mhurhangee/ep-ind-claims huggingface dataset:
A dispensing machine 1 for dispensing a frozen confectionary product 28, the machine 1 comprising: a first storage area 39 for storing a first storage tray 95 with one or more first tubes in the dispensing machine 1, a serving station 17 for receiving one or more first tubes comprising a composition that is a frozen confectionary from the first storage tray 95, the serving station 17 comprises a first position under the one or more first tubes for receiving a container 8, a means for extruding the frozen confectionary out of the tubes located in the serving station 17, a cutting device 5 for cutting at least a portion of the frozen confectionary into the container 8, means for transferring the one or more first tubes in the first storage area 39 to the serving station 17 and from the serving station 17 to a storage area 39, and wherein the one or more first tubes are reusable; and at least two zones, the at least two zones comprising a first zone wherein the temperature is lower than the temperature in the second zone, and wherein the first storage area 39 is located in the first zone and the serving station 17 is located in the second zone; wherein the means for transferring the one or more first tubes is a robotic arm 16, preferably a robotic arm 16 comprising a tube changer plate 33 configured to grip the one or more first tubes. a first storage area 39 for storing a first storage tray 95 with one or more first tubes in the dispensing machine 1, a serving station 17 for receiving one or more first tubes comprising a composition that is a frozen confectionary from the first storage tray 95, the serving station 17 comprises a first position under the one or more first tubes for receiving a container 8, a means for extruding the frozen confectionary out of the tubes located in the serving station 17, a cutting device 5 for cutting at least a portion of the frozen confectionary into the container 8, a first position under the one or more first tubes for receiving a container 8, a means for extruding the frozen confectionary out of the tubes located in the serving station 17, a cutting device 5 for cutting at least a portion of the frozen confectionary into the container 8, means for transferring the one or more first tubes in the first storage area 39 to the serving station 17 and from the serving station 17 to a storage area 39, and wherein the one or more first tubes are reusable; and at least two zones, the at least two zones comprising a first zone wherein the temperature is lower than the temperature in the second zone, and wherein the first storage area 39 is located in the first zone and the serving station 17 is located in the second zone; wherein the means for transferring the one or more first tubes is a robotic arm 16, preferably a robotic arm 16 comprising a tube changer plate 33 configured to grip the one or more first tubes.
Device for artificial respiration of a person in a medical emergency situation with a respiratory mask which can be placed on the nose and mouth section of the person, with a mouthpiece, through which respiratory air can be supplied by an aider, with a flow tube disposed between the respiratory mask and the mouthpiece, which flow tube forms a continuous flow channel from the mouthpiece to the respiratory mask, at least one flow sensor disposed in the flow channel of the flow tube, which flow sensor can determine a mass or volumetric flow of a gas flowing through the flow channel, with a processor that processes the mass or volumetric flow registered by the flow sensor into an output signal, with an output device, which emits the output signal, characterized in that, the processor is designed as a processor generating a penetration depth signal, which processor generates a characteristic penetration depth signal for the penetration depth from the mass or volumetric flow registered by the flow sensor during a cardiac massage as a result of a compression of the thorax down to a penetration depth, for air flowing out of the nose and/or mouth of the person and through the flow channel, and wherein the output device is designed to emit the penetration depth signal.
A preprocessing system that performs preprocessing of a sample before analysis by a chromatograph, comprising: a plurality of preprocessing units, each preprocessing unit including a belt conveyor that transports a sample bottle in which a sample is sealed, and a controller that controls an operation of the belt conveyor, wherein at least one of the plurality of preprocessing units further includes a processor that performs specific preprocessing based on control performed by the controller, and, the belt conveyor of each preprocessing unit is arranged adjacent to a belt conveyor of another preprocessing unit in a transport direction and is configured to transfer the sample bottle to the adjacent belt conveyor or to receive the sample bottle from the adjacent belt conveyor, characterized in that: each preprocessing unit further includes a mechanical stopper to temporarily stop the sample bottle on the belt conveyor at a predetermined position while the belt conveyor is operated, such that the belt conveyor of each preprocessing unit is configured to transport a sample bottle other than the sample bottle stopped by the stopper. a plurality of preprocessing units, each preprocessing unit including a belt conveyor that transports a sample bottle in which a sample is sealed, and a controller that controls an operation of the belt conveyor, wherein at least one of the plurality of preprocessing units further includes a processor that performs specific preprocessing based on control performed by the controller, and, the belt conveyor of each preprocessing unit is arranged adjacent to a belt conveyor of another preprocessing unit in a transport direction and is configured to transfer the sample bottle to the adjacent belt conveyor or to receive the sample bottle from the adjacent belt conveyor,
An automatic cover-opening device adapted for use with any of a pencil sharpener, an ink bottle or a beverage containing vessel comprising; a body having an insertion hole defined in the body; at least one cover panel mounted on the body for moveably opening or closing the insertion hole; and a recoil mechanism disposed on the body to push the at least one cover panel to a closed position for closing the insertion hole, each one of the at least one cover panel having a guiding segment having at least one guiding edge inclined relative to an axis of the insertion hole to guide an axial force along the axis of the insertion hole to a lateral direction that is non-parallel with the axis and to generate a lateral component force for opening the at least one cover panel, being characterized in that the guiding segment of each one of the at least one cover panel has at least one abutting rib, and each one of the at least one abutting rib has one of the at least one guiding edge formed on the abutting rib.
