mhurhangee/ep-ind-claims huggingface dataset:
A mold for molding a body or cap for a connector, the body or cap having a throughway defining an axis and, adjacent to one open end, in a radial plane, a plurality of first portions in which the inner wall has a first radius alternating with a plurality of second portions in which the inner wall has a second radius larger than the first radius; the mold comprising a mold body and an axial core which together define a mold cavity in the shape of the body or cap; the core having an outer sleeve and an inner pin, the pin having a distal end protruding axially from the outer sleeve and being provided with a plurality of first castellations, the sleeve having a plurality of second castellations which are complementary to the first castellations such that, in a first configuration, the first and second castellations interdigitate; wherein in the first configuration, the castellations (8,10) are arranged such that a respective recess is formed bound by the proximal end of a first castellation and the side walls of adjacent second castellations, each recess having a shape to form a respective first portion of the body or cap; the outer sleeve and inner pin being axially movable relative to one another to a second configuration in which the first and second castellations are disengaged from one another; the inner pin being subsequently rotatable to a third configuration circumferentially offset from the first and second configurations in which the first castellations can be axially withdrawn from the body or cap following a path occupied by the second castellations in the first configuration. the mold comprising a mold body and an axial core which together define a mold cavity in the shape of the body or cap; the core having an outer sleeve and an inner pin, the pin having a distal end protruding axially from the outer sleeve and being provided with a plurality of first castellations, the sleeve having a plurality of second castellations which are complementary to the first castellations such that, in a first configuration, the first and second castellations interdigitate; wherein in the first configuration, the castellations (8,10) are arranged such that a respective recess is formed bound by the proximal end of a first castellation and the side walls of adjacent second castellations, each recess having a shape to form a respective first portion of the body or cap; the outer sleeve and inner pin being axially movable relative to one another to a second configuration in which the first and second castellations are disengaged from one another; the inner pin being subsequently rotatable to a third configuration circumferentially offset from the first and second configurations in which the first castellations can be axially withdrawn from the body or cap following a path occupied by the second castellations in the first configuration.
Apparatus for wireless communications between communication modules, the apparatus comprising a main transmission line which has a plurality of coupling points, wherein the apparatus further comprises a plurality of main antennas, wherein each main antenna is linked to a coupling area for directional coupling between said main antenna and the main transmission line at a coupling point of the plurality of coupling points and each main antenna is adapted to communicate with an auxiliary antenna linked to a communication module, characterized in that the main transmission line has two terminator impedances having line-end impedances equal to the characteristic impedance of the main transmission line.
A computer-implemented method of operating an electronic flight planning system for aircraft, wherein the electronic flight planning system comprises a network interface, a flight plan deconfliction engine and a user interface, the method comprising: at the network interface, receiving as data input to the system from one or more users a plurality of flight plans forming a plurality of received flight plans, each received flight plan defining a flight by one of a plurality of aircraft (410, 415) and being associated with one of the said one or more users; determining by the flight plan deconfliction engine, for each flight by one of said plurality of aircraft, as defined in the respective received flight plan, a three-dimensional region (400, 405) of potential conflict, representative both of an uncertainty in the position of the aircraft and of a region of air exclusion appropriate for the aircraft or for the respective received flight plan; determining by the flight plan deconfliction engine, on the basis of the determined three-dimensional regions (400, 405) of potential conflict, whether any one of the received flight plans is in conflict with any one of the other received flight plans and identifying one or more conflicts between flight plans of said plurality of received flight plans; characterised in that the method further comprises: before the flight of said plurality of aircraft, communicating by the user interface the one or more conflicts to the users associated with the received flight plans for which the one or more conflicts were identified. at the network interface, receiving as data input to the system from one or more users a plurality of flight plans forming a plurality of received flight plans, each received flight plan defining a flight by one of a plurality of aircraft (410, 415) and being associated with one of the said one or more users; determining by the flight plan deconfliction engine, for each flight by one of said plurality of aircraft, as defined in the respective received flight plan, a three-dimensional region (400, 405) of potential conflict, representative both of an uncertainty in the position of the aircraft and of a region of air exclusion appropriate for the aircraft or for the respective received flight plan; determining by the flight plan deconfliction engine, on the basis of the determined three-dimensional regions (400, 405) of potential conflict, whether any one of the received flight plans is in conflict with any one of the other received flight plans and identifying one or more conflicts between flight plans of said plurality of received flight plans; characterised in that the method further comprises: before the flight of said plurality of aircraft, communicating by the user interface the one or more conflicts to the users associated with the received flight plans for which the one or more conflicts were identified.
