mhurhangee/ep-ind-claims huggingface dataset:
A control device for an AC rotating machine for an electrical power steering, for controlling the AC rotating machine including a plurality of sets of windings, the control device comprising: a plurality of inverters (21, 22) each including, in respective phases, high-potential switching elements (UP1, VP1, WP1, UP2, VP2, WP2) and low-potential switching elements (UN1, VN1, WN1, UN2, VN2, WN2) for controlling voltages to be applied to respective phases of the plurality of sets of windings; a current control portion for issuing voltage commands corresponding to the voltages to the respective plurality of inverters to control currents flowing through the plurality of sets of windings; and a failure detection portion for detecting at least one of a short-circuit failure or an open-circuit failure in each of the high-potential and low-potential switching elements, wherein the current control portion is arranged to set, in accordance with the at least one of the short-circuit failure or the open-circuit failure detected by the failure detection portion, the corresponding high-potential or low-potential switching elements of the respective phases of a faulty-side inverter into the same ON or OFF state as the detected faulty high-potential or low-potential switching element, and continue the control on a normal-side inverter except for the faulty-side inverter. a plurality of inverters (21, 22) each including, in respective phases, high-potential switching elements (UP1, VP1, WP1, UP2, VP2, WP2) and low-potential switching elements (UN1, VN1, WN1, UN2, VN2, WN2) for controlling voltages to be applied to respective phases of the plurality of sets of windings; a current control portion for issuing voltage commands corresponding to the voltages to the respective plurality of inverters to control currents flowing through the plurality of sets of windings; and a failure detection portion for detecting at least one of a short-circuit failure or an open-circuit failure in each of the high-potential and low-potential switching elements, wherein the current control portion is arranged to set, in accordance with the at least one of the short-circuit failure or the open-circuit failure detected by the failure detection portion, the corresponding high-potential or low-potential switching elements of the respective phases of a faulty-side inverter into the same ON or OFF state as the detected faulty high-potential or low-potential switching element, and continue the control on a normal-side inverter except for the faulty-side inverter.
A Monitoring and Diagnostics System, comprising: a monitoring unit, a monitored unit comprising a wind turbine, and communication means between said monitoring unit and said monitored unit, wherein said Monitoring and Diagnostics System is configured such that: said monitored unit comprises data acquisition means for providing fault data of said monitored unit, said communication means is adapted to communicate the fault data from said monitored unit to said monitoring unit, and said monitoring unit comprises a reasoning engine comprising a diagnostics knowledge for analyzing the information contained in the fault data and being adapted to deduce diagnostics information from said diagnostics knowledge and from said information; wherein said Monitoring and Diagnostics System is operable to automatically reset the wind turbine in response to said deduced diagnostics information. said monitored unit comprises data acquisition means for providing fault data of said monitored unit, said communication means is adapted to communicate the fault data from said monitored unit to said monitoring unit, and said monitoring unit comprises a reasoning engine comprising a diagnostics knowledge for analyzing the information contained in the fault data and being adapted to deduce diagnostics information from said diagnostics knowledge and from said information; wherein said Monitoring and Diagnostics System is operable to automatically reset the wind turbine in response to said deduced diagnostics information.
A composition comprising an endothelial growth factor inhibitor that inhibits stimulation of VEGFR-3 by VEGF-C or VEGF-D for use in inducing tolerance or inhibiting rejection of a cell, tissue or organ transplant or inhibiting arteriosclerosis in a mammalian transplant recipient, wherein the inhibitor is selected from: (i) an antibody substance that immunoreacts with VEGFR-3; (ii) a soluble VEGFR-3 polypeptide that binds VEGF-C or VEGF-D, the soluble VEGFR-3 polypeptide comprising the VEGFR-3 extracellular domain or a fragment thereof sufficient to bind VEGF-C or VEGF-D; (iii) an antisense nucleic acid or an interfering RNA nucleic acid that inhibits expression of VEGFR-3; (iv) a polypeptide comprising an amino acid sequence at least 95% identical to amino acids 138-226, 47-224, 47-314 or 24-775 of SEQ ID NO: 6; and (v) a nucleic acid that encodes a polypeptide of (ii) or (iv). (i) an antibody substance that immunoreacts with VEGFR-3; (ii) a soluble VEGFR-3 polypeptide that binds VEGF-C or VEGF-D, the soluble VEGFR-3 polypeptide comprising the VEGFR-3 extracellular domain or a fragment thereof sufficient to bind VEGF-C or VEGF-D; (iii) an antisense nucleic acid or an interfering RNA nucleic acid that inhibits expression of VEGFR-3; (iv) a polypeptide comprising an amino acid sequence at least 95% identical to amino acids 138-226, 47-224, 47-314 or 24-775 of SEQ ID NO: 6; and (v) a nucleic acid that encodes a polypeptide of (ii) or (iv).
