公开(公告)号：WO2017087399A1

公开(公告)日：2017-05-26

申请号：PCT/US2016/062060

申请日：2016-11-15

Applicant: TOP FLIGHT TECHNOLOGIES, INC.

Inventor： PHAN, Long N. ,  SARMA, Sanjay Emani ,  WOJCIK, Cody Miles ,  DAVIS, Eli M. ,  SENA, Benjamin Arthur ,  LEMUS, Julian

IPC: B64C39/02 ,  B64D27/24

CPC classification number: B64C39/024 ,  B64C27/001 ,  B64C27/08 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/063 ,  B64C2201/066 ,  B64C2201/108 ,  B64D1/08 ,  B64D1/22 ,  B64D27/02 ,  B64D27/24 ,  B64D33/08 ,  B64D2027/026 ,  B64D2221/00 ,  B64F3/02 ,  G05D1/101 ,  Y02T50/44 ,  Y02T50/64

Abstract: An unmanned aerial vehicle comprising at least one rotor motor. The rotor motor is powered by a micro hybrid generation system. The micro hybrid generator system comprises a rechargeable battery configured to provide power to the at least one rotor motor, a small engine configured to generate mechanical power, a generator motor coupled to the small engine and configured to generate AC power using the mechanical power generated by the small engine, a bridge rectifier configured to convert the AC power generated by the generator motor to DC power and provide the DC power to either or both the rechargeable battery and the at least one rotor motor, and an electronic control unit configured to control a throttle of the small engine based, at least in part, on a power demand of at least one load, the at least one load including the at least one rotor motor.

Abstract translation: 包括至少一个转子电动机的无人驾驶飞行器。 转子电机由微混合发电系统供电。 微混合发电机系统包括：可充电电池，被配置为向至少一个转子电动机提供电力;小型发动机，配置成产生机械动力;发电机电动机，连接到小型发动机并配置为使用由 小型发动机，被配置为将发电机马达产生的AC电力转换成DC电力并将DC电力提供给可再充电电池和至少一个转子电动机中的任一者或两者的桥式整流器，以及电子控制单元， 小型发动机的节气门至少部分地基于至少一个负载的功率需求，所述至少一个负载包括至少一个转子电动机。