A method for estimating a service capacity of a minimum battery cell in a battery system comprising a plurality of cells connected in series, wherein the minimum battery cell has a lowest voltage level among the plurality of cells, comprising the following steps: when a battery system is power-on, determining an initial state of charge, SOC 1, of the minimum battery cell in a battery system being charged; after the battery system is fully charged, determining a final state of charge, SOC 2, of the minimum battery cell at an end of charging, and calculating to obtain a charging capacity, Q 1, of the minimum battery cell based on the initial state of charge, SOC 1, and the final state of charge, SOC 2; and performing a computation to obtain the service capacity, Q d, of the minimum battery cell based on following equation: Q d = Q 1 + Q n ∗ 1 − SOC 2 1 − SOC 1 wherein Q n is a rated capacity of the minimum battery cell. when a battery system is power-on, determining an initial state of charge, SOC 1, of the minimum battery cell in a battery system being charged; after the battery system is fully charged, determining a final state of charge, SOC 2, of the minimum battery cell at an end of charging, and calculating to obtain a charging capacity, Q 1, of the minimum battery cell based on the initial state of charge, SOC 1, and the final state of charge, SOC 2; and performing a computation to obtain the service capacity, Q d, of the minimum battery cell based on following equation: Q d = Q 1 + Q n ∗ 1 − SOC 2 1 − SOC 1 wherein Q n is a rated capacity of the minimum battery cell.
Application unit (400; 600; 800), wherein the application unit (400; 600; 800) comprises at least one application mechanism (414; 614; 814), which has at least one impression cylinder (408; 608; 808), at least one forme cylinder (402; 602; 802), and at least one supply roller (403; 603; 803), along with at least one positioning device, and wherein the positioning device has at least one linear guide, and wherein the positioning device has at least one main supporting member, and wherein the at least one main supporting member is arranged to be movable in and counter to a positioning direction, guided by the at least one linear guide, and wherein the forme cylinder (402; 602; 802) is arranged rotatably on the at least one main supporting member by means of at least one rolling bearing, and wherein the positioning device has at least one transfer supporting member, and wherein the at least one transfer supporting member is arranged to be movable in and counter to the positioning direction relative to the at least one main supporting member, guided by the at least one linear guide, and wherein at least one component of a bearing seat is arranged on the at least one transfer supporting member, which bearing seat is configured to receive a rolling bearing arranged on the at least one supply roller (403; 603; 803), and wherein the positioning device has at least one reservoir supporting member, and wherein the at least one reservoir supporting member is arranged to be movable in and counter to the positioning direction, both relative to the at least one main supporting member and relative to the at least one transfer supporting member, guided by the at least one linear guide, and wherein an intermediate reservoir (404; 604; 804) for application fluid is arranged on the at least one reservoir supporting member, characterized in that the positioning direction deviates no more than 45° from at least one vertical direction, and in that the reservoir supporting member is arranged at least partially between the at least one main supporting member and the at least one transfer supporting member, as viewed in the positioning direction.
A system for measuring performance of an orthotic or prosthetic foot device, comprising: an orthotic or prosthetic foot device, the device capable of bending while in use; characterised in that the system further comprises a bending force sensor extending in an anterior/posterior direction along both sides of a bending axis of the device, wherein the bending force sensor is configured to bend with the device while in use, and wherein the bending force sensor produces a resistance output correlated to the bending of the device. an orthotic or prosthetic foot device, the device capable of bending while in use; characterised in that the system further comprises a bending force sensor extending in an anterior/posterior direction along both sides of a bending axis of the device, wherein the bending force sensor is configured to bend with the device while in use, and wherein the bending force sensor produces a resistance output correlated to the bending of the device.
