halves (4, 10) has a progressive spring characteristic which increases as deployment progresses and is intended to compensate for a friction moment which varies over the angle of deployment.
Combination of plastic sheeting for covering silage, with at least two layers of sheeting, comprising a first folded sheet and a second folded sheet, wherein the sheets (2, 3) are folded along folding lines which are parallel to the longitudinal direction and the lateral edges (23, 24, 33, 34) of sheet, and, as seen in cross section in a plane perpendicular to the folding lines of the sheets (2, 3), the second sheet is folded into said first sheet and said second sheet is enclosed by said first sheet, wherein the sheets have first (23, 33) and second lateral edges (24, 34) and, seen in the cross section, at least the first lateral edges (23, 33) of the two sheets (2, 3) extend in close proximity to each other in the folded combination of sheets, wherein each of the folded sheets (2,3) in the combination comprises at least one folded structure (26, 36) between the lateral edges, wherein a folded structure (26, 36) comprises a plurality of, seen in the cross section, zigzagging layers of sections of sheeting, wherein the folded structures (26, 36) of the two sheets (2, 3) are stacked.
A power control system for optimizing power production from a two-blades and yaw controlled wind turbine, the wind turbine has a teetering hub and operates in four operation modalities, respectively from cut-in wind speed to quasi-rated wind speed, from quasi-rated wind speed to rated wind speed, from rated wind speed to quasi-cut-out wind speed and from quasi cut-out wind speed to cut-out wind speed, such power control system comprising a controller, a yaw actuation subsystem and a drivetrain restraining torque subsystem, wherein the controller is adapted to: - receive in input the sensed output power, the sensed rotor running speed and the sensed wind direction relative to the rotor axis direction; - direct the drivetrain restraining torque subsystem and the yaw actuation subsystem to modify the operating condition of the wind turbine as a function of the changes in the sensed output power, the sensed rotor running speed and the sensed wind direction relative to the rotor axis direction; characterized in that the controller directs the drivetrain restraining torque subsystem to maintain drivetrain restraining torque constant at its rated value when the turbine operates from quasi-rated wind speed to cut-out wind speed operation modalities. - receive in input the sensed output power, the sensed rotor running speed and the sensed wind direction relative to the rotor axis direction; - direct the drivetrain restraining torque subsystem and the yaw actuation subsystem to modify the operating condition of the wind turbine as a function of the changes in the sensed output power, the sensed rotor running speed and the sensed wind direction relative to the rotor axis direction;
A high strength galvanized steel sheet, composed of a steel sheet having a chemical composition consisting of, by mass%, C: 0.02% or more and 0.30% or less, Si: 0.01% or more and 2.5% or less, Mn: 0.1% or more and 3.0% or less, P: 0.003% or more and 0.08% or less, S: 0.01% or less, Al: 0.001% or more and 0.20% or less, Ti: 0.03% or more and 0.40% or less and optionally at least one selected from Nb: 0.001% or more and 0.2% or less, V: 0.001% or more and 0.5% or less, Mo: 0.01% or more and 0.5% or less and W: 0.001% or more and 0.2% or less and B: 0.0002% or more and 0.005% or less and the balance being Fe and inevitable impurities, and a zinc-coated layer on both surfaces of the base steel sheet having a coating weight per surface of 20 g/m 2 or more and 120 g/m 2 or less, wherein the concentration ratio of C to Ti (C/Ti) in a portion within 10 μm from the surface of the base steel sheet immediately under the zinc-coated layer is, in terms of atomic ratio, 0.8 or more and 1.5 or less, and wherein the total amount of oxides of one or more selected from Fe, Si, Mn, P, Al and Ti formed in a portion within 100 μm from the surface of the base steel sheet immediately under the zinc-coated layer is, in terms of oxygen amount, 0.05 g/m 2 or less per side.
A combination comprising dinaciclib or a pharmaceutically acceptable salt thereof and a B cell chronic lymphocytic leukemia/lymphoma 2 inhibitor for use in the treatment of cancer.