A method of securing an operator to a component of an aircraft, the component including a forward attachment point, and an aft attachment point, the method comprising: connecting a first adapter to the forward attachment point of the component of the aircraft, the first adapter including a first body including: a plurality of holes, the plurality of holes configured to correspond to holes in the forward attachment point of the component of the aircraft to allow for fastening the first adapter to the forward attachment point; a first ring connected to the first body; and a first fastening component comprising a plurality of bolts configured to be received in the holes; connecting a second adapter to the aft attachment point of the component of the aircraft, the second adapter including a second body, a second ring connected to the second body, and a second fastening component that connects the second body to the aft attachment point, the second fastening component including a plurality of legs defining a slot between the legs, each leg of the plurality of legs having a hole for receiving a pin therethrough, the pin arranged to extend through the plurality of legs and through the aft attachment point, wherein the first fastening component has a different physical structure from the second fastening component; and connecting a lanyard to each of the adapters and connecting each lanyard to a harness worn by the operator. connecting a first adapter to the forward attachment point of the component of the aircraft, the first adapter including a first body including: a plurality of holes, the plurality of holes configured to correspond to holes in the forward attachment point of the component of the aircraft to allow for fastening the first adapter to the forward attachment point; a first ring connected to the first body; and a first fastening component comprising a plurality of bolts configured to be received in the holes; connecting a second adapter to the aft attachment point of the component of the aircraft, the second adapter including a second body, a second ring connected to the second body, and a second fastening component that connects the second body to the aft attachment point, the second fastening component including a plurality of legs defining a slot between the legs, each leg of the plurality of legs having a hole for receiving a pin therethrough, the pin arranged to extend through the plurality of legs and through the aft attachment point, wherein the first fastening component has a different physical structure from the second fastening component; and connecting a lanyard to each of the adapters and connecting each lanyard to a harness worn by the operator.
A static electric induction apparatus comprising: - a winding including a plurality of winding units, - a plurality of first spacer elements (5; 5a-d) extending radially between respective winding units and arranged above each other, wherein each of the first spacer elements has a first groove (18; 18a-d) defined in the surface thereof and an outer end facing outwardly from the winding, wherein the first groove (18; 18a-d) enters and exits the first spacer element at the outer end thereof, - a sensor system for monitoring the temperature in the apparatus, wherein the sensor system comprises an elongated and flexible temperature sensing element disposed in the first grooves, each of the first grooves (18; 18a-d) has a curved part and the flexible temperature sensing element is wound at least one revolution in each of said curved parts, - an elongated second spacer element extending in an axial direction on the outside of the winding, the second spacer element comprises an elongated second groove arranged in communication with the first grooves (18; 18a-d) to allow the flexible temperature sensing element to run between the second groove and the first grooves, and the flexible temperature sensing element is disposed in the first grooves (18; 18a-d) of the first spacer elements and in the second groove of the second spacer element. - a winding including a plurality of winding units, - a plurality of first spacer elements (5; 5a-d) extending radially between respective winding units and arranged above each other, wherein each of the first spacer elements has a first groove (18; 18a-d) defined in the surface thereof and an outer end facing outwardly from the winding, wherein the first groove (18; 18a-d) enters and exits the first spacer element at the outer end thereof, - a sensor system for monitoring the temperature in the apparatus, wherein the sensor system comprises an elongated and flexible temperature sensing element disposed in the first grooves, each of the first grooves (18; 18a-d) has a curved part and the flexible temperature sensing element is wound at least one revolution in each of said curved parts, - an elongated second spacer element extending in an axial direction on the outside of the winding, the second spacer element comprises an elongated second groove arranged in communication with the first grooves (18; 18a-d) to allow the flexible temperature sensing element to run between the second groove and the first grooves, and the flexible temperature sensing element is disposed in the first grooves (18; 18a-d) of the first spacer elements and in the second groove of the second spacer element.
