mhurhangee/ep-ind-claims huggingface dataset:
An optical measurement module comprising: a light source configured to emit an original light beam; a collimator configured to collimate the original light beam into a collimated light beam; a first beam splitter configured to direct the collimated light beam to an analyte, wherein the analyte transforms the collimated light beam into a measurement light beam; a second beam splitter configured to receive a first part of the measurement light beam via the first beam splitter and divides the first part of the measurement light beam into a first detection light beam and a second detection light beam; a third beam splitter (33; 34; 35) and a third light receiving module (53;54;55), the third beam splitter being configured to direct a second part of the measurement light beam to the third light receiving module (53;54;55); a first light receiving module configured to detect the first detection light beam; a second light receiving module configured to detect the second detection light beam, and each of the first light receiving module and the second light receiving module is configured to determine one of the optical properties of the analyte, the optical property being selected from the group consisting of absorbance, refractive index, polarization, fluorescence, and inelastic scattering; wherein the third light receiving module is a thermometer, a telemeter or an image sensor. a light source configured to emit an original light beam; a collimator configured to collimate the original light beam into a collimated light beam; a first beam splitter configured to direct the collimated light beam to an analyte, wherein the analyte transforms the collimated light beam into a measurement light beam; a second beam splitter configured to receive a first part of the measurement light beam via the first beam splitter and divides the first part of the measurement light beam into a first detection light beam and a second detection light beam; a third beam splitter (33; 34; 35) and a third light receiving module (53;54;55), the third beam splitter being configured to direct a second part of the measurement light beam to the third light receiving module (53;54;55); a first light receiving module configured to detect the first detection light beam; a second light receiving module configured to detect the second detection light beam, and each of the first light receiving module and the second light receiving module is configured to determine one of the optical properties of the analyte, the optical property being selected from the group consisting of absorbance, refractive index, polarization, fluorescence, and inelastic scattering; wherein the third light receiving module is a thermometer, a telemeter or an image sensor.
Method comprising computing apparatuses, required for its execution, for calculating parameters for operation of a system with optimal availability, comprising an operating apparatus comprising a production installation for generating products, or comprising an operating apparatus comprising one or more vehicles, parts of vehicles, rails or power supply for the operation of the vehicles, a carriage or a switch of a railway system, in each case with a first component, a first warehouse with a first number of examples of a second component and a second warehouse with a second number of examples of the second component, wherein the second component is identical in construction to the first component, and the first and the second component (11, 12) have a first or second arrival time and a first or second service end time ( t eos1, t eos2), wherein the first and second arrival time identify that point in time in each case at which the respective component (11, 12) is received in the system, and at least one example of the second component is provided from the first warehouse to the second warehouse as soon as the second number drops below an optimal warehouse size and the second number therefore once again reaches the optimal warehouse size, wherein the optimal warehouse size is determined using the first and second arrival time and the first and second service end time ( t eos1, t eos2), and during operation of the operating apparatus, when the first service end time ( t eos1) of the first component is reached, an example of the second component is provided from the second warehouse to the operating apparatus and in the operating apparatus the first component is replaced with the second component. wherein the second component is identical in construction to the first component, and the first and the second component (11, 12) have a first or second arrival time and a first or second service end time ( t eos1, t eos2), wherein the first and second arrival time identify that point in time in each case at which the respective component (11, 12) is received in the system, and at least one example of the second component is provided from the first warehouse to the second warehouse as soon as the second number drops below an optimal warehouse size and the second number therefore once again reaches the optimal warehouse size, wherein the optimal warehouse size is determined using the first and second arrival time and the first and second service end time ( t eos1, t eos2), and during operation of the operating apparatus, when the first service end time ( t eos1) of the first component is reached, an example of the second component is provided from the second warehouse to the operating apparatus and in the operating apparatus the first component is replaced with the second component.
