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    Airship
    3.
    发明授权
    Airship 失效
    飞艇

    公开(公告)号：US5358200A

    公开(公告)日：1994-10-25

    申请号：US109256

    申请日：1993-08-20

    申请人： Masahiko Onda

    发明人： Masahiko Onda

    IPC分类号： B64B1/10

    CPC分类号： B64B1/10

    摘要： An airship includes a gas envelope filled with a buoyant gas, a duct equipped with an internal propulsion fan and attached to the aft of the gas bag, a boom projecting aft along an extension of the axis of the propulsion fan and an empennage provided on the distal end of the boom and is constituted to prevent boundary layer separation by causing the propulsion fan to suck air flowing along the hull surface into the duct and jet it aft. The duct attached to the aft of the gas bag is formed of a basket-like framework made of rigid light-weight material and covered with taut fabric material, the boom and empennage are formed of airtight fabric material and rigidified by internal pressures, and the internal pressure of the boom and the empennage are regulated so that when load forces received from the empennage side exceed prescribed values above which some part of the airship is liable to be damaged, the boom bends and/or the empennage deforms to relieve the load forces before the damage occurs and the original shape and rigidity is thereafter restored.

    摘要翻译： 飞艇包括填充有浮力气体的气体信封，配备有内部推进风扇并附接到气囊的后部的管道，沿着推进风扇的轴线的延伸部向后突出的悬臂，以及设置在 并且构成为通过使推进风扇将沿着船体表面流动的空气吸入管道并将其向后喷射来防止边界层分离。 附着在气袋后部的导管由刚性轻质材料制成的篮状框架形成，并用绷紧的织物材料覆盖，吊杆和尾翼由气密织物材料形成，并由内部压力硬化， 吊臂和尾翼的内部压力受到管制，以便在从尾翼接收到的载荷力超过规定值以上时，飞艇的某些部分可能受到损坏，起重臂弯曲和/或尾翼变形以减轻载荷力 在发生损坏之前，恢复原来的形状和刚度。

    System and method for varying airship aerostatic buoyancy
    5.
    发明授权
    System and method for varying airship aerostatic buoyancy 有权
    改变飞艇空气静力浮力的系统和方法

    公开(公告)号：US08899514B2

    公开(公告)日：2014-12-02

    申请号：US14032806

    申请日：2013-09-20

    申请人： John Goelet

    发明人： John Goelet

    IPC分类号： B64B1/34 ,  B64B1/28 ,  B64B1/00 ,  B64B1/30 ,  B64B1/58 ,  B64B1/20 ,  B64B1/10 ,  B64B1/16 ,  B64B1/08 ,  B64B1/22

    CPC分类号： B64B1/06 ,  B64B1/005 ,  B64B1/08 ,  B64B1/10 ,  B64B1/16 ,  B64B1/20 ,  B64B1/22 ,  B64B1/28 ,  B64B1/30 ,  B64B1/58 ,  B64D9/00

    摘要： An airship is disclosed. The airship may include a plurality of frame members defining a support structure for a hull of the airship. The airship may further include a plurality of bladders disposed within the hull, and retaining a volume of a lighter-than-air gas. The airship may also include a plurality of valves operatively coupled to at least one of the bladders. The airship may additionally include a computer configured to operate the valves to vary aerostatic buoyancy of the airship to achieve a desired lift force.

    摘要翻译： 飞艇被披露。 飞艇可以包括限定用于飞艇的船体的支撑结构的多个框架构件。 飞艇还可以包括设置在船体内的多个气囊，并且保持一定体积的轻于空气的气体。 飞艇还可以包括可操作地联接到至少一个气囊的多个阀。 飞艇还可以包括计算机，该计算机构造成操作阀以改变飞艇的空气静力浮力以实现期望的提升力。

    Lenticular airship
    6.
    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

    申请人： Pierre Balaskovic

    发明人： Pierre Balaskovic

    IPC分类号： B64B1/12 ,  B64B1/10

    CPC分类号： B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

    摘要： 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.