Rotor intended for an axial-flux electromagnetic motor or generator, the rotor including a body with a disc having two circular faces connected by a thickness, the disc being delimited between an outer periphery and an inner periphery, the inner periphery delimiting a recess for a rotation shaft, at least two permanent magnets being applied against at least one of the two circular faces of the body referred to as the support face while each being held on said face, a gap being left between said at least two magnets, said at least two magnets are magnets semi-embedded in a respective housing in the disc, projecting from their respective housing, characterised in that the rotor includes at least one axial holding means being housed in each gap and comprising at least one tenon locally and directly covering at least one of said at least two semi-embedded magnets.
A malleable cannula (50, 52, 130) comprising: a jacket; and a malleable member (94, 128) surrounded by the jacket, the malleable member having a proximal end, a distal end, and a lumen extending therebetween and along a lengthwise axis of the malleable cannula, a liner coupled to an inner surface of the lumen of the malleable member, the malleable member including a longitudinal strut extending parallel to the lengthwise axis and a plurality of transverse struts (100, 132) coupled to and extending laterally from the longitudinal strut and around at least a portion of the lumen of the liner, wherein the longitudinal strut is discontinuous along a longitudinal length of the malleable member and is comprised of a plurality of segments, each of the plurality of segments being circumferentially displaced from an adjacent one of the plurality of segments and about the plurality of transverse struts, the malleable member being configured to assume and maintain a formed shape of the malleable cannula. a jacket; and a malleable member (94, 128) surrounded by the jacket, the malleable member having a proximal end, a distal end, and a lumen extending therebetween and along a lengthwise axis of the malleable cannula, a liner coupled to an inner surface of the lumen of the malleable member, the malleable member including a longitudinal strut extending parallel to the lengthwise axis and a plurality of transverse struts (100, 132) coupled to and extending laterally from the longitudinal strut and around at least a portion of the lumen of the liner, wherein the longitudinal strut is discontinuous along a longitudinal length of the malleable member and is comprised of a plurality of segments, each of the plurality of segments being circumferentially displaced from an adjacent one of the plurality of segments and about the plurality of transverse struts, the malleable member being configured to assume and maintain a formed shape of the malleable cannula.
A cell mobilizing composition for use in an in vivo intraosseous method to mobilize stem cells from their native milieu, the method comprising: inserting an aspiration device into a bone marrow tissue; wherein the aspiration device has at least one elongate member with a lumen extending between a proximal opening and a distal opening; and administering a cell mobilizing composition through the at least one elongate member into the bone marrow tissue, thereby mobilizing stem cells in the bone marrow tissue from their native milieu. inserting an aspiration device into a bone marrow tissue; wherein the aspiration device has at least one elongate member with a lumen extending between a proximal opening and a distal opening; and administering a cell mobilizing composition through the at least one elongate member into the bone marrow tissue, thereby mobilizing stem cells in the bone marrow tissue from their native milieu.
A method of patterning a wavelength converting layer for LED arrays comprising depositing a wavelength converting layer onto a surface, the wavelength converting layer comprising a photoinitiator and a binder material; and patterning the wavelength converting layer by applying a nanoimprint lithography process to the wavelength converting layer, the nanoimprint lithography process comprising: applying a nanoimprint mold on the wavelength converting layer; curing the wavelength converting layer such that the photoinitiator experiences decarboxylation; and removing the nanoimprint mold from the wavelength converting layer after the curing. depositing a wavelength converting layer onto a surface, the wavelength converting layer comprising a photoinitiator and a binder material; and patterning the wavelength converting layer by applying a nanoimprint lithography process to the wavelength converting layer, the nanoimprint lithography process comprising: applying a nanoimprint mold on the wavelength converting layer; curing the wavelength converting layer such that the photoinitiator experiences decarboxylation; and removing the nanoimprint mold from the wavelength converting layer after the curing. applying a nanoimprint mold on the wavelength converting layer; curing the wavelength converting layer such that the photoinitiator experiences decarboxylation; and removing the nanoimprint mold from the wavelength converting layer after the curing.
