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    HOVERING AERIAL VEHICLE AND METHOD OF FLYING SAME
    2.
    发明公开
    HOVERING AERIAL VEHICLE AND METHOD OF FLYING SAME 审中-公开

    公开(公告)号：EP3209560A4

    公开(公告)日：2017-11-29

    申请号：EP16861722

    申请日：2016-11-02

    申请人： ISRAEL AEROSPACE IND LTD

    发明人： MAROM DANIEL

    IPC分类号： B64C39/02 ,  B64D1/02

    CPC分类号： B64D1/12 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/128 ,  B64D1/02 ,  B64D1/08 ,  B64D1/10 ,  B64D1/22

    摘要： A hovering aerial vehicle is provided, comprising an airborne unit and an auxiliary unit. The airborne unit is configured to carry the auxiliary unit during flight and comprises a flight system configured to facilitate providing aerodynamic lift to facilitate hovering of the vehicle. The auxiliary unit comprises an electrical power source in electrical communication with the flight system to provide electrical power for its operation. The hovering aerial vehicle further comprises a decoupling system configured to facilitate selectively switching the vehicle between a detached configuration thereof wherein the airborne and auxiliary units are remote from each other, and an attached configuration thereof wherein the airborne and auxiliary units are secured to one another, and to maintain the electrical communication when the vehicle is in its detached configuration.

    PACKAGING FOR A PARACHUTE
    3.
    发明公开
    PACKAGING FOR A PARACHUTE 审中-公开
    包装为PARACHUTE

    公开(公告)号：EP3221218A1

    公开(公告)日：2017-09-27

    申请号：EP15800893.8

    申请日：2015-11-17

    申请人： Strategic Support Limited

    发明人： COOK, Jonathan ,  COOK, Michael ,  COOK, George Michael

    IPC分类号： B64D17/46 ,  B64D17/50 ,  B64D1/08

    CPC分类号： B64D17/46 ,  B64D1/08 ,  B64D17/50

    摘要： A parachute arrangement comprising a parachute having a canopy, a plurality of shroud lines coupled to the canopy, and a plurality of connectors (23) coupled to the shroud lines for attachment to a load; and a packaging (10) for the parachute, the packaging comprising an enclosure formed of a web material, wherein each of the shroud lines and/or connectors is engaged with the enclosure to thereby maintain the connectors in a spaced-apart arrangement for attachment to the load.

    摘要翻译： 一种降落伞装置，包括具有顶篷21的降落伞，联接到顶篷22的多个罩线以及联接到罩线以连接到负载30的多个连接器23; 以及用于降落伞的包装10，所述包装包括由网状材料形成的外壳，其中每个外壳管线和/或连接器与外壳接合，从而将所述连接器保持为间隔布置以连接至负载 。 护罩线与外壳之间的接合可以是粘合附件或机械附件，例如缝合。 外壳可以隐藏连接器（图1）并且可以包括用于撕开网状材料以暴露连接器的装置（13）（图2）。 降落伞包装可以包括一次性可生物降解材料。

    PAYLOAD SHROUD FOR AIR VEHICLE
    4.
    发明公开
    PAYLOAD SHROUD FOR AIR VEHICLE 审中-公开
    NUTZLASTUMMANTELUNGFÜRLUFTFAHRZEUG

    公开(公告)号：EP3094554A4

    公开(公告)日：2017-09-06

    申请号：EP14876435

    申请日：2014-10-08

    申请人： AAI CORP

    发明人： ATZERT MONICA ,  WALLACE JASON ,  HURN ROBERT ,  DEARDORFF DOUG ,  ZELENY TERRY

    IPC分类号： B64D1/08 ,  B64C1/36 ,  B64C7/00 ,  B64C39/02

    CPC分类号： B64C7/00 ,  B64C1/36 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64D1/08 ,  B64D47/08

    摘要： A UAV includes a body. The body defines a payload opening 14. The payload opening is circular, but any shape may be used. A payload of the UAV is arranged in the payload opening. The payload may be a camera, sensors, a package, etc. A payload shroud may be installed which prohibits or reduced ingress of foreign material via payload opening. A payload shroud may include a diverter. The diverter may act as a barrier wall preventing the water or debris from entering the body of the UAV. The diverter should fit flush with the payload opening in the body of the UAV.

    摘要翻译： 一架无人机包括一个机体。 主体限定有效载荷开口14.有效载荷开口是圆形的，但是可以使用任何形状。 无人机的有效载荷布置在有效载荷开口中。 有效载荷可以是照相机，传感器，包装等。可以安装有效载荷遮板，其阻止或减少通过有效载荷开口进入的异物。 有效载荷罩可以包括转向器。 分流器可以充当隔离墙，防止水或碎屑进入无人机的主体。 分流器应与无人机主体中的有效载荷开口齐平。

    HOVERING AERIAL VEHICLE AND METHOD OF FLYING SAME
    5.
    发明公开
    HOVERING AERIAL VEHICLE AND METHOD OF FLYING SAME 审中-公开
    驾驶空中车辆和飞行的方法

    公开(公告)号：EP3209560A1

    公开(公告)日：2017-08-30

    申请号：EP16861722.3

    申请日：2016-11-02

    申请人： Israel Aerospace Industries Ltd.

