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公开(公告)号:US20180118374A1
公开(公告)日:2018-05-03
申请号:US15663238
申请日:2017-07-28
Applicant: STABILIS INC.
Inventor: Manuel Lombardini , Joseph Koehler , Rashad Moarref
CPC classification number: B64F3/02 , B60L9/00 , B60L2200/10 , B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/148 , B64C2201/201
Abstract: An unmanned aerial vehicle system includes a ground station including a case, a power supply housed in the case, and a tether having a first end and a second end opposite to the first end. The first end of the tether is coupled to the case. The unmanned aerial vehicle system also includes a module including smart battery authentication circuitry configured to be coupled to the second end of the tether. The module is configured to be connected to an unmanned aerial vehicle. The smart battery authentication circuitry enables the unmanned aerial vehicle to receive power from the power supply housed in the case when the module is connected to the unmanned aerial vehicle.
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公开(公告)号:US10710746B2
公开(公告)日:2020-07-14
申请号:US15663238
申请日:2017-07-28
Applicant: STABILIS INC.
Inventor: Manuel Lombardini , Joseph Koehler , Rashad Moarref
Abstract: An unmanned aerial vehicle system includes a ground station including a case, a power supply housed in the case, and a tether having a first end and a second end opposite to the first end. The first end of the tether is coupled to the case. The unmanned aerial vehicle system also includes a module including smart battery authentication circuitry configured to be coupled to the second end of the tether. The module is configured to be connected to an unmanned aerial vehicle. The smart battery authentication circuitry enables the unmanned aerial vehicle to receive power from the power supply housed in the case when the module is connected to the unmanned aerial vehicle.
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公开(公告)号:US20160327073A1
公开(公告)日:2016-11-10
申请号:US14706823
申请日:2015-05-07
Applicant: STABILIS INC.
Inventor: Faisal Amlani , Manuel Lombardini , Jonathan Miller
IPC: F15D1/00
CPC classification number: F15D1/007 , B63H9/02 , B64C23/02 , B64C23/08 , F03D7/0232 , F05B2240/30 , Y02T70/58
Abstract: A dynamically controllable force-generating device configured to be incorporated into a vehicle, such as an aircraft or a ship, or an energy-harvesting device, such as a wind turbine, is disclosed. The dynamically controllable force-generating device includes a force-generating motive surface, a motor operatively coupled to the force-generating motive surface to move at least a portion of the force-generating motive surface to generate a force, at least one controlling motive surface spaced apart from the force-generating motive surface, and a motor operatively coupled to the at least one controlling motive surface to move at least a portion of the controlling motive surface to change at least one of a direction and a magnitude of the force generated by the force-generating motive surface.
Abstract translation: 公开了一种动态可控的力产生装置,其被配置成结合到诸如飞行器或船舶的车辆中,或诸如风力涡轮机的能量收集装置。 动态可控的力产生装置包括产生力的动力表面,可操作地联接到力产生动力表面的马达,以移动至少一部分力产生动力表面以产生力,至少一个控制动力面 与力产生动力表面间隔开,以及电动机,其可操作地联接到所述至少一个控制动力表面以移动所述控制动力表面的至少一部分,以改变由所述至少一个控制动力表面产生的力的方向和大小的至少一个, 力产生动力面。
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