mhurhangee/ep-ind-claims huggingface dataset:
Method for smoothing a surface region of a component (11; 21) consisting of an electrically conductive material at least within the surface region, wherein within a vacuum chamber the surface region of the component (11; 21) is swept over by means of at least one focused electron beam (13; 23) with a first surface energy, which causes melting of the component material within the surface region, wherein a) before melting the surface region is swept over at least twice by the electron beam (13; 23), in each case with a different focal length (27a; 27b; 27c) of the electron beam (13; 23), wherein b) a second surface energy is set for the electron beam (13; 23), which second surface energy does not cause melting of the component material in the surface region, wherein c) data are acquired by means of a number of sensors (14; 24) arranged within the vacuum chamber, said data characterizing the electric current caused by the backscattered electrons impinging on the sensors (14; 24), wherein d) within an evaluation device (15; 25), an actual value for the roughness in the surface region is derived from the data acquired by the sensors (14; 24), the actual value of the roughness is compared with a target value of the roughness and, if the actual value of the roughness has not reached the target value of the roughness, a value for the first surface energy is determined depending on the result of the comparison, and thereafter e) the surface region is swept over by the electron beam (13; 23) with the first surface energy, after which the method continues with method step a). a) before melting the surface region is swept over at least twice by the electron beam (13; 23), in each case with a different focal length (27a; 27b; 27c) of the electron beam (13; 23), wherein b) a second surface energy is set for the electron beam (13; 23), which second surface energy does not cause melting of the component material in the surface region, wherein c) data are acquired by means of a number of sensors (14; 24) arranged within the vacuum chamber, said data characterizing the electric current caused by the backscattered electrons impinging on the sensors (14; 24), wherein d) within an evaluation device (15; 25), an actual value for the roughness in the surface region is derived from the data acquired by the sensors (14; 24), the actual value of the roughness is compared with a target value of the roughness and, if the actual value of the roughness has not reached the target value of the roughness, a value for the first surface energy is determined depending on the result of the comparison, and thereafter e) the surface region is swept over by the electron beam (13; 23) with the first surface energy, after which the method continues with method step a).
Device for water purification having: - an outer container, - a cover for closing the outer container, - an inner container, which comprises a filter on the bottom side, - that the inner container comprises a valve arranged on the bottom side which seals the inner container in the closed position, characterised in that - the inner container can be installed in the outer container, - a passage opening and a first control element are provided in the cover, wherein the first control element opens the valve on the inner container when the cover is placed on the inner container and thereby an overflow of the water stored in the inner container through the filter and the passage opening in the cover into the outer container is possible, - a second control element is arranged within the base of the outer container which opens the valve of the inner container when the inner container is installed in the outer container and thereby an overflow of the water stored in the inner container through the filter into the outer container is possible. - an outer container, - a cover for closing the outer container, - an inner container, which comprises a filter on the bottom side, - that the inner container comprises a valve arranged on the bottom side which seals the inner container in the closed position, - the inner container can be installed in the outer container, - a passage opening and a first control element are provided in the cover, wherein the first control element opens the valve on the inner container when the cover is placed on the inner container and thereby an overflow of the water stored in the inner container through the filter and the passage opening in the cover into the outer container is possible, - a second control element is arranged within the base of the outer container which opens the valve of the inner container when the inner container is installed in the outer container and thereby an overflow of the water stored in the inner container through the filter into the outer container is possible.
Method for controlling a headlight arrangement for a vehicle with which at least two overall light distributions (39, 40, 41) can be generated, wherein it is possible to change over between the overall light distributions (39, 40, 41), in which - the driving behaviour is detected, and - a changeover from one overall light distribution to another overall light distribution takes place during a time interval (ΔT) for the transition, wherein the time interval is determined as a function of the driving behaviour, characterized in that - the driving behaviour is determined by the magnitude of the acceleration and - the time interval (ΔT) is shorter the larger the acceleration. - the driving behaviour is detected, and - a changeover from one overall light distribution to another overall light distribution takes place during a time interval (ΔT) for the transition, wherein the time interval is determined as a function of the driving behaviour, - the driving behaviour is determined by the magnitude of the acceleration and - the time interval (ΔT) is shorter the larger the acceleration.
A modular portable weapon comprising module, constituted by the barrel of the weapon, and one or more modules (101, 102, 103, 104, 105) which are functionally mutually independent and are associated with said supporting module; characterised in that having a sheath or barrel extension; said one or more modules including a locking and recocking module insertable in said sheath or barrel extension and contained therein; a stock or handle module directly connectable to a rear end of said sheath or barrel extension, a containment module connectable directly to said barrel at a location forward of said sheath or barrel extension, a magazine module and a cartridge lifting and firing mechanism module, said locking and recocking module including a breech-lock and a locking head, said cartridge lifting and firing mechanism module being received substantially entirely in a receiver portion of said containment module.
