中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

319 records (took 0.03 seconds)

    BUOYANT FLYING BODY
    41.
    发明公开
    BUOYANT FLYING BODY 审中-公开
    浮躁的飞行体

    公开(公告)号：EP3150483A1

    公开(公告)日：2017-04-05

    申请号：EP16811654.9

    申请日：2016-06-15

    Applicant: Nakamura, Kohei

    Inventor： Nakamura, Kohei

    IPC: B64B1/30 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02

    CPC classification number: B64B1/30 ,  B64B1/58 ,  B64C25/06 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/127

    Abstract: Provided is a buoyant aerial vehicle which can secure high safety by reducing the risk of crashing, and which can facilitate control of movement by suppressing the influence of wind and exhibit high mobility capability. The buoyant aerial vehicle is configured by including: a buoyant vehicle body in which gas having a specific gravity smaller than air is hermetically filled; a vertical propulsion propeller which provides vertical propulsive force to the buoyant vehicle body; and a horizontal propulsion propeller which provides horizontal propulsive force to the buoyant vehicle body, and is configured such that the buoyant vehicle body has horizontal wind passages formed in at least two directions, and has outer peripheral edges each formed into an acute angle in side view.

    Abstract translation: 本发明提供一种浮力飞行器，其能够通过降低碰撞风险来确保较高的安全性，并且能够通过抑制风的影响来促进对运动的控制，并且具有高运动能力。 所述浮力飞行器通过包括：浮力车体，在所述浮力车体中气密地填充比重小于空气的气体; 向浮力车体提供垂直推进力的垂直推进螺旋桨; 以及向浮力车体提供水平推进力的水平推进螺旋桨，并且浮力车体具有形成在至少两个方向上的水平风道，并且具有在侧视图中形成为锐角的外周边缘 。

    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS
    46.
    发明公开
    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 有权
    系统方法FURR LANGANHALTENDER LUFTSCHIFFBETRIEB

    公开(公告)号：EP2897860A2

    公开(公告)日：2015-07-29

    申请号：EP13843055.8

    申请日：2013-09-20

    Applicant: Heppe, Stephen

    Inventor： Heppe, Stephen

    IPC: B64B1/06 ,  B64C37/02

    CPC classification number: B64C37/02 ,  B64B1/06 ,  B64C2201/022 ,  B64C2201/063

    Abstract: In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.

    Abstract translation: 在一个例子中，长期耐力飞艇系统包括有效载客飞艇和机械地连接到有效载客飞艇上以形成第一组合的飞艇的第一物流飞艇，有效载运飞艇和具有至少两倍的设计能力的后勤飞艇， 至少有以下至少一项：发电能力，推进能力，耐力能力和提升能力，第一组合飞艇自由飞行，轻于空气，并配置为在没有物理连接的情况下保持高达30天以上 到地面。 还提供了长期耐力飞艇作业的说明性方法。

    Vorrichtung zur Entfernung von Schadgasen aus der Atmosphäre
    49.
    发明公开
    Vorrichtung zur Entfernung von Schadgasen aus der Atmosphäre 有权
    Vorrichtung zur Entfernung von Schadgasen aus derAtmosphäre

    公开(公告)号：EP2103340A1

    公开(公告)日：2009-09-23

    申请号：EP09001803.7

    申请日：2009-02-10

    Applicant: Astrium GmbH

    Inventor： Konigorski, Detlev

    IPC: B01D53/74

    CPC classification number: B64B1/20 ,  B01D53/002 ,  B01D2257/2025 ,  B01D2257/2064 ,  B01D2259/4558 ,  B64B2201/00 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/125 ,  Y10S244/90

    Abstract: Eine Vorrichtung zur Entfernung von Schadgasen aus der Atmosphäre besteht aus einer in der Erdatmosphäre autonom operierenden Plattform, deren Gehäuse in Leichtbauweise konstruiert und mit Einlässen für die umgebende Atmosphäre sowie mit Auslässen für die aufbereiteten Produkte ausgestattet ist. Im Inneren des Gehäuses sind Einheiten zur Gasextrahierung und -separation sowie zur Speicherung und Aufbereitung von flüssigen und gasförmigen Produkten angeordnet. Die Energie zum Betrieb der einzelnen Einheiten dieses geschlossenen kryogenen Kreislaufsystems wird dabei von Solarzellen erzeugt.

    Abstract translation: 该装置具有在地球大气的预定区域中可自主操作的平台，并且包括轻量壳体（1）。 壳体具有入口（3）和出口（4）。 压缩单元（5），分离和/或气体提取单元（6），储存罐（7），辐射单元（8）和氧气发生器（9）设置在壳体中，用于提取，分离，储存 以及流体和气态产品的加工。 太阳能电池与低温循环系统连接，其中电池被提供用于产生能量以操作压缩单元。

    AIRSHIP AND METHOD OF OPERATION
    50.
    发明授权
    AIRSHIP AND METHOD OF OPERATION 有权
    飞艇工作程序

    公开(公告)号：EP1519873B1

    公开(公告)日：2007-10-24

    申请号：EP03737791.8

    申请日：2003-06-25

    Applicant: 21st Century Airships Inc.

    Inventor： COLTING, Hokan

    IPC: B64B1/00

    CPC classification number: B64B1/34 ,  B64B1/02 ,  B64B1/32 ,  B64C21/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  Y02T50/166

    Abstract: An airship (20) has a generally spherical shape and has an internal envelope (24) for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system (36, 38) that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7 % full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module (180) that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors (44, 46) of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit (52) that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.

Patent Agency Ranking