mhurhangee/patent-ind-claim-en huggingface dataset:
Method for communication between at least one meter device and a flying device , wherein the meter device is configured for recording a consumption and/or for collecting captured consumption data, wherein the flying device performs the following steps: a) movement of the flying device , which is capable of flight, to a prescribed target position associated with the meter device , b) reception of received signals on a radio channel associated with the meter device by a reception device of the flying device and ascertaining at least one piece of quality information, relating to a communication quality on the radio channel, on the basis of the received signals, wherein nonsatisfaction of a quality condition, satisfaction of which is dependent on the piece of quality information, results in the reception of received signals and the ascertainment of the piece of quality information being repeated after a communication protocol for communication with the meter device has been changed and/or while a position of the flying device and/or a directivity of the reception device are altered until the quality condition or a termination condition is satisfied, and in the event of satisfaction of the quality condition c) capturing at least one piece of meter information sent by the meter device by means of evaluation of the received signals and/or sending a control message for controlling the operation of the meter device to the meter device . a) movement of the flying device , which is capable of flight, to a prescribed target position associated with the meter device , b) reception of received signals on a radio channel associated with the meter device by a reception device of the flying device and ascertaining at least one piece of quality information, relating to a communication quality on the radio channel, on the basis of the received signals, wherein nonsatisfaction of a quality condition, satisfaction of which is dependent on the piece of quality information, results in the reception of received signals and the ascertainment of the piece of quality information being repeated after a communication protocol for communication with the meter device has been changed and/or while a position of the flying device and/or a directivity of the reception device are altered until the quality condition or a termination condition is satisfied, and in the event of satisfaction of the quality condition c) capturing at least one piece of meter information sent by the meter device by means of evaluation of the received signals and/or sending a control message for controlling the operation of the meter device to the meter device .
A rotary wing aircraft comprising a first variable pitch rotor blade supported for rotation about a common rotor axis of rotation in a first rotor plane of rotation and the first variable pitch rotor blade includes cyclic pitch control, a second variable pitch rotor blade supported for rotation about the common rotor axis of rotation in a second rotor plane of rotation and the second variable pitch rotor blade includes cyclic pitch control, three first servo actuators located between the first rotor plane of rotation and the second rotor plane of rotation and configured to vary a pitch of the first variable pitch rotor blade , a non-rotating structural backbone formed to include a generally hollow interior extending along the common rotor axis of rotation through the second rotor plane of rotation and the first servo actuators are coupled to the non-rotating structural backbone , a first blade pitch controller located between the first rotor plane of rotation and the second rotor plane of rotation for controlling a pitch of the first variable pitch rotor blade and the first servo actuators are coupled to the first blade pitch controller by three first pitch linkages, characterized in that the rotary wing aircraft further comprises three second servo actuators coupled to the non-rotating structural backbone between the first rotor plane of rotation and the second rotor plane of rotation and three second pitch linkages interconnecting the second servo actuators and a second blade pitch controller to vary a pitch of the second variable pitch rotor blade . a first variable pitch rotor blade supported for rotation about a common rotor axis of rotation in a first rotor plane of rotation and the first variable pitch rotor blade includes cyclic pitch control, a second variable pitch rotor blade supported for rotation about the common rotor axis of rotation in a second rotor plane of rotation and the second variable pitch rotor blade includes cyclic pitch control, three first servo actuators located between the first rotor plane of rotation and the second rotor plane of rotation and configured to vary a pitch of the first variable pitch rotor blade , a non-rotating structural backbone formed to include a generally hollow interior extending along the common rotor axis of rotation through the second rotor plane of rotation and the first servo actuators are coupled to the non-rotating structural backbone , a first blade pitch controller located between the first rotor plane of rotation and the second rotor plane of rotation for controlling a pitch of the first variable pitch rotor blade and the first servo actuators are coupled to the first blade pitch controller by three first pitch linkages, characterized in that the rotary wing aircraft further comprises three second servo actuators coupled to the non-rotating structural backbone between the first rotor plane of rotation and the second rotor plane of rotation and three second pitch linkages interconnecting the second servo actuators and a second blade pitch controller to vary a pitch of the second variable pitch rotor blade .
