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    PORTABLE LAUNCH SYSTEM
    1.
    发明申请
    PORTABLE LAUNCH SYSTEM 审中-公开

    公开(公告)号：WO2019079394A3

    公开(公告)日：2019-04-25

    申请号：PCT/US2018/056216

    申请日：2018-10-17

    Applicant: TOP FLIGHT TECHNOLOGIES, INC.

    Inventor： PHAN, Long N. ,  SARMA, Sanjay ,  DEBITETTO, Paul A.

    IPC: B64C39/02 ,  B64C27/00 ,  B64C27/08 ,  B64D1/02 ,  B64D1/12 ,  G05D1/10 ,  G06F7/00

    Abstract: An unmanned aerial vehicle includes a platform configured to transport a second unmanned aerial vehicle and release the second unmanned aerial vehicle in response to satisfying a condition. The unmanned aerial vehicle includes a hybrid generator system including an engine configured to generate mechanical power; and a generator motor coupled to the engine and configured to generate electrical power from the mechanical power generated by the engine; and at least one rotor motor configured to drive at least one propeller to rotate, wherein the at least one rotor motor is powered by the electrical power generated by the generator motor.

    COOLING A POWER SYSTEM FOR AN UNMANNED AERIAL VEHICLE
    2.
    发明申请
    COOLING A POWER SYSTEM FOR AN UNMANNED AERIAL VEHICLE 审中-公开

    公开(公告)号：WO2018165498A1

    公开(公告)日：2018-09-13

    申请号：PCT/US2018/021649

    申请日：2018-03-09

    Applicant: TOP FLIGHT TECHNOLOGIES, INC. ,  PHAN, Long N. ,  IMANI NEJAD, Mohammad ,  SWEETLAND, Matthew

    Inventor： PHAN, Long N. ,  IMANI NEJAD, Mohammad ,  SWEETLAND, Matthew

    IPC: B64D27/02 ,  B64D13/00 ,  B64D33/08

    Abstract: An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; and a micro hybrid generator system configured to provide power to the at least one rotor motor. The micro hybrid generator system includes a rechargeable battery configured to provide power to the at least one rotor motor; a small engine configured to generate mechanical power; and a generator motor coupled to the small engine and configured to generate electrical power from the mechanical power generated by the small engine. The unmanned aerial vehicle also includes a cooling system configured to couple to the micro hybrid generator system. The cooling system includes one or more plates; and a plurality of fins extending from each of the one or more plates. The cooling system is configured to dissipate heat from the micro hybrid generator system.

    NAVIGATION SYSTEM FOR A DRONE
    3.
    发明申请
    NAVIGATION SYSTEM FOR A DRONE 审中-公开

    公开(公告)号：WO2019010428A1

    公开(公告)日：2019-01-10

    申请号：PCT/US2018/041105

    申请日：2018-07-06

    Applicant: TOP FLIGHT TECHNOLOGIES, INC. ,  RASMUSSEN, Scott ,  SARMA, Sanjay

    Inventor： RASMUSSEN, Scott ,  SARMA, Sanjay ,  DEBITETTO, Paul, A. ,  PHAN, Long, N.

    IPC: G05D1/00 ,  G05D3/00

    Abstract: This document describes an unmanned aerial vehicle (UAV) configured to navigate an unmanned aerial vehicle highway. The UAV includes a navigation system that includes a sensor, configured to gather environmental data, and a computing system configured to navigate the UAV. The computing system compares the environmental data to a specified data signature in the one or more spectra and determines a position of the unmanned aerial vehicle in the unmanned aerial vehicle highway. The UAV includes a hybrid generator system including an engine configured to generate mechanical energy and a generator motor coupled to the engine and configured to generate electrical energy from the mechanical energy generated by the engine. The UAV includes a rotor motor configured to drive a propeller to rotate. The navigation system is powered by the electrical energy generated by the generator motor.

    DATA CENTER POWERED BY A HYBRID GENERATOR SYSTEM
    4.
    发明申请
    DATA CENTER POWERED BY A HYBRID GENERATOR SYSTEM 审中-公开
    数据中心由混合发电机系统供电

    公开(公告)号：WO2017197325A1

    公开(公告)日：2017-11-16

    申请号：PCT/US2017/032506

    申请日：2017-05-12

    Applicant: TOP FLIGHT TECHNOLOGIES, INC. ,  DEBITETTO, Paul A.

    Inventor： DEBITETTO, Paul A. ,  PHAN, Long N. ,  NAYFEH, Samir ,  POLO, John J. ,  DAVIS, Eli M.