A method of communication by a machine type communications, MTC, device comprising: estimating (430; 1305 a signal to interference noise ratio, SINR, of one or more resource blocks of one or more target devices; characterized by selecting one or more of the resource blocks of the one or more target devices based at least in part on the estimated SINR; allocating the one or more selected resource blocks to be in a first resource pool; estimating (450; 1325) a SINR of the MTC device on one or more resource blocks of a target device of the one or more target devices; selecting one or more of the resource blocks of the target device to be in a second resource pool based at least in part on the estimated SINR of the MTC device; and transmitting a signal to the target device over one or more resource blocks common to both the first resource pool and the second resource pool. estimating (430; 1305 a signal to interference noise ratio, SINR, of one or more resource blocks of one or more target devices; characterized by selecting one or more of the resource blocks of the one or more target devices based at least in part on the estimated SINR; allocating the one or more selected resource blocks to be in a first resource pool; estimating (450; 1325) a SINR of the MTC device on one or more resource blocks of a target device of the one or more target devices; selecting one or more of the resource blocks of the target device to be in a second resource pool based at least in part on the estimated SINR of the MTC device; and transmitting a signal to the target device over one or more resource blocks common to both the first resource pool and the second resource pool.
A method of testing a cable (12, 206), the method comprising: providing a tester which is a boundary scan compliant device comprising a boundary scan interface for communicating with a computer (16, 204), wherein the computer has boundary scan software installed on it, for communicating with and controlling the tester (14, 202); providing at least one connector(30, 32) on a board of the tester, each connector having multiple connector electrical contacts, and a computer electrically coupled to the connector electrical contacts, wherein the at least one connector (30, 32) includes more than two connectors having different number of contacts; electrically coupling ends (40, 42) of cable electrical conductors of the cable (12, 206) to respective of the connector electrical contacts of the tester (14, 202) that have a corresponding number of contacts; sending a signal from the computer (16, 204) to one of the connector electrical contacts, which is in contact with one of the cable electrical conductors; and at the same time as the sending, monitoring, using the computer (16, 204), at least multiple other of the connector electrical contacts; wherein the sending and the monitoring are accomplished through the tester (14, 202) that includes the at least one connector and that is operatively coupled to both the computer (16, 204) and the ends (40, 42) of the cable (12, 206). providing a tester which is a boundary scan compliant device comprising a boundary scan interface for communicating with a computer (16, 204), wherein the computer has boundary scan software installed on it, for communicating with and controlling the tester (14, 202); providing at least one connector(30, 32) on a board of the tester, each connector having multiple connector electrical contacts, and a computer electrically coupled to the connector electrical contacts, wherein the at least one connector (30, 32) includes more than two connectors having different number of contacts; electrically coupling ends (40, 42) of cable electrical conductors of the cable (12, 206) to respective of the connector electrical contacts of the tester (14, 202) that have a corresponding number of contacts; sending a signal from the computer (16, 204) to one of the connector electrical contacts, which is in contact with one of the cable electrical conductors; and at the same time as the sending, monitoring, using the computer (16, 204), at least multiple other of the connector electrical contacts; wherein the sending and the monitoring are accomplished through the tester (14, 202) that includes the at least one connector and that is operatively coupled to both the computer (16, 204) and the ends (40, 42) of the cable (12, 206).
Elevator lift, in particular for conveying persons, with a cabin consisting of side walls, which can be moved in the direction of travel of the cabin in a surrounding shaft wall, wherein the cabin and the shaft wall surrounding it are in each case formed in an at least approximately cylindrical external shape, wherein they are dimensioned in cross-section as circular, polygonal, or oval, and at least the side walls of the cabin and the shaft wall preferably consist of a transparent material, preferably glass panes, characterized in that three longitudinal elements are arranged in the shaft wall, offset to one another as required by more or less than 120°, or, in the event of a door being provided on the front and rear side of the cabin, four longitudinal elements are provided offset by 90°, which project into an intermediate space between the shaft wall and the cabin, and at which sliding elements are guided, projecting laterally at the cabin, wherein the sliding elements secured to the profiles are placed below and above the interior space of the cabin.
Freehand writing device (10, 80, 90, 120) for insertion, storage, transport and use of a ring / spiral pad comprising a front cover, a rear cover and at least two joint devices arranged between mutually facing corners of an inner face of the front cover and of an inner face of the rear cover and connecting the front cover and the rear cover to one another in a fold-openable and fold-closable manner, characterized in that a receptacle for a holding rod (20, 22) is provided at each joint device, and the pad is fastenable captively between the joint devices by means of the holding rod(s) (20, 22), which are insertable longitudinal-axially into the rings / spiral of the pad.
