mhurhangee/ep-ind-claims huggingface dataset:
A reversible adjustable eyeglass structure with polarized and/or prescription lenses operable in one of two configurations to present two different outward appearances, comprising: an eyeglass frame assembly including: a main frame assembly having rotatable side arms and rotatable leg seats pivotally connected to the rotatable side arms and to the main frame assembly, the rotatable leg seats being configured to pivot to allow rotatable side arms to be rotated 180 degrees relative to the main frame assembly to interchange interior and exterior sides of the eyeglass frame assembly and thereby provide said eyeglass frame assembly with two different outward appearances; and a rotatable secondary frame assembly holding left and right lenses and pivotally connected to the center of the main frame assembly about a vertical axis; a correct lens orientation indicator to verify that the right lens is facing the right eye and the left lens is facing the left eye; and a mechanism to allow the rotational movement of the rotatable secondary frame assembly around the center of the main frame assembly and prevent the undesirable movement of the rotatable secondary frame assembly. an eyeglass frame assembly including: a main frame assembly having rotatable side arms and rotatable leg seats pivotally connected to the rotatable side arms and to the main frame assembly, the rotatable leg seats being configured to pivot to allow rotatable side arms to be rotated 180 degrees relative to the main frame assembly to interchange interior and exterior sides of the eyeglass frame assembly and thereby provide said eyeglass frame assembly with two different outward appearances; and a rotatable secondary frame assembly holding left and right lenses and pivotally connected to the center of the main frame assembly about a vertical axis; a main frame assembly having rotatable side arms and rotatable leg seats pivotally connected to the rotatable side arms and to the main frame assembly, the rotatable leg seats being configured to pivot to allow rotatable side arms to be rotated 180 degrees relative to the main frame assembly to interchange interior and exterior sides of the eyeglass frame assembly and thereby provide said eyeglass frame assembly with two different outward appearances; and a rotatable secondary frame assembly holding left and right lenses and pivotally connected to the center of the main frame assembly about a vertical axis; a correct lens orientation indicator to verify that the right lens is facing the right eye and the left lens is facing the left eye; and a mechanism to allow the rotational movement of the rotatable secondary frame assembly around the center of the main frame assembly and prevent the undesirable movement of the rotatable secondary frame assembly.
Switchable explosive charge of a warhead, having a casing that forms splinters and having a cylindrical explosive charge, in which, within the payload, there is arranged a tubular holder with a multiplicity of pellets arranged in a distributed manner, having a first ignition device, which is arranged at the end and which corresponds to a plate-like transfer charge, in the area of which a central detonation wave deflector is arranged, and a further ignition device, which is positioned in the area of the longitudinal axis of the explosive charge, it being possible for the ignition devices to be initiated independently of each other, at least three ignition devices (Z3a, Z3b) being arranged distributed over the circumference in the area of the tubular holder, characterized in that the charge located within the holder has a first central part and a second part (SP1, SP2) directly surrounding the central part, wherein the first part consists of a powerful explosive and the second part (SP1, SP2) consists of an explosive with a lower power than the explosive of the first part, and wherein the layer of the second explosive has a thickness in the range from 5 - 25 mm.
A thin film transistor array substrate comprising: a substrate; at least one thin film transistor over the substrate; a capacitor (Cst) over the substrate, the capacitor comprising: a first electrode over the substrate; a second electrode overlapping the first electrode, the second electrode comprising an opening having a single closed curve shape; and a dielectric layer between the first electrode and the second electrode; an interlayer insulating layer covering the capacitor; and a node connection line (153, 154) over the interlayer insulating layer and electrically connecting the capacitor to the at least one thin film transistor, wherein an overlapping area of the first electrode and the second electrode is divided by the opening into two separate areas, characterized in that the opening exposes opposing ends of the first electrode in a direction. a substrate; at least one thin film transistor over the substrate; a capacitor (Cst) over the substrate, the capacitor comprising: a first electrode over the substrate; a second electrode overlapping the first electrode, the second electrode comprising an opening having a single closed curve shape; and a dielectric layer between the first electrode and the second electrode; a first electrode over the substrate; a second electrode overlapping the first electrode, the second electrode comprising an opening having a single closed curve shape; and a dielectric layer between the first electrode and the second electrode; an interlayer insulating layer covering the capacitor; and a node connection line (153, 154) over the interlayer insulating layer and electrically connecting the capacitor to the at least one thin film transistor, wherein an overlapping area of the first electrode and the second electrode is divided by the opening into two separate areas, characterized in that the opening exposes opposing ends of the first electrode in a direction.
