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公开(公告)号：EP4123905A3
公开(公告)日：2023-05-03
申请号：EP22179989.3
申请日：2022-06-20
发明人： HOEKSTRA, Eric
IPC分类号： H03K17/95
摘要： A proximity sensor (200) comprises a reference inductor (L21), a first set of sensor inductors (L22, L23, L24), a first set of comparators (U22, U23, U24), each comparator of the first set of comparators corresponding to one of the sensor inductors of the first set of sensor inductors, and an alternative current voltage source (V21) to output a sinusoidal voltage to the reference inductor and each of the sensor inductors. Each comparator of the first set of comparators (U22, U23, U24) receives a voltage across the reference inductor (L21) as a reference voltage and each comparator of the first set of comparators (U22, U23, U24) receives a voltage across a corresponding sensor inductor (L22, L23, L24) as an input voltage.
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公开(公告)号：EP4152297A1
公开(公告)日：2023-03-22
申请号：EP22195478.7
申请日：2022-09-13
发明人： MENON, Anup
IPC分类号： G08G5/00
摘要： A method may comprise receiving (300) airspace surveillance data from a plurality of sensors, the airspace surveillance data comprising tracks associated with one or more targets, aggregating (302) the airspace surveillance data to obtain aggregated data, performing (304) density-based clustering of the aggregated data to obtain a plurality of clusters, determining (306) one or more candidate associations between the tracks and the clusters, associating (308) each of the tracks with one of the one or more targets based on the candidate associations, and estimating (310) a track for each of the one or more targets based on the associations between the tracks and the one or more targets.
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公开(公告)号：EP4123905A2
公开(公告)日：2023-01-25
申请号：EP22179989.3
申请日：2022-06-20
发明人： HOEKSTRA, Eric
IPC分类号： H03K17/95
摘要： A proximity sensor (200) comprises a reference inductor (L21), a first set of sensor inductors (L22, L23, L24), a first set of comparators (U22, U23, U24), each comparator of the first set of comparators corresponding to one of the sensor inductors of the first set of sensor inductors, and an alternative current voltage source (V21) to output a sinusoidal voltage to the reference inductor and each of the sensor inductors. Each comparator of the first set of comparators (U22, U23, U24) receives a voltage across the reference inductor (L21) as a reference voltage and each comparator of the first set of comparators (U22, U23, U24) receives a voltage across a corresponding sensor inductor (L22, L23, L24) as an input voltage.
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公开(公告)号：EP4102483A1
公开(公告)日：2022-12-14
申请号：EP22178019.0
申请日：2022-06-09
IPC分类号： G08G5/00
摘要： A method to validate a flight plan (70) for an aircraft includes receiving aviation data (56), determining a flight plan (70) based on the aviation data (56), determining a set of flight parameters (71) for the flight plan (70), receiving terrain data (55), and performing a safety validation of the flight plan (70), wherein the safety validation comprises comparing the set of flight parameters (71) with the terrain data (55), and determining, based on the comparison, whether the flight plan (70)satisfies predetermined flight criteria (72), and in the event of a determination that the flight plan (70) does not satisfy the predetermined flight criteria (72), displaying a first notification (60) indicative of the determination.
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公开(公告)号：EP4009171A1
公开(公告)日：2022-06-08
申请号：EP21203834.3
申请日：2021-10-20
发明人： HOOKER, Brent
摘要： A system and method for compiling and dynamically reconfiguring the management of functionalities (34) carried among a set of multiple common compute nodes (32a-c). During the inoperation of one node (32) of the set of multiple common compute nodes (32a-c), higher-criticality functionalities (34a) can be reassigned to other common nodes (32a-c) to ensure maintained operation of the higher-criticality functionalities (34a).
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公开(公告)号：EP3961339A3
公开(公告)日：2022-05-11
申请号：EP21192483.2
申请日：2021-08-20
IPC分类号： G05B23/02
摘要： A method of performing fault isolation for an aircraft comprises identifying a fault that occurs during a flight of the aircraft; identifying a first set of parameters associated with the aircraft based on the identification of the fault; automatically determining values of the first set of parameters to obtain a first set of measured values; determining whether the first set of measured values are within acceptable ranges; and identifying a source of the fault based on the determination of whether the first set of measured values are within the acceptable ranges.