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

    Abstract: An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate. The unmanned aerial vehicle includes a data center including a processor; a data storage component; and a wireless communications component. The unmanned aerial vehicle includes a hybrid generator system configured to provide power to the at least one rotor motor and to the data center, the hybrid generator system including a rechargeable battery configured to provide power to the at least one rotor motor; an engine configured to generate mechanical power; and a generator motor coupled to the engine and configured to generate electrical power from the mechanical power generated by the engine. The data center may include an intelligent data management module configured to control power distribution and execution of mission tasks in response to available power generation and mission task priorities.

    Abstract translation: 无人驾驶飞行器包括至少一个转子马达，该马达构造成驱动至少一个螺旋桨旋转。 无人机包括包含处理器的数据中心; 数据存储组件; 和无线通信组件。 无人驾驶飞行器包括混合动力发电机系统，该混合动力发电机系统构造成向至少一个转子电动机和数据中心提供动力，混合动力发电机系统包括可充电电池，该可充电电池构造成向至少一个转子电动机提供动力; 配置成产生机械动力的发动机; 以及发电机电动机，所述发电机电动机联接到所述发动机并且构造成从由所述发动机产生的机械动力产生电力。 数据中心可以包括智能数据管理模块，其被配置为响应于可用的发电和任务任务优先级来控制任务任务的电力分配和执行。

    PORTABLE LAUNCH SYSTEM
    7.
    发明申请
    PORTABLE LAUNCH SYSTEM 审中-公开

    公开(公告)号：WO2019079394A2

    公开(公告)日：2019-04-25

    申请号：PCT/US2018/056216

    申请日：2018-10-17

    Applicant: TOP FLIGHT TECHNOLOGIES, INC.

    Inventor： PHAN, Long N. ,  SARMA, Sanjay ,  DEBITETTO, Paul A.

    IPC: B64C39/02 ,  B64D5/00

    Abstract: An unmanned aerial vehicle includes a platform configured to transport a second unmanned aerial vehicle and release the second unmanned aerial vehicle in response to satisfying a condition. The unmanned aerial vehicle includes a hybrid generator system including an engine configured to generate mechanical power; and a generator motor coupled to the engine and configured to generate electrical power from the mechanical power generated by the engine; and at least one rotor motor configured to drive at least one propeller to rotate, wherein the at least one rotor motor is powered by the electrical power generated by the generator motor.

    PASSENGER CARRYING UNMANNED AERIAL VEHICLE POWERED BY A HYBRID GENERATOR SYSTEM
    9.
    发明申请
    PASSENGER CARRYING UNMANNED AERIAL VEHICLE POWERED BY A HYBRID GENERATOR SYSTEM 审中-公开
    搭载混合动力发动机系统的无人驾驶空中客车

    公开(公告)号：WO2017197316A1

    公开(公告)日：2017-11-16

    申请号：PCT/US2017/032493

    申请日：2017-05-12

    Applicant: TOP FLIGHT TECHNOLOGIES, INC.

    Inventor： PHAN, Long N. ,  NAYFEH, Samir ,  DAVIS, Eli M.

    IPC: B64C39/02 ,  B64C27/00 ,  B64C27/16 ,  B64C27/32 ,  B64C29/00 ,  B64C29/02

    Abstract: An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate; a passenger compartment sized to contain a human or animal passenger; and a hybrid generator system configured to provide power to the at least one rotor motor and to generate lift sufficient to carry the human or animal passenger. The hybrid generator system includes a rechargeable battery configured to provide power to the at least one rotor motor; an engine configured to generate mechanical power; and a generator motor coupled to the engine and configured to generate electrical power from the mechanical power generated by the engine.

    Abstract translation: 无人飞行器包括至少一个转子马达，该马达构造成驱动至少一个螺旋桨旋转; 一个大小足以容纳人或动物乘客的乘客舱; 以及混合动力发电机系统，其被配置为向所述至少一个转子电动机提供动力并产生足以承载人或动物乘客的升力。 混合动力发电机系统包括可充电电池，该可充电电池构造成向至少一个转子电动机提供动力; 配置成产生机械动力的发动机; 以及发电机电动机，该发电机电动机联接到发动机并且被配置为从发动机产生的机械动力产生电力。

    MICRO HYBRID GENERATOR SYSTEM DRONE
    10.
    发明申请
    MICRO HYBRID GENERATOR SYSTEM DRONE 审中-公开
    微型混合发电机系统无人机

    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。

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