mhurhangee/ep-ind-claims huggingface dataset:
Apparatus for use on a construction or worksite machine which is provided with a main body and at least one lift/lower element coupled to the main body, the apparatus comprising: at least one hydraulic cylinder (3, 4, 5) for operating the lift/lower element: at least one hydraulic pump that has at least one electric motor coupled thereto for operating the hydraulic pump, the pump being configured for pumping hydraulic fluid along a flowline for operating at least one hydraulic cylinder that is coupled to the lift/lower element; and energy supply means comprising: at least one battery to provide electrical energy to the electric motor; and at least one hydrogen fuel cell for generating and supplying the battery with electrical energy for charging the battery; wherein the hydraulic cylinder is configured to provide volumetric neutral operation; wherein the hydraulic cylinder is configured to retract or extend to under load, and characterised in that the hydraulic pump is operable in motor mode using hydraulic fluid driven by the load to communicate energy from the cylinder to transfer the energy produced by the hydraulic cylinder under load to at least one energy storage unit, wherein the energy storage unit comprises the battery. at least one hydraulic pump that has at least one electric motor coupled thereto for operating the hydraulic pump, the pump being configured for pumping hydraulic fluid along a flowline for operating at least one hydraulic cylinder that is coupled to the lift/lower element; and energy supply means comprising: at least one battery to provide electrical energy to the electric motor; and at least one hydrogen fuel cell for generating and supplying the battery with electrical energy for charging the battery; at least one battery to provide electrical energy to the electric motor; and at least one hydrogen fuel cell for generating and supplying the battery with electrical energy for charging the battery; wherein the hydraulic cylinder is configured to provide volumetric neutral operation; wherein the hydraulic cylinder is configured to retract or extend to under load, and characterised in that the hydraulic pump is operable in motor mode using hydraulic fluid driven by the load to communicate energy from the cylinder to transfer the energy produced by the hydraulic cylinder under load to at least one energy storage unit, wherein the energy storage unit comprises the battery.
A piezoelectric material containing: a first component that is a rhombohedral crystal at room temperature that is configured to comprise a complex oxide with a perovskite structure and that has a Curie temperature of Tc1 in a single composition; a second component that is a crystal other than a rhombohedral crystal at room temperature that is configured to comprise a complex oxide with a perovskite structure and that has a Curie temperature of Tc2 in a single composition; and a third component that is configured to comprise a complex oxide with a perovskite structure in which the component is a crystal other than a rhombohedral crystal at room temperature that has a Curie temperature of Tc3 in a single composition, wherein Tc1 is higher than Tc2, wherein Tc3 is equal to or higher than Tc1, and characterized in that the value of (0.9×Tc1+0.1×Tc2) is equal to or lower than 280°C. a first component that is a rhombohedral crystal at room temperature that is configured to comprise a complex oxide with a perovskite structure and that has a Curie temperature of Tc1 in a single composition; a second component that is a crystal other than a rhombohedral crystal at room temperature that is configured to comprise a complex oxide with a perovskite structure and that has a Curie temperature of Tc2 in a single composition; and a third component that is configured to comprise a complex oxide with a perovskite structure in which the component is a crystal other than a rhombohedral crystal at room temperature that has a Curie temperature of Tc3 in a single composition,
Catheter system comprising cannulas for vascular puncture with double or triple cut tip comprising, (i) an outer part (non-cutting element), a tube-like construction of 0,9 to 1,2 mm in outer diameter, and 0,8 - 1,1 mm inner diameter which is slightly flexible, of a metal or plastic material, (a) the tip zone being optionally tapered to ease introduction, (b) the edges being optionally rounded to provide atraumatic advancement (c) optionally with a Luer-lock connector. (ii) a hollow needle which is flexible and bendable (a) with a transparent flashback chamber, wherein (b) the diameter of the needle is below the diameter of the catheter, wherein (iii) the needle and catheter are connected by a temporary lock to ensure the needle tip is fixed in adequate position outside the catheter during skin puncture and introduction towards the target region. (i) an outer part (non-cutting element), a tube-like construction of 0,9 to 1,2 mm in outer diameter, and 0,8 - 1,1 mm inner diameter which is slightly flexible, of a metal or plastic material, (a) the tip zone being optionally tapered to ease introduction, (b) the edges being optionally rounded to provide atraumatic advancement (c) optionally with a Luer-lock connector. (a) the tip zone being optionally tapered to ease introduction, (b) the edges being optionally rounded to provide atraumatic advancement (c) optionally with a Luer-lock connector. (ii) a hollow needle which is flexible and bendable (a) with a transparent flashback chamber, wherein (b) the diameter of the needle is below the diameter of the catheter, wherein (a) with a transparent flashback chamber, wherein (b) the diameter of the needle is below the diameter of the catheter, wherein (iii) the needle and catheter are connected by a temporary lock to ensure the needle tip is fixed in adequate position outside the catheter during skin puncture and introduction towards the target region.