Hydraulic operating apparatus for the operation of actuating elements in a motor vehicle transmission, having a multiplicity of piston-cylinder arrangements (14.1, 14.2, 14.3, 14.4, 14.5) which have in each case one actuating piston (16.1, 16.2, 16.3, 16.4, 16.5) which is operatively connectable to an actuating element and which can be hydraulically acted on a first side and on a second side of the actuating pistons by means of in each case one associated pressure space (18.1, 18.1', 18.2, 18.2', 18.3, 18.3', 18.4, 18.4', 18.5, 18.5'), wherein each piston-cylinder arrangement (14.1, 14.2, 14.3, 14.4, 14.5) is assigned a control device (20.1, 20.2, 20.3, 20.4, 20.5) which permits or prevents an actuating movement of the respective actuating piston (16.1, 16.2, 16.3, 16.4, 16.5) in a first direction or in an opposite, second direction, and wherein the pressure spaces (18.1, 18.2, 18.3, 18.4, 18.5) on the first side of the actuating pistons (16.1, 16.2, 16.3, 16.4, 16.5) are hydraulically connected to one another via a common first pressure line, whereas the pressure spaces (18.1', 18.2', 18.3', 18.4', 18.5') on the second side of the actuating pistons (16.1, 16.2, 16.3, 16.4, 16.5) are hydraulically connected to one another via a common second pressure line, characterized in that to each pressure line (22, 24) is assigned at least one ventilation valve (26, 28) with an exit (30, 32) for air, and the exits (30, 32) of the ventilation valves (26, 28) are connected to a common ventilation line.
Manufacturing and assembly method of parts of an aircraft comprising the following steps: - providing a first aircraft part comprising at least a receptor surface on which a coupling surface of a second aircraft part is to be assembled, - providing in a computer program a model of the first and the second aircraft parts located in its assembled position, the model of the second aircraft part comprising machining allowances in its coupling surface, - digitalising by a digitalising system the receptor surface of the first aircraft part obtaining a digitalised surface, the method being characterised in that it further comprises the steps of: - positioning the digitalisation of the receptor surface in the computer model of the first and the second aircraft parts in the assembled position such that the digitalisation of the receptor surface intersects the machining allowances of the coupling surface of the second aircraft part, - obtaining in the computer model a computer designed model of the second part in which the coupling surface of the second aircraft part adapted to be assembled on the receptor surface of the first aircraft part fits to the digitalised receptor surface, - mechanising the second aircraft part to be assembled from the above obtained computer model, - assembling the mechanised second aircraft part to the provided first aircraft part. - providing a first aircraft part comprising at least a receptor surface on which a coupling surface of a second aircraft part is to be assembled, - providing in a computer program a model of the first and the second aircraft parts located in its assembled position, the model of the second aircraft part comprising machining allowances in its coupling surface, - digitalising by a digitalising system the receptor surface of the first aircraft part obtaining a digitalised surface, - positioning the digitalisation of the receptor surface in the computer model of the first and the second aircraft parts in the assembled position such that the digitalisation of the receptor surface intersects the machining allowances of the coupling surface of the second aircraft part, - obtaining in the computer model a computer designed model of the second part in which the coupling surface of the second aircraft part adapted to be assembled on the receptor surface of the first aircraft part fits to the digitalised receptor surface, - mechanising the second aircraft part to be assembled from the above obtained computer model, - assembling the mechanised second aircraft part to the provided first aircraft part.
A rotary aircraft, comprising: a fuselage; an engine carried by the fuselage; a rotor rotatably attached to the engine; and a tail boom (301; 701) rotatably attached to and extending from the fuselage, the tail boom having: a body having: a first side surface and an opposing second side surface, the first side surface contoured to act as a pressure surface of an airfoil and the second side surface contoured to act as a suction surface of an airfoil; such that when the engine rotates the rotor, thereby creating downward rotorwash and thereby exerting a torque on the fuselage, the rotorwash flows around the first side surface and the second side surface of the tail boom (301; 701), resulting in a high-pressure region forming near the first side surface and resulting in a low-pressure region forming near the second side surface; and the pressure difference between the high-pressure region and the low-pressure region causes the tail boom (301; 701) to move towards the low-pressure region, resulting in a lateral force opposing the torque on the fuselage; the first and second side surfaces (309, 311) gradually tapering toward each other to form a surface, which acts as leading edge of an airfoil and a surface and which acts as trailing edge of an airfoil; the surface acting as trailing edge is a flat surface configured to provide a well-defined flow separation line between the first side surface and the flat surface or between the second side surface and the flat surface; and the tail boom is further provided with a flap pivotally attached to the trailing edge via an attachment device for providing additional flow control of rotorwash travelling around the contoured surfaces of the tail boom. a fuselage; an engine carried by the fuselage; a rotor rotatably attached to the engine; and a tail boom (301; 701) rotatably attached to and extending from the fuselage, the tail boom having: a body having: a first side surface and an opposing second side