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    AIRSHIP/SPACECRAFT
    242.
    发明公开
    AIRSHIP/SPACECRAFT 审中-公开
    飞艇/航天器

    公开(公告)号：EP1175332A2

    公开(公告)日：2002-01-30

    申请号：EP00953628.5

    申请日：2000-04-11

    Applicant: Provitola, Anthony I.

    Inventor： Provitola, Anthony I.

    IPC: B64B1/58

    CPC classification number: B64G1/401 ,  B64B1/08 ,  B64B1/58 ,  B64B2201/00 ,  B64C39/001 ,  B64G1/002 ,  B64G1/005 ,  B64G1/402

    Abstract: An airship/spacecraft, which, in a preferred embodiment, uses its lifting gas (64) as fuel for thrusters, which may be of the turbo-type or rocket type, or both, to achieve transition to space flight. The airship aspect has gas retaining structures (61) that can withstand internal and external pressure and can change in volume and shape. The gas retaining structures (61) may be compartmentalized with a folded diaphragm membrane (63) and also configured as pressure vessels. The spacecraft aspect provides control, power, services, and space for missions of the airship/spacecraft. The best mode includes a turbo-rocket thruster in which the turbine compressor is used to intake and compress a gaseous fuel for combustion with a stored oxidizer injected into the compressed gaseous fuel stream. The compressor stage (6) is driven by the turbine stage (7), which is driven by burning gaseous fuel passing across the turbine blades (13). The burned gases are then expanded through an exhaust nozzle and thereby ejected to produce reaction thrust.

    FLYING VEHICLE
    244.
    发明公开
    FLYING VEHICLE 失效
    FLUGOBJEKT。

    公开(公告)号：EP0596131A1

    公开(公告)日：1994-05-11

    申请号：EP93905682.6

    申请日：1993-01-21

    Applicant: NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA "EKIP"

    Inventor： SAVITSKY, Anatoly Ivanovich ,  SCHUKIN, Lev Nikolaevich ,  KARELIN, Viktor Georgievich ,  PUSHKIN, Rostislav Mikhailovich ,  MASS, Alexandr Mikhailovich ,  SHIBANOV, Anatoly Petrovich ,  SCHUKIN, Ilya Lvovich ,  KHUTSISCHVILI, Vladimir Georgievich ,  FISCHENKO, Sergei Viktorovich ,  ERMISCHIN, Alexandr Viktorovich ,  SOBKO, Alexandr Pavlovich

    IPC: B64C39/00 ,  B64C29/00 ,  B60V3/08

    CPC classification number: B64C39/10 ,  B60V1/22 ,  B64B2201/00 ,  B64C39/00 ,  Y02T50/12

    Abstract: The invention relates to aviation namely to flying vehicles adapted to ride on an air cushion and to effect a take-off and landing on aerodromes of any category. The goal of the invention is to design a flying vehicle capable of aerodinamically efficient flight both at low and high level flight, as well as take-off and landing from non-prepared aerodromes and from water under the conditions of stabilization and movement control of all flight regimes. The goal is achieved due to the fact that in a flying vehicle comprising a fuselage in the form of a carrying wing, a power installation, a take-off and landing air cushion device, a gasodynamic system of boundary layer control, a device for controlling the position of flow leaving the trailing edge as well as stabilization and flight control systems, the take-off and landing air cushion device consists of a propelling slot nozzle (12) and side skegs (17) between which are mounted rotatable flaps (21, 22, 23) controlling the flight of the vehicle and regulating the position of the pressure centre on the bottom. The fuselage has the form of a cylindrical segment conjugating at its sides with spherical fairings.

    Abstract translation: 本发明涉及航空，即适用于乘坐气垫的飞行车辆，以及在任何类别的机场上起飞和降落。 本发明的目的是设计一种能够在低和高水平飞行中进行航空飞行高效飞行的飞行器，以及在所有的稳定和运动控制的条件下从未准备的机场和水中起飞和着陆 飞行政权 目标是实现这样的事实，即在飞行载体中包括机身形式的机身，动力装置，起飞和着陆气垫装置，边界层控制的气动系统，控制装置 离开后缘的流动位置以及稳定和飞行控制系统，起飞和着陆气垫装置包括推进式狭缝喷嘴（12）和侧部销钉（17），在其间安装有可旋转的折翼（21， 控制车辆的飞行并且调节压力中心在底部的位置。 机身具有圆柱形段的形式，其侧面与球形整流罩共轭。

    Aircraft having buoyancy gas balloon
    246.
    发明公开
    Aircraft having buoyancy gas balloon 失效
    Flugzeug mit Gasballonauftrieb。

    公开(公告)号：EP0078713A2

    公开(公告)日：1983-05-11

    申请号：EP82305838.3

    申请日：1982-11-03

    Applicant: Ferguson, Frederick

    Inventor： Ferguson, Frederick

    IPC: B64B1/00

    CPC classification number: B64B1/00 ,  B64B2201/00

    Abstract: An airship having a spherical balloon filled with buoyant gas such as helium at a pressure substantially greater than atmospheric and which is mounted for rotation about a normally horizontal axis, the airship including a rigid load supporting yoke having two support arms extending upwardly from a central gondola and each with an upper end rotatably connected to the balloon, is characterized by the gondola and support arms having surfaces close to and conforming to the shape of the balloon so as to inhibit air flow between the gondola and the bottom of the balloon and to redirect this air to the sides and back of the balloon.

