mhurhangee/patent-ind-claim-en huggingface dataset:
Method for aligning two workpieces (102, 103; 602, 603) using the manipulator of Claim 12 for forming a join, wherein the method comprises the following steps: - placing or keeping available at least two workpieces (102, 103; 602, 603) in a preparation station (3; 503); - gripping the first workpiece (102; 602) by the first gripper (13; 513); - gripping the second workpiece (103; 603) by the second gripper (14; 514); - retrieving the workpieces (102, 103; 602, 603) from the preparation station (3; 503) and transporting the workpieces (102, 103; 602, 603) to a machining station (4; 504); - wherein, in a longitudinal alignment step, the first workpiece (103; 603) is aligned relative to the second workpiece (103; 603) along at least one of the workpiece edges (104a, 105a; 604a, 604b) by a linear movement of at least one of the grippers (13, 14; 513, 514) relative to the respective other gripper (13, 14; 513, 514); and - wherein the longitudinal alignment step is carried out while transporting the workpieces (102, 103; 602, 603) from the preparation station (3; 503) to the machining station(4; 504); wherein the first gripper (13; 513) and the second gripper (14; 514) are disposed on a common manipulator (2; 502), preferably on a common multi-axis robot, and are conjointly moved in space from the preparation station (3; 503) to the machining station (4; 504) by means of this manipulator (2; 502). - placing or keeping available at least two workpieces (102, 103; 602, 603) in a preparation station (3; 503); - gripping the first workpiece (102; 602) by the first gripper (13; 513); - gripping the second workpiece (103; 603) by the second gripper (14; 514); - retrieving the workpieces (102, 103; 602, 603) from the preparation station (3; 503) and transporting the workpieces (102, 103; 602, 603) to a machining station (4; 504); - wherein, in a longitudinal alignment step, the first workpiece (103; 603) is aligned relative to the second workpiece (103; 603) along at least one of the workpiece edges (104a, 105a; 604a, 604b) by a linear movement of at least one of the grippers (13, 14; 513, 514) relative to the respective other gripper (13, 14; 513, 514); and - wherein the longitudinal alignment step is carried out while transporting the workpieces (102, 103; 602, 603) from the preparation station (3; 503) to the machining station(4; 504); wherein the first gripper (13; 513) and the second gripper (14; 514) are disposed on a common manipulator (2; 502), preferably on a common multi-axis robot, and are conjointly moved in space from the preparation station (3; 503) to the machining station (4; 504) by means of this manipulator (2; 502).
An apparatus comprising: first circuitry at a first device capable of executing one or more applications using a hierarchical memory architecture including a first near memory and a first far memory maintained at the first device, the first near memory having a lower latency than the first far memory ; a detect logic (882-1) to detect second circuitry at a second device that is capable of executing the one or more applications using the hierarchical memory architecture that also includes a second near memory maintained at the second device, the second near memory having a lower latency than the first far memory ; a migration logic (822-2) to cause a copy of memory contents and a computational state associated with the first circuitry's execution of the one or more applications to be migrated over a wired or wireless interconnect from the first near memory to the second near memory for the second circuitry to execute the one or more applications; and a buffer logic (822-3) to configure the first near memory to function as a buffer capable of periodically receiving data copied from dirty blocks at the second near memory. first circuitry at a first device capable of executing one or more applications using a hierarchical memory architecture including a first near memory and a first far memory maintained at the first device, the first near memory having a lower latency than the first far memory ; a detect logic (882-1) to detect second circuitry at a second device that is capable of executing the one or more applications using the hierarchical memory architecture that also includes a second near memory maintained at the second device, the second near memory having a lower latency than the first far memory ; a migration logic (822-2) to cause a copy of memory contents and a computational state associated with the first circuitry's execution of the one or more applications to be migrated over a wired or wireless interconnect from the first near memory to the second near memory for the second circuitry to execute the one or more applications; and a buffer logic (822-3) to configure the first near memory to function as a buffer capable of periodically receiving data copied from dirty blocks at the second near memory.
Gas burner for a cooking zone , with a gas shut-off valve , a burner housing , which can be fastened to a gas supply line of the gas burner , and a burner head which can be moved relative to the burner housing , wherein the burner head can be moved from an open position into a closed position for optionally opening and closing the gas shut-off valve , wherein the burner head is pretensioned in the direction of the closed position with the aid of a spring device , wherein the burner housing and/or the burner head has at least one primary air supply opening for supplying primary air into a mixing chamber of the gas burner , wherein the gas shut-off valve has a valve body , which is received at least in sections in the burner head , characterised in that the valve body has at least one radially arranged burner gas inlet opening .