System for connecting pipes in an inserted manner, comprising an inner sleeve and an outer sleeve, wherein a pipe to be connected rests on the inner sleeve and a clamping part is arranged between the inner sleeve and the outer sleeve, wherein the inner and outer sleeve (3, 4) and the clamping part also have a given axial length in the insertion direction and wherein the outer sleeve also has on the insertion side a first circumferential seal which is made of a sealing material that is different from a material of the outer sleeve and which is intended for interacting with an outer surface of the pushed-in pipe, and wherein the circumferential seal is rigidly connected to the wall, wherein the sealing material of the circumferential seal (41, 42) penetrates the wall of the outer sleeve at least in one place and is introduced in the plastics injection-moulding process, wherein the outer sleeve has a second circumferential seal which is downstream of the first seal in the insertion direction of the pipe and is intended for interacting with an outer surface of the pushed-in pipe, wherein the sealant of the second circumferential seal penetrates the wall of the outer sleeve at least in one place and wherein the second circumferential seal is rigidly connected to the wall of the outer sleeve, and is introduced in the plastics injection-moulding process, and wherein an impact protection projection is integrally formed with the first and the second seal in a materially uniform manner and rises above an outer surface of the outer sleeve in the radial direction.
Use of a lubricating composition comprising at least one base oil and at least one organomolybdenum compound for reducing the wear of bearings and for lubricating metallic surfaces, polymeric surfaces and/or amorphous carbon surfaces of thermal internal combustion engines of micro hybrid vehicles equipped with a starter-alternator or a heavy-duty starter.
A multi-coupling device comprising a movable plate and a fixed plate and further comprising a coupling/uncoupling device for the simultaneous connection of a plurality of hydraulic and/or electrical and/or pneumatic lines each of said plates (31, 32) supporting a plurality of quick semi-couplings, said coupling/uncoupling device comprising a pair of plate-like elements (13, 14) each hinged on one side of the movable plate, and further comprising a lever that can be operated by the user, connected to one of said plate-like elements (13, 14), each of said plate-like elements (13, 14) having an eccentric guide or groove (13', 14') configured to receive suitable clamping pins provided on said fixed plate so that the action of said eccentric groove (13', 14') on said pins causes the nearing of the movable plate to the fixed plate and the connection of the couplings due to the effect of the action of the user on said lever, the coupling/uncoupling device further comprising safety locking means comprising a trigger element that can be operated by the user and is associated with one of said plate-like elements (13, 14) in a translatable manner, wherein said trigger element of said safety locking means is slidingly associated with a first plate-like element of said plate-like elements (13, 14) connected to said lever comprising a handle that can be gripped by the user, said trigger element and said handle of said lever being mutually positioned so that the user may grip the handle with the palm of his/her hand and operate said trigger with his/her fingers of the same hand, and wherein said trigger element comprises a first portion (21a, 21b, 21c) that can be operated by the operator with one finger and projects outwards from said first plate-like element, and a second pin portion that projects from said plate-like element towards the inside of the device, characterized in that said first portion (21a, 21b, 21c) of said trigger element comprises a substantially cylindrical intermediate stretch ending towards the outside with a disc element having outer diameter greater with respect to the diameter of said intermediate stretch so that an operator may position a finger around said intermediate stretch, between said outer disc and a corresponding inner disc adjacent to said first plate-like element.
An antenna structure, comprising: a plurality of array elements; at least one radio frequency component comprising a plurality of feed ports; and a radio frequency switch, wherein the radio frequency switch is connected to at least two array elements and to at least two feed ports of the radio frequency component, and wherein the radio frequency switch is configured to switch a feed object of each feed port connected to the radio frequency switch to form a preset antenna array, the feed object being any array element of the at least two array elements connected to the radio frequency switch, characterized in that, the at least one radio frequency component comprises a plurality of radio frequency components (21, 22), each of the plurality of radio frequency components (21, 22) comprises a plurality of feed ports, and includes one or more of an amplifier, a filter and a frequency converter, and each feed port corresponds to at least one array element; and each feed port of the plurality of radio frequency components (21, 22) is connected to the radio frequency switch, and the radio frequency switch is configured to switch the feed object corresponding to each feed port. a plurality of array elements; at least one radio frequency component comprising a plurality of feed ports; and a radio frequency switch, wherein the radio frequency switch is connected to at least two array elements and to at least two feed ports of the radio frequency component, and wherein the radio frequency switch is configured to switch a feed object of each feed port connected to the radio frequency switch to form a preset antenna array, the feed object being any array element of the at least two array elements connected to the radio frequency switch, characterized in that, the at least one radio frequency component comprises a plurality of radio frequency components (21, 22), each of the plurality of radio frequency components (21, 22) comprises a plurality of feed ports, and includes one or more of an amplifier, a filter and a frequency converter, and each feed port corresponds to at least one array element; and each feed port of the plurality of radio frequency components (21, 22) is connected to the radio frequency switch, and the radio frequency switch is configured to switch the feed object corresponding to each feed port.
