mhurhangee/patent-ind-claim-en huggingface dataset:
Fitting for a vehicle seat, in particular for a motor vehicle seat, having a first fitting part and a second fitting part which are rotatable relative to one another and are in geared connection with one another, or are lockable with one another, and a third fitting part which is mounted on a bearing ring , which is fastened on the first fitting part , so as to be pivotable about an axis (A) relative to the first fitting part , wherein the third fitting part is lockable with the first fitting part , or with a component which is fixedly connected to the first fitting part , by means of pawl which is mounted in a first pivot point (D1) on the third fitting part , wherein the bearing ring comprises several run-up cams which interact with several elevations of the third fitting part in such a manner that, with the pawl locked, free play in the radial direction between the bearing ring and the third fitting part is minimized, characterized in that the third fitting part , a blocking cam which is mounted in a second pivot point (D2) on the third fitting part , a coupler which is flexibly connected to the blocking cam in a third pivot point (D3) and to the pawl in a fourth pivot point (D4), and the pawl define a four-pivot chain .
Pneumatic valve apparatus for a compressed air device, in particular comprising a pneumatic cylinder, in particular for an automatic clutch system or an automated transmission control and clutch system, the apparatus comprising: - a pneumatic solenoid valve comprising a housing body having a supply channel , a receiving channel and a vent channel , - the housing body surrounding a valve chamber in which a valve body is movable, by means of an actuator, along a valve axis (A1), against the force of a valve spring , relative to a vent valve seat to the vent channel and a supply valve seat to the supply channel , - the valve body opening, in a first position (E), the valve chamber and the vent valve seat to a vent channel and opening, in a second position (V), a supply channel to the supply valve seat and the valve chamber , - the housing body comprising a diffuser which adjoins the vent valve seat to the vent channel , a diffuser channel of the diffuser widening in cross-section from the vent valve seat to the vent channel , and - the diffuser channel running transversely to the valve axis (A1), and a vent valve seat passage having a clearance which is smaller than a second clearance of the diffuser channel , characterized in that the diffuser channel - comprises a first portion having a cylindrical and/or blunt conical form, and/or - comprises a second portion having a curved form, and in the diffuser channel , - opposite the vent valve seat passage , a flow baffle element is formed as a mandrel-shaped flow guide element on the valve axis (A1). - a pneumatic solenoid valve comprising a housing body having a supply channel , a receiving channel and a vent channel , - the housing body surrounding a valve chamber in which a valve body is movable, by means of an actuator, along a valve axis (A1), against the force of a valve spring , relative to a vent valve seat to the vent channel and a supply valve seat to the supply channel , - the valve body opening, in a first position (E), the valve chamber and the vent valve seat to a vent channel and opening, in a second position (V), a supply channel to the supply valve seat and the valve chamber , - the housing body comprising a diffuser which adjoins the vent valve seat to the vent channel , a diffuser channel of the diffuser widening in cross-section from the vent valve seat to the vent channel , and - the diffuser channel running transversely to the valve axis (A1), and a vent valve seat passage having a clearance which is smaller than a second clearance of the diffuser channel , characterized in that the diffuser channel - comprises a first portion having a cylindrical and/or blunt conical form, and/or - comprises a second portion having a curved form, and in the diffuser channel , - opposite the vent valve seat passage , a flow baffle element is formed as a mandrel-shaped flow guide element on the valve axis (A1).
Method for secure and efficient access to connection data of at least one telecommunications provider (TK), wherein - the connection data (VD) are collected by the telecommunications provider and encrypted by the telecommunications provider, - the encrypted connection data (VDv) are transmitted to a secured environment (U) by the telecommunications provider (TK), - the transmitted encrypted connection data (VDv) are decrypted in the secured environment (U) and are stored exclusively in a volatile memory (S) of the secured environment (U) as decrypted connection data (VDe) for a first predetermined time period (t1), - access to the connection data is granted exclusively via a predetermined interface (IF) of the secured environment (U) as access to the decrypted connection data (VDe) stored in the volatile memory (S) of the secured environment (U), - at least one encryption key (KV) is generated by an automatic key generator (SA) in the secured environment (U) and is transmitted to the telecommunications provider (TK) for encrypting the connection data (VD), - in order to decrypt the transmitted encrypted connection data (VDv), at least one decryption key (KE) is generated by the automatic key generator (SA) in the secured environment (U), wherein the decryption key (KE) is stored exclusively in a volatile memory (S) of the secured environment (U), and - the connection data (VD) are deleted at the telecommunications provider after the encrypted connection data (VDv) have been generated. - the connection data (VD) are collected by the telecommunications provider and encrypted by the telecommunications provider, - the encrypted connection data (VDv) are transmitted to a secured environment (U) by the telecommunications provider (TK), - the transmitted encrypted connection data (VDv) are decrypted in the secured environment (U) and are stored exclusively in a volatile memory (S) of the secured environment (U) as decrypted connection data (VDe) for a first predetermined time period (t1), - access to the connection data is granted exclusively via a predetermined interface (IF) of the secured environment (U) as access to the decrypted connection data (VDe) stored in the volatile memory (S) of the secured environment (U), - at least one encryption key (KV) is generated by an automatic key generator (SA) in the secured environment (U) and is transmitted to the telecommunications provider (TK) for encrypting the connection data (VD), - in order to decrypt the transmitted encrypted connection data (VDv), at least one decryption key (KE) is generated by the automatic key generator (SA) in the secured environment (U), wherein the decryption key (KE) is stored exclusively in a volatile memory (S) of the secured environment (U), and - the connection data (VD) are deleted at the telecommunications provider after the encrypted connection data (VDv) have been generated.