A method of generating an ultrasonic signal comprising the steps of carrying out a first scan of the generated signal over a predetermined portion of the signal; determining a number of resonance modes within the predetermined portion and the frequencies thereof; characterised by selecting from said resonance modes that one mode which is at or nearest to a target frequency within said predetermined portion of the signal; and setting scanning limits on each side of the selected resonance mode, wherein said scanning limits are a predetermined fraction of said predetermined portion of the signal.
Protector for a shelf, door, pillar or similar structure having support legs, the protector comprising - a covering element of the support legs of the structure, formed by a profile (1.1) with a C-shaped section suitable for being adjusted on the exterior lateral contour of said support legs with a height which covers the lower part of the legs, and with a support base (1.2) to the ground and. - at least one element with a hollow truncated pyramid shape, with three inclined sides (2.1) and one open side, an open lower base and an upper base, smaller than the lower base, which is open towards the open side, which has a horizontal flat surface (2.2) in the contour of the same corresponding to the three inclined sides (2.1), where the shape of the interior contour of this horizontal flat surface (2.2) is suitable for fitting the surface around the covering element of the support leg, characterised in that the protector comprises at least one support crossbeam as a joint between two covering elements of the support legs of the structure, where said support crossbeam has, at each end of the same, means for fixing to the covering element of one of said support legs respectively, wherein the covering element of each support leg comprises at least one hole in at least one of its laterals and the fixing means of the support crossbeam to the same are formed by a groove arranged at each end and suitable for being situated to match a hole respectively, and screwing means. - a covering element of the support legs of the structure, formed by a profile (1.1) with a C-shaped section suitable for being adjusted on the exterior lateral contour of said support legs with a height which covers the lower part of the legs, and with a support base (1.2) to the ground and. - at least one element with a hollow truncated pyramid shape, with three inclined sides (2.1) and one open side, an open lower base and an upper base, smaller than the lower base, which is open towards the open side, which has a horizontal flat surface (2.2) in the contour of the same corresponding to the three inclined sides (2.1), where the shape of the interior contour of this horizontal flat surface (2.2) is suitable for fitting the surface around the covering element of the support leg,
A saddle-riding type vehicle comprising: a body frame comprising a main tube extending from a headstock to a rear of a vehicle body and a seat rail (18L, 18R) extending from the main tube to the rear; a front wheel brake configured to brake a front wheel; a rear wheel brake configured to brake a rear wheel; and a linked brake system configured to apply a braking force to the front wheel brake, too, in association with operation of a brake actuator of the rear wheel brake, the front wheel brake being a drum brake disposed on a left side of the vehicle body, the brake actuator being disposed on a right side of the vehicle body, the linked brake system comprising an equalizer configured to be attached to the brake actuator and a linking brake cable configured to connect together the equalizer and the front wheel brake, the linking brake cable pulled out from the equalizer to the rear extending to a front via a curved portion projecting to the rear to be connected to the front wheel brake, characterized in that the linking brake cable is passed from the right side of the vehicle body to the left side of the vehicle body below the seat rail (18L, 18R) and extends to the front of the vehicle body along a left side of the main tube.
A target capture oligomer comprising first and second stem segments differing in length by at least two nucleobases flanking a target-binding segment complementary to a target nucleic acid,, wherein the first stem segment comprises polyA, and the second stem segment comprises polyT or vice versa, wherein the first stem segment and the second stem segment differ in length by at least 5 nucleobase units, wherein under hybridizing conditions: in the absence of the target nucleic acid the target capture oligomer forms a stem-loop, intramolecular hybridization of the polyA and polyT of the first and second stem segments forming the stem, and the target-binding segment forming the loop; and in the presence of the target nucleic acid, the target-binding segment hybridizes to the target nucleic acid disrupting the intramolecular hybridization of the first and second stem segments resulting in the polyA or polyT of the first and second stem segments being accessible to hybridize to a complementary immobilized probe. in the absence of the target nucleic acid the target capture oligomer forms a stem-loop, intramolecular hybridization of the polyA and polyT of the first and second stem segments forming the stem, and the target-binding segment forming the loop; and in the presence of the target nucleic acid, the target-binding segment hybridizes to the target nucleic acid disrupting the intramolecular hybridization of the first and second stem segments resulting in the polyA or polyT of the first and second stem segments being accessible to hybridize to a complementary immobilized probe.
An abuse-deterrent formulation, comprising medicament, poloxamer, water-soluble anionic polysaccharide, and PEG ester; wherein: the medicament is or a pharmaceutically acceptable salt thereof; the poloxamer is poloxamer 124, the water-soluble anionic polysaccharide is gellan gum, and the PEG ester is polyoxyl stearate; wherein the weight ratio of poloxamer 124:gellan gum:polyoxyl stearate is about 40:30:30; and wherein the formulation comprises 10 mg to 50 mg of medicament. the medicament is or a pharmaceutically acceptable salt thereof; the poloxamer is poloxamer 124, the water-soluble anionic polysaccharide is gellan gum, and the PEG ester is polyoxyl stearate; wherein the weight ratio of poloxamer 124:gellan gum:polyoxyl stearate is about 40:30:30; and wherein the formulation comprises 10 mg to 50 mg of medicament.