An ice crushing device, comprising an ice storage container and a rotatable ice knife assembly, the rotatable ice knife assembly being disposed in the ice storage container, the ice knife assembly includes a rotary shaft, a plurality of fixed ice knives, a movable ice knife and an ice cube separation structure, wherein a rotary shaft of the ice knife assembly is capable of driving the movable ice knife to rotate; the plurality of fixed ice knives and the ice cube separation structure are located at two sides of the rotary shaft of the ice knife assembly separately, and both fixed relative to the ice storage container; the movable ice knife is provided on the rotary shaft of the ice knife assembly between two adjacent fixed ice knives; and the rotary shaft of the ice knife assembly is configured to drive the movable ice knife to rotate in a first direction to break ice cubes in the ice storage container under a cooperation of the movable ice knife and the plurality of fixed ice knives, and drive the movable ice knife to rotate in a second direction opposite to the first direction to separate frozen ice cubes under a cooperation of the movable ice knife and the ice cube separation structure, and at least one of the fixed ice knives is connected to the ice cube separation structure; characterized in that a gap between an inner wall of the ice storage container and a closer ice cube separation structure in an axial direction of the rotary shaft of the ice knife assembly allows only one ice cube to pass through. the ice knife assembly includes a rotary shaft, a plurality of fixed ice knives, a movable ice knife and an ice cube separation structure, wherein a rotary shaft of the ice knife assembly is capable of driving the movable ice knife to rotate; the plurality of fixed ice knives and the ice cube separation structure are located at two sides of the rotary shaft of the ice knife assembly separately, and both fixed relative to the ice storage container; the movable ice knife is provided on the rotary shaft of the ice knife assembly between two adjacent fixed ice knives; and the rotary shaft of the ice knife assembly is configured to drive the movable ice knife to rotate in a first direction to break ice cubes in the ice storage container under a cooperation of the movable ice knife and the plurality of fixed ice knives, and drive the movable ice knife to rotate in a second direction opposite to the first direction to separate frozen ice cubes under a cooperation of the movable ice knife and the ice cube separation structure, and at least one of the fixed ice knives is connected to the ice cube separation structure; characterized in that a gap between an inner wall of the ice storage container and a closer ice cube separation structure in an axial direction of the rotary shaft of the ice knife assembly allows only one ice cube to pass through.
A method for providing flight operational consequence information, the method comprising: receiving a status indication associated with an aircraft component at a processing device in the aircraft during a flight; ascertaining in the processing device one or more operational consequences comprising text strings associated with the status indication, wherein each of the one or more operational consequences are associated with one or more flight segments of the flight; displaying at least a subset of the one or more operational consequences on a display associated with the processing device; indicating the one or more flight segments on the display in association with the one or more operational consequences; receiving user input selecting a flight segment, wherein the selected flight segment is not a current flight segment; ascertaining another one or more operational consequences associated with the status indication that is associated with the aircraft component, wherein the another one or more operational consequences is associated with the selected flight segment that is not a current flight segment; displaying the another one or more operational consequences on the display of the processing device; and indicating the selected flight segment on the display in association with the another one or more operational flight consequences. receiving a status indication associated with an aircraft component at a processing device in the aircraft during a flight; ascertaining in the processing device one or more operational consequences comprising text strings associated with the status indication, wherein each of the one or more operational consequences are associated with one or more flight segments of the flight; displaying at least a subset of the one or more operational consequences on a display associated with the processing device; indicating the one or more flight segments on the display in association with the one or more operational consequences; receiving user input selecting a flight segment, wherein the selected flight segment is not a current flight segment; ascertaining another one or more operational consequences associated with the status indication that is associated with the aircraft component, wherein the another one or more operational consequences is associated with the selected flight segment that is not a current flight segment; displaying the another one or more operational consequences on the display of the processing device; and indicating the selected flight segment on the display in association with the another one or more operational flight consequences.
