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    A THRUST PRODUCING UNIT WITH AT LEAST TWO ROTOR ASSEMBLIES AND A SHROUDING
    3.
    发明公开
    A THRUST PRODUCING UNIT WITH AT LEAST TWO ROTOR ASSEMBLIES AND A SHROUDING 审中-公开

    公开(公告)号：EP3354560A1

    公开(公告)日：2018-08-01

    申请号：EP18152689.8

    申请日：2018-01-22

    申请人： AIRBUS HELICOPTERS DEUTSCHLAND GmbH

    发明人： MORES, Sebastian ,  KIESEWETTER, Uwe ,  BEBESEL, Marius

    IPC分类号： B64C11/00 ,  B64C29/00 ,  B64C27/20

    CPC分类号： B64C11/46 ,  B64C11/001 ,  B64C27/08 ,  B64C27/20 ,  B64C29/0033

    摘要： The invention is related to a thrust producing unit 3d for producing thrust in a predetermined direction 23, comprising a shrouding 6d and at least two rotor assemblies 7d, 8d, wherein the shrouding 6d defines an internal volume 20c, and wherein a first rotor assembly 7d of the at least two rotor assemblies 7d, 8d defines a first rotor axis and a second rotor assembly 8d of the at least two rotor assemblies 8d defines a second rotor axis, the first and second rotor axes 12d being one of: (i) coaxially arranged, and (ii) inclined by associated inclination angles 21a, 22a with respect to the predetermined direction 23, the associated inclination angles 21a, 22a being comprised in a range between -60° and +60°, and preferably amounting to 0°, and wherein the first rotor assembly 7d is arranged outside of the internal volume 20c of the shrouding 6d.

    FIXED ROTOR THRUST VECTORING
    4.
    发明公开
    FIXED ROTOR THRUST VECTORING 审中-公开

    公开(公告)号：EP3152112A4

    公开(公告)日：2018-01-17

    申请号：EP15803884

    申请日：2015-06-03

    申请人： CYPHY WORKS INC

    发明人： SEBESTA KENNETH D

    IPC分类号： B64C15/02 ,  B64C27/20 ,  B64C39/02 ,  B64D47/08

    CPC分类号： B64C27/20 ,  B64C15/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/127 ,  B64D47/08

    摘要： An aerial vehicle includes a body having a center and a number of spatially separated thrusters. The spatially separated thrusters are statically coupled to the body at locations around the center of the body and are configured to emit thrust along a number of thrust vectors. The thrust vectors have a number of different directions with each thruster configured to emit thrust along a different one of the thrust vectors. One or more of the thrust vectors have a component in a direction toward the center of the body or away from the center of the body.

    VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS
    5.
    发明公开
    VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS 审中-公开
    VTOL-FAHRZEUG MIT KOAXIAL GENEIGTEN ODER NEIGBAREN ROTOREN

    公开(公告)号：EP2318273A4

    公开(公告)日：2017-09-06

    申请号：EP09811177

    申请日：2009-08-28

    申请人： URBAN AERONAUTICS LTD

    发明人： YOELI RAPHAEL

    IPC分类号： B64C27/08 ,  B64C27/20 ,  B64C29/00

    CPC分类号： B64C27/20 ,  B64C29/0033

    摘要： A VTOL vehicle includes a forward rotor, an aft rotor and a fuselage, the forward and aft rotor lying in a longitudinal axis of the vehicle, with the fuselage located axially between the forward and aft rotors. The vehicle has an in-flight configuration wherein the forward rotor is tilted downwardly at a negative tilt angle relative to the fuselage and the aft rotor is tilted upwardly at a positive tilt angle relative to the fuselage.

