mhurhangee/patent-ind-claim-en huggingface dataset:
A method of manufacturing an aesthetic structural plastic part , comprising: hot-stamping a decorative film to a thermoplastic composite sheet , wherein the thermoplastic composite sheet includes a thermoplastic resin and fibers, wherein the decorative film includes a top layer , a pigmented middle layer , and a bottom adhesion layer in contact with the thermoplastic composite sheet; thermoforming the composite sheet; and overmolding a thermoplastic material to the composite sheet, wherein overmolding a thermoplastic material to the composite sheet comprises forming one or more mounting features in the thermoplastic material, wherein the aesthetic structural plastic part includes the decorative film, the composite sheet, and the one or more mounting features, and wherein thermoforming the composite sheet includes forming features configured to mechanically interface with the overmolded thermoplastic material. hot-stamping a decorative film to a thermoplastic composite sheet , wherein the thermoplastic composite sheet includes a thermoplastic resin and fibers, wherein the decorative film includes a top layer , a pigmented middle layer , and a bottom adhesion layer in contact with the thermoplastic composite sheet; thermoforming the composite sheet; and overmolding a thermoplastic material to the composite sheet, wherein overmolding a thermoplastic material to the composite sheet comprises forming one or more mounting features in the thermoplastic material, wherein the aesthetic structural plastic part includes the decorative film, the composite sheet, and the one or more mounting features, and wherein thermoforming the composite sheet includes forming features configured to mechanically interface with the overmolded thermoplastic material.
An axial magnetic bearing for a rotating machine, comprising a rotatable shaft ; at least one fixed stator , each stator comprising layers of a first magnetically-permeable material; and a rotor secured to the shaft and disposed adjacent to the at least one stator , the rotor comprising layers of a second magnetically-permeable material that is wound onto the rotatable shaft , the layers being arranged one on top of another in a radial direction of the rotor , characterized in that the layers of a second magnetically-permeable material are in the form of a roll.
Method for cutting to length a tyre component of an elastomer for producing a green tyre, comprising the following steps: a) transporting a front end portion of a tyre component to a tyre building drum, the front end portion of the tyre component being positioned on the upper side of the tyre building drum by a transporting means , the tyre building drum then winding up the tyre component on the tyre building drum by rotation and the tyre component that is to be cut to length being fed on a servicer , b) positioning the tyre component to be cut to length on the servicer under a cutting device , c) fixing the tyre component against the upper side of the front end of the servicer with a uniform compressive force, the tyre component being pressed on its upper side against the upper side of the servicer by a flexible hold-down device , the hold-down device taking the form of a comb, having individual fingers and the individual fingers being flexibly connected to the main body of the hold-down device in each case by individual tubular connecting means , d) carrying out the cutting operation with a cutting device , the cutting device being guided at a constant speed along the cutting bar and thereby cutting through the tyre component , e) transporting the cut-to-length rear end of the tyre component to the tyre building drum , the rear end of the tyre component being placed by a transporting means against the front end of the tyre component on the tyre building drum . a) transporting a front end portion of a tyre component to a tyre building drum, the front end portion of the tyre component being positioned on the upper side of the tyre building drum by a transporting means , the tyre building drum then winding up the tyre component on the tyre building drum by rotation and the tyre component that is to be cut to length being fed on a servicer , b) positioning the tyre component to be cut to length on the servicer under a cutting device , c) fixing the tyre component against the upper side of the front end of the servicer with a uniform compressive force, the tyre component being pressed on its upper side against the upper side of the servicer by a flexible hold-down device , the hold-down device taking the form of a comb, having individual fingers and the individual fingers being flexibly connected to the main body of the hold-down device in each case by individual tubular connecting means , d) carrying out the cutting operation with a cutting device , the cutting device being guided at a constant speed along the cutting bar and thereby cutting through the tyre component , e) transporting the cut-to-length rear end of the tyre component to the tyre building drum , the rear end of the tyre component being placed by a transporting means against the front end of the tyre component on the tyre building drum .