A secure communication management, SCM, computer device for providing secure data connections in an aviation environment, said SCM computer device comprising a processor in communication with a memory, said processor programmed to: receive, from a first user computer device, a first data message for a first aircraft, wherein the first data message is in a standardized data format; analyze the first data message for potential cybersecurity threats; if the analysis is that the first data message does not contain a cybersecurity threat, convert the first data message into a first data format associated with the first aircraft; and transmit the converted first data message to the first aircraft using a first communication protocol associated with the first aircraft; wherein the first data message is also configured to be transmitted to a second aircraft, and wherein the processor is further programmed to: convert the first data message into a second format associated with the second aircraft; and transmit the converted first data message to the second aircraft using a second communication protocol associated with the second aircraft. receive, from a first user computer device, a first data message for a first aircraft, wherein the first data message is in a standardized data format; analyze the first data message for potential cybersecurity threats; if the analysis is that the first data message does not contain a cybersecurity threat, convert the first data message into a first data format associated with the first aircraft; and transmit the converted first data message to the first aircraft using a first communication protocol associated with the first aircraft; wherein the first data message is also configured to be transmitted to a second aircraft, and wherein the processor is further programmed to: convert the first data message into a second format associated with the second aircraft; and transmit the converted first data message to the second aircraft using a second communication protocol associated with the second aircraft. convert the first data message into a second format associated with the second aircraft; and transmit the converted first data message to the second aircraft using a second communication protocol associated with the second aircraft.
Blind rivet nut for insertion into an aperture formed in one or more layers of material comprising: - a head forming a flange; - a shank comprising a head end, a foot end and a cylindrical bore extending along a longitudinal axis from the head end to the foot end, the bore having a first bore segment near the foot end, provided with an internal thread and a second bore segment near the head end whose diameter is greater than the diameter of the first bore segment, the wall surrounding the second bore segment forming a deformable region of the shank and having an external wall diameter, the foot end having a foot end diameter, characterized in that the foot end of the shank comprises a tapered chamfer making a foot end angle of 21 to 25 degrees with the longitudinal axis, and wherein the ratio of the foot end diameter to the external wall diameter is between 0.65 and 0.82. - a head forming a flange; - a shank comprising a head end, a foot end and a cylindrical bore extending along a longitudinal axis from the head end to the foot end, the bore having a first bore segment near the foot end, provided with an internal thread and a second bore segment near the head end whose diameter is greater than the diameter of the first bore segment, the wall surrounding the second bore segment forming a deformable region of the shank and having an external wall diameter, the foot end having a foot end diameter,
Agricultural plant, in particular for productive life stock, comprising a stationarily installed suspension rail route and at least one self-propelled robot running at the suspension rail route, the robot having at least one container and at least one rotary driven robot-drive for moving the robot along the suspension rail route, wherein for transmitting driving and braking torques between the robot and the suspension rail route a mechanic drive connection is provided and a positive locking drive connection can be established at least in a section of the suspension rail route between the robot-drive of the robot and the suspension rail route, characterized in that the robot-drive of the robot is a combination of a friction wheel drive for a frictionally engaged mechanic drive connection with the suspension rail route and a gear wheel drive for a positive locking mechanic drive connection with the suspension rail route and that the robot-drive can be shifted between both drive modes.
A fuel injector comprising a high pressure circuit, a low pressure circuit, an actuator located within the low pressure circuit, and an inverter/amplifier assembly located within the high pressure circuit and coupled to a nozzle needle; wherein the high pressure circuit and the low pressure circuit are separated by a separating assembly comprising a separating member and a connecting pin located in a through bore of the separating member, the connecting pin being coupled to the actuator and to the inverter/amplifier assembly; wherein the actuator is arranged to selectively apply a force to the inverter/amplifier assembly, via the connecting pin, thereby to initiate an injection event; wherein the separating assembly further comprises a sleeve (138,138') located around part of the connecting pin, such that the through bore and the connecting pin are separated by the sleeve (138,138'), the connecting pin being movable within the sleeve (138,138') and, a sub-assembly comprising the sleeve and connecting pin being inserted in a press fit into the through bore, and wherein a first shoulder surface is provided on a projection of the sleeve (138,138'), and a second shoulder surface is provided at a junction of a first through bore section remote from the low pressure circuit and a second through bore section between the first through bore section and the low pressure circuit, the second through bore section being of a smaller diameter than the first through bore section, and wherein the first shoulder surface is arranged for complementary abutment with the second shoulder surface thereby providing a restraining means. wherein the high pressure circuit and the low pressure circuit are separated by a separating assembly comprising a separating member and a connecting pin located in a through bore of the separating member, the connecting pin being coupled to the actuator and to the inverter/amplifier assembly; wherein the actuator is arranged to selectively apply a force to the inverter/amplifier assembly, via the connecting pin, thereby to initiate an injection event; wherein the separating assembly further comprises a sleeve (138,138') located around part of the connecting pin, such that the through bore and the connecting pin are separated by the sleeve (138,138'), the connecting pin being movable within the sleeve (138,138') and, a sub-assembly comprising the sleeve and connecting pin being inserted in a press fit into the through bore, and wherein a first shoulder surface is provided on a projection of the sleeve (138,138'), and a second shoulder surface is provided at a junction of a first through bore section remote from the low pressure circuit and a second through bore section between the first through bore section and the low pressure circuit, the second through bore section being of a smaller diameter than the first through bore section, and wherein the first shoulder surface is arranged for complementary abutment with the second shoulder surface thereby providing a restraining means.
