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    UNMANNED AERIAL SYSTEM
    231.
    发明申请
    UNMANNED AERIAL SYSTEM 审中-公开

    公开(公告)号：US20170158320A1

    公开(公告)日：2017-06-08

    申请号：US15269314

    申请日：2016-09-19

    Applicant: Daniel Bosch

    Inventor： Daniel Bosch

    IPC: B64C27/52 ,  B64C15/12 ,  B64D27/24 ,  B64C27/08 ,  B64C27/02 ,  B64C39/02 ,  B64D47/08

    CPC classification number: B64C27/52 ,  B64C15/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/14 ,  B64C2201/165

    Abstract: A multi-propeller unmanned aerial system (UAS) with a wind-resistant software platform that allows for motor support arm rotation, thereby allowing two propellers to move the drone forward and backward, or rotate it, through thrust vectoring, while the other propellers maintain hover. Horizontal movement is possible without losing the level stability necessary for a number of drone-related functions such as aerial photography. The software platform of the UAS provides for the rotational movement of the motor support arm and motors to engage and disengage to allow for tiltrotor control, specifically two motors rotate to advance the UAS forward or reverse while the remaining propellers maintain hover. Propeller guards are provided for safety which do not affect the maximum thrust or flight maneuverability of the drone.

    Aircraft with integrated single sensor
    235.
    发明授权
    Aircraft with integrated single sensor 有权
    集成单传感器的飞机

    公开(公告)号：US09567105B2

    公开(公告)日：2017-02-14

    申请号：US14722921

    申请日：2015-05-27

    Applicant: Sikorsky Aircraft Corporation

    Inventor： Mark R. Alber

    IPC: B64D47/08 ,  B64C29/02

    CPC classification number: B64C29/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/18 ,  B64D47/00 ,  B64D47/08 ,  H01Q1/42

    Abstract: An aircraft is provided and includes a single sensor and wings extending outwardly in opposite directions from a fuselage. Each wing includes a main section, an engine section supported on the main section and tail surfaces extending transversely relative to the main section. The single sensor is mountable to one of the tail surfaces with a field of view (FOV) representable as a spherical wedge having a dihedral angle exceeding 180°.

    Abstract translation: 设有飞机并且包括单个传感器和从机身向相反方向向外延伸的翼。 每个翼包括主部分，支撑在主部分上的发动机部分和相对于主部分横向延伸的尾部表面。 单个传感器可安装到一个尾部表面，其视场（FOV）可表示为具有超过180°的二面角的球形楔形物。

    PROPELLER HAVING EXTENDING OUTER BLADE
    236.
    发明申请
    PROPELLER HAVING EXTENDING OUTER BLADE 审中-公开
    螺旋桨有扩展外刀片

    公开(公告)号：US20170029091A1

    公开(公告)日：2017-02-02

    申请号：US14810109

    申请日：2015-07-27

    Applicant: JONATHON J. LINCH ,  KYLE M. RAHRIG

    Inventor： JONATHON J. LINCH ,  KYLE M. RAHRIG

    IPC: B64C11/00 ,  B64C39/02

    CPC classification number: B64C11/001 ,  B64C39/024 ,  B64C39/10 ,  B64C2039/105 ,  B64C2201/028 ,  B64C2201/104 ,  B64C2201/165

    Abstract: A propeller includes a hub coaxially surrounding a longitudinal axis. A ring shroud coaxially surrounds the longitudinal axis and is spaced radially from the hub. The ring shroud includes an inner ring surface and a radially spaced, oppositely facing outer ring surface. At least one propeller blade is fixedly attached to both the hub and the inner ring surface and extends radially therebetween for mutual rotation therewith. At least one extending blade has a first extending blade end radially spaced from a second extending blade end. The first extending blade end is fixedly attached to the outer ring surface. The second extending blade end is cantilevered from the first extending blade end and is radially spaced from the ring shroud.

    Abstract translation: 螺旋桨包括同轴地围绕纵向轴线的轮毂。 环形护罩同轴地围绕纵向轴线并与轮毂径向间隔开。 环形护罩包括内环表面和径向间隔开的相对的外环表面。 至少一个螺旋桨叶片固定地附接到轮毂和内环表面并且在其间径向延伸以与其相互旋转。 至少一个延伸叶片具有与第二延伸叶片端部径向间隔开的第一延伸叶片端部。 第一延伸叶片端固定地附接到外环表面。 第二延伸叶片端部从第一延伸叶片端部悬臂并且与环形护罩径向间隔开。

    Controlled Take-Off And Flight System Using Thrust Differentials
    238.
    发明申请
    Controlled Take-Off And Flight System Using Thrust Differentials 审中-公开
    使用推力差速控制起飞和飞行系统

    公开(公告)号：US20160244159A1

    公开(公告)日：2016-08-25

    申请号：US14862134

    申请日：2015-09-22

    Applicant: Transition Robotics, Inc.

    Inventor： JoeBen Bevirt

    IPC: B64C29/02 ,  B64C39/02

    CPC classification number: B64C29/02 ,  B64C15/00 ,  B64C29/0025 ,  B64C39/024 ,  B64C2201/02 ,  B64C2201/021 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/165

    Abstract: A manned/unmanned aerial vehicle adapted for vertical takeoff and landing using the same set of engines for takeoff and landing as well as for forward flight. An aerial vehicle which is adapted to takeoff with the wings in a vertical as opposed to horizontal flight attitude which takes off in this vertical attitude and then transitions to a horizontal flight path. An aerial vehicle which controls the attitude of the vehicle during takeoff and landing by alternating the thrust of engines, which are separated in least two dimensions relative to the horizontal during takeoff. An aerial vehicle which uses a rotating platform of engines in fixed relationship to each other and which rotates relative to the wings of the vehicle for takeoff and landing.

    Abstract translation: 一种适用于垂直起飞和着陆的载人/无人机，使用相同的发动机起飞和着陆以及向前飞行。 一种飞行器，其适于在垂直方向上与翼起飞，而不是水平飞行姿态，以垂直姿态起飞，然后转变到水平飞行路径。 一种飞行器，其通过交替发动机的推力来控制起飞和着陆期间车辆的姿态，发动机的推力在起飞期间相对于水平线至少二维分开。 一种飞行器，其使用彼此固定关系并且相对于车辆的翼部旋转以便起飞和着陆的发动机的旋转平台。

    Modular articulated-wing aircraft
    240.
    发明授权
    Modular articulated-wing aircraft 有权
    模块化铰接翼飞机

    公开(公告)号：US09387926B2

    公开(公告)日：2016-07-12

    申请号：US13154796

    申请日：2011-06-07

    Applicant: Geoffrey S. Sommer

    Inventor： Geoffrey S. Sommer

    IPC: B64D5/00 ,  B64C39/02 ,  B64C37/02

    CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/143 ,  B64C2201/165 ,  B64C2201/206

    Abstract: Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

    Abstract translation: 提供了用于形成具有高纵横比翼平台的多关节飞行系统（天基）的系统和/或方法，其可操作以在高海拔地区的感兴趣区域上游荡。 在某些示例性实施例中，自主模块化飞行器以翼尖到翼尖的方式连接在一起。 这样的模块化飞行器可以从日晒中获得其功率。 自主传单可以包括单独操作的传感器，或者在形成天空基础之后集体运行。 天空基优选地可以按照主要条件的要求进行聚合，分解和/或再聚集。 因此，可能提供“永远在车”的飞机。

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