surface, the first side surface contoured to act as a pressure surface of an airfoil and the second side surface contoured to act as a suction surface of an airfoil; a body having: a first side surface and an opposing second side surface, the first side surface contoured to act as a pressure surface of an airfoil and the second side surface contoured to act as a suction surface of an airfoil; a first side surface and an opposing second side surface, the first side surface contoured to act as a pressure surface of an airfoil and the second side surface contoured to act as a suction surface of an airfoil; such that when the engine rotates the rotor, thereby creating downward rotorwash and thereby exerting a torque on the fuselage, the rotorwash flows around the first side surface and the second side surface of the tail boom (301; 701), resulting in a high-pressure region forming near the first side surface and resulting in a low-pressure region forming near the second side surface; and
A conductive paste comprising: (a) 85% to 99.5% by weight of a conductive metal, based on the weight of solids; (b) 0.5% to 15% by weight of a lead-free glass frit containing tellurium-bismuth-selenium-lithium-oxide, based on the weight of solids; and (c) an organic vehicle; wherein the weight of solids is the total weight of the conductive metal (a) and the lead-free glass frit (b), and wherein the tellurium oxide is present in an amount of 55 wt.% to 90 wt.%, the selenium oxide is present in an amount of 0.1 wt.% to 15 wt.% in the lead-free glass frit, the bismuth oxide is present in an amount of 0.1 wt.% to 15 wt.%, and the lithium oxide is present in an amount of 0.1 wt.% to 15 wt.% in the lead-free glass frit. (a) 85% to 99.5% by weight of a conductive metal, based on the weight of solids; (b) 0.5% to 15% by weight of a lead-free glass frit containing tellurium-bismuth-selenium-lithium-oxide, based on the weight of solids; and (c) an organic vehicle;
Device for mechanical actuation of an electrical or electronic input unit, in particular for centre console units of motor vehicles, with a rotary element rotatably mounted by means of a roller bearing, wherein a thrust element is provided for actuating the device in the axial direction, wherein the roller bearing 6 is braced in the axial direction by a bearing tensioning element 3, and in that a bearing ring 12 of the roller bearing 6 is axially movable within the bearing clearance of the roller bearing 6 by axial movement of the thrust element 14, wherein the device 1 comprises a spring receiving element 2 which passes through a spiral spring 3 and forms a stop for the spiral spring 3 via an annular shoulder 4, wherein the spring receiving element 2, on the side of the spiral spring 3 opposite the annular shoulder 4, bears against an inner ring 5 of a roller bearing 6, wherein the roller bearing 6 is in the form of a ball bearing with bearing balls 7 and the spiral spring 3 acts on a knurled rotary ring 10 via a thrust ring 8 and an intermediate ring 9, which in turn bears via an annular shoulder 11 on the side of an outer ring 12 of the roller bearing 6 opposite the thrust ring 8 and the intermediate ring 9, characterized in that the thrust element is operatively connected to a bearing ring independently of the rotary element.
An equipment on an aircraft for transferring content to and from the aircraft, the equipment comprising: a first communication device; and a transceiver connected to an antenna on the aircraft and the first communication device, the transceiver is configured to establish a terrestrial communication link through the antenna directly to a second communication device disposed at a ground based entity to communicate the content between the first communication device and the second communication device; and the first communication device operating to provide a traffic prioritization mechanism that prioritizes transfer of the content between the first communication device and the second communication device in accordance with at least one of available link speed, importance of the content, and anticipated connection time between the first communication device and the second communication device. a first communication device; and a transceiver connected to an antenna on the aircraft and the first communication device, the transceiver is configured to establish a terrestrial communication link through the antenna directly to a second communication device disposed at a ground based entity to communicate the content between the first communication device and the second communication device; and the first communication device operating to provide a traffic prioritization mechanism that prioritizes transfer of the content between the first communication device and the second communication device in accordance with at least one of available link speed, importance of the content, and anticipated connection time between the first communication device and the second communication device.
A flywheel rotor for use in an open-core flywheel assembly, said rotor comprising: a material having a tensile strength of from about 2 GPa to about 20 GPa, said rotor material capable of expanding outward radially upon circumferential velocities of from about 300 m/s to about 3000 m/s; wherein said rotor has an inner and outer surface and at least one flexible rotor magnet (34, 36, 38) affixed to the inner surface of the rotor; and wherein the flexible rotor magnet (34, 36, 38) comprises a material having a Young's modulus of from about 0.01 GPa to about 2 GPa. a material having a tensile strength of from about 2 GPa to about 20 GPa, said rotor material capable of expanding outward radially upon circumferential velocities of from about 300 m/s to about 3000 m/s; wherein said rotor has an inner and outer surface and at least one flexible rotor magnet (34, 36, 38) affixed to the inner surface of the rotor; and wherein the flexible rotor magnet (34, 36, 38) comprises a material having a Young's modulus of from about 0.01 GPa to about 2 GPa.