An extractor tube assembly for a beverage container , comprising a gas valve and a beverage valve adapted to cooperate with each other, the gas valve and beverage valve comprising a ring-shaped gasket , the gasket being made of an elastomeric material and comprising an insert made of a rigid material, and the gasket having a top part with an upper face visible from outside the extractor tube assembly, the top part being arranged above the insert , wherein the elastomeric material encloses the insert and a portion of the top part of the gasket is adapted to be released from the insert when a pressure inside the beverage container exceeds a predetermined level so that fluid communication between an interior of the beverage container and the surroundings is provided, whereby the pressure is released from the beverage container, the gasket comprising an identification detectable from the upper face of the gasket so that it is easily detectable if a pressure release function of the gasket has been partly or fully initiated, the identification is part of the upper face of the gasket .
A method of facilitating takeoff and landing of an aircraft comprising: obtaining aircraft information including a current position and a current altitude of the aircraft; retrieving , from a database, vertiport information for a desired landing or takeoff location area including current environmental information and current traffic information; determining , based on the aircraft information and the vertiport information, an aircraft path including a vertical path portion and a cruise path portion ; determining , based on the aircraft path, a dynamic switchover point between the vertical path portion and the cruise path portion along the aircraft path; and transmitting control information to one or more aircraft propulsion systems wherein the control information includes a vertical control portion and a cruise control portion; wherein the one or more aircraft propulsion systems will operate under one of the vertical control portion or the cruise control portion of the control information until the aircraft reaches the dynamic switchover point, and wherein the one or more aircraft propulsion systems will operate under the other of the vertical control portion or the cruise control portion of the control information after the aircraft reaches the dynamic switchover point. obtaining aircraft information including a current position and a current altitude of the aircraft; retrieving , from a database, vertiport information for a desired landing or takeoff location area including current environmental information and current traffic information; determining , based on the aircraft information and the vertiport information, an aircraft path including a vertical path portion and a cruise path portion ; determining , based on the aircraft path, a dynamic switchover point between the vertical path portion and the cruise path portion along the aircraft path; and transmitting control information to one or more aircraft propulsion systems wherein the control information includes a vertical control portion and a cruise control portion; wherein the one or more aircraft propulsion systems will operate under one of the vertical control portion or the cruise control portion of the control information until the aircraft reaches the dynamic switchover point, and wherein the one or more aircraft propulsion systems will operate under the other of the vertical control portion or the cruise control portion of the control information after the aircraft reaches the dynamic switchover point.
A friction stir spot welding method of performing friction stir spot welding of a pair of workpieces (W) by using a refill friction stir spot welding device including a rotary tool including a pin member that rotates around a predetermined axis (P) and is provided to be able to advance and retract in a direction of the axis (P), a shoulder member that rotates around the axis (P) while surrounding an outer periphery of the pin member and is provided independently of the pin member so as to be able to advance and retract in the direction of the axis (P), and a clamp member that has an end face able to press a surface of one of the pair of workpieces (W) by coming into surface contact with the surface and is provided to surround an outer periphery of the shoulder member , the pair of workpieces (W) having a coating film (R1) formed on at least one of welding surfaces overlaid on each other, the method being characterized by : a coating film removal step of decomposing the coating film (R1) by heating the coating film to a temperature equal to or more than the thermal decomposition temperature by using the heat generated by the rotation of the shoulder member and removing the coating film (R1) by plunging a distal end of the shoulder member into the one workpiece (W) up to a position closer to the surface of the one workpiece (W) than the at least one of the welding surfaces, while rotating the shoulder member around the axis (P), and rotating the shoulder member in a state in which the surface of the one workpiece (W), with the welding surfaces being overlaid on each other, is pressed by the end face of the clamp member ; and a welding step of performing friction stir spot welding of the pair of workpieces (W) after the coating film removal step by using the pin member and the shoulder member . a coating film removal step of decomposing the coating film (R1) by heating the coating film to a temperature equal to or more than the thermal decomposition temperature by using the heat generated by the rotation of the shoulder member and removing the coating film (R1) by plunging a distal end of the shoulder member into the one workpiece (W) up to a position closer to the surface of the one workpiece (W) than the at least one of the welding surfaces, while rotating the shoulder member around the axis (P), and rotating the shoulder member in a state in which the surface of the one workpiece (W), with the welding surfaces being overlaid on each other, is pressed by the end face of the clamp member ; and a welding step of performing friction stir spot welding of the pair of workpieces (W) after the coating film removal step by using the pin member and the shoulder member .