Device for locking sterilisation boxes comprising a rod able to be slid into a device for closing a sterilisation box, and a support part of the proximal end of the rod such that: - said support part comprises a locking part (3 1) able to engage and be fastened irreversibly on the distal end (2 1) of the rod in order to form with the latter a closed loop that prevents the opening of the device for closing and comprises a portion that is additional to that (1 1) for the support required solely for the sealing function, said additional portion comprises a surface (8 2) with facial dimensions that are sufficient to be able to receive a legible identification label, - the additional portion is a flat tab that can be folded over the support portion (1 1) of the rod, that it covers, by folding along a line (8 1) that forms a hinge and which then offers as seen the surface (8 2) opposite that facing the support portion (1 1), and able to receive the identification label, characterised in that the additional portion comprises an opening that corresponds, when it is folded back, to the location where the distal end (2 1) of the rod and the locking part (3 1) are locked together. - said support part comprises a locking part (3 1) able to engage and be fastened irreversibly on the distal end (2 1) of the rod in order to form with the latter a closed loop that prevents the opening of the device for closing and comprises a portion that is additional to that (1 1) for the support required solely for the sealing function, said additional portion comprises a surface (8 2) with facial dimensions that are sufficient to be able to receive a legible identification label, - the additional portion is a flat tab that can be folded over the support portion (1 1) of the rod, that it covers, by folding along a line (8 1) that forms a hinge and which then offers as seen the surface (8 2) opposite that facing the support portion (1 1), and able to receive the identification label,
A turbine blade, comprising: a first set of ceramic matrix composite plies forming at least a portion of a suction side skin of the turbine blade; a second set of ceramic matrix composite plies forming at least a portion of a pressure side skin of the turbine blade; characterised in that the turbine blade further comprises a woven fabric having fabric layers and fiber tows, said woven fabric preventing contact between the first set of ceramic matrix composite plies and the second set of ceramic matrix composite plies, wherein the woven fabric having fiber tows includes interlocking stitches that run through the thickness of the fabric layers to tie them together and provide enhanced interlaminar strength, and wherein the fiber tows include surface contoured regions for mechanical interlocking. a first set of ceramic matrix composite plies forming at least a portion of a suction side skin of the turbine blade; a second set of ceramic matrix composite plies forming at least a portion of a pressure side skin of the turbine blade; characterised in that the turbine blade further comprises a woven fabric having fabric layers and fiber tows, said woven fabric preventing contact between the first set of ceramic matrix composite plies and the second set of ceramic matrix composite plies, wherein the woven fabric having fiber tows includes interlocking stitches that run through the thickness of the fabric layers to tie them together and provide enhanced interlaminar strength, and wherein the fiber tows include surface contoured regions for mechanical interlocking.
