-
公开(公告)号:US12006053B2
公开(公告)日:2024-06-11
申请号:US17317066
申请日:2021-05-11
Applicant: HYUNDAI MOTOR COMPANY , KIA CORPORATION
Inventor: Hee Kwang Lee , Hyun Seok Hong , Woo Suk Jung , Keun Seok Lee , Hyun Woo Jun
CPC classification number: B64D31/06 , B60L50/61 , B60L58/12 , B64D27/02 , B64D27/24 , B64D41/00 , B60L2200/10 , B64D27/026
Abstract: A hybrid air mobility vehicle can make a long-distance flight through an efficient operation of an engine and a battery, and can reduce discomfort by reducing noise according to flight surroundings. The hybrid air mobility vehicle includes: an engine and a generator; a battery and a drive motor electrically connected to the generator; a first propeller connected to the drive motor and a second propeller connected to the generator through a clutch; and a controller that controls driving of the engine, the clutch, and the drive motor, based on a flight factor including at least one of a flight mode, a required power, a battery charging amount, or a surrounding flight environment of the hybrid air mobility vehicle.
-
公开(公告)号:US20220194566A1
公开(公告)日:2022-06-23
申请号:US17378444
申请日:2021-07-16
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Hee Kwang LEE , Hyun Seok Hong , Hyun Ki Cho
Abstract: A noise reduction system for air mobility, may include a plurality of propeller modules provided on the air mobility and each including an inverter, a motor electrically connected to the inverter, and a propeller mounted to the motor; and a control unit configured to perform PWM control of power to be provided to the inverters to reduce noise attributable to carrier frequencies generated by the plurality of inverters or reduce noise attributable to fundamental frequencies generated by the plurality of motors.
-
公开(公告)号:US20240128810A1
公开(公告)日:2024-04-18
申请号:US18122115
申请日:2023-03-15
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Hyun Seok Hong , Hyun Woo Jun , Hee Kwang Lee
CPC classification number: H02K1/182 , H02K1/148 , H02K2203/12
Abstract: Disclosed are an easily manufacturable stator for an axial flux motor, and a method of manufacturing the same. A stator includes a core, a bobbin having a hollow portion into which the core is inserted, and a winding wound around the bobbin. A radial outer corner portion of the core is formed to have a cross-sectional shape bent at least twice.
-
公开(公告)号:US11664652B2
公开(公告)日:2023-05-30
申请号:US17389585
申请日:2021-07-30
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Yoon Cheol Jeon , Hyun Woo Jun , Hee Kwang Lee , Hyun Ki Cho , Gwi Taek Kim , Hyun Seok Hong , Woo Suk Jung
CPC classification number: H02H3/20 , B60L3/0046 , B60L50/60 , B64D27/24 , H01H39/00 , H01H85/04 , H02H1/0007 , B60L2200/10
Abstract: An emergency power management system of a mobility, may include a fuse device connected to a battery and including a first circuit and a second circuit in which a first fuse and a second fuse are respectively provided and are connected in parallel, a pyro switch provided between the first circuit and the second circuit, and configured to establish electric connection with the first circuit in ordinary times and to release electric connection with the first circuit and to establish electric connection with the second circuit in a case of emergency, a determiner configured to determine abnormality of the first fuse based on current applied from the high-voltage battery or voltages at opposite end portions of the first fuse, and a controller configured to operate the pyro switch when abnormality occurs in the first fuse.
-
公开(公告)号:US20220123675A1
公开(公告)日:2022-04-21
申请号:US17411921
申请日:2021-08-25
Applicant: Hyundai Motor Company , Kia Corporation , POSTECH Research and Business Development Foundation
Inventor: Hee Kwang Lee , Hyun Seok Hong , Kwang Hee Nam , Tae Yeon Lee
Abstract: A method for determining a motor angle, may include deriving a sensor weight and a sensorless weight via a cross product of an actual current vector and a model-based sensored current vector and a cross product of the actual current vector and a model-based sensorless current vector; and determining a final motor angle by applying the sensor weight and the sensorless weight to each of a sensored angle and a sensorless angle.
