mhurhangee/patent-ind-claim-en huggingface dataset:
A clot retrieval device for removing occlusive clot from a blood vessel, the device comprising: an inner elongate body having a collapsed delivery configuration and an expanded deployed configuration; an outer elongate body at least partially overlying the inner elongate body; the outer elongate body being expandable relative to the inner elongate body to a radial extent which is greater than the radial extent of the inner body in the deployed configuration such that in the expanded configuration, the outer elongate body is radially spaced-apart from the inner elongate body to define therebetween an interior reception space ; wherein the outer elongate body comprises a plurality of longitudinally spaced-apart outer clot engaging regions , wherein at least two of said outer clot engaging regions are connected by members comprising hinge elements , and a plurality of clot-receiving openings are located between the outer clot engaging regions, the clot engaging regions being adapted, on engagement with clot, to urge clot towards at least one of the clot-receiving openings and into the reception space. an inner elongate body having a collapsed delivery configuration and an expanded deployed configuration; an outer elongate body at least partially overlying the inner elongate body; the outer elongate body being expandable relative to the inner elongate body to a radial extent which is greater than the radial extent of the inner body in the deployed configuration such that in the expanded configuration, the outer elongate body is radially spaced-apart from the inner elongate body to define therebetween an interior reception space ; wherein the outer elongate body comprises a plurality of longitudinally spaced-apart outer clot engaging regions , wherein at least two of said outer clot engaging regions are connected by members comprising hinge elements , and a plurality of clot-receiving openings are located between the outer clot engaging regions, the clot engaging regions being adapted, on engagement with clot, to urge clot towards at least one of the clot-receiving openings and into the reception space.
A device for covering and/or reconstructing a bone defect site , - having a cap which has an edge and a wall directed away from the bone defect and a wall directed towards the bone defect, wherein the cap is made of a dimensionally stable material and a wall of the cap directed towards the bone defect or a wall of the cap directed away from the bone defect corresponds to the shape of the regenerated bone, characterized in that at least one positioning means without an opening is arranged on the edge of the cap , said positioning means having a wall directed towards a healthy bone adjacent to the bone defect and corresponding thereto, at least in part, or that the device has at least one fixing means for fixing the cap within the bone defect site and at least one positioning means without an opening on the edge of the cap , said positioning means having a wall directed towards a healthy bone adjacent to the bone defect and corresponding thereto, at least in part. - having a cap which has an edge and a wall directed away from the bone defect and a wall directed towards the bone defect, wherein the cap is made of a dimensionally stable material and a wall of the cap directed towards the bone defect or a wall of the cap directed away from the bone defect corresponds to the shape of the regenerated bone, characterized in that at least one positioning means without an opening is arranged on the edge of the cap , said positioning means having a wall directed towards a healthy bone adjacent to the bone defect and corresponding thereto, at least in part, or that the device has at least one fixing means for fixing the cap within the bone defect site and at least one positioning means without an opening on the edge of the cap , said positioning means having a wall directed towards a healthy bone adjacent to the bone defect and corresponding thereto, at least in part.
A liquid dispenser for watering animals, which comprises a main body including a main duct , wherein the main body develops along a longitudinal axis (A) from a rear side to a front side of the dispenser, wherein an animal can drink from the front side of the dispenser liquids dispensed through the main duct , wherein a stem is arranged in the main duct and includes a head urged by elastic means towards the main duct , wherein an auxiliary body is fixed to the main body and includes an auxiliary duct , wherein the head of the stem and the elastic means are arranged in a chamber connecting the main duct with the auxiliary duct , characterized in that the auxiliary body is fixed to the main body by means of extensions engaged with protuberances to prevent reciprocal axial movements between the main body and the auxiliary body , wherein the protuberances are spaced apart to form channels and the extensions are spaced apart to form notches , each notch being comprised between two extensions , wherein a locking element is fixed to the main body and/or to the auxiliary body , wherein the locking element comprises a collar provided with a plurality of ribs which are arranged in the channels and/or in the notches to prevent mutual rotations around the longitudinal axis (A) of the main body with respect to the auxiliary body .