A method for treating a refrigerant fluid that performs a refrigeration cycle in a refrigeration machine, comprising the consecutive steps of a. compressing the refrigerant fluid in a compressor of said refrigeration machine, b. cooling the refrigerant fluid in a main cooling unit of the refrigeration machine, c. expanding the refrigerant fluid in an expander of the refrigeration machine, d. placing the refrigerant fluid in a heat exchange with a fluid to be cooled, in a main heat exchanger of the refrigeration machine, e. cooling adiabatically an air flow f. placing in a heat exchange the adiabatically cooled air flow with the refrigerant fluid, at least step f. being performed between steps b. and c.. a. compressing the refrigerant fluid in a compressor of said refrigeration machine, b. cooling the refrigerant fluid in a main cooling unit of the refrigeration machine, c. expanding the refrigerant fluid in an expander of the refrigeration machine, d. placing the refrigerant fluid in a heat exchange with a fluid to be cooled, in a main heat exchanger of the refrigeration machine, e. cooling adiabatically an air flow f. placing in a heat exchange the adiabatically cooled air flow with the refrigerant fluid,
A device for repetitive needleless injection of a liquid into a surface, the device comprising: a handheld unit that includes at least a cell that is fillable with the liquid, and a propulsion mechanism configured to apply a sequence of pressure pulses to the liquid, each pulse of the sequence of pressure pulses to eject a micro-jet of the liquid from the cell via an orifice between the cell and the exterior of the handheld unit with a velocity that is sufficient to enable the micro-jet to penetrate into the surface, wherein the orifice is separated from the cell by a unidirectional valve that is configured to enable flow of the liquid from the cell to the orifice and to prevent inflow of atmospheric air from the orifice to the cell; a reservoir that is connected to the cell by a conduit to enable the liquid to flow from the reservoir to the cell to replace the liquid that is ejected in the micro-jet; and a controller that is configured to operate the propulsion mechanism repeatedly so as to eject the sequence of the micro-jets. a handheld unit that includes at least a cell that is fillable with the liquid, and a propulsion mechanism configured to apply a sequence of pressure pulses to the liquid, each pulse of the sequence of pressure pulses to eject a micro-jet of the liquid from the cell via an orifice between the cell and the exterior of the handheld unit with a velocity that is sufficient to enable the micro-jet to penetrate into the surface, wherein the orifice is separated from the cell by a unidirectional valve that is configured to enable flow of the liquid from the cell to the orifice and to prevent inflow of atmospheric air from the orifice to the cell; a reservoir that is connected to the cell by a conduit to enable the liquid to flow from the reservoir to the cell to replace the liquid that is ejected in the micro-jet; and a controller that is configured to operate the propulsion mechanism repeatedly so as to eject the sequence of the micro-jets.
Metal sheet comprising a substrate having at least one face coated by a metal coating comprising Al and Mg, the remainder of the metallic coating being Zn, unavoidable impurities and possibly one or more additional elements selected from among Si, Sb, Pb, Ti, Ca, Mn, Sn, La, Ce, Cr, or Bi, wherein the content by weight of each additional element in the metallic coating is less than 0.3%, the metal coating having an aluminium content by weight t Al of between 3.6 and 3.8% and a magnesium content by weight t Mg of between 2.7 and 3.3 %, the metal coating having a microstructure comprising a lamellar matrix of ternary eutectic of Zn/Al/MgZn 2 and: - dendrites of Zn with an accumulated surface content at the outer surface of the coating in the raw state null or of less than or equal to 5.0%, - flowers of binary eutectic of Zn/MgZn 2 with an accumulated surface content at the outer surface of the coating in the raw state null or of less than or equal to 15.0%, - dendrites of binary eutectic of Zn/Al with an accumulated surface content at the outer surface of the metal coating in the raw state null or of less than or equal to 1.0%, - islets of MgZn 2 with an accumulated surface content at the outer surface of the coating in the raw state null or of less than or equal to 1.0%. - dendrites of Zn with an accumulated surface content at the outer surface of the coating in the raw state null or of less than or equal to 5.0%, - flowers of binary eutectic of Zn/MgZn 2 with an accumulated surface content at the outer surface of the coating in the raw state null or of less than or equal to 15.0%, - dendrites of binary eutectic of Zn/Al with an accumulated surface content at the outer surface of the metal coating in the raw state null or of less than or equal to 1.0%, - islets of MgZn 2 with an accumulated surface content at the outer surface of the coating in the raw state null or of less than or equal to 1.0%.
