VARIABLE GEOMETRY WING
    1.
    发明公开
    VARIABLE GEOMETRY WING 审中-公开
    FLÜGELMIT VARIABLER GEOMETRIE

    公开(公告)号:EP2895388A1

    公开(公告)日:2015-07-22

    申请号:EP13762851.7

    申请日:2013-09-17

    IPC分类号: B64C3/40 B64C3/54 B64C33/02

    摘要: Embodiments of the present invention relate to an adaptable wing having a variable geometry for influencing aerodynamic performance, the wing comprising a jointed leading edge having a main pivot, and a wrist joint, with a wing arm therebetween, 5 and a distal wing hand depending from the wrist joint; the wing being reciprocally actuable, via the main pivot and wrist joint, between a first state having an extended wing planform and a second state having a tucked wing planform.

    摘要翻译: 本发明的实施例涉及一种具有可变几何形状以用于影响空气动力学性能的适应翼,所述机翼包括具有主枢轴的接合前缘和在其间具有翼臂的腕关节5,并且远侧翼手从 腕关节; 所述机翼通过所述主枢轴和腕关节在具有延伸机翼平面图的第一状态和具有卷起的机翼平面图的第二状态之间可往复地起动。

    UNMANNED VEHICLE
    4.
    发明公开
    UNMANNED VEHICLE 审中-公开

    公开(公告)号:EP3494048A1

    公开(公告)日:2019-06-12

    申请号:EP17748795.6

    申请日:2017-08-07

    摘要: An unmanned vehicle, such as a UAV, comprises a main body portion 306, a neck portion (418 fig 4) and a head portion 318. The main body of the vehicle includes control surfaces and/or control actuators which are able to influence vehicle movement. The vehicle includes flight control sensors that are carried in the head of the vehicle which is stabilised relative to the vehicle body. The stabilized flight control sensors experience less noise or generate less noise as a consequence of vehicle manoeuvring.