A method for diagnosing computer readable instructions, the method comprising: Logging , into a data structure, a state transition of a unit of execution within an asynchronous logical operation during runtime of the computer readable instructions; Associating diagnostic information of the asynchronous logical operation with the state transition in the data structure, and Providing the state transition and associated diagnostic information for retrieval from the data structure at a selected point in the computer readable instructions; wherein the logging comprises broadcasting the state transition by publishing events or invoking callbacks registered for notification; and wherein the broadcasting the state transition occurs in response to receiving metadata associated with a code location that indicates the information should be broadcast. Logging , into a data structure, a state transition of a unit of execution within an asynchronous logical operation during runtime of the computer readable instructions; Associating diagnostic information of the asynchronous logical operation with the state transition in the data structure, and Providing the state transition and associated diagnostic information for retrieval from the data structure at a selected point in the computer readable instructions; wherein the logging comprises broadcasting the state transition by publishing events or invoking callbacks registered for notification; and wherein the broadcasting the state transition occurs in response to receiving metadata associated with a code location that indicates the information should be broadcast.
An underactuated mechanism , which allows the actuation of a distal degree of freedom of the human shoulder joint and the transfer of the reaction moments and force generated by the actuation system on the frame solidal to the torso , through a hyper-redundant kinematic mechanism , composed of: a. a first non-actuated rotoidal joint connected to the human torso , which rotates about the axis X, b. a connection mechanism connected to the first rotoidal joint , c. a second rotoidal joint which (i) rotates about the axis Y arranged according to the degree of flexion-extension of the shoulder joint, which is coplanar with the axis X, (ii) is remotely actuated by a direct drive actuation system with co-located motor, (iii) is fixed to the connection mechanism on one side and to the human arm on the other side, with the connection mechanism comprising: at least three or more members , two of which being rigidly fastened to one of the rotoidal joints , respectively, all with parallel joints, referred to as minimum joints A and B, arranged so as to connect one member with the next one to form a rotation constraint about the axis of said parallel joints; wherein the co-located motor is integrated in the second rotoidal joint . a. a first non-actuated rotoidal joint connected to the human torso , which rotates about the axis X, b. a connection mechanism connected to the first rotoidal joint , c. a second rotoidal joint which (i) rotates about the axis Y arranged according to the degree of flexion-extension of the shoulder joint, which is coplanar with the axis X, (ii) is remotely actuated by a direct drive actuation system with co-located motor, (iii) is fixed to the connection mechanism on one side and to the human arm on the other side, with the connection mechanism comprising: at least three or more members , two of which being rigidly fastened to one of the rotoidal joints , respectively, all with parallel joints, referred to as minimum joints A and B, arranged so as to connect one member with the next one to form a rotation constraint about the axis of said parallel joints;
An aircraft , comprising: a composite structure ; a signal return network spaced from the composite structure ; a first non-conductive component attached between the signal return network and the composite structure at a first attachment point ; a second non-conductive component attached between the signal return network and the composite structure at a second attachment point ; and a conductive component attached between the signal return network and the composite structure at a third attachment point for electrically coupling the signal return network to the composite structure to split the conductive path current into first and second signal return network currents which are routed though the signal return network in opposite directions toward at least one electrical system of the aircraft; wherein the conductive component is a sole electrical path from the composite structure to the signal return network , and wherein the remainder of the signal return network is electrically floating. a composite structure ; a signal return network spaced from the composite structure ; a first non-conductive component attached between the signal return network and the composite structure at a first attachment point ; a second non-conductive component attached between the signal return network and the composite structure at a second attachment point ; and a conductive component attached between the signal return network and the composite structure at a third attachment point for electrically coupling the signal return network to the composite structure to split the conductive path current into first and second signal return network currents which are routed though the signal return network in opposite directions toward at least one electrical system of the aircraft; wherein the conductive component is a sole electrical path from the composite structure to the signal return network , and wherein the remainder of the signal return network is electrically floating.
A method carried out by a mobile device, comprising: measuring a characteristic of a radio link between the mobile device and a base station to generate a measurement value; receiving a system information block broadcast by the base station ; extracting information from the system information block to generate a set of configurations ; selecting a random access channel format from the set of configurations in accordance with the measurement value; transmitting a random access preamble to the base station in accordance with the selected format; and identifying a component carrier on which random access is occurring, wherein the characteristic of the radio link and the set of configurations are unique to the component carrier identified. measuring a characteristic of a radio link between the mobile device and a base station to generate a measurement value; receiving a system information block broadcast by the base station ; extracting information from the system information block to generate a set of configurations ; selecting a random access channel format from the set of configurations in accordance with the measurement value; transmitting a random access preamble to the base station in accordance with the selected format; and identifying a component carrier on which random access is occurring, wherein the characteristic of the radio link and the set of configurations are unique to the component carrier identified.