A gas turbine engine comprising: a combustor section arranged between a compressor section and a turbine section, wherein the compressor section includes at least a low pressure compressor and a high pressure compressor, the high pressure compressor being arranged immediately upstream of the combustor section; a fan section having an array of twenty-six or fewer fan blades, wherein the fan section has a low fan pressure ratio of less than 1.55; a geared architecture coupling the fan section to the turbine section or the compressor section; the low pressure compressor being counter-rotating relative to the fan blades; and an airfoil arranged in a compressor section outside the high compressor section, wherein the airfoil is fixed relative to an engine axis of an engine static structure, the airfoil comprising pressure and suction sides (72, 74) and extending in a radial direction from a 0% span position to a 100% span position, characterized in that the airfoil has a relationship between a leading edge angle (β1*) and span position that defines a curve (88; 90; 92; 94; 96) with a leading edge angle (β1*), measured against a tangential plane normal to the engine axis, of less than 40° at 100% span. a combustor section arranged between a compressor section and a turbine section, wherein the compressor section includes at least a low pressure compressor and a high pressure compressor, the high pressure compressor being arranged immediately upstream of the combustor section; a fan section having an array of twenty-six or fewer fan blades, wherein the fan section has a low fan pressure ratio of less than 1.55; a geared architecture coupling the fan section to the turbine section or the compressor section; the low pressure compressor being counter-rotating relative to the fan blades; and an airfoil arranged in a compressor section outside the high compressor section, wherein the airfoil is fixed relative to an engine axis of an engine static structure, the airfoil comprising pressure and suction sides (72, 74) and extending in a radial direction from a 0% span position to a 100% span position, characterized in that the airfoil has a relationship between a leading edge angle (β1*) and span position that defines a curve (88; 90; 92; 94; 96) with a leading edge angle (β1*), measured against a tangential plane normal to the engine axis, of less than 40° at 100% span.
Complex comprising: a) Pt; b) a ligand corresponding to formula: where R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R 9 are selected from: -H, -(C 1 -C 12)-alkyl, -(C 6 -C 20)-aryl; c) an iodine ligand or bromine ligand. a) Pt; b) a ligand corresponding to formula: where R 1, R 2, R 3, R 4, R 5, R 6, R 7, R 8, R 9 are selected from: -H, -(C 1 -C 12)-alkyl, -(C 6 -C 20)-aryl; c) an iodine ligand or bromine ligand.
A method of monitoring, with a processor, a cloud service provided over a number of computing devices, the cloud service modeled as a topology, wherein the topology comprises data representing a graph of nodes (302-1, 302-2, 302-3, 302-4, 302-5, 302-6, 302-7) and relationships between the nodes, and wherein each node comprises one or more of the computing devices, the method comprising: establishing (1101, 1201) a number of monitoring policies to monitor an instantiated cloud service, the instantiated cloud service provided over a number of computing devices in accordance with the topology and associated with a realized topology, the realized topology derived from the instantiated service and comprising characteristics and computing parameters of the computing devices, wherein the monitoring policies comprise metadata on how to provision a monitoring system for monitoring the instantiated service; executing (1102, 1202) and instantiating a monitoring system based on the monitoring policies, wherein executing and instantiating a monitoring system comprises provisioning, configuring, delegating, or combinations thereof, a monitoring system based on the monitoring policies; collecting (1103, 1203) metric data at a node based on the number of monitoring policies; determining from the collected metric data that the instantiated service is to be modified; and updating the monitoring policies, in which the updated monitoring policies remain associated with the realized topology such that an update to a monitoring policy may be promulgated to instances of the realized topology. establishing (1101, 1201) a number of monitoring policies to monitor an instantiated cloud service, the instantiated cloud service provided over a number of computing devices in accordance with the topology and associated with a realized topology, the realized topology derived from the instantiated service and comprising characteristics and computing parameters of the computing devices, wherein the monitoring policies comprise metadata on how to provision a monitoring system for monitoring the instantiated service; executing (1102, 1202) and instantiating a monitoring system based on the monitoring policies, wherein executing and instantiating a monitoring system comprises provisioning, configuring, delegating, or combinations thereof, a monitoring system based on the monitoring policies; collecting (1103, 1203) metric data at a node based on the number of monitoring policies; determining from the collected metric data that the instantiated service is to be modified; and updating the monitoring policies, in which the updated monitoring policies remain associated with the realized topology such that an update to a monitoring policy may be promulgated to instances of the realized topology.
