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公开(公告)号：US20240343403A1
公开(公告)日：2024-10-17
申请号：US18386074
申请日：2023-11-01
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Hyun Ki Cho , Jin Soo Jang , Yoon Cheol Jeon , Jong Pil Kim
IPC: B64D31/00
CPC classification number: B64D31/00 , B64D2221/00
Abstract: The present disclosure relates to a flight system and a failure responding method therefor. A flight system includes: a plurality of fuse boxes configured to control application of a voltage to at least one propulsion device; and an interlock control apparatus configured to control interlock lines between fuse boxes connected using the interlock lines among the fuse boxes to synchronize and control opening of the fuse boxes connected using the interlock lines.
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公开(公告)号：US20240343118A1
公开(公告)日：2024-10-17
申请号：US18386059
申请日：2023-11-01
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Hyun Ki Cho , Jin Soo Jang , Yoon Cheol Jeon , Jong Pil Kim
CPC classification number: B60L3/0046 , B60L58/18 , G01R31/1263 , G01R31/14
Abstract: A system for a vehicle may include a first battery pack diagnosis apparatus connected to a first battery pack, a second battery pack diagnosis apparatus connected to a second battery pack, a third battery pack diagnosis apparatus connected to a third battery pack, and a fourth battery pack diagnosis apparatus connected to a fourth battery pack. The first battery pack diagnosis apparatus may be configured to determine, based on a measured value of an integrated insulation resistance of an inverter terminal associated with the vehicle, whether a battery, of the first battery pack, the second battery pack, the third battery pack, or the fourth battery pack, is in a failure state, and based on a determination that the battery is in the failure state and based on individually measured insulation resistance of the first-fourth battery packs, determine a failure position of the battery.
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公开(公告)号：US20240157808A1
公开(公告)日：2024-05-16
申请号：US18385549
申请日：2023-10-31
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Jong Pil Kim , Woo Young Lee , Hee Kwang Lee , Jung Hyun Lee , Sae Kwon Chang , Mi Jin Kim
CPC classification number: B60L15/007 , B60L3/12 , B60L50/75 , B60L58/40 , B60L2200/10 , B60L2220/42
Abstract: A power supply system for an aircraft and a control method thereof are provided. The power supply system of the aircraft includes a fuel cell configured to generate electrical energy, a converter device configured to supply a voltage generated by the fuel cell to a first motor device for driving the aircraft through a first output terminal and switch a connection with the fuel cell depending on a predetermined driving mode, a battery configured to supply the voltage to a second motor device for driving the aircraft through a second output terminal, the second output terminal being connected with an output node of the fuel cell, and a processor configure to control a connection between the fuel cell and the converter device depending on the driving mode.
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公开(公告)号：US20240359805A1
公开(公告)日：2024-10-31
申请号：US18380850
申请日：2023-10-17
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Yoon Cheol Jeon , Jin Soo Jang , Jong Pil Kim , Hyun Ki Cho
CPC classification number: B64D31/00 , B60L50/60 , B60L53/00 , B60L58/10 , H01M10/4264 , H01M10/441 , B60L2200/10 , B60L2210/10 , B64D2221/00 , H01M2220/20
Abstract: A power control device is provided for an aircraft. The power control device may include at least one first battery, a second battery having a lower power density and higher energy density than the at least one first battery, at least one lift motor connected, via a first electrical path, to the at least one first battery, a cruise motor connected, via a second electrical path, to the second battery, and a power control circuit configured to control the at least one first battery, the second battery, the at least one lift motor, and the cruise motor.
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公开(公告)号：US20240177615A1
公开(公告)日：2024-05-30
申请号：US18133682
申请日：2023-04-12
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Hyun Ki Cho , Jin Soo Jang , Yoon Cheol Jeon , Jong Pil Kim
CPC classification number: G08G5/003 , B64U10/20 , B64U50/32 , G08G5/0013 , B64U2101/60
Abstract: The present disclosure relates to a flight control apparatus, a system including the same, and a method thereof. An example embodiment of the present disclosure provides a flight control apparatus, including: at least one processor, and memory storing instructions that, when executed by the at least one processor, cause the flight control apparatus to determine, based on environmental information and based on variations of a parameter for each operation mode of an aerial vehicle, a flight path among at least one candidate path associated with a destination for the aerial vehicle.