A guide wire for intravascular investigations comprising: a core wire (54; 84; 96); an electric sensor connected at a distal end (68; 78) of the guide wire; at least one electrical conductor (54, 62, 64; 84, 62, 64; 96, 100, 102; 94, 96, 100; 96, 118, 120) extending along a length of said guide wire, said core wire (54; 84; 96) being covered with concentric layers of alternatingly conductive (62, 64) and insulating (56, 58, 60) materials, the outermost of which is an insulating layer; characterised in that at least a portion of one of said at least one electrical conductors is provided as one of said layers (62, 64; 100, 102; 118, 120) of electrically conductive material, extending concentrically over the circumference of, and along said core wire (54; 84; 96) forming a part of said guide wire, wherein the at least one layer (62, 64; 100, 102; 118, 120) of conductive material is exposed at the distal end of the guide wire to form a contact element (70, 72, 74) to which the electric sensor is electrically connected; and in that each layer (62, 64; 100, 102; 118, 120) of conductive material is exposed in a consecutive manner at the proximal end (66; 76; 86) of the guide wire, and present a contact surface extending circumferentially around the core wire (54; 84; 96) to form a contact element adapted to be engaged by a female connector. a core wire (54; 84; 96); an electric sensor connected at a distal end (68; 78) of the guide wire; at least one electrical conductor (54, 62, 64; 84, 62, 64; 96, 100, 102; 94, 96, 100; 96, 118, 120) extending along a length of said guide wire, said core wire (54; 84; 96) being covered with concentric layers of alternatingly conductive (62, 64) and insulating (56, 58, 60) materials, the outermost of which is an insulating layer; at least a portion of one of said at least one electrical conductors is provided as one of said layers (62, 64; 100, 102; 118, 120) of electrically conductive material, extending concentrically over the circumference of, and along said core wire (54; 84; 96) forming a part of said guide wire, wherein the at least one layer (62, 64; 100, 102; 118, 120) of conductive material is exposed at the distal end of the guide wire to form a contact element (70, 72, 74) to which the electric sensor is electrically connected; and in that each layer (62, 64; 100, 102; 118, 120) of conductive material is exposed in a consecutive manner at the proximal end (66; 76; 86) of the guide wire, and present a contact surface extending circumferentially around the core wire (54; 84; 96) to form a contact element adapted to be engaged by a female connector.
A method for generating at least one high fidelity resource state, the method comprising: selecting a classical error correcting code, having a generator matrix, in which all of the rows of the generator matrix associated with the code have a weight of zero mod 2g, where g is a positive integer power of two; puncturing the classical error correcting code, by deleting at least one column of the generator matrix, such that a first set of generators retains a weight of zero mod 2g and a second set of generators has a weight of 2g -1 mod 2g; mapping the first set of generators to a set of stabilizer generators; mapping the second set of generators to a set of logical operators; preparing a set of relatively low fidelity resource states in a plurality of physical qubits (14, 15, 16, 17), said preparing comprising: encoding the plurality of physical qubits (14, 15, 16, 17) with the punctured classical code via a series of gates; and applying a transversal rotation across the plurality of physical qubits; performing a decoding process, according to a quantum CSS code represented by the set of stabilizer generators and the set of logical operators, on the physical qubits (14, 15, 16, 17); and performing, on a set of the physical qubits (14, 15, 16, 17), measurements, whose values correspond to stabilizers of the quantum CSS code to provide a set of measurement values. selecting a classical error correcting code, having a generator matrix, in which all of the rows of the generator matrix associated with the code have a weight of zero mod 2g, where g is a positive integer power of two; puncturing the classical error correcting code, by deleting at least one column of the generator matrix, such that a first set of generators retains a weight of zero mod 2g and a second set of generators has a weight of 2g -1 mod 2g; mapping the first set of generators to a set of stabilizer generators; mapping the second set of generators to a set of logical operators; preparing a set of relatively low fidelity resource states in a plurality of physical qubits (14, 15, 16, 17), said preparing comprising: encoding the plurality of physical qubits (14, 15, 16, 17) with the punctured classical code via a series of gates; and applying a transversal rotation across the plurality of physical qubits; encoding the plurality of physical qubits (14, 15, 16, 17) with the punctured classical code via a series of gates; and applying a transversal rotation across the plurality of physical qubits; performing a decoding process, according to a quantum CSS code represented by the set of stabilizer generators and the set of logical operators, on the physical qubits (14, 15, 16, 17); and performing, on a set of the physical qubits (14, 15, 16, 17), measurements, whose values correspond to stabilizers of the quantum CSS code to provide a set of measurement values.