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    EXTENDED ENDURANCE AIR VEHICLE
    2.
    发明申请
    EXTENDED ENDURANCE AIR VEHICLE 审中-公开
    延伸耐用空气车辆

    公开(公告)号：US20150076279A1

    公开(公告)日：2015-03-19

    申请号：US14485685

    申请日：2014-09-13

    Applicant: William Edmund Nelson

    Inventor： William Edmund Nelson

    IPC: B64B1/02 ,  B64D33/00 ,  B64D31/00

    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 so that the vehicle body generates lift when air flows over the vehicle body. The vehicle body has a body longitudinal axis, and includes a first hull and a second hull that are secured together side-by-side, the hulls having longitudinal axes that are substantially parallel to the body longitudinal axis. 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. The propulsion assembly generates thrust and includes a port front engine, a port rear engine, a starboard front engine, and a starboard rear engine, 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。 车身具有翼型件的形状，使得当空气流过车体时车身产生升力。 车体具有主体纵向轴线，并且包括并排固定在一起的第一船体和第二船体，所述船体具有基本上平行于主体纵向轴线的纵向轴线。 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。 推进组件固定在车体上。 推进组件产生推力并且包括端口前置发动机，端口后部发动机，右舷前置发动机和右舷后部发动机，其中至少两个发动机具有独立控制的推力矢量。

    Retracting Air Cushioned Landing System for Air Vehicles
    3.
    发明申请
    Retracting Air Cushioned Landing System for Air Vehicles 有权
    航空航空器撤回空气缓冲着陆系统

    公开(公告)号：US20100001128A1

    公开(公告)日：2010-01-07

    申请号：US12168393

    申请日：2008-07-07

    Applicant: John P. Morehead ,  Douglas H. Greiner ,  Renee Pasman ,  Robert R. Boyd

    Inventor： John P. Morehead ,  Douglas H. Greiner ,  Renee Pasman ,  Robert R. Boyd

    IPC: B60V3/08

    CPC classification number: B60V3/08 ,  B64B1/06 ,  B64B1/32 ,  B64B2201/00

    Abstract: A hybrid air vehicle is disclosed in which a cover is provided for a plurality of air cushioned landing pads to reduce drag when airborne. The pad is inflatable to provide an air cushioned during touchdown and deflatable during flight of the air vehicle. The cover can include a first cover portion and a second cover portion. A first cover roller of the first cover portion and a matching second cover roller of the second cover portion abut to cover the corresponding pad. The first cover roller and the second cover roller, which are separate and free from a physical linkage there between, are separable in an eyelid fashion to expose the corresponding pad. A separation gap between the first cover roller and the second cover roller is increased or decreased by roller straps to cover or expose the corresponding pad.

    Abstract translation: 公开了一种混合动力车辆，其中为多个气垫着陆垫提供了一个盖子，以减少空降时的阻力。 垫子是可充气的，以便在空中飞行的飞行期间在着陆期间提供气垫并且可以充气。 盖可以包括第一盖部分和第二盖部分。 第一盖部分的第一覆盖辊和第二盖部分的匹配的第二盖辊邻接以覆盖相应的垫。 第一覆盖辊和第二覆盖辊分离并且不存在于其间的物理连接，可以以眼睑的方式分离以暴露相应的垫。 第一覆盖辊和第二覆盖辊之间的分离间隙由辊带增加或减小以覆盖或暴露相应的垫。

    Articulated drive
    4.
    发明授权
    Articulated drive 失效
    铰接式驱动

    公开(公告)号：US06467724B2

    公开(公告)日：2002-10-22

    申请号：US09903782

    申请日：2001-07-11

    Applicant: Hermann Kuenkler

    Inventor： Hermann Kuenkler

    IPC: B64C2752

    CPC classification number: B64C29/0033 ,  B63H5/125 ,  B64B1/32 ,  B64B2201/00 ,  B64C11/02 ,  B64C27/28 ,  B64C27/52 ,  B64D35/00

    Abstract: An aircraft has a fuselage designed essentially as an aerostatic lift body and combined lift and propulsion devices which are articulated on the fuselage, are provided with propellers and form propulsion units and which in each case are tiltable between a lift position, in which the respective propeller rotation plane is essentially horizontal and the output shaft of the associated drive, said output shaft acting on the respective propeller shaft, is essentially vertical, and a propulsion position, in which the respective propeller rotation plane is essentially vertical and the output shaft of the associated drive, said output shaft acting on the respective propeller shaft, is essentially horizontal. The propeller rotation plane has all-round inclinability relative to the output shaft of the associated drive, said output shaft acting on the propeller shaft.