An optical measuring device, comprising: a plurality of microfluidic channels (11; 12; 13; 14; 15) extending in parallel to each other; and scanning means configured to scan a plurality of measuring light beams (21; 22; 23) in a scanning direction in which said microfluidic channels are juxtaposed to optically measure fine particles introduced into said microfluidic channels, wherein said microfluidic channels are arranged in a predetermined spaced relationship from each other in the scanning direction and the scanning means is configured so that the measuring light beams are irradiated and scanned in such a manner as to be spaced from each other at distances in the scanning direction, and characterized in that each of the distances between said microfluidic channels in the scanning direction is divided into a plurality of zones of a predetermined dimension in the scanning direction, each of the measuring light beams is irradiated in one of the zones and one of the zones in which one of the measuring light beams is irradiated and another one of the zones in which another one of the measuring light beams is irradiated are different from each other and are not continuous to each other, wherein said scanning means is configured to scan the measuring light beams such that, when one of the measuring light beams is irradiated upon one of said microfluidic channels, the other measuring light beams are not irradiated upon any one of said microfluidic channels. a plurality of microfluidic channels (11; 12; 13; 14; 15) extending in parallel to each other; and scanning means configured to scan a plurality of measuring light beams (21; 22; 23) in a scanning direction in which said microfluidic channels are juxtaposed to optically measure fine particles introduced into said microfluidic channels, wherein said microfluidic channels are arranged in a predetermined spaced relationship from each other in the scanning direction and the scanning means is configured so that the measuring light beams are irradiated and scanned in such a manner as to be spaced from each other at distances in the scanning direction, and characterized in that each of the distances between said microfluidic channels in the scanning direction is divided into a plurality of zones of a predetermined dimension in the scanning direction, each of the measuring light beams is irradiated in one of the zones and one of the zones in which one of the measuring light beams is irradiated and another one of the zones in which another one of the measuring light beams is irradiated are different from each other and are not continuous to each other, wherein said scanning means is configured to scan the measuring light beams such that, when one of the measuring light beams is irradiated upon one of said microfluidic channels, the other measuring light beams are not irradiated upon any one of said microfluidic channels.
A method for preparing a 2',3'-dideoxyguanosine support structure, the method comprising: (a) reacting 2',3'-dideoxyguanosine with N,N-dimethylformamide dimethylacetal, to obtain a first intermediate; (b) reacting the first intermediate with 4,4-dimethoxytriphenylmethyl chloride, to obtain a second intermediate comprising a dimethylformamide protecting group; (c) cleaving the dimethylformamide protecting group off the second intermediate, to obtain a third intermediate; and (d) reacting the third intermediate with adipic anhydride to obtain a precursor of the 2',3'-dideoxyguanosine support structure, and (e) coupling the precursor to a suitable solid support, thereby obtaining the 2',3'-dideoxyguanosine support structure. (a) reacting 2',3'-dideoxyguanosine with N,N-dimethylformamide dimethylacetal, to obtain a first intermediate; (b) reacting the first intermediate with 4,4-dimethoxytriphenylmethyl chloride, to obtain a second intermediate comprising a dimethylformamide protecting group; (c) cleaving the dimethylformamide protecting group off the second intermediate, to obtain a third intermediate; and (d) reacting the third intermediate with adipic anhydride to obtain a precursor of the 2',3'-dideoxyguanosine support structure, and (e) coupling the precursor to a suitable solid support, thereby obtaining the 2',3'-dideoxyguanosine support structure.
Method for providing control data for an application vehicle when selectively applying pesticides, comprising the following steps: providing location data of sub-areas (13, 14) of a field to which at least one first pesticide has been applied in a first application; determining transition areas associated with the sub-areas (13, 14) to which the at least one first pesticide has been applied and the adjacent areas to which the at least one first pesticide has not been applied, based on the provided sub-area location data; providing control data for controlling an application vehicle for applying at least one second pesticide to the determined transition areas in a second application. providing location data of sub-areas (13, 14) of a field to which at least one first pesticide has been applied in a first application; determining transition areas associated with the sub-areas (13, 14) to which the at least one first pesticide has been applied and the adjacent areas to which the at least one first pesticide has not been applied, based on the provided sub-area location data; providing control data for controlling an application vehicle for applying at least one second pesticide to the determined transition areas in a second application.