A marine route verifying apparatus , comprising: a display for displaying a user-scheduled route on a map, the user-scheduled route being defined by one or more ship positions input by the user; a user interface for accepting input of a travel starting time and date and a travel ending time and date on the route; memory that stores maritime caution information that is associated with ship position, time and date so as to define a range of ship positions, time periods and associated maritime caution levels, wherein the maritime caution levels include prohibited travel and travel caution; and a control unit executing a maritime caution information reading portion that is configured to extract maritime caution information, the extracted maritime caution information being associated with a defined range of ship positions and time periods on the user-scheduled route, and wherein the control unit further executes a route verifying portion that is configured to verify whether the user-scheduled route can be traveled based on the defined range of ship positions and time periods on the user-scheduled route and based on the extracted maritime caution information in correspondence with one or more ship positions on the route and the time points and dates that have been input via the user interface , wherein the display is configured to display the extracted associated maritime caution information, including the associated maritime caution level. a display for displaying a user-scheduled route on a map, the user-scheduled route being defined by one or more ship positions input by the user; a user interface for accepting input of a travel starting time and date and a travel ending time and date on the route; memory that stores maritime caution information that is associated with ship position, time and date so as to define a range of ship positions, time periods and associated maritime caution levels, wherein the maritime caution levels include prohibited travel and travel caution; and a control unit executing a maritime caution information reading portion that is configured to extract maritime caution information, the extracted maritime caution information being associated with a defined range of ship positions and time periods on the user-scheduled route, and wherein the control unit further executes a route verifying portion that is configured to verify whether the user-scheduled route can be traveled based on the defined range of ship positions and time periods on the user-scheduled route and based on the extracted maritime caution information in correspondence with one or more ship positions on the route and the time points and dates that have been input via the user interface , wherein the display is configured to display the extracted associated maritime caution information, including the associated maritime caution level.
A method for implementing a logical router in a network, the method comprising: receiving a definition of a logical router of a logical network for implementation by a plurality of network elements (510-520), the definition of the logical router comprising specification of a plurality of interfaces for connecting to an external network ; defining a plurality of routing components (405-415) for the logical router, each of the defined routing components (405-415) comprising a separate set of routes and separate set of logical interfaces, wherein defining the plurality of routing components (405-415) comprises: defining a distributed routing component that interfaces with other logical forwarding elements of the logical network ; and defining at least two centralized routing components to which the plurality of interfaces for connecting with the external network are assigned, each centralized routing component (i) for implementation on a different gateway machine and (ii) comprising at least one interface connecting the centralized routing component to the external network and at least one interface for connecting the centralized routing component to the distributed routing component ; and generating data for the implementation of the plurality of routing components (405-415) of the logical router in the network. receiving a definition of a logical router of a logical network for implementation by a plurality of network elements (510-520), the definition of the logical router comprising specification of a plurality of interfaces for connecting to an external network ; defining a plurality of routing components (405-415) for the logical router, each of the defined routing components (405-415) comprising a separate set of routes and separate set of logical interfaces, wherein defining the plurality of routing components (405-415) comprises: defining a distributed routing component that interfaces with other logical forwarding elements of the logical network ; and defining at least two centralized routing components to which the plurality of interfaces for connecting with the external network are assigned, each centralized routing component (i) for implementation on a different gateway machine and (ii) comprising at least one interface connecting the centralized routing component to the external network and at least one interface for connecting the centralized routing component to the distributed routing component ; and defining a distributed routing component that interfaces with other logical forwarding elements of the logical network ; and defining at least two centralized routing components to which the plurality of interfaces for connecting with the external network are assigned, each centralized routing component (i) for implementation on a different gateway machine and (ii) comprising at least one interface connecting the centralized routing component to the external network and at least one interface for connecting the centralized routing component to the distributed routing component ; and generating data for the implementation of the plurality of routing components (405-415) of the logical router in the network.