    Abstract translation: 飞机具有基本上被设计为空气静力升降机体的机身，并且在机身上铰接的组合的升降机和推进装置设置有螺旋桨和形式推进单元，并且在每种情况下都能够在提升位置之间倾斜， 旋转平面基本上是水平的，并且相关联的驱动器的输出轴（所述输出轴作用在相应的传动轴上）基本上是垂直的，以及推进位置，其中相应的螺旋桨旋转平面基本上垂直并且相关联的输出轴 驱动，所述输出轴作用在相应的传动轴上，基本上是水平的。 螺旋桨旋转平面相对于相关驱动器的输出轴具有全方位的倾斜性，所述输出轴作用在传动轴上。

    CARGO AIRSHIP
    8.
    发明申请
    CARGO AIRSHIP 有权
    货运航空

    公开(公告)号：US20150291269A1

    公开(公告)日：2015-10-15

    申请号：US14531481

    申请日：2014-11-03

    Applicant: LTA Corporation

    Inventor： John Goelet ,  Loginn Kapitan ,  Ron Hochstetler

    IPC: B64B1/08 ,  B64D1/22 ,  B64D1/02 ,  B64B1/22

    CPC classification number: B64B1/08 ,  B64B1/10 ,  B64B1/20 ,  B64B1/22 ,  B64B1/32 ,  B64B1/34 ,  B64B1/58 ,  B64B1/70 ,  B64D1/02 ,  B64D1/22 ,  B64D9/003 ,  Y02T50/46

    Abstract: A cargo airship is disclosed. The cargo airship may include a hull configured to contain a gas and at least one propulsion assembly coupled to the airship and including a propulsion device. The cargo airship may further include a payload bay comprising an external cargo area located outside of the hull. The cargo airship may also include a cargo handling system including at least one hoisting mechanism configured to lift cargo into the external cargo area while the airship is hovering.

    Abstract translation: 披露了货船。 货物飞艇可以包括构造成容纳气体的船体和联接到飞艇的至少一个推进组件，并且包括推进装置。 货物飞艇还可以包括有效载荷舱，其包括位于船体外部的外部货物区域。 货物飞艇还可以包括货物处理系统，其包括至少一个起重机构，其构造成在飞艇盘旋时将货物提升到外部货物区域。

    Aerial transporter
    9.
    发明授权
    Aerial transporter 失效
    空中运输

    公开(公告)号：US08152092B2

    公开(公告)日：2012-04-10

    申请号：US12095385

    申请日：2006-12-06

    Applicant: Rolf Zulkowski ,  Jürgen Henk ,  Carl Von Gablenz ,  Christoph Von Kessel

    Inventor： Rolf Zulkowski ,  Jürgen Henk ,  Carl Von Gablenz ,  Christoph Von Kessel

    IPC: B64B1/02

    CPC classification number: B64B1/32 ,  B64B1/06 ,  B64B1/08 ,  B64D1/22

    Abstract: This invention relates to an aerial transporter comprising rigid cell structures which are covered with light materials as a skin, composed of modules. The invention aerial transporter represents some type of airship without a tail unit as well as an approximate balloon construction comprising a rigid structure and an independent drive unit. Said aerial transporter can transport loads in the range of about 20 t and more over short to medium distances using lighter-than-air technology while meeting air traffic regulations. Furthermore, the disclosed aerial transporter can be used as an air crane in the tied state.

    Abstract translation: 本发明涉及一种航空运输机，其包括由轻质材料作为皮肤覆盖的刚性电池结构，其由模块组成。 本发明的空中运输机代表某种类型的没有尾部单元的飞艇以及包括刚性结构和独立驱动单元的近似气囊结构。 所述空中运输机可以在短时间至中等距离的情况下使用轻于空气技术在满足空中交通管制的条件下运输大约20t以上的载荷。 此外，公开的空中运输机可以用作捆扎状态的空气起重机。

    AERIAL TRANSPORTER
    10.
    发明申请
    AERIAL TRANSPORTER 失效
    空中交通工具

    公开(公告)号：US20090078818A1

    公开(公告)日：2009-03-26

    申请号：US12095385

    申请日：2006-12-06

    Applicant: Rolf Zulkowski ,  Jurgen Henk ,  Carl Von Gablenz ,  Christoph Von Kessel

    Inventor： Rolf Zulkowski ,  Jurgen Henk ,  Carl Von Gablenz ,  Christoph Von Kessel

    IPC: B64B1/08

    CPC classification number: B64B1/32 ,  B64B1/06 ,  B64B1/08 ,  B64D1/22

    Abstract: This invention relates to an aerial transporter comprising rigid cell structures which are covered with light materials as a skin, composed of modules. The invention aerial transporter represents some type of airship without a tail unit as well as an approximate balloon construction comprising a rigid structure and an independent drive unit. Said aerial transporter can transport loads in the range of about 20 t and more over short to medium distances using lighter-than-air technology while meeting air traffic regulations. Furthermore, the disclosed aerial transporter can be used as an air crane in the tied state.

    Abstract translation: 本发明涉及一种航空运输机，其包括由轻质材料作为皮肤覆盖的刚性电池结构，其由模块组成。 本发明的空中运输机代表某种类型的没有尾部单元的飞艇以及包括刚性结构和独立驱动单元的近似气囊结构。 所述空中运输机可以在短时间至中等距离的情况下使用轻于空气技术在满足空中交通管制的条件下运输大约20t以上的载荷。 此外，公开的空中运输机可以用作捆扎状态的空气起重机。

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