A mixed-drink set for preparing a mixed drink, comprising: - a disposable packaging, - at least one first container for a first mixing component, - at least one second container for a second mixing component, and - at least one drinking vessel (6, 7), said at least one first container, said at least one second container and said at least one drinking vessel (6, 7) being packed in said disposable packaging and said disposable packaging having an openable filling opening through which ice for cooling said at least one first container and said at least one second container can be filled into the disposable packaging. - a disposable packaging, - at least one first container for a first mixing component, - at least one second container for a second mixing component, and - at least one drinking vessel (6, 7),
A minimally invasive surgical device comprising: a main body (110, 310, 410) comprising an inner tube (112, 212, 312, 412) and an outer tube (114, 314, 414), the inner tube (112, 212, 312, 412) being disposed in the outer tube (114, 314, 414); a buffer assembly (120, 220, 320, 420), one end of the buffer assembly (120, 220, 320, 420) being connected to the inner tube (112, 212, 312, 412); a cutter bit (130, 230, 330, 430) connected to the other end of the buffer assembly (120, 220, 320, 420) and having a cutting portion (132, 232, 332, 432), wherein when the cutting portion (132, 232, 332, 432) is in contact with an object, the buffer assembly (120, 220, 320, 420) is adapted to enable the cutter bit (130, 230, 330, 430) to move relatively to the inner tube (112, 212, 312, 412) to decrease a cutting force between the cutting portion (132, 232, 332, 432) and the object, and is adapted to enable the cutting portion (132, 232, 332, 432) to be tilted along with a surface of the object; characterised in that the minimally invasive surgical device further comprises a driver unit connected between the buffer assembly and the cutter bit and adapted to drive the cutter bit to rotate relatively to the inner tube, wherein the driver unit comprises an actuator and a gear set, the actuator is connected to the buffer assembly, and the gear set is connected between the actuator and the cutter bit. a main body (110, 310, 410) comprising an inner tube (112, 212, 312, 412) and an outer tube (114, 314, 414), the inner tube (112, 212, 312, 412) being disposed in the outer tube (114, 314, 414); a buffer assembly (120, 220, 320, 420), one end of the buffer assembly (120, 220, 320, 420) being connected to the inner tube (112, 212, 312, 412); a cutter bit (130, 230, 330, 430) connected to the other end of the buffer assembly (120, 220, 320, 420) and having a cutting portion (132, 232, 332, 432), wherein when the cutting portion (132, 232, 332, 432) is in contact with an object, the buffer assembly (120, 220, 320, 420) is adapted to enable the cutter bit (130, 230, 330, 430) to move relatively to the inner tube (112, 212, 312, 412) to decrease a cutting force between the cutting portion (132, 232, 332, 432) and the object, and is adapted to enable the cutting portion (132, 232, 332, 432) to be tilted along with a surface of the object; characterised in that the minimally invasive surgical device further comprises a driver unit connected between the buffer assembly and the cutter bit and adapted to drive the cutter bit to rotate relatively to the inner tube, wherein the driver unit comprises an actuator and a gear set, the actuator is connected to the buffer assembly, and the gear set is connected between the actuator and the cutter bit.