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    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS
    115.
    发明申请
    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开

    公开(公告)号：US20170297672A1

    公开(公告)日：2017-10-19

    申请号：US15297051

    申请日：2016-10-18

    Applicant: STRATOSPHERIC AIRSHIPS, LLC

    Inventor： Stephen B. Heppe

    IPC: B64B1/00 ,  B64C37/02

    CPC classification number: B64B1/00 ,  B64C37/02 ,  B64C2201/022 ,  B64C2201/06

    Abstract: In one example, a long endurance airship system includes a first combined airship with a payload airship and a first logistics airship. The first combined airship is configured for stationkeeping at a predetermined station during meteorological conditions with wind speeds below a predetermined threshold. The airship system also includes a second combined airship which is a reconfiguration of the first combined airship and includes the payload airship and a second logistics airship. The second combined airship is configured for stationkeeping at the predetermined station in all meteorological conditions, including meteorological conditions with wind speeds above the predetermined threshold.

    Aircraft hybrid fuel system
    116.
    发明授权
    Aircraft hybrid fuel system 有权

    公开(公告)号：US09688415B2

    公开(公告)日：2017-06-27

    申请号：US14963716

    申请日：2015-12-09

    Applicant: AAI Corporation

    Inventor： Brandon R. Hall

    IPC: B64D37/04 ,  B64D37/06 ,  B64D37/16 ,  B64C39/02

    CPC classification number: B64D37/04 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/06 ,  B64D37/06 ,  B64D37/16

    Abstract: An aircraft hybrid fuel system includes a main tank and a set of flexible bladders, the main tank and the set of flexible bladders defining a fuel containment space. The system further includes a set of pathways coupling the set of flexible bladders to the main tank. The set of pathways is constructed and arranged to vent gas out of the set of flexible bladders into the main tank while fuel from a fuel source is provided into the fuel containment space defined by the main tank and the set of flexible bladders. Along these lines, each flexible bladder can be provisioned with a fuel port to provide fuel, and a separate vent port to vent gas to the main tank.

    METHODS AND APPARATUS FOR A DISTRIBUTED AIRBORNE WIRELESS COMMUNICATIONS FLEET
    118.
    发明申请
    METHODS AND APPARATUS FOR A DISTRIBUTED AIRBORNE WIRELESS COMMUNICATIONS FLEET 有权
    分布式空中通信无线通信的方法和装置

    公开(公告)号：US20160046387A1

    公开(公告)日：2016-02-18

    申请号：US14462152

    申请日：2014-08-18

    Applicant: Sunlight Photonics Inc.

    Inventor： SERGEY V. FROLOV ,  MICHAEL CYRUS ,  ALLAN J. BRUCE ,  JOHN PETER MOUSSOURIS

    IPC: B64D47/00 ,  B64D35/02 ,  B64C19/00 ,  B64D31/00 ,  H04B7/185 ,  B64B1/00 ,  G08G5/00 ,  G05D1/10 ,  G08G5/04 ,  B64D33/00 ,  B64C39/02

    CPC classification number: B64D47/00 ,  B64B1/00 ,  B64C19/00 ,  B64C39/02 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/122 ,  B64C2201/143 ,  B64D31/00 ,  B64D33/00 ,  B64D35/02 ,  G05D1/104 ,  G08G5/0069 ,  H04B7/18508

    Abstract: Embodiments of methods and apparatus for providing distributed airborne wireless communications are provided herein. In some embodiments, a communication fleet includes: an airborne communication payload subdivided into multiple payload sections; and a plurality of airborne platforms each including a payload section, wherein each airborne platform comprises an airframe, a propulsion system, a power system, and flight control electronics, wherein the propulsion system is configured to provide propulsion power and thrust to maintain level flight, ascend, descend and maneuver the airborne platform, wherein the power system provides electrical power to the propulsion system, the flight control electronics, and the payload section, and wherein the flight control electronics provide capability to control a position, speed, and flight pattern of the airborne platform.

