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    142.
    发明申请
    "VESTAPLAN" GLIDING HELISTAT 审中-公开

    公开(公告)号：US20170096209A1

    公开(公告)日：2017-04-06

    申请号：US15316902

    申请日：2015-03-30

    Applicant: Nikolai Borisowich SHULGIN

    Inventor： Nikolai Borisowich SHULGIN

    IPC: B64B1/66 ,  B64B1/08

    CPC classification number: B64B1/66 ,  B64B1/08 ,  B64B1/14 ,  B64B1/20 ,  B64B1/22 ,  B64B1/34 ,  B64B1/60 ,  B64B2201/00

    Abstract: The invention relates to the field of aviation, and specifically to aircraft structures. The present hybrid aircraft comprises an aerostat with a rigid frame, ballonets with helium, a suspension system, and a bearing platform with a cargo/passenger cabin. The cabin includes controls, engines, electrical equipment and measurement devices. The aerostat is composed of two envelopes connected by a cylindrical hinge and provided with affixing elements, controlling the rotation of which allows for changing and securing the aerostat in the form of a wing or in the form of an A-shape with an opened fairing. The suspension system includes rigid and flexible connections and is capable of being transformed and secured. The stationing and securing of the device in a stable position can be carried out on a sloped solid ground surface, on a water surface, or on a vertical structure.

    Extended endurance air vehicle
    145.
    发明授权
    Extended endurance air vehicle 有权
    延长耐力飞行器

    公开(公告)号：US09428257B2

    公开(公告)日：2016-08-30

    申请号：US14485685

    申请日：2014-09-13

    Applicant: William Edmund Nelson

    Inventor： William Edmund Nelson

    IPC: B64B1/02 ,  B64B1/10 ,  B64B1/12 ,  B64B1/20 ,  B64B1/22 ,  B64B1/28 ,  B64B1/32 ,  B64B1/34 ,  B64B1/58

    CPC classification number: B64B1/02 ,  B64B1/10 ,  B64B1/12 ,  B64B1/20 ,  B64B1/22 ,  B64B1/28 ,  B64B1/32 ,  B64B1/34 ,  B64B1/58 ,  B64B2201/00 ,  B64D27/24 ,  B64D2211/00 ,  G05D1/0011

    Abstract: An air vehicle comprises a vehicle body and a propulsion assembly. The vehicle body has the shape of a wing airfoil to generate lift when air flows over the vehicle body. The vehicle body has a body longitudinal axis and substantially planar port and starboard sides of composite material, and includes first and second hulls that are secured together side-by-side, the hulls having longitudinal axes that are substantially parallel to the body longitudinal axis and two substantially planar side walls at least one of which is of composite material. Each hull defines a separate fluid chamber that is filled with a fluid that is at least partially buoyant. The propulsion assembly is secured to the vehicle body port and starboard sides. The propulsion assembly includes port front and rear engines and starboard front and rear engines, wherein at least two of the engines have independently controlled thrust vectors.

    Abstract translation: 一种机动车辆包括车体和推进组件。 车体具有翼型的形状，以在空气流过车体时产生升力。 车身具有主体纵向轴线和复合材料的基本上平面的端口和右舷侧面，并且包括并排固定在一起的第一和第二船体，船体具有基本上平行于主体纵向轴线的纵向轴线，并且 两个基本平坦的侧壁，其至少一个是复合材料。 每个船体限定了一个单独的流体室，其中填充有至少部分浮力的流体。 推进组件被固定到车体端口和右舷。 推进组件包括前端和后部发动机和右舷前发动机，其中至少两个发动机具有独立控制的推力矢量。

    Airship with internal propulsion system
    146.
    发明授权
    Airship with internal propulsion system 有权
    具有内部推进系统的飞艇

    公开(公告)号：US09296460B2

    公开(公告)日：2016-03-29

    申请号：US13767844

    申请日：2013-02-14

    Applicant: Phillip R. Barber

    Inventor： Phillip R. Barber

    IPC: B64B1/26 ,  B64B1/20 ,  B64B1/10 ,  B64B1/12 ,  B64B1/58 ,  B64G1/26 ,  B64G1/40

    CPC classification number: B64B1/26 ,  B64B1/10 ,  B64B1/12 ,  B64B1/20 ,  B64B1/58 ,  B64B2201/00 ,  B64G1/26 ,  B64G1/40

    Abstract: An airship is presented having a plurality of resilient gas bags and gas containers, a straight fuselage tubular hull, with an inner air passageway and propulsion system located therein, and, connecting air inlet, and outlet funnels fore, and aft, with air deflector cones axially positioned therein. The ship also contains propulsion, reverse, and directional rocket thrusters, in addition to typical airship components.

    Abstract translation: 具有多个弹性气体袋和气体容器的飞艇，其具有位于其中的内部空气通道和推进系统的直的机身管状船体，以及前部和后部与空气导流锥连接的空气入口和出口漏斗 轴向定位在其中。 除了典型的飞艇部件外，该船还包含推进，反向和定向火箭推进器。

    Airship
    150.
    发明申请
    Airship 审中-公开
    飞艇

    公开(公告)号：US20140224938A1

    公开(公告)日：2014-08-14

    申请号：US13907320

    申请日：2013-05-31

    Applicant: Philip Richard Barber

    Inventor： Philip Richard Barber

    IPC: B64B1/06 ,  B64B1/20 ,  B64D45/00 ,  B64G1/40 ,  B64G1/26 ,  B64B1/58 ,  B64B1/12 ,  B64B1/22

    CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/20 ,  B64B1/22 ,  B64B1/26 ,  B64B1/58 ,  B64B2201/00 ,  B64D45/00 ,  B64G1/24 ,  B64G1/26 ,  B64G1/40

    Abstract: An improved airship having a plurality of resilient gasbags & gas containers, a straight fuselage tubular hull with an inner air passageway & propulsion means located therein, connecting air inlet & outlet funnels fore & aft, with air deflector cones axially positioned therein, and a plurality of bifurcated winged air control surfaces axially affixed vertically & horizontally across the air inlet & outlet funnels fore & aft; further, a plurality of vectored air passageways & mechanisms, and propulsion, reverse, & directional rocket thrusters, positioned fore & aft, top, bottom, port & starboard; thereby providing improved speed, maneuverability, efficiency, adverse weather capability, reduced forward air resistance, & rearward drag; furthermore space, outer & inner atmosphere ingress & egress.

    Abstract translation: 具有多个弹性气囊和气体容器的改进的飞艇，具有位于其中的内部空气通道和推进装置的直的机身管状船体，其中前后空气入口和出口漏斗与其中轴向定位的空气导流器锥体，以及多个 的双向翼状空气控制表面，轴向垂直和水平地安装在空气入口和出口漏斗前后; 另外还有多个向心的空气通道和机构，以及推进，反向和定向火箭推进器，位于前后，顶部，底部，端口和右舷; 从而提高速度，机动性，效率，不利的天气能力，减小的前进空气阻力和向后阻力; 进一步的空间，外部和内部的大气进出口。

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