Method for operating a wind power installation having a rotor and having a generator driven via the rotor for generating an electrical power, having the steps of: - determining an environmental variable relevant to the wind power installation and comprising at least an air density relevant to the wind power installation, - determining a rotational speed of the rotor, - specifying an electrical power to be output by the generator, - adjusting the wind power installation for generating the power to be output according to operational management which indicates a relationship between the rotational speed of the rotor and the electrical power to be output, wherein - the operational management is adapted on the basis of the air density relevant to the wind power installation, characterized in that - an adapted rotational speed of the rotor of the wind power installation for generating an electrical power to be output is specified using the adapted operational management and therefore using the air density relevant to the wind power installation, wherein, for generating an optimized electrical power to be output, the adapted rotational speed is an increased rotational speed for a reduced air density, wherein additionally - a sound emission of the wind power installation is determined for the adapted rotational speed of the rotor using the air density relevant to the wind power installation, and - the adapted rotational speed is corrected on the basis of the determined sound emission using the air density relevant to the wind power installation. - determining an environmental variable relevant to the wind power installation and comprising at least an air density relevant to the wind power installation, - determining a rotational speed of the rotor, - specifying an electrical power to be output by the generator, - adjusting the wind power installation for generating the power to be output according to operational management which indicates a relationship between the rotational speed of the rotor and the electrical power to be output, wherein - the operational management is adapted on the basis of the air density relevant to the wind power installation, characterized in that - an adapted rotational speed of the rotor of the wind power installation for generating an electrical power to be output is specified using the adapted operational management and therefore using the air density relevant to the wind power installation, wherein, for generating an optimized electrical power to be output, the adapted rotational speed is an increased rotational speed for a reduced air density, wherein additionally - a sound emission of the wind power installation is determined for the adapted rotational speed of the rotor using the air density relevant to the wind power installation, and - the adapted rotational speed is corrected on the basis of the determined sound emission using the air density relevant to the wind power installation.
A rail vehicle, a tram in particular, which comprises supporting car units provided with bogies, and at least one supported bogieless car unit being supported between two supporting car units by means of lower supports between the car units (2, 3), the lower supports comprising a pivot system to allow turning between the car units (2, 3) in all directions; and being supported by at least one upper support between the supported car unit and the supporting car unit, the upper support guiding a vertical position of the supported car unit with respect to the supporting car unit, characterized in that for passengers to get on and off at stops the upper support comprises an inclination device for deviating at least one supported car unit from a vertical angle of the supporting car unit, wherein the upper support comprises a reaction bar which is substantially transverse to a longitudinal direction of the cars (2, 3) and on which the inclination device is arranged for elongating or shortening the reaction bar and thus for causing inclination of the supported car unit. supported between two supporting car units by means of lower supports between the car units (2, 3), the lower supports comprising a pivot system to allow turning between the car units (2, 3) in all directions; and being supported by at least one upper support between the supported car unit and the supporting car unit, the upper support guiding a vertical position of the supported car unit with respect to the supporting car unit, characterized in that for passengers to get on and off at stops the upper support comprises an inclination device for deviating at least one supported car unit from a vertical angle of the supporting car unit, wherein the upper support comprises a reaction bar which is substantially transverse to a longitudinal direction of the cars (2, 3) and on which the inclination device is arranged for elongating or shortening the reaction bar and thus for causing inclination of the supported car unit.
A twine tensioner arrangement for a baler comprises a pair of rollers (4,6), each of the rollers (4,6) being rotatable about a shaft (8,10) and having circumferential lobes (14,16), characterised by at least one of the shafts being mounted on a displaceable armature, and the arrangement further comprising a displacement measurement apparatus to measure the displacement of the displaceable armature and a signalling apparatus to generate a signal if the displacement of the displaceable armature exceeds a predetermined value.