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公开(公告)号：US20220097846A1
公开(公告)日：2022-03-31
申请号：US17465365
申请日：2021-09-02
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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公开(公告)号：US11661191B2
公开(公告)日：2023-05-30
申请号：US17465365
申请日：2021-09-02
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18 , B64D27/02 , B64D27/04
CPC分类号： B64C39/024 , B64C27/08 , B64C27/26 , B64C29/0033 , B64C39/04 , B64D27/24 , B64D45/00 , H02J7/14 , H02J7/34 , H02K7/1815 , B64C2201/021 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/141 , B64D27/04 , B64D2027/026 , B64D2045/0085 , B64D2221/00 , Y02T50/60
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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3.发明申请公开(公告)号：US20190375502A1
公开(公告)日：2019-12-12
申请号：US16432753
申请日：2019-06-05
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed, A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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公开(公告)号：US12049311B2
公开(公告)日：2024-07-30
申请号：US18134798
申请日：2023-04-14
IPC分类号： B64C39/02 , B64C27/08 , B64C27/26 , B64C29/00 , B64C39/04 , B64D27/24 , B64D45/00 , H02J7/14 , H02J7/34 , H02K7/18 , B64D27/02 , B64D27/04 , B64U10/13 , B64U10/25 , B64U50/11 , B64U50/19
CPC分类号： B64C39/024 , B64C27/08 , B64C27/26 , B64C29/0033 , B64C39/04 , B64D27/24 , B64D45/00 , H02J7/14 , H02J7/34 , H02K7/1815 , B64D27/026 , B64D27/04 , B64D2045/0085 , B64D2221/00 , B64U10/13 , B64U10/25 , B64U50/11 , B64U50/19 , B64U2201/10 , Y02T50/60
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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5.发明申请公开(公告)号：US20200001996A1
公开(公告)日：2020-01-02
申请号：US16559420
申请日：2019-09-03
IPC分类号： B64C39/02 , B64D27/24 , B64D45/00 , H02K7/18 , H02J7/34 , B64C27/26 , B64C27/08 , H02J7/14 , B64C39/04 , B64C29/00
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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6.发明公开公开(公告)号：US20230294829A1
公开(公告)日：2023-09-21
申请号：US18134798
申请日：2023-04-14
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18
CPC分类号： B64C39/024 , B64C27/08 , B64C27/26 , B64C29/0033 , B64C39/04 , B64D27/24 , B64D45/00 , H02J7/14 , H02J7/34 , H02K7/1815 , B64D2027/026
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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公开(公告)号：US11142315B2
公开(公告)日：2021-10-12
申请号：US16559420
申请日：2019-09-03
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18 , B64D27/02 , B64D27/04
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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公开(公告)号：US10676191B2
公开(公告)日：2020-06-09
申请号：US16432753
申请日：2019-06-05
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18 , B64D27/02 , B64D27/04
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed, A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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公开(公告)号：US10351238B2
公开(公告)日：2019-07-16
申请号：US15261780
申请日：2016-09-09
IPC分类号： B64C39/02 , B64C27/08 , B64D27/24 , B64C27/26 , B64C29/00 , B64C39/04 , H02J7/14 , H02J7/34 , B64D45/00 , H02K7/18 , B64D27/02 , B64D27/04
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
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10.发明申请UAV CONFIGURATIONS AND BATTERY AUGMENTATION FOR UAV INTERNAL COMBUSTION ENGINES, AND ASSOCIATED SYSTEMS AND METHODS 审中-公开无人机配置和无人机内燃机的电池补充及相关系统和方法公开(公告)号：US20170066531A1
公开(公告)日：2017-03-09
申请号：US15261780
申请日：2016-09-09
CPC分类号： B64C39/024 , B64C27/08 , B64C27/26 , B64C29/0033 , B64C39/04 , B64C2201/021 , B64C2201/027 , B64C2201/042 , B64C2201/044 , B64C2201/141 , B64D27/04 , B64D27/24 , B64D45/00 , B64D2027/026 , B64D2045/0085 , B64D2221/00 , H02J7/14 , H02J7/34 , H02K7/1815 , Y02T50/64
摘要： UAV configurations and battery augmentation for UAV internal combustion engines, and associated systems and methods are disclosed. A representative configuration includes a fuselage, first and second wings coupled to and pivotable relative to the fuselage, and a plurality of lift rotors carried by the fuselage. A representative battery augmentation arrangement includes a DC-powered motor, an electronic speed controller, and a genset subsystem coupled to the electronic speed controller. The genset subsystem can include a battery set, an alternator, and a motor-gen controller having a phase control circuit configurable to rectify multiphase AC output from the alternator to produce rectified DC feed to the DC-powered motor. The motor-gen controller is configurable to draw DC power from the battery set to produce the rectified DC feed.
摘要翻译： 公开了UAV内燃机的UAV配置和电池增加以及相关的系统和方法。 代表性的配置包括机身，相对于机身联接并可枢转的第一和第二翼，以及由机身承载的多个提升转子。 代表性的电池增加装置包括直流动力马达，电子速度控制器和耦合到电子速度控制器的发电机组子系统。 发电机组子系统可以包括电池组，交流发电机和电动机控制器，其具有相位控制电路，该相位控制电路可配置为整流来自交流发电机的多相交流输出，以产生经直流供电的电动机的整流直流馈电。 电机控制器可配置为从电池组中抽取直流电源，以产生整流的直流电源。
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