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    Lenticular airship
    16.
    发明授权
    Lenticular airship 有权
    透镜飞艇

    公开(公告)号：US08109462B2

    公开(公告)日：2012-02-07

    申请号：US12957989

    申请日：2010-12-01

    Applicant: Pierre Balaskovic

    Inventor： Pierre Balaskovic

    IPC: B64B1/12 ,  B64B1/10

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

    Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

    HYBRID AIRSHIP
    17.
    发明申请
    HYBRID AIRSHIP 审中-公开
    混合航空

    公开(公告)号：US20100270424A1

    公开(公告)日：2010-10-28

    申请号：US12429542

    申请日：2009-04-24

    Applicant: James D. DeLaurier

    Inventor： James D. DeLaurier

    IPC: B64B1/20 ,  G09F21/08 ,  B64B1/12

    CPC classification number: B64B1/06 ,  B64B1/14 ,  B64B1/20 ,  B64B1/30 ,  B64B2201/00 ,  B64C2201/00 ,  G09F21/08 ,  G09F21/10

    Abstract: A hybrid airship comprises a non-rigid body having a delta-wing shape and an airfoil cross-section. The body is shaped for generating aerodynamic lift during forward flight, and contains a gas for generating buoyancy lift. At least one splitter plate is pivotally connected along a trailing edge of the body. The splitter plate is configured to be controllably pivoted for controlling the airship.

    Abstract translation: 混合式飞艇包括具有三角翼形状和翼型横截面的非刚性体。 身体形状适合在向前飞行期间产生空气动力升力，并且包含产生浮力升力的气体。 至少一个分离板沿主体的后缘枢转地连接。 分离板构造成可控地枢转以控制飞艇。

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