-
公开(公告)号:US11942615B2
公开(公告)日:2024-03-26
申请号:US17379215
申请日:2021-07-19
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Hyun Woo Jun , Woo Suk Jung , Hee Kwang Lee , Hyun Seok Hong
IPC: H01M10/655 , H01M10/613 , H01M10/643 , H01M10/653 , H01M50/213 , H01M50/249
CPC classification number: H01M10/655 , H01M10/613 , H01M10/643 , H01M10/653 , H01M50/213 , H01M50/249 , H01M2220/20
Abstract: An air-cooled battery cooling system for an air mobility vehicle may ensure the cooling performance for batteries using air flows during the flight of the air mobility vehicle, since the cooling of the batteries is performed using an air flow in the top-bottom direction due to the hovering of the air mobility vehicle and an air flow in the front and rear direction due to the cruising of the air mobility vehicle, the efficient cooling performance for the batteries is ensured in a variety of flight modes. Furthermore, the batteries are securely fixed while being cooled by air flows via the heat transfer pads within the battery packs.
-
公开(公告)号:US11705769B2
公开(公告)日:2023-07-18
申请号:US17382929
申请日:2021-07-22
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Hyun Woo Jun , Woo Suk Jung , Hyun Seok Hong , Hee Kwang Lee
Abstract: A magnetic gear may include a stator, having a stator core having a plurality of teeth extending toward a rotation shaft and a plurality of coils wound around the plurality of teeth, a rotor, having a rotor core disposed inside the stator and fixed to the rotation shaft and a plurality of permanent magnets attached to the external surface of the rotor core, and a pole-piece unit, having a plurality of first pole pieces and a plurality of second pole pieces arranged radially about the rotation shaft between the stator core and the rotor core such that the plurality of first pole pieces and the plurality of second pole pieces are alternately arranged in a circumferential direction thereof.
-
公开(公告)号:US11591082B2
公开(公告)日:2023-02-28
申请号:US17307721
申请日:2021-05-04
Applicant: HYUNDAI MOTOR COMPANY , KIA CORPORATION
Inventor: Woo Suk Jung , Hee Kwang Lee , Hyun Seok Hong , Hyun Woo Jun
Abstract: An apparatus for generating thrust for air transport includes a main thrust device, and an auxiliary thrust device configured to generate auxiliary thrust so as to enable an aircraft to vertically take off and land. The apparatus further includes: wings fixed to left and right sides of a fuselage of the aircraft, rotors installed on the wings and configured to generate thrust. In particular, the main thrust device provides driving force to the rotors using motors and an engine, and the auxiliary thrust device is installed in the fuselage and has a center of gravity configured to coincide with a center of gravity of the aircraft.
-
公开(公告)号:US11581834B2
公开(公告)日:2023-02-14
申请号:US17411921
申请日:2021-08-25
Applicant: Hyundai Motor Company , Kia Corporation , POSTECH Research and Business Development Foundation
Inventor: Hee Kwang Lee , Hyun Seok Hong , Kwang Hee Nam , Tae Yeon Lee
Abstract: A method for determining a motor angle, may include deriving a sensor weight and a sensorless weight via a cross product of an actual current vector and a model-based sensored current vector and a cross product of the actual current vector and a model-based sensorless current vector; and determining a final motor angle by applying the sensor weight and the sensorless weight to each of a sensored angle and a sensorless angle.
-
公开(公告)号:US11939049B2
公开(公告)日:2024-03-26
申请号:US17947357
申请日:2022-09-19
Applicant: Hyundai Motor Company , Kia Corporation
Inventor: Woo Suk Jung , Hee Kwang Lee , Hyun Seok Hong , Hyun Woo Jun
IPC: B64D35/02 , B60L53/00 , B60L58/12 , B64C27/32 , B64C27/82 , B64C29/00 , B64D27/02 , B64D27/24 , B64D31/00 , B64D31/10 , B64D31/12 , B64D33/02
CPC classification number: B64C27/82 , B60L53/00 , B60L58/12 , B64C27/32 , B64C29/0025 , B64D27/02 , B64D27/24 , B64D31/00 , B64D31/10 , B64D31/12 , B64D33/02 , B64D35/02 , B60L2200/10 , B64C2027/8227 , B64D27/026 , B64D2033/0213
Abstract: In an air mobility vehicle, an engine operates as required to provide mechanical driving force or electric energy. A battery is charged with the electric energy from the engine. Main rotors operate using the electric energy of the battery and electric power generated by the engine to perform takeoff, landing, and cruising. Auxiliary rotors are disposed at or adjacent to the center of gravity of a vehicle body and mechanically connected to the engine via a clutch. The auxiliary rotors perform the takeoff, the landing, or the cruising by receiving the mechanical driving force from the engine when the clutch is in an engaged position. A controller monitors the states of the battery and the main rotors and controls the operations of the engine and the clutch.
-
-
-
-
-
-
-
-
-