    Abstract translation: 具有填充有诸如氦气之类的浮力气体的球形气球，其大小大致上大于和大于空气的涡轮被安装成围绕正常水平的轴线旋转，所述飞艇包括刚性负载支撑轭，其具有从 中央吊舱，并且每个都具有可旋转地连接到气球的上端，其特征在于吊舱和支撑臂具有接近并且符合气球的斜面的表面，以便抑制平台车与底部或气球之间的空气流动， 将空气重新定向到气球的两侧和背面。

    Aircraft having buoyant gas balloon
    247.
    发明公开
    Aircraft having buoyant gas balloon 失效
    Luftfahrzeug mit Traggasballon。

    公开(公告)号：EP0023843A2

    公开(公告)日：1981-02-11

    申请号：EP80302686.3

    申请日：1980-08-06

    Applicant: Ferguson, Frederick

    Inventor： Ferguson, Frederick

    IPC: B64B1/00

    CPC classification number: B64B1/00 ,  B64B2201/00

    Abstract: An aircraft is provided utilizing a spherical balloon filled with buoyant gas such as helium at a pressure substantially greater than atmospheric so that its dimensions are substantially unaffected by changes in atmospheric pressure or temperature. The aircraft may take the form of a self-propelled and self-contained airship, or may be merely a passive device for providing lift and intended to be towed by and controlled from a helicopter. The spherical balloon is mounted on a normally horizontal axle having end portions projecting from opposite sides of the balloon, and includes a rigid load supporting yoke including two arms extending upwardly from a central load supporting structure and each with an upper end suspended from the axle.

    Abstract translation: 使用充满浮力气体（例如氦气）的球形气球，其压力基本上大于大气压，使其尺寸基本上不受大气压力或温度的变化的影响。 飞机可以采取自行式和独立式飞艇的形式，或者可以仅仅是用于提供升降机的被动装置，并且意图由直升机牵引和控制。 球形球囊安装在具有从球囊的相对侧突出的端部的正常水平轴上，并且包括刚性负载支撑轭，其包括从中心负载支撑结构向上延伸的两个臂，并且每个具有从轴悬挂的上端。

    TACTICAL HYBRID STRATOSPHERIC AIRSHIP
    249.
    发明公开
    TACTICAL HYBRID STRATOSPHERIC AIRSHIP 审中-公开

    公开(公告)号：US20230234693A1

    公开(公告)日：2023-07-27

    申请号：US18011987

    申请日：2021-06-16

    Applicant: C.I.R.A. (CENTRO ITALIANO RICERCHE AEROSPAZIALI) - S.C.P.A.

    Inventor： Giuseppe PERSECHINO ,  Vincenzo Rosario BARANIELLO ,  Roberto BORSA

    IPC: B64B1/20 ,  B64B1/08 ,  B64B1/32

    CPC classification number: B64B1/20 ,  B64B1/08 ,  B64B1/32 ,  B64B2201/00

    Abstract: A hybrid stratospheric airship for the combined and optimized use of aerostatic and aerodynamic force, including: an inflatable central body; a first and second inflatable wing extending from the central body protruding laterally from two opposite sides of the central body, each wing having a portion proximal to the central body, an end portion distal from said central body, a leading edge, and a trailing edge; an outer shell having a main shell portion associated with the main body, and a first and a second side shell portion associated with each wing, respectively; at least one main spar extending transversely to the central body, which supports the first and second wing and crosses the central body, the at least one main spar a rectilinear spar interposed between the leading edge and the trailing edge of the first and second wings, and connected to the distal end portions of the wings.

    AUTONOMOUS LOW-ALTITUDE UAV DETECTION SYSTEM
    250.
    发明公开
    AUTONOMOUS LOW-ALTITUDE UAV DETECTION SYSTEM 审中-公开

    公开(公告)号：US20230222809A1

    公开(公告)日：2023-07-13

    申请号：US17591757

    申请日：2022-02-03

    Applicant: Mazen A. Al-Sinan

    Inventor： Mazen A. Al-Sinan

    IPC: G06V20/58 ,  G06V10/74 ,  B64C39/02 ,  B64D47/08

    CPC classification number: G06V20/58 ,  B64C39/024 ,  B64D47/08 ,  G06V10/761 ,  B64B2201/00 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/127 ,  B64D2211/00

    Abstract: An autonomous unmanned aerial vehicle detecting system for monitoring a geographic area includes an unmanned blimp adapted to hover in air, at least one camera mounted on the blimp to scan at least a portion of the geographic area, a location sensor to determine a location of the blimp, and a controller arranged in communication with blimp, the at least one camera, and the location sensor. The controller is configured to position the blimp at a desired location in the air based on inputs received from the location sensor, and monitor the geographic area based on the images received from at least one camera. The controller is also configured to detect a presence of an unmanned aerial vehicle within the geographic area based on the received images, and determine whether the detected unmanned aerial vehicle is an unauthorized unmanned aerial vehicle based on the received images.

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