A landing structure for use with an unmanned aerial vehicle, UAV, comprising a) a winch system comprising a tether coupleable to a payload and b) a boom with a first landing pad and a second landing pad , wherein the first landing pad and the second landing pad each have a pin that extends below the pad, wherein the landing structure comprises: a landing platform for the UAV; a cavity within the landing platform , wherein the cavity is aligned over a predetermined target location and is sized to allow the winch system of the UAV to pass the payload , when such is coupled to the tether, through the cavity ; a touchdown area for the UAV; a track comprising a slot in the landing platform that runs along the landing platform and along at least a portion of the cavity such that the track guides the UAV to a docked position in which the tether is positioned over the cavity , such that the tether can raise or lower the payload , when such is coupled to the tether , through the cavity , wherein the slot at least partially surrounds the touchdown area such that the UAV is able to land in the touchdown area at a number of different orientations and thrust forward in order to engage the slot which then guides the UAV to the docked position over the cavity , and wherein the slot is configured such that, when the UAV lands in the touchdown area and thrusts forward, the pin in the first landing pad will engage the slot, then the pin in the second landing pad will engage the slot so, as the UAV continues thrust forward, the UAV will follow a path of the slot to the docked position over the cavity . a landing platform for the UAV; a cavity within the landing platform , wherein the cavity is aligned over a predetermined target location and is sized to allow the winch system of the UAV to pass the payload , when such is coupled to the tether, through the cavity ; a touchdown area for the UAV; a track comprising a slot in the landing platform that runs along the landing platform and along at least a portion of the cavity such that the track guides the UAV to a docked position in which the tether is positioned over the cavity , such that the tether can raise or lower the payload , when such is coupled to the tether , through the cavity , wherein the slot at least partially surrounds the touchdown area such that the UAV is able to land in the touchdown area at a number of different orientations and thrust forward in order to engage the slot which then guides the UAV to the docked position over the cavity , and wherein the slot is configured such that, when the UAV lands in the touchdown area and thrusts forward, the pin in the first landing pad will engage the slot, then the pin in the second landing pad will engage the slot so, as the UAV continues thrust forward, the UAV will follow a path of the slot to the docked position over the cavity .
A method for communicating in a wireless communications system , the method comprising: receiving, by a station , a frame comprising scheduling information and a first indicator indicating a first length of a first cyclic prefix, wherein the scheduling information comprises information for an uplink transmission scheduled for the station, and the frame is received in accordance with the first cyclic prefix; determining, by the station , a second length of a second cyclic prefix for the uplink transmission based on that the scheduling information includes scheduling information for more than one station , and the first indicator, the second length of the second cyclic prefix being 1.6 us or 3.2 us, wherein, the second length of the second cyclic prefix is 1.6 us when the first length of the first cyclic prefix is 0.8 us, and the second length of the second cyclic prefix is 3.2 us when the first length of the first cyclic prefix is 1.6 us or 3.2 us; and transmitting, by the station , the uplink transmission in accordance with the second cyclic prefix. receiving, by a station , a frame comprising scheduling information and a first indicator indicating a first length of a first cyclic prefix, wherein the scheduling information comprises information for an uplink transmission scheduled for the station, and the frame is received in accordance with the first cyclic prefix; determining, by the station , a second length of a second cyclic prefix for the uplink transmission based on that the scheduling information includes scheduling information for more than one station , and the first indicator, the second length of the second cyclic prefix being 1.6 us or 3.2 us, wherein, the second length of the second cyclic prefix is 1.6 us when the first length of the first cyclic prefix is 0.8 us, and the second length of the second cyclic prefix is 3.2 us when the first length of the first cyclic prefix is 1.6 us or 3.2 us; and transmitting, by the station , the uplink transmission in accordance with the second cyclic prefix.
A joint, comprising: a first panel having a first honeycomb core having a first thickness, the first honeycomb core being sandwiched between a first skin and a second skin , wherein a first longitudinal edge of the first panel has a rabbet formed along a majority of an entire length of the first longitudinal edge; a second panel having a second honeycomb core having a second thickness, the second honeycomb core being sandwiched between a third skin and a fourth skin , wherein a second longitudinal edge of the second panel has a notch formed along a majority of an entire length of the second longitudinal edge, wherein at least a portion of the rabbet is positioned within the notch such that the first longitudinal edge and the second longitudinal edge are aligned to form the joint; and an adhesive applied to at least one of the first longitudinal edge and the second longitudinal edge wherein the second skin of the first panel and the third skin of the second panel are oriented at a joint angle with respect to one another, the joint angle being non-parallel and non-perpendicular. a first panel having a first honeycomb core having a first thickness, the first honeycomb core being sandwiched between a first skin and a second skin , wherein a first longitudinal edge of the first panel has a rabbet formed along a majority of an entire length of the first longitudinal edge; a second panel having a second honeycomb core having a second thickness, the second honeycomb core being sandwiched between a third skin and a fourth skin , wherein a second longitudinal edge of the second panel has a notch formed along a majority of an entire length of the second longitudinal edge, wherein at least a portion of the rabbet is positioned within the notch such that the first longitudinal edge and the second longitudinal edge are aligned to form the joint; and an adhesive applied to at least one of the first longitudinal edge and the second longitudinal edge wherein the second skin of the first panel and the third skin of the second panel are oriented at a joint angle with respect to one another, the joint angle being non-parallel and non-perpendicular.