A suture locking device comprising: a. an adapter (80, 84) for insertion into a body, said adapter (80, 84) having a proximal end, a distal end and a lip within said distal end projecting towards an interior of said distal end, wherein said distal end of said adaptor (80, 84) is at least partially cut away; b. a knot tying element releasably attachable to said distal end of said adapter (80, 84), said knot tying element having a distal and a proximal end, said proximal end of said knot tying element having a recess thereon, said proximal end of said knot tying element being insertable by angling said proximal end of said knot tying element within said at least partially cut away distal end of said adapter (80, 84) and then repositioning said knot tying element into said adaptor (80, 84) such that said knot tying element is axially aligned with said adaptor (80, 84) and said lip and said recess mate with each other to form a releasable lock. a. an adapter (80, 84) for insertion into a body, said adapter (80, 84) having a proximal end, a distal end and a lip within said distal end projecting towards an interior of said distal end, wherein said distal end of said adaptor (80, 84) is at least partially cut away; b. a knot tying element releasably attachable to said distal end of said adapter (80, 84), said knot tying element having a distal and a proximal end, said proximal end of said knot tying element having a recess thereon, said proximal end of said knot tying element being insertable by angling said proximal end of said knot tying element within said at least partially cut away distal end of said adapter (80, 84) and then repositioning said knot tying element into said adaptor (80, 84) such that said knot tying element is axially aligned with said adaptor (80, 84) and said lip and said recess mate with each other to form a releasable lock.
A method for receiving a downlink signal by a subscriber station in a wireless network, the method comprising: receiving a first pilot signal transmitted from a first antenna of a base station; receiving a second pilot signal transmitted from a second antenna of the base station; generating antenna correlation information based on the first pilot signal and the second pilot signal; transmitting, to the base station, a feedback message including the antenna correlation information; and receiving a downlink signal transmitted from the base station based on one of a transmit diversity scheme and a beamforming scheme, wherein the transmit diversity scheme is used if an amount of antenna correlation based on the antenna correlation information is lower than a threshold value, and the beamforming scheme is used if the amount of antenna correlation is higher than or equal to the threshold value. receiving a first pilot signal transmitted from a first antenna of a base station; receiving a second pilot signal transmitted from a second antenna of the base station; generating antenna correlation information based on the first pilot signal and the second pilot signal; transmitting, to the base station, a feedback message including the antenna correlation information; and receiving a downlink signal transmitted from the base station based on one of a transmit diversity scheme and a beamforming scheme, wherein the transmit diversity scheme is used if an amount of antenna correlation based on the antenna correlation information is lower than a threshold value, and the beamforming scheme is used if the amount of antenna correlation is higher than or equal to the threshold value.
A riveting method comprising riveting a first aircraft part to a second aircraft part, by means of a riveting system comprising: a riveting tooling configured to assemble the first part to the second part by riveting, wherein the riveting tooling comprises a riveting head that is intended to come into contact with the first part and/or the second part, and a plenoptic image acquisition device, wherein the plenoptic image acquisition device is secured to the riveting head, characterized in that the riveting method further comprises: capturing a plenoptic image of a rivet and of the surroundings of the rivet, by the image acquisition device, after riveting the first part to the second part, and detecting the positioning and the surface condition of the rivet, from the plenoptic image captured by the image acquisition device. a riveting tooling configured to assemble the first part to the second part by riveting, wherein the riveting tooling comprises a riveting head that is intended to come into contact with the first part and/or the second part, and a plenoptic image acquisition device, wherein the plenoptic image acquisition device is secured to the riveting head, characterized in that the riveting method further comprises: capturing a plenoptic image of a rivet and of the surroundings of the rivet, by the image acquisition device, after riveting the first part to the second part, and detecting the positioning and the surface condition of the rivet, from the plenoptic image captured by the image acquisition device. capturing a plenoptic image of a rivet and of the surroundings of the rivet, by the image acquisition device, after riveting the first part to the second part, and detecting the positioning and the surface condition of the rivet, from the plenoptic image captured by the image acquisition device.
A clutch device comprising: - a first and a second input side; - a first and a second output side; - wherein the input sides (110, 115) and the output sides (120, 125) can be rotated about a common rotational axis; - a first clutch between the first input side and the first output side; - a second clutch between the first input side and the second output side; and characterised in that it is further configured with - a third clutch between the first input side and the second input side; and - a centrifugal pendulum. - a first and a second input side; - a first and a second output side; - wherein the input sides (110, 115) and the output sides (120, 125) can be rotated about a common rotational axis; - a first clutch between the first input side and the first output side; - a second clutch between the first input side and the second output side; and characterised in that it is further configured with - a third clutch between the first input side and the second input side; and - a centrifugal pendulum.