    摘要翻译： 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。

    Airship tail fin construction for improved control
    7.
    发明授权
    Airship tail fin construction for improved control 失效
    飞艇尾翼施工改善控制

    公开(公告)号：US6019312A

    公开(公告)日：2000-02-01

    申请号：US938467

    申请日：1997-02-28

    申请人： Jesse Blenn

    发明人： Jesse Blenn

    IPC分类号： B64B1/10 ,  B64B1/24 ,  B64C19/00

    CPC分类号： B64B1/10 ,  B64B1/24

    摘要： Airship tail fins (20) deflect under excessive load on axii (108,110) to protect the airship hull (22) and also reduce angles of attack to disturbing airflow. A propulsion engine (24) may be mounted to the tail fin structure. A longitudinally elongated roller (36) may be mounted to the lower tail fin to act as landing gear. Two widely separated lower tail fins may control pitch and roll when moored by providing secure attachment points, as at shaft (38), for ground handling.

    摘要翻译： 飞艇尾翼（20）在axii（108,110）的过载负载下偏转，以保护飞艇的船体（22），并且还可以减少扰动气流的攻角。 推进发动机（24）可以安装到尾翼结构。 纵向细长的辊（36）可以安装到下尾翼以用作起落架。 两个广泛分开的下尾翼可以通过提供牢固的连接点（如在轴（38））处理系泊而控制俯仰和滚动，用于地面处理。

    Trailer for autonomous vehicle
    8.
    发明授权
    Trailer for autonomous vehicle 有权

    公开(公告)号：US10131265B2

    公开(公告)日：2018-11-20

    申请号：US14912474

    申请日：2014-09-11

    申请人： Silicis Technologies, Inc.

    发明人： Michael J. Stigler ,  Nicholas James Setar

    IPC分类号： B64C39/02 ,  B60P7/06 ,  B60P7/08 ,  B60P3/11 ,  B64B1/66 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

    摘要： The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

    SAIL-EQUIPPED AMPHIBIOUS AEROSTAT OR DIRIGIBLE
    10.
    发明申请
    SAIL-EQUIPPED AMPHIBIOUS AEROSTAT OR DIRIGIBLE 审中-公开
    安全的大型航空航天或可靠的

    公开(公告)号：US20150203184A1

    公开(公告)日：2015-07-23

    申请号：US14157798

    申请日：2014-01-17

    申请人： JOSEPH NILO SARMIENTO

    发明人： JOSEPH NILO SARMIENTO

    IPC分类号： B64B1/24 ,  B64B1/36 ,  B64B1/10 ,  B64B1/58 ,  B64B1/70 ,  B64B1/66 ,  B64B1/68 ,  B64B1/02 ,  B64B1/20

    CPC分类号： B64B1/24 ,  B64B1/02 ,  B64B1/10 ,  B64B1/20 ,  B64B1/36 ,  B64B1/66 ,  B64B1/68 ,  B64B1/70

    摘要： A highly maneuverable craft or airship with aerostatic lift which may be manned or operated autonomously and remotely consists, in particular, a sail or similar device for main propulsion; the aerostat or dirigible sustains lift from gasbags containing helium or hydrogen or other similar lighter-than-air gas. Further, said aerostat may be mounted with a wind turbine for electrical power generation and mechanical operation; and, ballast tanks and landing gear to enable amphibious capability.

    摘要翻译： 具有空气静力升降机的高度机动的飞艇或飞艇可以自主和远程地进行人员操作或操作，特别是用于主推进的帆或类似装置; 空气稳定器或气体可以从包含氦气或氢气或其他类似轻型空气气体的气囊中维持升力。 此外，所述空气净化器可以安装有用于发电和机械操作的风力涡轮机; 以及压载舱和起落架，以实现两栖能力。