公开(公告)号：AU2019201540A1

公开(公告)日：2019-03-28

申请号：AU2019201540

申请日：2019-03-06

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64D27/24

Abstract: Abstract 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. WO 2015/138217 PCT/US2015/019004 0 ~xM C~) C~) co Oo ro 2 C >n .E-0 -0 0 Ca 00J)I ITi o- U

公开(公告)号：AU2015229860A1

公开(公告)日：2016-09-29

申请号：AU2015229860

申请日：2015-03-05

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64D27/24

Abstract: 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.

公开(公告)号：AU2019201540B2

公开(公告)日：2021-03-18

申请号：AU2019201540

申请日：2019-03-06

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64D27/24

Abstract: Abstract 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. WO 2015/138217 PCT/US2015/019004 0 ~xM C~) C~) co Oo ro 2 C >n .E-0 -0 0 Ca 00J)I ITi o- U

公开(公告)号：AU2015229860B2

公开(公告)日：2018-12-06

申请号：AU2015229860

申请日：2015-03-05

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64D27/24

Abstract: 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.

公开(公告)号：AU2023203515B2

公开(公告)日：2025-01-30

申请号：AU2023203515

申请日：2023-06-06

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64C27/26 ,  B64C29/00 ,  B64D27/24 ,  B64U10/13 ,  B64U10/25 ,  B64U50/11 ,  B64U50/19

Abstract: Abstract 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. WO 2015/138217 PCT/US2015/019004 0 ~xM C~) C~) co Oo ro 2 C >n .E-0 -0 0 Ca 00J)I ITi o- U

公开(公告)号：AU2021203788A1

公开(公告)日：2021-07-08

申请号：AU2021203788

申请日：2021-06-09

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64D27/24

Abstract: WO 2015/138217 PCT/US2015/019004 0 ~xM C~) C~) co Oo ro 2 C >n .E-0 -0 0 Ca 00J)I ITi o- U Abstract 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.

公开(公告)号：EP3116781A4

公开(公告)日：2017-12-20

申请号：EP15762275

申请日：2015-03-05

Applicant: ENDURANT SYSTEMS LLC

Inventor： MCADOO GREGORY LEONARD

IPC: B64C39/02 ,  B64C27/08 ,  B64D27/04 ,  B64D27/24

CPC classification number: 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

Abstract: 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.