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公开(公告)号：US20240300659A1
公开(公告)日：2024-09-12
申请号：US18663960
申请日：2024-05-14
Applicant: Archer Aviation, Inc.
Inventor： Alan TEPE , Stephen SPITERI , Wei WU , Diederik MARIUS
IPC: B64D27/24 , B60L15/06 , B60L15/38 , B64C27/54 , B64C29/00 , B64D33/08 , B64D35/02 , F16B2/06 , F16H57/08 , H02K1/27 , H02K1/32 , H02K5/124 , H02K5/20 , H02K7/00 , H02K7/08 , H02K7/116 , H02K9/19 , H02K11/33 , H02K15/03 , H02M7/5395 , H02P21/00 , H02P25/16 , H02P27/06 , H02P27/08
CPC classification number: B64D27/24 , B60L15/06 , B60L15/38 , B64C27/54 , B64C29/0008 , B64C29/0033 , B64D33/08 , B64D35/02 , F16B2/06 , F16H57/08 , H02K1/27 , H02K1/32 , H02K5/124 , H02K5/203 , H02K7/08 , H02K7/116 , H02K9/19 , H02K11/33 , H02K15/03 , H02M7/5395 , H02P21/50 , H02P25/16 , H02P27/06 , H02P27/08 , B60L2200/10 , B60L2210/40 , H02K7/006
Abstract: An electrical propulsion system includes an electrical motor configured to drive one or more propellers of the aircraft, a capacitor configured to stabilize a direct current (DC) bus voltage, a first inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to alternate current (AC) voltages to drive a first set of stator windings of the electrical motor, in response to a first pulse width modulation (PWM) vector, and a second inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to AC voltages to drive a second set of stator windings of the electrical motor, in response to a second PWM vector. The first PWM vector and the second PWM vector are substantially equal and opposite vectors.
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Patent Agency Ranking
公开(公告)号：US20240120869A1
公开(公告)日：2024-04-11
申请号：US18363535
申请日：2023-08-01
Applicant: Archer Aviation, Inc.
Inventor： Alan TEPE , Stephen SPITERI , Wei WU , Diederik MARIUS
CPC classification number: H02P27/08 , B60L15/06 , B60L15/38 , B64D27/24 , H02M7/5395 , H02P21/50 , B60L2200/10 , B60L2210/40
Abstract: An electrical propulsion system includes an electrical motor configured to drive one or more propellers of the aircraft, a capacitor configured to stabilize a direct current (DC) bus voltage, a first inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to alternate current (AC) voltages to drive a first set of stator windings of the electrical motor, in response to a first pulse width modulation (PWM) vector, and a second inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to AC voltages to drive a second set of stator windings of the electrical motor, in response to a second PWM vector. The first PWM vector and the second PWM vector are substantially equal and opposite vectors.
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公开(公告)号：US20250038689A1
公开(公告)日：2025-01-30
申请号：US18911555
申请日：2024-10-10
Applicant: Archer Aviation Inc.
Inventor： Scott GRAVES , Alan BALDWIN , Stephen Michael SPITERI , Wei WU , Alan D. TEPE
Abstract: “An electrical propulsion system comprises an inverter, an electrical motor assembly, an assembly, and a rotor position sensor. The inverter comprises a printed circuit board assembly (PCBA). The electrical motor assembly comprises a stator and a rotor. The assembly is configured to rotate a propeller and comprises a moving component and a stationary component. The rotor position sensor comprises at least one sensor coupled to the PCBA, and a magnet located on the moving component. The at least one sensor is configured to detect a magnetic field of the magnet through the stationary component.”
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公开(公告)号：US20240351694A1
公开(公告)日：2024-10-24
申请号：US18761099
申请日：2024-07-01
Applicant: Archer Aviation Inc.
Inventor： Scott GRAVES , Alan BALDWIN , Stephen Michael SPITERI , Wei WU , Alan D. TEPE
CPC classification number: B64D27/24 , B64C29/0033 , H02P25/16 , H02P27/06
Abstract: An electrical propulsion system for a vertical take-off and landing (VTOL) aircraft comprises an electrical motor assembly and an inverter assembly. The inverter assembly comprises a housing, a capacitor assembly, at least one printed circuit board assembly (PCBA), and a plurality of positioning pins. The capacitor assembly comprises a center hole, at least one capacitor, a capacitor housing having at least one busbar, and a plurality of through holes in the capacitor housing. The capacitor assembly and the at least one PCBA are positioned inside the housing. The plurality of positioning pins pass through the through the plurality of through holes of the capacitor housing and the at least one PCBA and are connected to the housing.
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公开(公告)号：US20240116641A1
公开(公告)日：2024-04-11
申请号：US18306275
申请日：2023-04-25
Applicant: Archer Aviation Inc.
Inventor： Alan D. TEPE , Stephen Michael SPITERI , Scott GRAVES , Alan BALDWIN , Wei WU , Robert Wayne MOORE , Michael ZWIERS , Diederik MARIUS
CPC classification number: B64D27/24 , B64C29/0033 , H02M7/003
Abstract: An electrical propulsion system for a vertical take-off and landing (VTOL) aircraft comprises an electrical motor assembly and an inverter assembly. The inverter assembly comprises a housing, a capacitor assembly, at least one printed circuit board assembly (PCBA), and a plurality of positioning pins. The capacitor assembly comprises a center hole, at least one capacitor, a capacitor housing having at least one busbar, and a plurality of through holes in the capacitor housing. The capacitor assembly and the at least one PCBA are positioned inside the housing. The plurality of positioning pins pass through the through the plurality of through holes of the capacitor housing and the at least one PCBA and are connected to the housing.
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公开(公告)号：US20250153853A1
公开(公告)日：2025-05-15
申请号：US18664029
申请日：2024-05-14
Applicant: Archer Aviation, Inc.
Inventor： Alan TEPE , Stephen SPITERI , Wei WU , Diederik MARIUS
IPC: B64D27/24 , B60L15/06 , B60L15/38 , B64C27/54 , B64C29/00 , B64D27/30 , B64D33/08 , B64D35/02 , F16B2/06 , F16H57/08 , H02K1/27 , H02K1/32 , H02K5/124 , H02K5/20 , H02K7/00 , H02K7/08 , H02K7/116 , H02K9/19 , H02K11/33 , H02K15/03 , H02M7/5395 , H02P21/00 , H02P25/16 , H02P27/06 , H02P27/08
Abstract: An electrical propulsion system includes an electrical motor configured to drive one or more propellers of the aircraft, a capacitor configured to stabilize a direct current (DC) bus voltage, a first inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to alternate current (AC) voltages to drive a first set of stator windings of the electrical motor, in response to a first pulse width modulation (PWM) vector, and a second inverter circuit coupled to the capacitor and configured to convert the DC bus voltage to AC voltages to drive a second set of stator windings of the electrical motor, in response to a second PWM vector. The first PWM vector and the second PWM vector are substantially equal and opposite vectors.
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