An audio processing device comprising: an earphone including a speaker unit, a microphone, a cord, and a cord holding part; and a main unit, wherein the main unit is adapted to process an audio signal sent from the microphone and is adapted to output the processed signal to the speaker unit; the earphone includes a housing storing the microphone and the speaker unit; the cord electrically connects the main unit with the earphone, and the housing includes a microphone hole part; characterised in that the cord holding part, having bending rigidity greater than that of the cord, projects outside the housing so that a gap is provided between the cord holding part and the microphone hole part. an earphone including a speaker unit, a microphone, a cord, and a cord holding part; and a main unit, wherein the main unit is adapted to process an audio signal sent from the microphone and is adapted to output the processed signal to the speaker unit; the earphone includes a housing storing the microphone and the speaker unit; the cord electrically connects the main unit with the earphone, and the housing includes a microphone hole part; characterised in that the cord holding part, having bending rigidity greater than that of the cord, projects outside the housing so that a gap is provided between the cord holding part and the microphone hole part.
A staple cartridge assembly for use with a surgical stapling instrument, wherein the staple cartridge assembly comprises: a staple cartridge, comprising: a plurality of staples; and a cartridge deck defining a proximal end and a distal end; and a compressible adjunct releasably secured to the cartridge deck, wherein the staples are deployable into tissue captured against the compressible adjunct, and wherein the compressible adjunct comprises: a tissue-facing layer; a deck-facing layer, wherein the tissue-facing layer is spaced apart from the deck-facing layer, and wherein the deck-facing layer comprises: an outer surface; and an inner surface; a first spacer fiber extending from the tissue-facing layer toward the inner surface; a second spacer fiber extending from the tissue-facing layer toward the inner surface, wherein the first spacer fiber and the second spacer fiber extend through the deck-facing layer; and characterized in that the compressible adjunct comprises a loop defined by the first spacer fiber and the second spacer fiber on the outer surface. a staple cartridge, comprising: a plurality of staples; and a cartridge deck defining a proximal end and a distal end; and a plurality of staples; and a cartridge deck defining a proximal end and a distal end; and a compressible adjunct releasably secured to the cartridge deck, wherein the staples are deployable into tissue captured against the compressible adjunct, and wherein the compressible adjunct comprises: a tissue-facing layer; a deck-facing layer, wherein the tissue-facing layer is spaced apart from the deck-facing layer, and wherein the deck-facing layer comprises: an outer surface; and an inner surface; a first spacer fiber extending from the tissue-facing layer toward the inner surface; a second spacer fiber extending from the tissue-facing layer toward the inner surface, wherein the first spacer fiber and the second spacer fiber extend through the deck-facing layer; and characterized in that the compressible adjunct comprises a loop defined by the first spacer fiber and the second spacer fiber on the outer surface. a tissue-facing layer; a deck-facing layer, wherein the tissue-facing layer is spaced apart from the deck-facing layer, and wherein the deck-facing layer comprises: an outer surface; and an inner surface; an outer surface; and an inner surface; a first spacer fiber extending from the tissue-facing layer toward the inner surface; a second spacer fiber extending from the tissue-facing layer toward the inner surface, wherein the first spacer fiber and the second spacer fiber extend through the deck-facing layer; and characterized in that the compressible adjunct comprises a loop defined by the first spacer fiber and the second spacer fiber on the outer surface.