A mattress insert comprising supporting blocks (10, 12, 14) made of a foam material and arranged on a base body, characterised in that - the supporting blocks (10, 12, 14) are arranged on the top of the base body, and the supporting blocks (10, 12, 14) are formed integrally with the base body, - the supporting blocks (10, 12, 14) comprise first supporting blocks arranged with spacings from one another, and second supporting blocks (12, 14) arranged in the spacings, wherein a height of the second supporting blocks (12, 14) relative to the bottom of the base body is lower than that of the first supporting blocks, and - gaps or cuttings are formed between the first supporting blocks and the second supporting blocks (12, 14), the first supporting blocks and the second supporting blocks (12, 14) being next to each other are compressible independently of one another, wherein the gaps or the cuttings are perpendicular to the bottom of the base body. - the supporting blocks (10, 12, 14) are arranged on the top of the base body, and the supporting blocks (10, 12, 14) are formed integrally with the base body, - the supporting blocks (10, 12, 14) comprise first supporting blocks arranged with spacings from one another, and second supporting blocks (12, 14) arranged in the spacings, wherein a height of the second supporting blocks (12, 14) relative to the bottom of the base body is lower than that of the first supporting blocks, and - gaps or cuttings are formed between the first supporting blocks and the second supporting blocks (12, 14), the first supporting blocks and the second supporting blocks (12, 14) being next to each other are compressible independently of one another, wherein the gaps or the cuttings are perpendicular to the bottom of the base body.
Method for lifting a load, in which at least one aerial drone carries at least a portion of the load and the load is connected to a further aerial drone and is partially carried and/or directed by the further aerial drone, wherein the two aerial drones (9a, b) are controlled in coordination with each other by a common controller for controlling flight movements, characterised in that a lifting and/or tensile force and/or a flight trajectory of the aerial drones (9a; 9b) is controlled by varying a rotor speed and/or a rotor torque, wherein the aerial drones (9a; 9b) each have a hydrostatic drive train for driving at least one rotor comprising at least one hydrostatic device that operates as a pump and can be driven by a drive motor, and each have at least one further hydrostatic device (133, 134) that operates as a motor and can be connected to the rotor, and said rotor speed and/or rotor torque is controlled by adjusting a hydrostatic displacement volume and/or a hydrostatic swivel angle and/or a hydrostatic pumping capacity.
A probe which is configured for a treatment device which is configured to treat a body tissue using ultrasonic vibration, the probe comprising: a waveguide main body which is extended along the longitudinal direction; and an end effecter (16, 16a, 16b) which is provided at a tip end portion of the waveguide main body and which is configured to treat the body tissue by the ultrasonic vibration transmitted through the waveguide main body, characterized in that the probe comprises: a base member (12, 12a) which includes a base surface defined by a longitudinal direction and a width direction shorter than the longitudinal direction; a waveguide main body which has a width smaller than a width of the base surface in a width direction, protrudes with respect to the base surface, and is extended along the longitudinal direction of the base surface; x wherein the base member (12, 12a) is a member which is more difficult to transmit the ultrasonic vibration than the waveguide main body. a waveguide main body which is extended along the longitudinal direction; and an end effecter (16, 16a, 16b) which is provided at a tip end portion of the waveguide main body and which is configured to treat the body tissue by the ultrasonic vibration transmitted through the waveguide main body, characterized in that the probe comprises: a base member (12, 12a) which includes a base surface defined by a longitudinal direction and a width direction shorter than the longitudinal direction; a waveguide main body which has a width smaller than a width of the base surface in a width direction, protrudes with respect to the base surface, and is extended along the longitudinal direction of the base surface; x wherein the base member (12, 12a) is a member which is more difficult to transmit the ultrasonic vibration than the waveguide main body. a base member (12, 12a) which includes a base surface defined by a longitudinal direction and a width direction shorter than the longitudinal direction; a waveguide main body which has a width smaller than a width of the base surface in a width direction, protrudes with respect to the base surface, and is extended along the longitudinal direction of the base surface; x wherein the base member (12, 12a) is a member which is more difficult to transmit the ultrasonic vibration than the waveguide main body.
