Pressure stabilized inflated air transport vehicle
    131.
    发明授权
    Pressure stabilized inflated air transport vehicle 有权
    压力稳定的充气运输车辆

    公开(公告)号:US06302357B1

    公开(公告)日:2001-10-16

    申请号:US09648416

    申请日:2000-08-28

    Applicant: John B. Kalisz

    Inventor: John B. Kalisz

    CPC classification number: B64B1/02 B64B1/58 B64B2201/00 B64C1/12 B64C2039/105

    Abstract: This invention relates to a pressure stabilized inflated air transport vehicle having means for limiting crack propagation in the hull envelope whereby leakage of the gas in the haul due to the crack will not exceed the gas pressure maintaining means.

    Abstract translation: 本发明涉及一种具有用于限制船体外壳中的裂纹扩展的装置的压力稳定的膨胀空气输送车辆,由此由于裂缝引起的运输工具中的气体泄漏不会超过气体压力保持装置。

    Radio-controlled flying apparatus
    132.
    发明授权
    Radio-controlled flying apparatus 失效
    无线电遥控飞行器具

    公开(公告)号:US5071383A

    公开(公告)日:1991-12-10

    申请号:US565390

    申请日:1990-08-10

    Inventor: Koichi Kinoshita

    Abstract: A radio-controlled flying apparatus comprising an annular buoyant body and having an overall center of gravity below the center of buoyant force of the buoyant body. The annular buoyant body contains a gas of lighter weight than air. A main body is supported by the annular buoyant body by means of a dual-axis gimbal. The main body is provided with a pair of propellers which are rotatably supported by the main body and are driven by variable-speed motors into rotation in opposite directions. The main body is further provided with a rocking mechanism for causing said main body to rock about the dual-axis gimbal. An electric circuit resides in the main body for receiving a radio wave from an external transmitter to control the rocking mechanism and variable-speed motors. The electric components in the electric circuit are supplied their power from a battery carried on the main body.

    Abstract translation: 一种无线电控制的飞行装置,包括一个环形浮力体,其整体重心低于浮力体浮力的中心。 环形浮体包含比空气轻的气体。 主体通过双轴万向节由环形浮力体支撑。 主体设有一对螺旋桨,它们由主体可旋转地支撑,并由变速马达驱动,以相反的方向转动。 主体还设置有使所述主体围绕双轴万向节摇摆的摆动机构。 电路位于主体中,用于接收来自外部发射器的无线电波,以控制摇摆机构和变速电动机。 电路中的电气部件由主体上承载的电池供电。

    Heavier-than-air passenger aircraft
    133.
    发明授权
    Heavier-than-air passenger aircraft 失效
    重型客机

    公开(公告)号:US3913871A

    公开(公告)日:1975-10-21

    申请号:US46641774

    申请日:1974-05-02

    Applicant: MILLER RALPH H

    Inventor: MILLER RALPH H

    CPC classification number: B64C39/00 B64B2201/00 B64C1/34

    Abstract: Improvement in heavier-than-air passenger aircraft having forward thrust engines, wings, a rear fin and rudder, and a lighter-than-air gas lift mechanism for enhancing the aerodynamic lift provided by the forward thrust engines and wings, such improvement comprising respective forward and rear wings, two equally widthwise spaced apart gas compartments containing lighter-than-air gas disposed vertically above the forward wing, a passenger compartment having a pilot compartment at the front end thereof, the passenger compartment disposed vertically above the forward wing and transversely centrally between the gas compartments, the forward and rear wings and the three compartments joined to each other to provide framing rigidity for said aircraft, the rear fin and rudder mounted upon the passenger compartment so as to upstand vertically therefrom to obtain a clear aerodynamic cut into the air, each compartment of substantially uniform transverse cross-section, each compartment extending axially substantially full length of said aircraft, the rear wing being a substantially full width rear wing disposed vertically above the forward wing so as to have a substantially clear aerodynamic cut into the air.

    Abstract translation: 具有向前推力发动机,翼,后翼和方向舵的重型客机的改进,以及用于增强由前推力发动机和机翼提供的空气动力升力的轻于空气的气举升降机构,其改进包括各自的 前翼和后翼,两个等宽度方向间隔开的气室,其包含垂直设置在前翼上方的轻于空气的气室,在其前端具有先导舱的乘客舱,在前翼上方垂直设置的乘客舱 在气室之间的中央,前翼和后翼与三个隔间相互连接,为所述飞机提供框架刚性,后鳍和方向舵安装在乘客舱上,从而垂直向上竖立,以获得清晰的气动切割 空气,每个隔室的横截面基本均匀,每个隔室延伸一个 所述飞行器的基本上全长,后翼是垂直设置在前翼上方的基本上全宽度的后翼,以便具有基本上清楚的空气动力学切入空气。

    Configurable Buoyancy And Geometry (CBAG) Airship

    公开(公告)号:US20230399093A1

    公开(公告)日:2023-12-14

    申请号:US17806160

    申请日:2022-06-09

    Applicant: Charles G Bagg

    Inventor: Charles G Bagg

    CPC classification number: B64B1/62 B64B2201/00 B64B1/08

    Abstract: A lighter-than-air semi-rigid airship has Configurable Buoyancy And Geometry (CBAG) allowing it to become short and plump for maximum buoyancy during takeoff and landing, but also allowing it to become long and slim for reduced drag (albeit less buoyancy) so that it may travel at high speed. It may be combined with a heavier-than-air structure having wings or rotors to form a hybrid aircraft whereby the wings or rotors provide enough lift to compensate for the reduced buoyancy during high-speed flight.

    Air cushioned landing system for air vehicles
    138.
    发明授权
    Air cushioned landing system for air vehicles 有权
    气垫式降落系统

    公开(公告)号:US09592906B2

    公开(公告)日:2017-03-14

    申请号:US14492154

    申请日:2014-09-22

    Abstract: An air cushioned landing system for an air vehicle comprises an inflatable and deflatable skirt (113) in the form of a tube having inner (101) and outer (100) walls. The inner wall defines a central plenum (116) within the skirt, the skirt including gas pockets (130) arranged to stiffen one or more regions of at least one of the inner (101) and outer (100) sidewalls during deflation of the skirt. A gas pocket fan inflates the gas pockets prior to and during deflation of the skirt, wherein the gas pockets are constrained to move from a mutually spaced apart position when the skirt is inflated, to a mutually closely adjacent position when the skirt is fully deflated.

    Abstract translation: 用于空中交通工具的气垫着陆系统包括具有内(101)和外(100)壁的管形式的可膨胀和可放气的裙部(113)。 所述内壁在所述裙部内限定中央增压室(116),所述裙部包括气囊(130),所述气囊布置成在所述裙部(13)的放气期间加强所述内(101)和外(100)侧壁中的至少一个的一个或多个区域 。 气囊袋风扇在裙部充气之前和期间使气袋膨胀,其中当裙部充气时,气囊被限制为从裙部膨胀时相互间隔开的位置移动到相邻的相邻位置。

Patent Agency Ranking