A lifting unit, which includes fastening columns and their lateral supports and a lifting cylinder with a piston, characterized in that the lifting unit comprises a telescopic fastening column formed by two parallel columns, a hydraulic lifting cylinder with a piston, positioned between the columns, a supporting slab attached to the lower end of the telescopic fastening column and a rectangular fastening plate fixed to the upper end, supporting posts , which are at an acute angle to the lifted object positioned between the parallel columns and a supporting slab , and optional fastening, tensioning and adjustment means, while lifting and lowering of the object is executed as a three-point lifting system of lifting cylinders .
A liquid propellant rocket engine comprising: a main turbo-pump having a main pump having an outlet fluidly coupled with a supply line ; and a boost turbo-pump having a housing ; a rotor ; an axial boost pump including a first portion of the housing and a first portion the rotor ; and an axial turbine including a second portion of the housing and a second portion of the rotor , wherein the turbine has turbine blades attached to the second portion of the rotor , wherein the turbine has an inlet fluidly coupled with the supply line , characterised in that the turbine has a plurality of circumferentially disposed feed lines defined by the second portion of the housing and not the first portion of the housing , wherein the circumferentially disposed feed lines are fluidly coupled between the inlet and the turbine blades , wherein the circumferentially disposed feed lines have an acute angle turn . a main turbo-pump having a main pump having an outlet fluidly coupled with a supply line ; and a boost turbo-pump having a housing ; a rotor ; an axial boost pump including a first portion of the housing and a first portion the rotor ; and an axial turbine including a second portion of the housing and a second portion of the rotor , wherein the turbine has turbine blades attached to the second portion of the rotor , wherein the turbine has an inlet fluidly coupled with the supply line , characterised in that the turbine has a plurality of circumferentially disposed feed lines defined by the second portion of the housing and not the first portion of the housing , wherein the circumferentially disposed feed lines are fluidly coupled between the inlet and the turbine blades , wherein the circumferentially disposed feed lines have an acute angle turn . a housing ; a rotor ; an axial boost pump including a first portion of the housing and a first portion the rotor ; and an axial turbine including a second portion of the housing and a second portion of the rotor , wherein the turbine has turbine blades attached to the second portion of the rotor , wherein the turbine has an inlet fluidly coupled with the supply line , characterised in that the turbine has a plurality of circumferentially disposed feed lines defined by the second portion of the housing and not the first portion of the housing , wherein the circumferentially disposed feed lines are fluidly coupled between the inlet and the turbine blades , wherein the circumferentially disposed feed lines have an acute angle turn .
A method comprising: receiving, by a wireless communication device , a first radio resource control, RRC, message including a conditional handover, CHO, configuration, wherein the CHO configuration includes a CHO configuration index, a CHO candidate cell configuration, and a CHO execution condition; selecting, by the wireless communication device responsive to receiving the first RRC message and based on the CHO execution condition, a special cell, SpCell, of a wireless communication node to perform a random access procedure, RAP; and transmitting, by the wireless communication device to the wireless communication node , a second RRC message to inform the wireless communication node that the wireless communication device selected the SPCell to perform the RAP. receiving, by a wireless communication device , a first radio resource control, RRC, message including a conditional handover, CHO, configuration, wherein the CHO configuration includes a CHO configuration index, a CHO candidate cell configuration, and a CHO execution condition; selecting, by the wireless communication device responsive to receiving the first RRC message and based on the CHO execution condition, a special cell, SpCell, of a wireless communication node to perform a random access procedure, RAP; and transmitting, by the wireless communication device to the wireless communication node , a second RRC message to inform the wireless communication node that the wireless communication device selected the SPCell to perform the RAP.