Airplane for civil transports comprising: - a fuselage element adapted to transport persons and/or merchandise; - gliding means (4, 5) associated with said fuselage element to assemble an aircraft body (2, 4, 5) fit for flight and comprising a couple of wing groups placed on opposite positions with respect to said fuselage element; - thrusting means associated with said aircraft body (2, 4, 5) and adapted to give a flight thrust to said aircraft body (2, 4, 5); wherein said thrusting means are adjustable with respect to said wing groups, and wherein the airplane comprises at least a stabilizing element associated with said aircraft body (2, 4, 5) and adapted to stabilize said aircraft body (2, 4, 5) in buoyancy; characterized in that said stabilizing element is movable with respect to said wing group between a closed configuration, in which said stabilizing element is adjacent to said wing group, and an open configuration in which said stabilizing element is wide apart from said wing group, wherein the fuselage element is provided with two sets of wheels adapted to enable the airplane to taxi when it is on the ground. - a fuselage element adapted to transport persons and/or merchandise; - gliding means (4, 5) associated with said fuselage element to assemble an aircraft body (2, 4, 5) fit for flight and comprising a couple of wing groups placed on opposite positions with respect to said fuselage element; - thrusting means associated with said aircraft body (2, 4, 5) and adapted to give a flight thrust to said aircraft body (2, 4, 5);
A user equipment comprising: a receiver configured to detect a Physical Downlink Control Channel, PDCCH, and a channel measurement unit configured to perform a measurement for computing a Channel Quality Indicator, CQI, value, wherein the receiver detects the PDCCH with Downlink Control Information, DCI, with a Cyclic Redundancy Check, CRC, scrambled by a Radio Network Temporary Identifier, RNTI, according to a DCI format 1C on a serving cell, characterized in that Z in a case that the receiver does not successively detect the PDCCH over a predetermined number of subframes in an ON/OFF cell for which the ON state is configured, the channel measurement unit (i) assumes that a base station does not perform downlink transmission in a specific subframe and (ii) does not use the specific subframe for Channel State Information, CSI, measurement. a receiver configured to detect a Physical Downlink Control Channel, PDCCH, and a channel measurement unit configured to perform a measurement for computing a Channel Quality Indicator, CQI, value, wherein the receiver detects the PDCCH with Downlink Control Information, DCI, with a Cyclic Redundancy Check, CRC, scrambled by a Radio Network Temporary Identifier, RNTI, according to a DCI format 1C on a serving cell, characterized in that Z in a case that the receiver does not successively detect the PDCCH over a predetermined number of subframes in an ON/OFF cell for which the ON state is configured, the channel measurement unit (i) assumes that a base station does not perform downlink transmission in a specific subframe and (ii) does not use the specific subframe for Channel State Information, CSI, measurement.
A relay device (R1, R2) constituting a relaying station that relays a communication between wireless terminal devices (1A,..., 1F), the relay device (R1, R2) comprising: a plurality of transmitting/receiving means (2A,..., 2D) which relays a communication between wireless terminal devices (1A,..., 1F) at a divisional bandwidth acquired by dividing a bandwidth of an allocated frequency utilized by the relay device (R1, R2) into two divisional bandwidths, one divisional bandwidth being lower than a center frequency and the other divisional bandwidth being higher than the center frequency, respectively; frequency allocating means which allocates each of the divided frequency bandwidth to the transmitting/receiving means (2A,..., 2D); relaying-operation termination instructing means which instructs each transmitting/receiving means (2A,..., 2D) to terminate a relaying operation of a communication between the wireless terminal devices (1A,..., 1F) at a certain time set beforehand; and information transmission instructing means which causes one specific transmitting/receiving means (2A,..., 2D) to transmit a defined signal that is unique identification information given to the relaying station after the relaying operation by each transmitting/receiving means (2A,..., 2D) is terminated, wherein the information transmission instructing means transmits a set signal that carries the identification information from specific transmitting/receiving means (2A,..., 2D) at a frequency common in each transmitting/receiving means (2A,..., 2D). a plurality of transmitting/receiving means (2A,..., 2D) which relays a communication between wireless terminal devices (1A,..., 1F) at a divisional bandwidth acquired by dividing a bandwidth of an allocated frequency utilized by the relay device (R1, R2) into two divisional bandwidths, one divisional bandwidth being lower than a center frequency and the other divisional bandwidth being higher than the center frequency, respectively; frequency allocating means which allocates each of the divided frequency bandwidth to the transmitting/receiving means (2A,..., 2D); relaying-operation termination instructing means which instructs each transmitting/receiving means (2A,..., 2D) to terminate a relaying operation of a communication between the wireless terminal devices (1A,..., 1F) at a certain time set beforehand; and information transmission instructing means which causes one specific transmitting/receiving means (2A,..., 2D) to transmit a defined signal that is unique identification information given to the relaying station after the relaying operation by each transmitting/receiving means (2A,..., 2D) is terminated, wherein the information transmission instructing means transmits a set signal that carries the identification information from specific transmitting/receiving means (2A,..., 2D) at a frequency common in each transmitting/receiving means (2A,..., 2D).