A mechanically driven hubless ship propeller comprising at least one rotor , the blades thereof being arranged in a ring, and said rotor being configured with a ring gear and being connected to a ship's engine via a drive shaft with a pinion for transmitting a rotational movement, and comprising a nozzle in which the at least one rotor is arranged, wherein the rotating blades of the at least one rotor are configured to be individually adjustable in terms of angle and with each rotation are able to be continuously adapted regarding the angular position thereof to local flow conditions, in particular the inflow conditions in the nozzle , wherein the ship propeller is configured as a double propeller and has two preferably counter-rotating rotors which are arranged one behind the other in the direction of flow of the water, characterized in that the ship propeller with the nozzle and the rotors arranged therein is rotatable by 360 degrees about a vertical axis, and in that the ship propeller has a drive gear which is connected in terms of drive to the pinion of the drive shaft and which meshes with external ring gears of the two rotors .
A lighting device , comprising a first interface for supplying the lighting device with electrical energy, and a second interface for transmitting at least one control signal (B, D) for controlling a lighting property of a light source of the lighting device , characterized in that the lighting device comprises a five-pin connector, which forms the first interface and the second interface , wherein the five-pin connector is formed as an M12 panel plug, wherein the first interface comprises two connections for supply voltage (V) and ground (M) and wherein the second interface comprises three connections for transmitting the at least one control signal, wherein the connections are occupied as follows: first contact, which is occupied by the supply voltage (V), second contact, which is occupied by a flash signal (B), third contact, which is occupied by the ground (M), fourth contact, which is occupied by a dimming signal (D), and fifth contact, which is occupied by a status signal (F). first contact, which is occupied by the supply voltage (V), second contact, which is occupied by a flash signal (B), third contact, which is occupied by the ground (M), fourth contact, which is occupied by a dimming signal (D), and fifth contact, which is occupied by a status signal (F).
Heat exchange device having a coil heat exchanger with inlets and outlets for the heat exchanging agents and a tank for one of the agents, where the tank is provided with an inlet and outlet stub pipes wherein the coil heat exchanger consists of at least one coil wound spirally around the tank on its outside, characterised in that the coil takes the form of three coaxial tubes, where the outer tube and inner tube serve as the first flow ducts (K1) for the first agent, and the central tube serves as the second flow duct (K2) for the second agent, and where at the first end of the coil its outer tube and inner tube are connected by way of the first collector to the inlet stub pipe for the supply of the first agent, and the central tube is connected by way of the second collector to the outlet of the second agent, while at the other end of the coil its outer tube and inner tube are connected with the inside of the tank by way of the third collector and a supply stub pipe , and the central tube is connected to the inlet of the second agent by way of the fourth collector and a supply pipe .
A fibre reinforced polymer composite pipe comprising: a first end and a second end , the pipe defining a central axis running in a longitudinal direction from the first end to the second end , and the pipe including at least one non-linear portion along the central axis between the first end and the second end ; a first material extending continuously from the first end to the second end , the first material being a fibre reinforced polymer material comprising fibre reinforcement in a polymer matrix and having an electrical resistivity determined by an electrically conductive fibre reinforcement and/or an electrically conductive additive in the polymer matrix; and wherein a second material arranged at the at least one non-linear portion and extending discontinuously between the first end and the second end , the second material being a carbon fibre reinforced polymer material comprising carbon fibre reinforcement in a polymer matrix and having an elastic modulus provided by the carbon fibre reinforcement, wherein the elastic modulus of the second material is greater than the elastic modulus of the first material in the longitudinal direction. a first end and a second end , the pipe defining a central axis running in a longitudinal direction from the first end to the second end , and the pipe including at least one non-linear portion along the central axis between the first end and the second end ; a first material extending continuously from the first end to the second end , the first material being a fibre reinforced polymer material comprising fibre reinforcement in a polymer matrix and having an electrical resistivity determined by an electrically conductive fibre reinforcement and/or an electrically conductive additive in the polymer matrix; and wherein a second material arranged at the at least one non-linear portion and extending discontinuously between the first end and the second end , the second material being a carbon fibre reinforced polymer material comprising carbon fibre reinforcement in a polymer matrix and having an elastic modulus provided by the carbon fibre reinforcement, wherein the elastic modulus of the second material is greater than the elastic modulus of the first material in the longitudinal direction.