    Abstract translation: 本文提供了用于提供分布式机载无线通信的方法和装置的实施例。 在一些实施例中，通信车队包括：被分为多个有效载荷部分的机载通信有效载荷; 以及多个机载平台，每个机载平台各自包括有效载荷部分，其中每个机载平台包括机体，推进系统，电力系统和飞行控制电子设备，其中所述推进系统被配置为提供推进力和推力以维持水平飞行， 上升，下降和操纵机载平台，其中电力系统向推进系统，飞行控制电子装置和有效载荷部分提供电力，并且其中飞行控制电子装置提供控制位置，速度和飞行模式的能力 机载平台。

    POWER MANAGEMENT METHOD AND SYSTEM FOR AN UNMANNED AIR VEHICLE
    119.
    发明申请
    POWER MANAGEMENT METHOD AND SYSTEM FOR AN UNMANNED AIR VEHICLE 有权
    无人空中车辆的电力管理方法与系统

    公开(公告)号：US20150314869A1

    公开(公告)日：2015-11-05

    申请号：US14447090

    申请日：2014-07-30

    Applicant: The Boeing Company

    Inventor： Jose Luis Lemus Martin ,  Sergio Pereira Mayan ,  Eduardo Gabriel Ferreyra

    IPC: B64C39/02 ,  B64D31/14 ,  B64D41/00 ,  G05B13/02

    CPC classification number: B64C39/024 ,  B64C2201/06 ,  B64C2201/141 ,  B64D31/14 ,  B64D41/00 ,  B64D2041/005 ,  B64D2211/00 ,  B64D2221/00 ,  G05B13/0275 ,  G05D1/0005 ,  Y02T90/36

    Abstract: Power management method and system for an unmanned air vehicle, wherein the unmanned air vehicle comprises a plurality of power demanding subsystems and a plurality of power sources. The invention establishes mission oriented fixed parameters. A fuzzy logic power management unit, comprised in the system, automatically calculates and assigns priorities for delivering power to the subsystems. It also automatically calculates and assigns amounts of power delivered to each subsystem and automatically decides which of the power sources to deliver power to which subsystem. The fuzzy logic power management system calculates and assigns the priorities and loads in function of a plurality of internal variables, external variables and the mission oriented fixed parameters.

    Abstract translation: 一种用于无人驾驶飞行器的电力管理方法和系统，其中所述无人驾驶飞行器包括多个电力需求子系统和多个电源。 本发明建立了面向任务的固定参数。 包括在系统中的模糊逻辑电源管理单元自动计算和分配用于向子系统传送电力的优先级。 它还自动计算和分配交付给每个子系统的功率量，并自动决定哪个电源向哪个子系统发送电力。 模糊逻辑电源管理系统根据多个内部变量，外部变量和面向任务的固定参数来计算和分配优先级和负载。

    HAND-LAUNCHED, SOLAR-POWERED AIRCRAFT
    120.
    发明申请
    HAND-LAUNCHED, SOLAR-POWERED AIRCRAFT 审中-公开
    手动发射，太阳能飞机

    公开(公告)号：US20150298017A1

    公开(公告)日：2015-10-22

    申请号：US14256898

    申请日：2014-04-18

    Applicant: Toy Labs, Inc.

    Inventor： Timothy J. CURLEY ,  Gordon Paul BRADLEY

    IPC: A63H29/22 ,  A63H27/00

    CPC classification number: A63H29/22 ,  A63H27/001 ,  B64C2201/021 ,  B64C2201/06 ,  B64C2203/00 ,  B64D2211/00 ,  Y02T50/55

    Abstract: Embodiments of a hand-launched solar-powered aircraft are disclosed. In addition, embodiments of kits are disclosed for the construction of a hand-launched solar-powered aircraft. Further, embodiments of methods of making a hand-launched aircraft are disclosed. In some embodiments, the hand-launched aircraft is solar-powered. Still further, embodiments of an educational kit for a hand-launched, solar-powered aircraft are disclosed. In various embodiments, the educational kit comprises educational material on one or more science and technology learning topics, which educational material is relevant to and supplemented by the assembly and/or operation of the aircraft. The education material can relate to, for example, one or more of flying techniques, aeronautics, renewable energy, electronics, mechanical engineering, and/or climatology.

    Abstract translation: 公开了一种手动发射的太阳能飞行器的实施例。 此外，公开了用于建造手持式太阳能飞行器的套件的实施例。 此外，公开了制造手持飞行器的方法的实施例。 在一些实施例中，手持飞行器是太阳能供电的。 此外，公开了一种用于手持太阳能飞行器的教具的实施例。 在各种实施例中，教育套件包括关于一个或多个科学和技术学习主题的教育材料，其教育材料与飞行器的组装和/或操作相关并由其补充。 教育材料可以涉及例如飞行技术，航空，可再生能源，电子，机械工程和/或气候学中的一种或多种。

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