A composite tank comprising: a tank body inside which a combustible material is to be stored, the tank body having a first resin portion (11;12;13;15) formed from a fiber reinforced resin, and a metal portion formed from a metal material, a second resin portion which covers at least those regions on an inner surface of the tank body where the first resin portion adjoins the metal portion , and a plurality of conductive portions that enable charge transfer through the second resin portion , from a surface that contacts the combustible material, when the same is stored in the tank body , through to the first resin portion (11;12;13;15), characterized in that the second resin portion is formed from a fiber reinforced resin, fiber incorporated within the second resin portion has a higher electrical resistivity than fiber incorporated within the first resin portion (11;12;13;15), and the second resin portion forms a layer that isolates the first resin portion (11;12;13;15) from the metal portion , and the conductive portions are portions from which the fibers have been removed, which are formed solely from the resin, and which penetrate from the surface that contacts the combustible material through to the first resin portion (11;12;13;15). a tank body inside which a combustible material is to be stored, the tank body having a first resin portion (11;12;13;15) formed from a fiber reinforced resin, and a metal portion formed from a metal material, a second resin portion which covers at least those regions on an inner surface of the tank body where the first resin portion adjoins the metal portion , and a plurality of conductive portions that enable charge transfer through the second resin portion , from a surface that contacts the combustible material, when the same is stored in the tank body , through to the first resin portion (11;12;13;15), characterized in that the second resin portion is formed from a fiber reinforced resin, fiber incorporated within the second resin portion has a higher electrical resistivity than fiber incorporated within the first resin portion (11;12;13;15), and the second resin portion forms a layer that isolates the first resin portion (11;12;13;15) from the metal portion , and the conductive portions are portions from which the fibers have been removed, which are formed solely from the resin, and which penetrate from the surface that contacts the combustible material through to the first resin portion (11;12;13;15).
Tyre , in particular vehicle tyre, wherein the tyre is formed by a plurality of tyre building components and at least one sensor element (9; 9a, 9b, 9c, 9d, 9e) is arranged in the tyre building components in such a way that an abrasion height (A) of the tread of the tyre can be inferred by means of the at least one sensor element (9; 9a, 9b, 9c, 9d, 9e), wherein for this purpose an electrical measured variable (R, C, L) characterizing the electrical property of the at least one sensor element (9; 9a, 9b, 9c, 9d, 9e) can be detected by way of a signal-conducting connection , and an abrasion height (A) of the tread can be inferred from a behaviour over time of the detectable electrical measured variable (R, C, L) of the respective sensor element (9; 9a, 9b, 9c, 9d, 9e), wherein the at least one sensor element (9; 9a, 9b, 9c, 9d, 9e) has a flexible support of a two-dimensional extent and deposited on the support is at least one conductive structure , wherein the detectable electrical measured variable (R, C, L) characterizes the electrical property of the at least one deposited conductive structure on the support and the flexible support with the deposited conductive structure is arranged in the tyre building components in such a way that an abrasion height (A) of the tread can be inferred from a change over time of the electrical measured variable (R, C, L), wherein the sensor element (9; 9a, 9b, 9c, 9d, 9e) is integrated at least in certain regions in at least one tyre building component, wherein the sensor element (9; 9a, 9b, 9c, 9d, 9e) is incorporated at least in certain regions in the tyre building component in the tyre building process, wherein the sensor element (9; 9a, 9b, 9c, 9d, 9e) is formed as a sensor element (9; 9a, 9b, 9c, 9d, 9e) that has been shaped at least in certain regions, with a shaped support and a shaped conductive structure , characterized in that the shaped sensor element (9; 9a, 9b, 9c, 9d, 9e) is made to extend two-dimensionally in the axial direction in the tread and is arranged in the tyre building component in such a way that the sensor element (9; 9a, 9b, 9c, 9d, 9e) is adapted to a contouring of the tyre , so that the sensor element (9; 9a, 9b, 9c, 9d, 9e) is placed around a tread groove or other structure incorporated in the tread .