A method for displaying information in particular in a vehicle, in which graphics data can be generated by a control device, which graphics data can control a display surface such that in a first display mode graphic objects (13, 14) and/or buttons (16, 17, 20) for visualizing information of a first vehicle device are displayed and in a second display mode graphic objects (18, 19) and/or buttons for visualizing information of a plurality of vehicle devices (9, 10-1, 10-2, 10-3) are displayed, characterized in that in a transition from the first display mode, which provides a display for the application of the vehicle device, into the second display mode, which provides an initial display, the representation of the graphic objects (13, 14) and/or buttons (16, 17, 20) for visualizing information of the first vehicle device is decreased in size and changed and, during the same, on the edge of the display surface graphic objects and/or buttons for visualizing information of other vehicle devices (10-1, 10-2, 10-3) are re-displayed and said graphic objects and/or buttons for visualizing information of other vehicle devices (10-1, 10-2, 10-3) are moved from the edge of the display surface in the direction of the center of the display surface.
Method for scanning a scanning angle and for evaluating a detector of a lidar apparatus, wherein - at least one beam is created by a beam source for scanning the scanning angle, - at least one beam that has been reflected at an object (10, 12, 14) is received by receiver optics and directed to a detector area of the detector, - a time-of-flight (t) of the at least one reflected beam is ascertained using the lidar apparatus, - the at least one received beam is evaluated for the purpose of ascertaining further information regarding the received beam, in particular the shape of the beam or the intensity of the beam or the reflectivity of the object (10, 12, 14), characterized in that, in order to reduce the amount of measurement values and accelerate the evaluation of the received beam, at least one region (22, 24, 26) of the detector area is selected on the basis of the ascertained time-of-flight (t) of the at least one received beam for the purpose of evaluating the at least one received beam for the purpose of ascertaining the further information regarding the received beam, wherein the at least one region (22, 24, 26) of the detector area is chosen on the basis of the speed of the light, a focal length (f) of the receiver optics and a distance between the beam source and the receiver optics. - at least one beam is created by a beam source for scanning the scanning angle, - at least one beam that has been reflected at an object (10, 12, 14) is received by receiver optics and directed to a detector area of the detector, - a time-of-flight (t) of the at least one reflected beam is ascertained using the lidar apparatus, - the at least one received beam is evaluated for the purpose of ascertaining further information regarding the received beam, in particular the shape of the beam or the intensity of the beam or the reflectivity of the object (10, 12, 14), characterized in that, in order to reduce the amount of measurement values and accelerate the evaluation of the received beam, at least one region (22, 24, 26) of the detector area is selected on the basis of the ascertained time-of-flight (t) of the at least one received beam for the purpose of evaluating the at least one received beam for the purpose of ascertaining the further information regarding the received beam, wherein the at least one region (22, 24, 26) of the detector area is chosen on the basis of the speed of the light, a focal length (f) of the receiver optics and a distance between the beam source and the receiver optics.
A security system for screening of individuals, comprising: two stationary cylinders, a revolving mechanism situated within each stationary cylinder comprising at least one blade forming a revolving door, and an isolated area comprising at least two walls, located between said two stationary cylinders, wherein a first means of for detection is employed within the isolated area as an individual travels through one of the stationary cylinders as an entrance cylinder, then through the isolated area, and finally through one of the stationary cylinders as an exit cylinder, characterized in that the revolving doors are configured to spin continuously around an axis in their respective stationary cylinders, creating a flow for continuous screening of moving individuals; each revolving door is configured to act as a means for entering and as a means for exiting for enabling individuals to move in either direction; and the at least one blade within each stationary cylinder forming a revolving door is comprised of a blast-resistant material. two stationary cylinders, a revolving mechanism situated within each stationary cylinder comprising at least one blade forming a revolving door, and an isolated area comprising at least two walls, located between said two stationary cylinders, wherein a first means of for detection is employed within the isolated area as an individual travels through one of the stationary cylinders as an entrance cylinder, then through the isolated area, and finally through one of the stationary cylinders as an exit cylinder, characterized in that the revolving doors are configured to spin continuously around an axis in their respective stationary cylinders, creating a flow for continuous screening of moving individuals; each revolving door is configured to act as a means for entering and as a means for exiting for enabling individuals to move in either direction; and the at least one blade within each stationary cylinder forming a revolving door is comprised of a blast-resistant material.