A method for gain shape vector encoding performed by an audio encoder, where the encoding of each vector segment is subjected to a constraint related to a maximum number of bits, B MAX , allowed for encoding a vector segment, the method comprising: - determining an initial number, Np_ init , of segments for a target vector x based at least on B MAX and number of bits allocated for encoding the entire vector x; - determining a log-energy of each Np _init target vector segment by summing energies of samples within the vector segment; - determining an average number of bits per segment, B AVG , based on the number of bits allocated for encoding the entire vector x and Np_ init ; - determining a final number of segments to be used in the gain shape vector encoding by increasing the number of segments, as compared to the initial number, for the target vector x, when the difference between B MAX and B AVG is smaller than a threshold , wherein the threshold depends on a maximum deviation of a target vector segment energy from an average per-segment energy value, E AVG , for the target vector x. - determining an initial number, Np_ init , of segments for a target vector x based at least on B MAX and number of bits allocated for encoding the entire vector x; - determining a log-energy of each Np _init target vector segment by summing energies of samples within the vector segment; - determining an average number of bits per segment, B AVG , based on the number of bits allocated for encoding the entire vector x and Np_ init ; - determining a final number of segments to be used in the gain shape vector encoding by increasing the number of segments, as compared to the initial number, for the target vector x, when the difference between B MAX and B AVG is smaller than a threshold , wherein the threshold depends on a maximum deviation of a target vector segment energy from an average per-segment energy value, E AVG , for the target vector x.
Method of operating an internal combustion engine with several cylinders , namely a method for the cylinder-specific detection of ignition misfires, with the aid of at least one exhaust gas sensor the exhaust gas from of each cylinder of the internal combustion engine for the respective cylinder at least one exhaust gas value is individually measured for the respective cylinder , and the respective measured actual value of the exhaust gas is compared with an exhaust gas setpoint value, which is dependent on the exhaust gas actual value of at least one other cylinder , in order to determine for each of the cylinders at least one cylinder-specific deviation between the exhaust gas setpoint value and the actual exhaust-gas value and wherein for each cylinder , on the basis of the deviation or each cylinder-individual deviation, it is determined individually whether misfires are present at the respective cylinder, wherein the actual exhaust gas value for each cylinder is an actual NOx value which is measured by an NOx sensor and/or a fuel/air ratio or residual oxygen content measured by a lambda sensor, and the exhaust gas setpoint of a cylinder is an average value of the exhaust gas actual values of at least one of the other cylinders , whereby for the calibration of the respective exhaust gas sensor , the respective exhaust gas sensor is exposed to a reference gas, wherein the calibration is carried out on the basis of a reference gas sensor with reference gas, wherein the calibration is carried out on the basis of a measured value and wherein, after calibration, the respective exhaust gas sensor is again exposed to exhaust gas.
A bushing (10; 110; 210), comprising: a body extending axially along a longitudinal axis between opposite ends (16, 18; 116, 118) and radially from an outer surface to an inner surface , said body including a first material (A) and a second material (B) different from said first material, and said first material is an iron-based material including 10 to 30 wt% Cr, 0 to 21 wt% Ni, 0 to 10 wt% Mo, 0 to 5 wt% W, 0 to 3 wt% C, 0 to 4 wt% V, 0 to 20 wt% Co, and Fe, based on the total weight of said first material characterised in that said second material (B) is a cobalt based material. a body extending axially along a longitudinal axis between opposite ends (16, 18; 116, 118) and radially from an outer surface to an inner surface , said body including a first material (A) and a second material (B) different from said first material, and said first material is an iron-based material including 10 to 30 wt% Cr, 0 to 21 wt% Ni, 0 to 10 wt% Mo, 0 to 5 wt% W, 0 to 3 wt% C, 0 to 4 wt% V, 0 to 20 wt% Co, and Fe, based on the total weight of said first material characterised in that said second material (B) is a cobalt based material.