Method for operating an electrical installation having a plurality of electrical loads (1, 2, 3, 4), which are connected to a basic supply voltage and upon failure of the basic supply voltage are connected to a buffer voltage in order to safeguard the supply to the electrical loads (1, 2, 3, 4) for a period of a buffer phase, wherein the buffer voltage is provided by means of an interruption-free power supply unit, characterised in that • the power supply unit is connected to the plurality of electrical loads (1, 2, 3, 4) in order to exchange data via a field bus, • the plurality of electrical loads (1, 2, 3, 4) are each provided with a software module (11,..., 15), which is included in the communication via the field bus, • the software module of at least one load and the software modules (11,..., 14) of the other loads (2, 3, 4) is/are set as a master and as a slave respectively within the meaning of a master-slave communication, • the master in the power supply unit is registered as a communication partner for realising a regulated cut-off process of the electrical loads (1, 2, 3, 4), • in the event of a fault in the basic supply voltage the power supply unit communicates this fault via the field bus to the master and the regulated cut-off process is started as a result. • the power supply unit is connected to the plurality of electrical loads (1, 2, 3, 4) in order to exchange data via a field bus, • the plurality of electrical loads (1, 2, 3, 4) are each provided with a software module (11,..., 15), which is included in the communication via the field bus, • the software module of at least one load and the software modules (11,..., 14) of the other loads (2, 3, 4) is/are set as a master and as a slave respectively within the meaning of a master-slave communication, • the master in the power supply unit is registered as a communication partner for realising a regulated cut-off process of the electrical loads (1, 2, 3, 4), • in the event of a fault in the basic supply voltage the power supply unit communicates this fault via the field bus to the master and the regulated cut-off process is started as a result.
Wind energy installation with a rotor, a rotor shaft (12, 21) connected fixedly to the rotor and a gearbox (13, 22) coupled to the rotor shaft (12, 21), where the rotor is mounted via a movable bearing (14, 24) arranged at the rotor-side end of the rotor shaft, and also, on the machine carrier of the wind energy installation, via two elastomer bearings (17, 25) arranged laterally on the gearbox, characterized in that the rotor is furthermore mounted via a fixed bearing which is arranged in or on the gearbox and is arranged directly or indirectly at the gearbox-side end of the rotor shaft, and the elastomer bearings (17, 25) are designed for absorbing axial forces acting on the rotor.
A device for ventilating a confined space (3, 3A) of the type comprising at least one ventilation duct (7, 29) which opens, on the one hand, into the confined space (3, 3A), and, on the other hand, outside this confined space (3, 3A), the confined space (3, 3A) being organised so as to accommodate a circulation of air according to a first pathway (27; 21, 39; 51) inside the confined space (3, 3A), and a circulation of air according to a second pathway (27; 18, 39; 62) extending from the inside of the confined space (3, 3A) to the ventilation duct (7, 29), the device comprising a transition area organised in the confined space (3, 3A), between the first pathway (27; 21, 39; 51) and the second pathway (27; 18, 39; 62), at least one fan unit arranged in the confined space (3, 3A) so as to expel air into the transition area and at least one damper (19, 59, 61) mounted in the confined space (3, 3A), in the transition area, and in that the damper (19, 59, 61) being able to be controlled between a first state where it conducts the air expelled by the fan unit predominantly according to the first pathway (27; 21, 39; 51) and a second state where it conducts the air expelled by the fan unit predominantly according to the second pathway (27; 18, 39; 62).
A method of mounting a printed circuit board, PCB, to a base comprising: providing a power supply in the base, the power supply comprising a cavity within the base for receiving a battery and a battery terminal; fixing a location of a PCB contact on the base by installing a battery contact into the base, wherein the battery contact comprises the battery terminal, the PCB contact and an adaptor element, the PCB contact being electrically connected to the battery terminal via the adaptor element; pushing the PCB in a direction perpendicular to a plane of the PCB into a position on the base, and mechanically engaging, simultaneously with pushing the PCB into the position on the base, a PCB-to-power-contact connected to the PCB to the PCB contact and electrically connecting the PCB-to-power-contact to the PCB contact, characterised in that the PCB contact comprises a rail and the mechanically engaging the PCB-to-power-contact connected to the PCB to the PCB contact and electrically connecting said PCB-to-power-contact to said PCB contact includes clasping the rail from opposite sides. providing a power supply in the base, the power supply comprising a cavity within the base for receiving a battery and a battery terminal; fixing a location of a PCB contact on the base by installing a battery contact into the base, wherein the battery contact comprises the battery terminal, the PCB contact and an adaptor element, the PCB contact being electrically connected to the battery terminal via the adaptor element; pushing the PCB in a direction perpendicular to a plane of the PCB into a position on the base, and mechanically engaging, simultaneously with pushing the PCB into the position on the base, a PCB-to-power-contact connected to the PCB to the PCB contact and electrically connecting the PCB-to-power-contact to the PCB contact, characterised in that the PCB contact comprises a rail and the mechanically engaging the PCB-to-power-contact connected to the PCB to the PCB contact and electrically connecting said PCB-to-power-contact to said PCB contact includes clasping the rail from opposite sides.