A holding device for use with a telescopically extensible crane boom that comprises a base section and one or more telescopic crane boom sections (57b 1 -57b 4) carried by the base section, wherein the holding device is adapted to co-operate with a load handling tool pivotally connected to an outer end of the crane boom, in order to keep the load handling tool in a given parking position in relation to the crane boom, characterized in that the holding device comprises: - an attachment, which is to be fixed to an outer end of one of the telescopic crane boom sections (57b 1 -57b 4) of the crane boom; - a tool holder, which is detachably mountable to the attachment and configured for engagement with the load handling tool in order to support the load handling tool against the crane boom and keep the load handling tool in said parking position, wherein the tool holder is provided with at least one sliding member, through which the tool holder is configured to slidably rest against an external surface on the crane boom when the tool holder is mounted to the attachment; and - a locking mechanism for locking the tool holder and the attachment to each other when the tool holder is mounted to the attachment. - an attachment, which is to be fixed to an outer end of one of the telescopic crane boom sections (57b 1 -57b 4) of the crane boom; - a tool holder, which is detachably mountable to the attachment and configured for engagement with the load handling tool in order to support the load handling tool against the crane boom and keep the load handling tool in said parking position, wherein the tool holder is provided with at least one sliding member, through which the tool holder is configured to slidably rest against an external surface on the crane boom when the tool holder is mounted to the attachment; and - a locking mechanism for locking the tool holder and the attachment to each other when the tool holder is mounted to the attachment.
Dynamic aircraft headlight, comprising: an LED group, comprising a plurality of LEDs, and an optical system, comprising at least one optical element (8, 9), the optical system being associated with the LED group for shaping an output light intensity distribution from the light emitted by the LED group, wherein the LED group and the optical system are stationary within the dynamic aircraft headlight, with each LED of the LED group having a set position with respect to the optical system and with a light output of each LED being affected differently by the optical system, wherein each LED of the LED group is individually controllable, and wherein the dynamic aircraft headlight is configured to be operated in a plurality of operating modes, with a respective selected subset of the plurality of LEDs being switched on in each of the plurality of operating modes and with a different output light intensity distribution being emitted by the dynamic aircraft headlight in each of the plurality of operating modes, wherein the plurality of operating modes comprises a plurality of landing light modes, wherein the output light emission distribution of each of the plurality of landing light modes has a respective main light emission direction and wherein the plurality of landing light modes have different respective main light emission directions, wherein the dynamic aircraft headlight is configured to select one of the landing light modes based on an aircraft yaw angle and an aircraft pitch angle and a descent angle. an LED group, comprising a plurality of LEDs, and an optical system, comprising at least one optical element (8, 9), the optical system being associated with the LED group for shaping an output light intensity distribution from the light emitted by the LED group, wherein the LED group and the optical system are stationary within the dynamic aircraft headlight, with each LED of the LED group having a set position with respect to the optical system and with a light output of each LED being affected differently by the optical system, wherein each LED of the LED group is individually controllable, and wherein the dynamic aircraft headlight is configured to be operated in a plurality of operating modes, with a respective selected subset of the plurality of LEDs being switched on in each of the plurality of operating modes and with a different output light intensity distribution being emitted by the dynamic aircraft headlight in each of the plurality of operating modes, wherein the plurality of operating modes comprises a plurality of landing light modes, wherein the output light emission distribution of each of the plurality of landing light modes has a respective main light emission direction and wherein the plurality of landing light modes have different respective main light emission directions, wherein the dynamic aircraft headlight is configured to select one of the landing light modes based on an aircraft yaw angle and an aircraft pitch angle and a descent angle.