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    Modular aircraft system
    21.
    发明授权
    Modular aircraft system 有权
    模块化飞机系统

    公开(公告)号：US09505484B1

    公开(公告)日：2016-11-29

    申请号：US15096216

    申请日：2016-04-11

    Applicant: Nasser M. Al-Sabah

    Inventor： Nasser M. Al-Sabah

    IPC: B64C3/38 ,  B64C13/00 ,  B64C9/00 ,  B64C13/20 ,  B64C9/32 ,  B64D27/02 ,  B64C3/34 ,  B64D47/08 ,  B64D15/00 ,  B64C39/02 ,  B64D37/00 ,  B64D27/14 ,  B64D27/20

    CPC classification number: B64C3/38 ,  B64C1/26 ,  B64C3/34 ,  B64C5/06 ,  B64C9/00 ,  B64C9/326 ,  B64C13/00 ,  B64C13/20 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/048 ,  B64C2201/063 ,  B64C2201/104 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/16 ,  B64C2201/165 ,  B64C2211/00 ,  B64D15/00 ,  B64D27/02 ,  B64D27/14 ,  B64D27/20 ,  B64D37/00 ,  B64D39/00 ,  B64D47/08 ,  Y02T50/32

    Abstract: The modular aircraft system includes a single fuselage having a permanently installed empennage and plural sets of wing modules and engine modules, with each wing and engine module optimized for different flight conditions and missions. The fuselage and each of the modules are configured for rapid removal and installation of the modules to minimize downtime for the aircraft. Short wings having relatively low aspect ratio are provided for relatively high speed flight when great endurance and/or weight carrying capacity are not of great concern. Long wings having high aspect ratio are provided for longer range and endurance flights where speed is not absolutely vital. A medium span wing module is also provided. Turboprop, single turbojet, and dual turbojet engine modules are provided for installation depending upon mission requirements for any given flight. The aircraft is primarily adapted for use as an autonomously operated or remotely operated unmanned aerial vehicle.

    Abstract translation: 模块化飞机系统包括具有永久安装的尾翼和多组翼模块和发动机模块的单个机身，每个机翼和发动机模块针对不同的飞行条件和任务进行了优化。 机身和每个模块配置为快速拆卸和安装模块，以最大限度地减少飞机的停机时间。 在具有较高耐久性和/或重量承载能力的情况下，为相对高速飞行提供具有相对较低纵横比的短翼。 为长距离和耐力航班提供高长宽比的长翼，速度并不是绝对重要的。 还提供了中跨翼模块。 提供涡轮螺旋桨发动机，单涡轮喷气发动机和双涡轮喷气发动机模块用于安装，具体取决于任何给定航班的任务要求。 该飞机主要适用于自主操作或远程操作的无人驾驶飞行器。

    Micro Hybrid Generator System Drone
    22.
    发明申请
    Micro Hybrid Generator System Drone 有权
    微型混合发电机系统无人机

    公开(公告)号：US20160311544A1

    公开(公告)日：2016-10-27

    申请号：US15202771

    申请日：2016-07-06

    Applicant: Top Flight Technologies, Inc.

    Inventor： Long N. Phan ,  Sanjay Emani Sarma ,  Cody Miles Wojcik ,  Eli M. Davis ,  Benjamin Arthur Sena ,  Julian Lemus

    IPC: B64D27/24 ,  B64D33/08 ,  B64C27/00 ,  B64C39/02 ,  B64C27/08

    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: 一种包括至少一个转子电动机的无人驾驶飞行器。 转子电机由微型混合发电系统供电。 微型混合发电机系统包括被配置为向至少一个转子电动机提供电力的可再充电电池，被配置为产生机械功率的小型发动机，耦合到小型发动机的发电机电动机，并且被配置为使用由 小型发动机，桥式整流器，被配置为将由发电电动机产生的交流电力转换为直流电力，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一个或两者;以及电子控制单元， 所述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所述至少一个转子电动机。

    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS
    24.
    发明申请
    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
    长期航空运行的系统和方法

    公开(公告)号：WO2014088680A3

    公开(公告)日：2014-08-28

    申请号：PCT/US2013060978

    申请日：2013-09-20

    Applicant: HEPPE STEPHEN

    Inventor： HEPPE STEPHEN

    IPC: B64B1/06 ,  B64C37/02

    CPC classification number: B64C37/02 ,  B64B1/06 ,  B64C2201/022 ,  B64C2201/063

    Abstract: In one example, a long endurance airship system includes a payload airship (210) and a first logistics airship (260) mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.

