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    Survivable and reusable launch vehicle
    21.
    发明授权
    Survivable and reusable launch vehicle 有权
    生存和可重复使用的运载火箭

    公开(公告)号：US06845937B2

    公开(公告)日：2005-01-25

    申请号：US10453777

    申请日：2003-06-03

    Applicant: Henry August

    Inventor： Henry August

    IPC: B64C5/12 ,  B64C39/02 ,  B64C39/06 ,  B64C39/12 ,  B64D1/06 ,  F42B10/16 ,  F42B10/62 ,  F42B12/58 ,  F42B12/62 ,  F42B15/00 ,  B64C37/02

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/046 ,  B64C2201/104 ,  B64C2201/121 ,  F42B10/16 ,  F42B10/62 ,  F42B12/58 ,  F42B12/62 ,  F42B15/00

    Abstract: A reusable, mach-velocity mobile platform delivers a weapons payload via vertical launch, powerless glide, weapons release, and landing operation phases. The platform includes a generally tubular shaped body having an aft and forward end, and a payload section. An arch wing is supported by the body aft end. The arch wing has an upper and a lower wing joined at distal ends by two curved end plates. A nose assembly is connected at the forward end having an upward directed fixed angle-of-attack to generate forward end lift. Thermal tiles attached under the body and the lower wing under-side radiate/dissipate heat generated during a high angle-of-attack platform reentry. Radar absorptive or radar translucent material is used. The platform preferably discharges payload from the aft end for safe separation. A landing gear is extended for the landing phase of operation.

    Abstract translation: 可重复使用的马赫速度移动平台通过垂直发射，无力滑翔，武器释放和着陆操作阶段提供武器有效载荷。 平台包括具有尾部和前端的大致管状的主体和有效载荷部分。 一个弓翼由身体后端支撑。 拱翼具有通过两个弯曲端板在远端连接的上翼和下翼。 前端组件在前端连接，具有向上定向的固定迎角，以产生前端提升。 安装在车体下方的散热瓦片和下部翼片下侧辐射/消散在高角度攻角平台折返期间产生的热量。 使用雷达吸收或雷达半透明材料。 该平台优选地从尾端排出有效载荷以进行安全分离。 起落架延伸到着陆阶段。

    Robotic or remotely controlled flying platform
    23.
    发明授权
    Robotic or remotely controlled flying platform 失效
    机器人或遥控飞行平台

    公开(公告)号：US4795111A

    公开(公告)日：1989-01-03

    申请号：US15100

    申请日：1987-02-17

    Applicant: Paul S. Moller

    Inventor： Paul S. Moller

    IPC: B64C27/00 ,  B64C27/20 ,  B64C39/02 ,  B64C29/02

    CPC classification number: B64C39/024 ,  B64C27/00 ,  B64C27/20 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2201/162

    Abstract: A flying platform, propelled by at least one ducted fan causing a vertically downwardly directed airstream in and through a cylindrical duct. A vane system in the duct has two mutually perpendicular pairs of diametrically opposite first vanes, each extending in from the duct rim toward the center of the duct. Each pair of first vanes provides a pair of generally vertical walls parallel to a diametral line across the duct, and they define duct passages between the pairs of vanes and define quadrants between adjacent pairs. Each first vane has an upper, fixed, rigid portion and a variable camber flap depending therefrom. A first servomotor with linkages vary the camber of each pair of flaps, so that the camber of the flaps of each pair is at all times the same amount but in opposite directions. Preferably, there are also four second vanes, one bisecting each quadrant, and a symmetric pair of spoilers is mounted on each second vane. Each pair of spoilers is independently movable, as a pair continuously between a position substantially blocking airflow through the outer portion of said quadrant and a position permitting substantially full airflow therethrough. A second servomotor with linkages symmetrically varies the position of its spoilers. There may be a radio receiver responsive to remote control signals for actuating each servomotor and its linkages.

    Remotely piloted vehicle
    24.
    发明授权
    Remotely piloted vehicle 失效
    遥控车

    公开(公告)号：US4194708A

    公开(公告)日：1980-03-25

    申请号：US944441

    申请日：1978-09-21

    Applicant: Daniel J. Tracy ,  John P. Palmer ,  Daniel J. O'Brien

    Inventor： Daniel J. Tracy ,  John P. Palmer ,  Daniel J. O'Brien

    IPC: B64C39/02 ,  B64C15/02 ,  B64D1/06

    CPC classification number: B60V3/08 ,  B64C39/024 ,  B64C2201/104 ,  B64C2201/121 ,  B64C2201/146

    Abstract: A recoverable remotely piloted vehicle (RPV) having: a deflectable canard/elevator placed very close to the nose tip; a constant (cross) section fuselage; wings mounted low and well aft on the fuselage; elevons; a centrally positioned weapons/payload bay, with doors, located internal of the upper portion of the fuselage; and, inflatable landing skids. The weapon/payload is dropped from the RVP, while the RVP is in flight in an inverted position.

    Abstract translation: 一种可恢复的遥控车辆（RPV），其具有：非常靠近鼻尖的可偏转的鸭子/电梯; 恒定（横）部分机身; 机身低矮，机身后方均匀; 电梯 一个位于中心的武器/有效载荷舱，带有位于机身上部内部的门; 和充气着陆滑行。 武器/有效载荷从RVP中丢弃，而RVP在倒置的位置飞行。

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