An apparatus , comprising: an axial shaft configured for insertion into, and rotation within, a ventricle of a heart of a subject; an impeller coupled to the axial shaft ; a frame surrounding the impeller ; a pump-outlet tube surrounding the frame such that, as the axial shaft rotates, the impeller pumps blood proximally, from the ventricle, through the pump-outlet tube ; and an inlet guard , which is flat and is shaped to define one or more holes , disposed around the axial shaft and within the frame distally to the impeller , such that the blood flows to the impeller via the holes . an axial shaft configured for insertion into, and rotation within, a ventricle of a heart of a subject; an impeller coupled to the axial shaft ; a frame surrounding the impeller ; a pump-outlet tube surrounding the frame such that, as the axial shaft rotates, the impeller pumps blood proximally, from the ventricle, through the pump-outlet tube ; and an inlet guard , which is flat and is shaped to define one or more holes , disposed around the axial shaft and within the frame distally to the impeller , such that the blood flows to the impeller via the holes .
A method for detecting a color of light received from a scene by a Time-of-Flight, ToF, sensor, the method comprising: applying a first electrical potential to a first modulation gate of a sensor pixel of the ToF sensor during a plurality of exposure times of the ToF sensor, wherein a value of the first electrical potential is equal for the plurality of exposure times; applying a second electrical potential to a second modulation gate of the sensor pixel during the plurality of exposure times, wherein the second electrical potential is different from the first electrical potential, wherein a value of the second electrical potential is different for each of the plurality of exposure times; receiving data indicating a respective first amount of charge collected at a first charge storage of the sensor pixel during the plurality of exposure times and a respective second amount of charge collected at a second charge storage of the sensor pixel during the plurality of exposure times; determining for the plurality of exposure times a respective ratio value representing a ratio of the respective first amount of charge to the respective second amount of charge; determining a slope of a course of the determined ratio values with respect to the values of the second electrical potential used for the plurality of exposure times; and determining the color of the light received by the sensor pixel based on the slope. applying a first electrical potential to a first modulation gate of a sensor pixel of the ToF sensor during a plurality of exposure times of the ToF sensor, wherein a value of the first electrical potential is equal for the plurality of exposure times; applying a second electrical potential to a second modulation gate of the sensor pixel during the plurality of exposure times, wherein the second electrical potential is different from the first electrical potential, wherein a value of the second electrical potential is different for each of the plurality of exposure times; receiving data indicating a respective first amount of charge collected at a first charge storage of the sensor pixel during the plurality of exposure times and a respective second amount of charge collected at a second charge storage of the sensor pixel during the plurality of exposure times; determining for the plurality of exposure times a respective ratio value representing a ratio of the respective first amount of charge to the respective second amount of charge; determining a slope of a course of the determined ratio values with respect to the values of the second electrical potential used for the plurality of exposure times; and determining the color of the light received by the sensor pixel based on the slope.
An air conditioner comprising: a compressor ; an outdoor heat exchanger ; a main expansion device ; an outdoor unit comprising a refrigerant pipe connecting the outdoor heat exchanger to the main expansion device , the refrigerant pipe comprising a suction pipe that guides suction of a refrigerant into the compressor ; an indoor unit comprising an indoor heat exchanger; a connection pipe connecting the outdoor unit to the indoor unit ; and a mixed refrigerant in which R32 is contained at a content of about 50% or more is used as the refrigerant, characterized in that the air conditioner has cooling capacity of about 11 kW to about 16 kW, the refrigerant pipe is made of a ductile stainless steel material having a delta ferrite matrix structure of about 1% or less on the basis of a grain area, an average grain diameter of the ductile stainless steel material being about 30 μm to about 60 μm, and the refrigerant pipe has an outer diameter of about 19.05 mm, or about 15.88 mm or about 22.20 mm. a compressor ; an outdoor heat exchanger ; a main expansion device ; an outdoor unit comprising a refrigerant pipe connecting the outdoor heat exchanger to the main expansion device , the refrigerant pipe comprising a suction pipe that guides suction of a refrigerant into the compressor ; an indoor unit comprising an indoor heat exchanger; a connection pipe connecting the outdoor unit to the indoor unit ; and a mixed refrigerant in which R32 is contained at a content of about 50% or more is used as the refrigerant, characterized in that the air conditioner has cooling capacity of about 11 kW to about 16 kW, the refrigerant pipe is made of a ductile stainless steel material having a delta ferrite matrix structure of about 1% or less on the basis of a grain area, an average grain diameter of the ductile stainless steel material being about 30 μm to about 60 μm, and the refrigerant pipe has an outer diameter of about 19.05 mm, or about 15.88 mm or about 22.20 mm.