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Patent Agency Ranking
公开(公告)号：US20240336150A1
公开(公告)日：2024-10-10
申请号：US18532539
申请日：2023-12-07
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Jong Pil Kim , Hyun Ki Cho , Yoon Cheol Jeon , Ji Han Lee
IPC: B60L50/75 , B60L3/00 , B60L58/40 , B64D27/355 , B64D27/357 , H01M16/00 , H02J4/00 , H02J7/00 , H02P5/74
CPC classification number: B60L50/75 , B60L3/0046 , B60L58/40 , B64D27/355 , B64D27/357 , H01M16/006 , H02J4/00 , H02J7/0063 , H02P5/74 , B60L2200/10 , B64D2041/005 , B64D2221/00 , H01M2220/20 , H01M2250/20 , H01M2250/402 , H02J2207/20 , H02J2300/30
Abstract: A power supply system of an aircraft includes a fuel cell that generates electrical energy, a converter device including a mode switch device that supplies power to a first motor device through a first output terminal and switches a connection between an output node of the fuel cell and the first output terminal, a first battery device that supplies a voltage from a first battery to a second motor device through a second output terminal and connects the second output terminal with the first output terminal under control of the mode switch device, and a processor that controls the mode switch device to enter an emergency mode when detecting an error in the converter device or the first battery device and connects the first output terminal with the second output terminal.
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公开(公告)号：US20240326977A1
公开(公告)日：2024-10-03
申请号：US18228988
申请日：2023-08-01
Applicant: Hyundai Motor Company , Kia Corporation
Inventor： Yoon Cheol Jeon , Jin Soo Jang , Jong Pil Kim , Hyun Ki Cho
IPC: B64C3/18
Abstract: A wing frame includes a front wing beam extending in a left-right direction; a rear wing beam extending in the left-right direction and spaced rearward from the front wing beam, and a plurality of rib parts, each of which includes a middle rib coupled to a rear side of the front wing beam and a front side of the rear wing beam.
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公开(公告)号：US11257617B2
公开(公告)日：2022-02-22
申请号：US16212498
申请日：2018-12-06
Applicant: HYUNDAI MOTOR COMPANY , KIA MOTORS CORPORATION
Inventor： Woo Young Lee , Sang Chan Jeong , Ju Man Yoon , Jong Pil Kim
Abstract: A converter for a vehicle including an inductor which includes at least one coil, a core including a first region having an annular planar shape, around which the at least one coil is wound, and a second region having at least one first through-hole, a case accommodating the at least one coil and the core and including at least one cooling rod inserted into the at least one first through-hole, and a fixing bolt fastened to the at least one cooling rod exposed through the at least one first through-hole to fix the core to the case.
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9.发明申请公开(公告)号：US20190283615A1
公开(公告)日：2019-09-19
申请号：US16299556
申请日：2019-03-12
Applicant: Hyundai Motor Company , Kia Motors Corporation , Research & Business Foundation Sungkyunkwan University
Inventor： Woo Young Lee , Jae Eun Cha , Gyu Yeong Choe , Jong Pil Kim , Min Jung Kim , Jong Eun Byun , Min Kook Kim , Sang Joon Ann , Byoung Kuk Lee
Abstract: A wireless power reception apparatus including a bridgeless rectifier in a wireless power transfer (WPT) system for an electric vehicle (EV) may include: a bridgeless rectifier configured to rectify power transferred from a reception coil and to supply a direct current to a battery mounted in the EV; and a controller configured to control operation of the bridgeless rectifier. The bridgeless rectifier may include at least one switch and at least one diode connected to the at least one switch.
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公开(公告)号：US09409489B2
公开(公告)日：2016-08-09
申请号：US13930646
申请日：2013-06-28
Applicant: Hyundai Motor Company
Inventor： Woo Young Lee , Byeong Seob Song , Dae Woo Lee , Jin Young Yang , Jong Pil Kim
CPC classification number: B60L11/182 , B60L3/0023 , B60L11/14 , B60L11/1805 , B60L11/1812 , B60L11/1829 , B60L11/1831 , B60L11/1881 , B60L2200/10 , B60L2200/18 , B60L2200/32 , B60L2200/36 , B60L2210/22 , B60L2210/30 , B60L2230/14 , H01F38/14 , H02J7/025 , H02J50/00 , H02J50/10 , H02J50/12 , H04B5/0037 , H04B5/0075 , H04B5/0093 , Y02T10/70 , Y02T10/7077 , Y02T10/7088 , Y02T10/7241 , Y02T10/725 , Y02T90/122 , Y02T90/127 , Y02T90/14 , Y02T90/34
Abstract: A magnetic connector apparatus that charges an electric vehicle through contactless magnetic coupling. The magnetic connector apparatus includes an external charger, an inlet, and a magnetic connector. The inlet is connected to a rechargeable battery of the vehicle. The magnetic connector is connected to a power source of the external charger and is transferred to the vehicle to be inserted into the inlet.
Abstract translation: 一种通过非接触式磁耦合对电动车辆充电的磁连接器装置。 磁性连接器装置包括外部充电器，入口和磁性连接器。 入口连接到车辆的可充电电池。 磁性连接器连接到外部充电器的电源，并被传送到车辆以插入入口。
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