A compound comprising a ligand L A of wherein: ring A is independently a 5-membered to 10-membered heterocyclic ring; X 1 -X 6 are each independently C or N; K 3 is a direct bond, O, or S; R A , R B , and R C each independently represents zero, mono, or up to the maximum allowed number of substitutions to its associated ring; and each of R 1 , R A , R B , R C is independently a hydrogen or a substituent selected from the group consisting of deuterium, halogen, alkyl, cycloalkyl, heteroalkyl, heterocycloalkyl, arylalkyl, alkoxy, aryloxy, amino, silyl, germyl, boryl, selenyl, alkenyl, cycloalkenyl, heteroalkenyl, alkynyl, aryl, heteroaryl, acyl, carboxylic acid, ether, ester, nitrile, isonitrile, sulfanyl, sulfinyl, sulfonyl, phosphino, and combinations thereof, wherein: the ligand L A is complexed to a metal M through the two indicated dashed lines; M is Pt, and can be coordinated to other ligands; the ligand L A can be joined with other ligands to form a tridentate, tetradentate, pentadentate, or hexadentate ligand; and any two adjacent R A , R B , R C , or R 1 can be joined or fused to form a ring, with a condition that the compound does not comprise either one of the following structures: ring A is independently a 5-membered to 10-membered heterocyclic ring; X 1 -X 6 are each independently C or N; K 3 is a direct bond, O, or S; R A , R B , and R C each independently represents zero, mono, or up to the maximum allowed number of substitutions to its associated ring; and each of R 1 , R A , R B , R C is independently a hydrogen or a substituent selected from the group consisting of deuterium, halogen, alkyl, cycloalkyl, heteroalkyl, heterocycloalkyl, arylalkyl, alkoxy, aryloxy, amino, silyl, germyl, boryl, selenyl, alkenyl, cycloalkenyl, heteroalkenyl, alkynyl, aryl, heteroaryl, acyl, carboxylic acid, ether, ester, nitrile, isonitrile, sulfanyl, sulfinyl, sulfonyl, phosphino, and combinations thereof, the ligand L A is complexed to a metal M through the two indicated dashed lines; M is Pt, and can be coordinated to other ligands; the ligand L A can be joined with other ligands to form a tridentate, tetradentate, pentadentate, or hexadentate ligand; and any two adjacent R A , R B , R C , or R 1 can be joined or fused to form a ring,
A method for producing NK cells said method comprising i- a sample of human CD34 positive cells being provided, ii- expanding said CD34 positive cells ex vivo, iii- culturing CD34 positive cells obtained in step ii ex vivo in an NK-cell differentiation medium, said method characterized in that said NK-differentiation medium comprises between 0,2 ngram/ml and 20 ngram/ml IL-12. i- a sample of human CD34 positive cells being provided, ii- expanding said CD34 positive cells ex vivo, iii- culturing CD34 positive cells obtained in step ii ex vivo in an NK-cell differentiation medium,
A SPAD device, comprising: a single-photon avalanche diode (AD1, AD2, AD3, AD4, AD5, AD6, AD7, AD8) having a breakdown voltage and a dark count rate, a further single-photon avalanche diode (AD9) having a further breakdown voltage and a further dark count rate, the dark count rate being at least a factor 100 higher than the further dark count rate at least at one temperature below 25°C, the further single-photon avalanche diode (AD9) being integrated with the single-photon avalanche diode (AD1, AD2, AD3, AD4, AD5, AD6, AD7, AD8), the breakdown voltage being equal to the further breakdown voltage or differing from the further breakdown voltage by less than 10%, the single-photon avalanche diode (AD1, AD2, AD3, AD4, AD5, AD6, AD7, AD8) being provided for adjusting or controlling an excess bias voltage, and the further single-photon avalanche diode (AD9) being provided for a detection of radiation. a single-photon avalanche diode (AD1, AD2, AD3, AD4, AD5, AD6, AD7, AD8) having a breakdown voltage and a dark count rate, a further single-photon avalanche diode (AD9) having a further breakdown voltage and a further dark count rate, the dark count rate being at least a factor 100 higher than the further dark count rate at least at one temperature below 25°C, the further single-photon avalanche diode (AD9) being integrated with the single-photon avalanche diode (AD1, AD2, AD3, AD4, AD5, AD6, AD7, AD8), the breakdown voltage being equal to the further breakdown voltage or differing from the further breakdown voltage by less than 10%, the single-photon avalanche diode (AD1, AD2, AD3, AD4, AD5, AD6, AD7, AD8) being provided for adjusting or controlling an excess bias voltage, and the further single-photon avalanche diode (AD9) being provided for a detection of radiation.