A hydrogen filling apparatus comprising: a plurality of filling systems (101, 102, ···); a filling control device (10, 20, ···) for each of the filling systems (101, 102, ···); a filling pipe (1, 11, ···) communicating with a rear facility (30, 40, •••) in each of the filling systems (101, 102, ···); a set of filling members interposed in each of the filling pipes (1, 11, •••) and connected to each of the filling control devices (10, 20, ··· ); and a filling hose (7, 17, •••) connected to each of the filling pipes (1, 11, •••), each filling hose (7, 17, •••) having a filling nozzle (6, 16, ···) at a tip; wherein one of the plurality of filling control devices (10, 20, ···) has a function of selectively exerting a first control mode configured to control only the filling system (101, 102, •••) including the filling control device (10, 20, ···) and a second control mode shared as a control device for the filling systems (101, 102, •••), and a switching means for switching between the first control mode and the second control mode in the one of the filling control devices (10, 20, ···) is provided, wherein said filling control device (10, 20, ···) having a function of selectively exerting the first control mode and the second control mode is connected to another filling control device via a relay device , and has a function of adjusting the filling member in the filling system (101, 102, ···) equipped with another filling control device via the relay device in the second control mode. a plurality of filling systems (101, 102, ···); a filling control device (10, 20, ···) for each of the filling systems (101, 102, ···); a filling pipe (1, 11, ···) communicating with a rear facility (30, 40, •••) in each of the filling systems (101, 102, ···); a set of filling members interposed in each of the filling pipes (1, 11, •••) and connected to each of the filling control devices (10, 20, ··· ); and a filling hose (7, 17, •••) connected to each of the filling pipes (1, 11, •••), each filling hose (7, 17, •••) having a filling nozzle (6, 16, ···) at a tip; wherein one of the plurality of filling control devices (10, 20, ···) has a function of selectively exerting a first control mode configured to control only the filling system (101, 102, •••) including the filling control device (10, 20, ···) and a second control mode shared as a control device for the filling systems (101, 102, •••), and a switching means for switching between the first control mode and the second control mode in the one of the filling control devices (10, 20, ···) is provided,
A method for measuring geometry deformations of a rotor groove with a fir-tree configuration, the rotor groove being a turbine component, the method comprising the steps of: providing a fir-tree attachment part and adjacent rotor grooves in various locations on their surfaces with measuring marks , the fir-tree attachment part being located between adjacent rotor grooves ; using the measuring marks as a reference point in determining, in a first measurement, a length (L2) on said rotor groove prior to the turbine being placed into service; operating the turbine for a period of time; determining, in a second measurement, said length (L2) on said rotor groove using again said measuring marks as a reference point, after said operating period; and comparing the measured lengths (L2) of said first and second measurement; and determining an amount of creep deformation in said rotor groove , based on a difference between said measured lengths. providing a fir-tree attachment part and adjacent rotor grooves in various locations on their surfaces with measuring marks , the fir-tree attachment part being located between adjacent rotor grooves ; using the measuring marks as a reference point in determining, in a first measurement, a length (L2) on said rotor groove prior to the turbine being placed into service; operating the turbine for a period of time; determining, in a second measurement, said length (L2) on said rotor groove using again said measuring marks as a reference point, after said operating period; and comparing the measured lengths (L2) of said first and second measurement; and determining an amount of creep deformation in said rotor groove , based on a difference between said measured lengths.
A method for generating a microservice application, comprising: determining (S 101) a service set of microservices according to a first user requirement; determining (S102) a deployment mode of devices to be controlled by the microservice application; determining (S 103) parameter information of the microservice application according to a second user requirement; and generating (S104) the microservice application according to the service set, the deployment mode and the parameter information, wherein the deployment mode comprises: physical location deployment and process architecture deployment; wherein the physical location deployment comprises at least one of: a centralized mode, a distributed mode, or a hybrid mode; and wherein the process architecture deployment comprises: a compact mode and/or a safe mode. determining (S 101) a service set of microservices according to a first user requirement; determining (S102) a deployment mode of devices to be controlled by the microservice application; determining (S 103) parameter information of the microservice application according to a second user requirement; and generating (S104) the microservice application according to the service set, the deployment mode and the parameter information, wherein the deployment mode comprises: physical location deployment and process architecture deployment; wherein the physical location deployment comprises at least one of: a centralized mode, a distributed mode, or a hybrid mode; and wherein the process architecture deployment comprises: a compact mode and/or a safe mode.
