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公开(公告)号：US12269586B2
公开(公告)日：2025-04-08
申请号：US17252502
申请日：2019-06-14
Applicant: The Texas A&M University System
Inventor： Moble Benedict , David Coleman , Atanu Halder , Bochan Lee , Andrew Riha , Farid Saemi , Carl Runco , Vishaal Subramanian , Eric Greenwood , Vinod Lakshminarayan
IPC: B64C27/68 , B60L15/20 , B60L50/60 , B64C27/10 , B64C27/467 , B64C27/605 , B64D17/80 , B64D27/24 , B64D31/00
Abstract: A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spaced blades, a first actuation assembly including a first plurality of electronically controlled actuators coupled to a first swashplate and configured to control the movement of the first swashplate relative to the body, and a control system coupled to the body and configured to control the first plurality of actuators, wherein the control system includes a cable extending through a passage formed in the tubular strut and in signal communication with the first plurality of actuators.
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公开(公告)号：US20230327533A1
公开(公告)日：2023-10-12
申请号：US18130775
申请日：2023-04-04
Inventor： Hamid A. Toliyat , Bryton Praslicka , Shrikesh Sheshaprasad , Farid Saemi , Matthew C. Gardner , Matthew C. Johnson
IPC: H02K49/10
CPC classification number: H02K49/102
Abstract: In some aspects, a magnetic gear system includes a flux focusing magnet arrangement having a low-pole count rotor, a pair of modulator rotors disposed on either side of the low-pole count rotor, and a pair of high-pole count outer rotors disposed outside of the pair of modulator rotors. In some aspects, a magnetic gear system includes a motor with a stator and a pair of low-pole count rotors disposed on either side of the stator. The magnetic gear system further includes a pair of modulator rotors disposed on either side of the motor, and a pair of high-pole outer rotors disposed on opposite sides of the pair of modulator rotors.
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公开(公告)号：US20210253232A1
公开(公告)日：2021-08-19
申请号：US17252502
申请日：2019-06-14
Applicant: The Texas A&M University System
Inventor： Moble Benedict , David Coleman , Atanu Halder , Bochan Lee , Andrew Riha , Farid Saemi , Carl Runco , Vishaal Subramanian , Eric Greenwood , Vinod Lakshminarayan
IPC: B64C27/68 , B64C27/605 , B64D27/24 , B64D17/80 , B64C27/467 , B60L50/60 , B60L15/20 , B64D31/00
Abstract: A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spaced blades, a first actuation assembly including a first plurality of electronically controlled actuators coupled to a first swashplate and configured to control the movement of the first swashplate relative to the body, and a control system coupled to the body and configured to control the first plurality of actuators, wherein the control system includes a cable extending through a passage formed in the tubular strut and in signal communication with the first plurality of actuators.
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