    摘要翻译： VTOL车辆包括前转子，后转子和机身，前后转子位于车辆的纵向轴线上，其中机身位于前转子和后转子之间。 该车辆具有飞行中构型，其中前转子相对于机身以负倾角向下倾斜，并且后转子相对于机身以正倾角向上倾斜。

    MULTI-ROTOR PASSENGER-CARRYING AIRCRAFT WITH FOLDABLE AIRCRAFT ARM
    6.
    发明公开
    MULTI-ROTOR PASSENGER-CARRYING AIRCRAFT WITH FOLDABLE AIRCRAFT ARM 审中-公开
    带有可折叠飞机臂的多旋翼载客飞机

    公开(公告)号：EP3184415A1

    公开(公告)日：2017-06-28

    申请号：EP16154601.5

    申请日：2016-02-08

    申请人： Guanghou Ehang Intelligent Technology Co., Ltd.

    发明人： DU, Hao ,  HU, Huazhi ,  LI, Zhiyi

    IPC分类号： B64C1/30

    CPC分类号： B64C1/30 ,  B64C27/10 ,  B64C27/20 ,  B64D27/24

    摘要： A multi-rotor passenger-carrying aircraft with foldable aircraft arm, including an aircraft body, a fixing mechanism, a connector and an aircraft arm. The fixing mechanism is fastened on the aircraft body, an end of the aircraft arm is articulated to the fixing mechanism, which is provided with a first mounting hole, and the aircraft arm is provided with a second mounting hole. When the aircraft arm is in a folded state, one end of the connector is removably attached to the fixing mechanism through a first fastener, and the other end is removably attached to the aircraft arm through a second fastener, keeping the fixing mechanism at a first angle with the aircraft arm. When the aircraft arm is in a working state, a third fastener is passes through both the first and second mounting holes to cause the fixing mechanism to be fixedly connected to the aircraft arm and kept at a second angle with the aircraft arm.

    摘要翻译： 搭载可折叠飞机手臂的多旋翼载客飞机，包括飞机机身，固定机构，连接器和飞机手臂。 固定机构固定在飞机主体上，飞机臂的一端铰接在固定机构上，固定机构上设有第一安装孔，飞机臂上设有第二安装孔。 当飞机臂处于折叠状态时，连接器的一端通过第一紧固件可拆卸地连接到固定机构，而另一端通过第二紧固件可拆卸地连接到飞机臂，将固定机构保持在第一位置 与飞机胳膊的角度。 当飞机臂处于工作状态时，第三紧固件穿过第一安装孔和第二安装孔两者，以使固定机构固定连接到飞机臂并与飞机臂保持第二角度。

    Fluggerät
    10.
    发明公开
    Fluggerät 审中-公开

    公开(公告)号：EP2733070A2

    公开(公告)日：2014-05-21

    申请号：EP13005423.2

    申请日：2013-11-19

    申请人： Airvionic UG

    发明人： Frank Fox

    IPC分类号： B64C27/20 ,  B64C39/02

    CPC分类号： B64C27/20 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108

    摘要： Es wird ein Fluggerät (1) mit einem Grundkörper (2) vorgeschlagen, an dem mehrere Antriebseinheiten (3, 4, 4A) vorgesehen sind, wobei zumindest vier lasttragende Antriebseinheiten (3) zur horizontalen Ausrichtung und zur im Wesentlichen vertikalen Beschleunigung des Grundkörpers (2) vorgesehen sind, wobei zumindest zwei den Grundkörper (2) im Wesentlichen horizontal beschleunigende Antriebseinheiten (4, 4A) vorgesehen sind und wobei die horizontal beschleunigenden Antriebseinheiten (4, 4A) und die lasttragenden Antriebseinheiten (3) bestimmten symmetrisch Anordnungen unterliegen, um dem Fluggerät ein höchst Maß an Flugstabilität zu gewähr-leisten.

    摘要翻译： 飞机（1）具有基体（2），在该基体上夹持有三个垂直作用的主驱动单元（3），夹紧平面。 平面相对于重力方向布置在相同高度或高于飞机重心（SP）的高度。 提供两个水平作用的二次驱动单元（4），其主动力传递点布置在平面的下方。 次级驱动单元的力传递点夹住另一平面，并且重心布置在后平面中或与之相邻。