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公开(公告)号：EP3930163A1
公开(公告)日：2021-12-29
申请号：EP21180172.5
申请日：2021-06-17
发明人： WANG, Ruxi , ZHANG, Zheyu
摘要： An interleaved DC-DC boost converter (291) is disclosed. The DC-DC converter (291) includes a filter portion (292) comprising first set of inductors (221) at a low voltage input (211) of the DC-DC power converter (291), a DC-DC converter portion (200) having a first and a second set of switches (251, 252) coupled to the filter portion (292), and a DC-link portion (293) coupled to the DC-DC converter portion (200), comprising a first and a second set of capacitors (231, 232). The DC-DC boost converter (291) further includes a coupled inductor portion (220) coupled to the DC-link portion (293) at a high voltage output (212) of said power converter (291), comprising a second set of coupled inductors (222, 223), each coupled inductor (222a, 222b) of the second set of coupled inductors (222) electrically in series with a respective inductor (221a, 221b)of the first set of inductors (221).
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公开(公告)号：EP3930113A1
公开(公告)日：2021-12-29
申请号：EP21178643.9
申请日：2021-06-09
发明人： MAUPIN, Brian Matthew , MEARS, John
摘要： A crimp pin (128) electrical connector (40) comprising a shell (100) defining an interior (102) with a first opening (44) and a second opening (46), a flange (48) circumscribing the shell (100), an insert located within the interior (102) and extending through the first opening (44). The insert comprising at least one crimp pin (128) including a crimp (140) and a pin (138) provided within at least one passage (122) included within the interior (102) of the shell (100).
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公开(公告)号：EP3926804A1
公开(公告)日：2021-12-22
申请号：EP21176359.4
申请日：2021-05-27
发明人： LI, Cong , SCHUTTEN, Michael , PAN, Di , XIE, Ren
摘要： A common-mode voltage cancellation (CMVC) circuit (117), is disclosed. The circuit includes a first set of coupled inductors (555), each having a primary winding (511) defining a first polarity, and a secondary winding (512, 522, 532). The secondary windings (512, 522, 532) are electrically coupled in series. Each primary winding (511) receives a phase voltage (VA1, VB1, VC1) having a common mode voltage (Vcm) component from a respective input line (110). The circuit (117) includes a second set of coupled inductors (620) comprising at least one primary winding (621) and at least one secondary winding (612, 622, 632). The at least one primary winding (621) receives a second voltage (VA2, VB2, VC2) from the series connected secondary windings (512, 522, 532) of the first set of coupled inductors (555). Each at least one secondary winding (612, 622, 632) is coupled in series with a respective input line (110) such that the common mode voltage component (Vcm) received on the input lines (110) will be reduced at an output of the set of secondary windings (612, 622, 632).
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公开(公告)号：EP3920403A1
公开(公告)日：2021-12-08
申请号：EP21173788.7
申请日：2021-05-13
IPC分类号： H02P1/16 , H02P1/46 , H02P1/56 , H02P6/20 , H02P9/30 , H02P21/18 , H02P21/34 , B64D27/00 , H01L29/00 , H02P6/16 , H02P6/18
摘要： An aircraft starting and generating system includes a starter/generator (100) and an inverter/converter/controller (200) that is connected to the starter/generator (100) and that generates AC power to drive the starter/generator (100) in a start mode for starting a prime mover of the aircraft, and that converts AC power, obtained from the starter/generator (100) after the prime mover have been started, to DC power in a generate mode of the starter/generator (100). A four leg inverter (550) is coupled with the DC power output (452) and has an Inverter/converter/controller (ICC) (200) with a four leg MOSFET-based bridge (580) configuration that drives the starter/generator (100) in a start mode for starting a prime mover of the aircraft, and converts DC power to AC power in a generate mode of the starter/generator (100). A four leg bridge gate driver is configured to drive the four leg MOSFET-based bridge (580) using pulse width modulation (PWM) during start and generate mode.
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