Mobile hydraulic construction machine, in particular hydraulic excavator, comprising an internal combustion engine and a hydraulics system powered by means of the hydraulic motor, wherein the hydraulics system comprises at least one hydraulic pressure accumulator from which at least one hydromotor for start-up of the internal combustion motor can be supplied, and wherein at least one secondary consumer of the hydraulics system can be supplied from the hydraulic pressure accumulator, wherein the hydraulic pressure accumulator can be directly connected with the hydraulics motor or the adjustment pump via a switchable start valve, characterized in that at least one non-return valve is connected downstream the start valve in order to ensure the prioritized operation of the primary consumer(s), and the hydraulics system comprises a priority valve so that at least a primary consumption of high priority and the hydraulic pressure accumulator or one or multiple secondary consumers of low priority can be supplied by means of the hydraulic pump. at least one non-return valve is connected downstream the start valve in order to ensure the prioritized operation of the primary consumer(s), and the hydraulics system comprises a priority valve so that at least a primary consumption of high priority and the hydraulic pressure accumulator or one or multiple secondary consumers of low priority can be supplied by means of the hydraulic pump.
A flame shield for a battery of an electric vehicle, in particular a lithium-ion battery, characterized in that it comprises at least one flame-resistant layer that is able to maintain a temperature drop of at least 350° C, more preferably at least 500° C and even more preferably at least 600° C in a Bunsen-burner test as described herein, lasting 5 minutes and whereby the flame resistant layer consists of a porous fibrous non-woven impregnated with polyurethane , wherein the fibers comprised in the porous fibrous non-woven have a melting temperature of at least 1100° C, wherein the polyurethane does not comprise any flame retardant and wherein the polyurethane impregnates the porous fibrous-non woven in such a way that the flame-resistant layer is impervious to air-flow.
An aircraft , comprising: an airframe ; an engine (E) mounted to the airframe ; and an engine inlet for receiving an ambient airflow and providing the ambient airflow to the engine (E), wherein an amount of airflow provided to the engine inlet is controllable, characterized in further comprising a deflector mounted to the airframe upstream from the engine inlet , the deflector being operable to control the amount of airflow provided to the engine inlet , wherein the deflector is configured to move between a first position and a second position along the longitudinal axis (L) of the aircraft . an airframe ; an engine (E) mounted to the airframe ; and an engine inlet for receiving an ambient airflow and providing the ambient airflow to the engine (E), wherein an amount of airflow provided to the engine inlet is controllable, characterized in further comprising a deflector mounted to the airframe upstream from the engine inlet , the deflector being operable to control the amount of airflow provided to the engine inlet , wherein the deflector is configured to move between a first position and a second position along the longitudinal axis (L) of the aircraft .
A bending section for an endoscope comprising a number of segments , where adjacent segments (11, 12; 12, 12; 12, 13) are connected by a first hinge and a second hinge defining a hinge plane, both the first and the second hinges are made integrally from the same material as the segments , the first and second hinges are arranged for allowing the connected segments (11, 12; 12, 12; 12, 13) to bend in a bending plane, characterized in that a second hinge at the distal end of a segment forms a continuous rib in said hinge plane and perpendicular to the bending plane, with the second hinge at the proximal end of the segment , so as to separate two passages , which are formed in each segment and continue through the whole bending section .
An image processing apparatus that converts three-dimensional voxel data to two-dimensional pixel data on an arbitrary projection plane, the image processing apparatus comprising: a voxel coordinate data generation unit configured to generate voxel coordinate data in which respective brightness values are associated with coordinate values of respective voxels and to rearrange the voxel coordinate data in order of magnitude of the brightness value; a coordinate conversion unit configured to read a predetermined number of the rearranged voxel coordinate data to a cache memory in order from the largest brightness value in the three-dimensional voxel data and to convert each voxel of the rearranged voxel coordinate data to corresponding pixels on the projection plane , characterized in that the predetermined number is set based on a capacity of the cache memory. a voxel coordinate data generation unit configured to generate voxel coordinate data in which respective brightness values are associated with coordinate values of respective voxels and to rearrange the voxel coordinate data in order of magnitude of the brightness value; a coordinate conversion unit configured to read a predetermined number of the rearranged voxel coordinate data to a cache memory in order from the largest brightness value in the three-dimensional voxel data and to convert each voxel of the rearranged voxel coordinate data to corresponding pixels on the projection plane , characterized in that the predetermined number is set based on a capacity of the cache memory.
Straightening head comprising a steam distribution circuit and a front wall provided with a treatment face intended to face a garment to be straightened, the treatment face comprising at least one steam outlet hole , the steam distribution circuit comprising an inlet channel comprising an inlet port intended to be connected to a steam duct , the steam distribution circuit further comprising an internal chamber , the inlet channel comprising an outlet port opening into the internal chamber , the internal chamber comprising a condensate drainage port communicating with a condensate return circuit , characterised in that the condensate return circuit opens into the steam duct or into the inlet channel .