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    FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES
    81.
    发明申请
    FLUIDIC PROPULSIVE SYSTEM AND THRUST AND LIFT GENERATOR FOR AERIAL VEHICLES 审中-公开
    流体推进系统和用于空中客车的起升和起跳发电机

    公开(公告)号：US20170057621A1

    公开(公告)日：2017-03-02

    申请号：US15256178

    申请日：2016-09-02

    Applicant: Jetoptera, Inc.

    Inventor： Andrei Evulet

    IPC: B64C21/04 ,  B64C39/02 ,  B64D27/16 ,  B64D27/00

    CPC classification number: B64D29/02 ,  B64C9/38 ,  B64C15/00 ,  B64C21/00 ,  B64C21/04 ,  B64C39/024 ,  B64C2201/10 ,  B64C2201/104 ,  B64D27/10 ,  B64D27/18 ,  B64D33/02 ,  B64D33/04 ,  B64D2033/0273 ,  Y02T50/166 ,  Y02T50/32 ,  Y02T50/44

    Abstract: A vehicle includes a main body and a gas generator producing a gas stream. At least one fore conduit and tail conduit are fluidly coupled to the generator. First and second fore ejectors are fluidly coupled to the at least one fore conduit. At least one tail ejector is fluidly coupled to the at least one tail conduit. The fore ejectors respectively include an outlet structure out of which gas from the at least one fore conduit flows. The at least one tail ejector includes an outlet structure out of which gas from the at least one tail conduit flows. First and second primary airfoil elements have leading edges respectively located directly downstream of the first and second fore ejectors. At least one secondary airfoil element has a leading edge located directly downstream of the outlet structure of the at least one tail ejector.

    Abstract translation: 车辆包括产生气流的主体和气体发生器。 至少一个前导管和尾管与流体耦合到发生器。 第一和第二前喷射器流体地联接到至少一个前导管。 至少一个尾喷射器流体地联接到所述至少一个尾管。 前喷射器分别包括出口结构，来自至少一个前导管的气体流出。 至少一个尾喷射器包括出口结构，来自至少一个尾管的气体从该出口结构流出。 第一和第二主翼元件具有分别位于第一和第二前部喷射器的下游的前缘。 至少一个副翼元件具有位于至少一个尾喷射器的出口结构的下游的前缘。

    Floating mobile object and floating mobile system using the same
    83.
    发明授权
    Floating mobile object and floating mobile system using the same 有权
    浮动移动物体和浮动移动系统使用相同

    公开(公告)号：US09308986B2

    公开(公告)日：2016-04-12

    申请号：US14385506

    申请日：2013-02-14

    Applicant: The Ritsumeikan Trust

    Inventor： Katsuya Kanaoka

    IPC: B64C15/12 ,  B63H25/04 ,  B64C39/02 ,  G05D1/10 ,  B63H25/46 ,  B63B35/00

    CPC classification number: B64C15/12 ,  B63B2035/008 ,  B63H25/04 ,  B63H25/46 ,  B63H2025/465 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/10 ,  B64C2201/146 ,  G05D1/10 ,  G05D1/102

    Abstract: A holonomic floating mobile object is operated under gravity and includes a main body and six or more thrusters for generating thrust by changing the momentum of a fluid. The six or more thrusters are controlled independently of one another such that the thrust is set at a desired value. The six or more thrusters are arranged in a fuselage coordinate system defined on the main body, such that the range in which a total thrust vector obtained by combining vectors of the thrust generated by all of the thrusters can be generated spans a six-dimensional space with three directions of translation and three directions of rotation. Incoming and outgoing flows to and from one of the thrusters are spaced apart from incoming and outgoing flows to and from the other thrusters and even apart from every other fuselage structure aside from that one thruster.

    Abstract translation: 完整的浮动移动物体在重力作用下运行，包括主体和六个或更多个用于通过改变流体动量产生推力的推进器。 六个或更多个推进器彼此独立地控制，使得推力被设定在期望的值。 六个或更多个推进器被布置在限定在主体上的机身坐标系中，使得可以产生通过组合由所有推进器产生的推力的矢量而获得的总推力向量的范围跨越六维空间 具有三个方向的翻译和三个方向的旋转。 来往于其中一个推进器的进出流量与进入和离开其它推进器的进出流量间隔开，甚至除了一个推进器之外的每个其他机身结构。

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