    Abstract translation: 在一个示例中，长期耐力飞艇系统包括有效载人飞艇（210）和机械地连接到有效载客飞艇上的第一物流飞艇（260），以形成第一组合飞艇，有效载运飞艇和后勤飞艇具有不同于 关于发电能力，推进能力，耐力能力和提升能力中的至少一个，至少有两个因素，其中第一组合的飞艇是自由飞行的，比空气轻，并且被配置为保持更高的高度 超过30天，没有物理连接到地面。 还提供了长期耐力飞艇作业的说明性方法。

    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS
    25.
    发明申请
    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
    长期航空运行的系统和方法

    公开(公告)号：WO2012125639A1

    公开(公告)日：2012-09-20

    申请号：PCT/US2012/028931

    申请日：2012-03-13

    Applicant: HEPPE, Stephen

    Inventor： HEPPE, Stephen

    IPC: B64B1/06 ,  B64C37/02

    CPC classification number: B64B1/32 ,  B64B1/06 ,  B64C37/02 ,  B64C2201/022 ,  B64C2201/063

    Abstract: In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain stationkeeping for greater than 30 days. Illustrative methods for long endurance airship operations are also provided.

    Abstract translation: 在一个例子中，长期耐力飞艇系统包括有效载运飞艇和与有效载客飞艇机械连接以形成第一组合飞艇的第一物流飞艇，有效载客飞艇和具有至少两倍的设计能力的物流飞艇， 至少有以下至少一种：发电能力，推进能力，耐力能力和提升能力，其中第一组合飞艇自由飞行，轻于空中，并配置为维持停机时间超过30天。 还提供了长期耐力飞艇作业的说明性方法。

    SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLES
    26.
    发明申请
    SYSTEMS AND METHODS FOR UNMANNED AERIAL VEHICLES 审中-公开
    用于无人机的系统和方法

    公开(公告)号：WO2017147188A1

    公开(公告)日：2017-08-31

    申请号：PCT/US2017/018951

    申请日：2017-02-22

    Applicant: CULVER, Matthew

    Inventor： CULVER, Matthew

    IPC: B64D47/08 ,  B64F3/02

    CPC classification number: B64D47/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/063 ,  B64C2201/108 ,  B64C2201/127 ,  B64D1/16 ,  B64D39/00 ,  B64F3/02 ,  Y02T50/53

    Abstract: An unmanned aerial system (UAS) may comprise an unmanned aerial vehicle (UAV), a portable power source, and a tether connecting a UAV to a portable power source. The tether may transmit power from the portable power source to the UAV. The UAS may be controlled by a remote control, which may command the UAV to surveil a location and transmit images back to the controller. The UAV may further include one or more components attached to the UAV, such as a camera, surveillance equipment, a Taser®, a LED strobe light, laser, or a claw. A remote control may control the flight of the UAV as well as the functionality of the one or more components. The UAS may be configured to, for example, surveil a location, intercept an intruder, inspect a building, and/or perform crowd control.

    Abstract translation: 无人机系统（UAS）可以包括无人飞行器（UAV），便携式电源以及将UAV连接到便携式电源的系绳。 绳索可以将电力从便携式电源传输到无人飞行器。 UAS可以由遥控器控制，遥控器可以命令UAV监视位置并将图像传回控制器。 无人飞行器可以进一步包括附接到无人飞行器的一个或多个部件，诸如照相机，监视设备，Taser＆reg;，LED频闪灯，激光器或爪。 遥控器可以控制无人飞行器的飞行以及一个或多个部件的功能。 UAS可以被配置为例如监视位置，拦截入侵者，检查建筑物和/或执行人群控制。

    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS
    27.
    发明申请
    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
    长期航空运行的系统和方法

    公开(公告)号：WO2014088680A2

    公开(公告)日：2014-06-12

    申请号：PCT/US2013/060978

    申请日：2013-09-20

    Applicant: HEPPE, Stephen

    Inventor： HEPPE, Stephen

    IPC: B64B1/06

    CPC classification number: B64C37/02 ,  B64B1/06 ,  B64C2201/022 ,  B64C2201/063

    Abstract: In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.

    Abstract translation: 在一个例子中，长期耐力飞艇系统包括有效载运飞艇和与有效载客飞艇机械连接以形成第一组合飞艇的第一物流飞艇，有效载客飞艇和具有至少两倍的设计能力的物流飞艇， 至少有以下至少一个：发电能力，推进能力，耐力能力和升力能力，其中第一组合飞艇是自由飞行的，比空中轻，并且被配置为在没有物理连接的情况下保持高达30天以上 到地面。 还提供了长期耐力飞艇作业的说明性方法。

    MICRO HYBRID GENERATOR SYSTEM DRONE
    28.
    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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