    发明人： MAROM, Daniel

    IPC分类号： B64C39/02 ,  B64D1/02

    CPC分类号： B64D1/12 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108 ,  B64C2201/128 ,  B64D1/02 ,  B64D1/08 ,  B64D1/10 ,  B64D1/22

    摘要： A hovering aerial vehicle is provided, comprising an airborne unit and an auxiliary unit. The airborne unit is configured to carry the auxiliary unit during flight and comprises a flight system configured to facilitate providing aerodynamic lift to facilitate hovering of the vehicle. The auxiliary unit comprises an electrical power source in electrical communication with the flight system to provide electrical power for its operation. The hovering aerial vehicle further comprises a decoupling system configured to facilitate selectively switching the vehicle between a detached configuration thereof wherein the airborne and auxiliary units are remote from each other, and an attached configuration thereof wherein the airborne and auxiliary units are secured to one another, and to maintain the electrical communication when the vehicle is in its detached configuration.

    摘要翻译： 提供悬停式飞行器，其包括机载单元和辅助单元。 机载单元被配置成在飞行期间携带辅助单元并且包括飞行系统，该飞行系统被配置为便于提供空气动力学升力以促进车辆的悬停。 辅助单元包括与飞行系统电通信的电源，以为其操作提供电力。 悬停式飞行器进一步包括解耦系统，该解耦系统被构造成便于在其中机载和辅助单元彼此远离的分离配置与其中机载单元和辅助单元彼此固定的附接配置之间选择性地切换车辆， 并且在车辆处于分离配置时保持电气通信。

    AIRCRAFT PYLON
    8.
    发明公开
    AIRCRAFT PYLON 审中-公开
    FLUGZEUGPYLON

    公开(公告)号：EP3122628A1

    公开(公告)日：2017-02-01

    申请号：EP15769963.8

    申请日：2015-03-22

    申请人： Israel Aerospace Industries Ltd.

    发明人： HERZIG, Yoav

    IPC分类号： B64D1/08 ,  B64D1/04

    CPC分类号： B64D1/08 ,  B64C1/1415 ,  B64D1/04 ,  B64D27/26

    摘要： An aircraft pylon comprising a body for mounting to an aircraft, a suspension mechanism mounted on said body and being configured for attaching thereto a payload, and a moving door configured for selectively covering and uncovering at least a part of said suspension mechanism

    摘要翻译： 一种包括用于安装到飞行器的主体的飞机塔架，安装在所述主体上并被构造成用于附接到其上的悬挂机构，以及移动门，其构造成用于选择性地覆盖和露出所述悬架机构的至少一部分

    WIND PARAMETER INDICATION
    9.
    发明公开
    WIND PARAMETER INDICATION 有权
    WIND参数显示屏

    公开(公告)号：EP2812719A4

    公开(公告)日：2015-08-05

    申请号：EP13747169

    申请日：2013-01-14

    申请人： VENTUS PRODUCT DEV & CONSULTING LTD

    发明人： HALFON ITZHAK ,  GALIM ITAY ,  GLOZMAN YANIV

    IPC分类号： G01S1/00 ,  B64D17/00 ,  G01S5/00 ,  G01S19/15 ,  G01W1/00

    CPC分类号： G01W1/02 ,  B64D1/08 ,  B64D17/00 ,  B64D45/00 ,  G01C5/00 ,  G01C17/00 ,  G01F1/76 ,  G01S7/003 ,  G01S17/023 ,  G01S17/88 ,  G01S17/95 ,  G01S19/14 ,  G01S19/15 ,  G01W1/08 ,  Y02A90/19

    摘要： Wind parameter indication device and method for providing an indication of wind speed and wind direction. The device is deployed along an aerial trajectory toward a ground surface, such as after being ejected from an aircraft in flight. The device includes an anemometer, an altimeter, a compass, a processor and a transmitter. The anemometer obtains local wind speed and local wind direction measurements along the trajectory. The altimeter obtains altitude measurements along the trajectory. The compass obtains direction measurements along the trajectory. The device may further include an accelerometer, for obtaining acceleration measurements along the trajectory. The processor determines a wind speed value and a wind direction value associated with a predetermined altitude of the device. The transmitter transmits the determined wind speed value and wind direction value to a remotely located receiver. The device may further include a stabilizing decelerator to stabilize and decelerate the device along the trajectory.