Method for assembling an aircraft pylon comprising a primary structure comprising upper and lower spars and first and second lateral panels , a secondary structure capping the primary structure , at least one internal system positioned at least partially inside the primary structure and at least one external system positioned between the primary structure and the secondary structure, the assembly method comprising: - a first step of assembling a subassembly comprising at least one of the upper and lower spars and at least one of the first and second lateral panels , - a step of mounting an internal systems module comprising at least one internal system and at least one support to which the internal system is connected, said at least one or each support being distinct from the primary structure , said at least one or each support comprising first and second parts that meet at a junction plane (PJ), each of the first and second parts of the support comprising a plate and a bracket positioned at a first side of the plate , - a second step of assembling the internal systems module and the subassembly assembled in the first assembly step, and during the second assembly step, each support for the internal systems module being connected to at least one upper or lower spar , and/or at least one first or second lateral panel of the subassembly assembled in the first assembly step, the bracket of each first and second parts of the support being connected to the first or second panel , - a third step of assembling those element(s) of the primary structure not assembled in the first assembly step, - a step of installing and securing the external systems and the secondary structure. - a first step of assembling a subassembly comprising at least one of the upper and lower spars and at least one of the first and second lateral panels , - a step of mounting an internal systems module comprising at least one internal system and at least one support to which the internal system is connected, said at least one or each support being distinct from the primary structure , said at least one or each support comprising first and second parts that meet at a junction plane (PJ), each of the first and second parts of the support comprising a plate and a bracket positioned at a first side of the plate , - a second step of assembling the internal systems module and the subassembly assembled in the first assembly step, and during the second assembly step, each support for the internal systems module being connected to at least one upper or lower spar , and/or at least one first or second lateral panel of the subassembly assembled in the first assembly step, the bracket of each first and second parts of the support being connected to the first or second panel , - a third step of assembling those element(s) of the primary structure not assembled in the first assembly step, - a step of installing and securing the external systems and the secondary structure.
A lift truck (C) comprising a driver protection having a roof comprising: - a supporting frame fixed or fixable to a load-bearing structure of said driver protection , said supporting frame being equipped with at least one opening defining a window; - a sheet of glass positioned above said supporting frame ; - at least one damping element interposed between said supporting frame and said load-bearing structure , configured for dissipating energy deriving from an impact striking the roof ; characterized in that the damping element comprises at least one hydraulic piston preferably preloaded with air. - a supporting frame fixed or fixable to a load-bearing structure of said driver protection , said supporting frame being equipped with at least one opening defining a window; - a sheet of glass positioned above said supporting frame ; - at least one damping element interposed between said supporting frame and said load-bearing structure , configured for dissipating energy deriving from an impact striking the roof ;
Device for printing on a first and/or a second side of a web of printing material, characterized by a printing device with at least two printing modules , wherein the printing modules are inkjet printing heads and the printing fluid is ink, and with an effective range that is associated with the printing device and in which printing fluid is transmitted to the web by means of the printing modules, a first guide element for guiding the web along at least a first part of the effective range, a turning device for turning the web, the turning device disposed downstream of the first guide element in terms of the direction of web travel, and a second guide element for guiding the web along at least a second part of the effective range, the second guide element disposed downstream of the turning device in terms of the direction of web travel and different from the first guide element , wherein at least one printing module is disposed to be movable relative to at least one of the two guide elements to carry out a relative movement and/or at least one of the two guide elements is disposed to be movable relative to at least one of the printing modules.
A dry-running, end-face mechanical seal, comprising: a gland plate in surrounding, non-contacting relationship with a rotatable shaft ; a stator seal face fixed to said gland plate in surrounding, non-contacting relationship with the rotatable shaft , a rear surface of the stator seal face being in direct, parallel contact with a seal-contacting surface of the gland plate , said rear surface of the stator seal face and said seal-contacting surface of the gland plate both being flat to within a tolerance of three microns and smooth to within 20 RMS; a rotor mounting structure arranged in a rotationally fixed, axially movable relationship with said rotatable shaft ; a rotor seal face supported by said rotor mounting structure and positioned such that a front surface of the rotor seal face is in direct parallel contact with a front surface of said stator seal face , thereby forming a dry contacting seal therebetween; a cooling annulus formed in said gland plate and bounded on at least one side by the rear surface of the stator seal face ; at least one inlet port configured to allow air to flow from a region proximal to said rotatable shaft into said cooling annulus ; and at least one outlet port configured to allow air to escape from said cooling annulus . a gland plate in surrounding, non-contacting relationship with a rotatable shaft ; a stator seal face fixed to said gland plate in surrounding, non-contacting relationship with the rotatable shaft , a rear surface of the stator seal face being in direct, parallel contact with a seal-contacting surface of the gland plate , said rear surface of the stator seal face and said seal-contacting surface of the gland plate both being flat to within a tolerance of three microns and smooth to within 20 RMS; a rotor mounting structure arranged in a rotationally fixed, axially movable relationship with said rotatable shaft ; a rotor seal face supported by said rotor mounting structure and positioned such that a front surface of the rotor seal face is in direct parallel contact with a front surface of said stator seal face , thereby forming a dry contacting seal therebetween; a cooling annulus formed in said gland plate and bounded on at least one side by the rear surface of the stator seal face ; at least one inlet port configured to allow air to flow from a region proximal to said rotatable shaft into said cooling annulus ; and at least one outlet port configured to allow air to escape from said cooling annulus .