A user equipment, UE, configured to communicate with a base station apparatus on one or more downlink bandwidth parts, DL BWPs, the one or more DL BWPs being configured for each of one or more serving cells, comprising: a receiving unit configured to receive a first radio resource control, RRC, message comprising first information used for configuring a monitoring periodicity of a physical downlink control channel, PDCCH, the receiving unit configured to receive a second RRC message comprising second information used for configuring more than one timing offset values, the receiving unit configured to monitor the PDCCH based on the first information, the receiving unit configured to receive on the PDCCH, a downlink control information, DCI, format comprising third information and fourth information, the third information triggering an aperiodic channel state information, CSI, report, the fourth information being used for indicating one timing offset value from the more than one timing offset values, the DCI format being used for scheduling of a physical uplink shared channel, PUSCH, and a transmitting unit configured to perform, based on decoding of the DCI format comprising the third information and the fourth information, an aperiodic CSI reporting on the PUSCH in a timing slot, the timing slot being determined based on the fourth information, wherein the first information is configured for each of one or more search space sets to monitor the PDCCH, the one or more search space sets being configured for each of the one or more DL BWPs, and the second information is configured for each of the one or more serving cells for configuring the more than one timing offset values. a receiving unit configured to receive a first radio resource control, RRC, message comprising first information used for configuring a monitoring periodicity of a physical downlink control channel, PDCCH, the receiving unit configured to receive a second RRC message comprising second information used for configuring more than one timing offset values, the receiving unit configured to monitor the PDCCH based on the first information, the receiving unit configured to receive on the PDCCH, a downlink control information, DCI, format comprising third information and fourth information, the third information triggering an aperiodic channel state information, CSI, report, the fourth information being used for indicating one timing offset value from the more than one timing offset values, the DCI format being used for scheduling of a physical uplink shared channel, PUSCH, and a transmitting unit configured to perform, based on decoding of the DCI format comprising the third information and the fourth information, an aperiodic CSI reporting on the PUSCH in a timing slot, the timing slot being determined based on the fourth information, wherein the first information is configured for each of one or more search space sets to monitor the PDCCH, the one or more search space sets being configured for each of the one or more DL BWPs, and the second information is configured for each of the one or more serving cells for configuring the more than one timing offset values.
A fastener assembly for affixing an insulation blanket to an engine nacelle of an aircraft, comprising: a substrate ; an insulation blanket having a mounting hole ; an attachment member including a base adhered to said substrate and a male threaded element ; a cap fastener including a radially enlarged cap member having a radial size and shape greater than said mounting hole , said cap member having an exterior side and an interior side , said cap fastener further including a second fastener element made of metal which includes a head and a metal female threaded element extending from said cap member's interior side projecting at least partially through said mounting hole to threadably affix to said male threaded element , wherein said cap member's interior side overlies and engages said insulation blanket in a region surrounding said mounting hole so as to affix said insulation blanket to said substrate ; and said cap member's interior side having a substantially concave surface forming a circular recess surrounding said second fastener element creating a circular insulating cavity in conjunction with said insulation blanket , characterized in that the cap fastener is made of a composite plastic material and that said cap member encapsulates said head so as to prevent rotation of said cap member relative to said second fastener element . a substrate ; an insulation blanket having a mounting hole ; an attachment member including a base adhered to said substrate and a male threaded element ; a cap fastener including a radially enlarged cap member having a radial size and shape greater than said mounting hole , said cap member having an exterior side and an interior side , said cap fastener further including a second fastener element made of metal which includes a head and a metal female threaded element extending from said cap member's interior side projecting at least partially through said mounting hole to threadably affix to said male threaded element , wherein said cap member's interior side overlies and engages said insulation blanket in a region surrounding said mounting hole so as to affix said insulation blanket to said substrate ; and said cap member's interior side having a substantially concave surface forming a circular recess surrounding said second fastener element creating a circular insulating cavity in conjunction with said insulation blanket , characterized in that the cap fastener is made of a composite plastic material and that said cap member encapsulates said head so as to prevent rotation of said cap member relative to said second fastener element .
A method for reading an optical code , wherein a brightness profile of the code is recorded, light and dark subregions are identified in the brightness profile, and the code content of the optical code is read, characterized in that first sum measures for the amount of light in the respective light subregions and second sum measures for the amount of light missing from a white level in the respective dark subregions are determined from the brightness profile, and the code content is read on the basis of the first and second sum measures.