Calibration method for a nuclear magnetic flowmeter with a measuring tube through which a multiphase medium can flow, wherein the measuring tube can be connected to an inlet tube arranged upstream of the measuring tube in the flow direction of the medium and to an outlet tube arranged downstream of the measuring tube in the flow direction , wherein a medium bypass is assigned to the measuring tube , wherein the medium bypass includes a bypass tube , an inlet valve and/or an outlet valve , and wherein for a calibration mode, the bypass tube can be connected on the one hand to the inlet tube and on the other hand to the outlet tube , namely via the inlet valve or via the outlet valve or via the inlet valve and via the outlet valve , characterized in that the flowmeter can operate in a measuring mode on the one hand and in a calibration mode on the other hand wherein, in the measuring mode, the medium is led from the inlet tube via the inlet valve of the medium bypass into the measuring tube and from the measuring tube via the outlet valve of the medium bypass into the outlet tube and, in the calibration mode, the medium is led from the inlet tube via the inlet valve of the medium bypass into the bypass tube and from the bypass tube via the outlet valve of the medium bypass into the outlet tube , and wherein during calibration, operation measurements are performed by the flowmeter on the medium residing in the measuring tube . wherein the measuring tube can be connected to an inlet tube arranged upstream of the measuring tube in the flow direction of the medium and to an outlet tube arranged downstream of the measuring tube in the flow direction , wherein a medium bypass is assigned to the measuring tube , wherein the medium bypass includes a bypass tube , an inlet valve and/or an outlet valve , and wherein for a calibration mode, the bypass tube can be connected on the one hand to the inlet tube and on the other hand to the outlet tube , namely via the inlet valve or via the outlet valve or via the inlet valve and via the outlet valve , characterized in that the flowmeter can operate in a measuring mode on the one hand and in a calibration mode on the other hand wherein, in the measuring mode, the medium is led from the inlet tube via the inlet valve of the medium bypass into the measuring tube and from the measuring tube via the outlet valve of the medium bypass into the outlet tube and, in the calibration mode, the medium is led from the inlet tube via the inlet valve of the medium bypass into the bypass tube and from the bypass tube via the outlet valve of the medium bypass into the outlet tube , and wherein during calibration, operation measurements are performed by the flowmeter on the medium residing in the measuring tube .
A method of wireless communication, performed by a base station, comprising: serving data to a user equipment, UE, or receiving data from the UE via a first communication link that uses a first radio access technology, RAT; transmitting a configuration message to the UE indicating that data will be served or received via a second communication link that uses a second RAT; transmitting a protocol layer status report to the UE, wherein the protocol layer status report is transmitted on a data bearer that is being switched to the second RAT; determining unacknowledged data of the data served to the UE using the first RAT based on at least one protocol layer status report received from the UE; initiating a configuration procedure to switch service or reception of data from the first communication link that uses the first RAT to the second communication link that uses the second RAT; and forwarding the unacknowledged data to be served using the second RAT. serving data to a user equipment, UE, or receiving data from the UE via a first communication link that uses a first radio access technology, RAT; transmitting a configuration message to the UE indicating that data will be served or received via a second communication link that uses a second RAT; transmitting a protocol layer status report to the UE, wherein the protocol layer status report is transmitted on a data bearer that is being switched to the second RAT; determining unacknowledged data of the data served to the UE using the first RAT based on at least one protocol layer status report received from the UE; initiating a configuration procedure to switch service or reception of data from the first communication link that uses the first RAT to the second communication link that uses the second RAT; and forwarding the unacknowledged data to be served using the second RAT.