Aircraft configuration for micro and mini UAV
    1.
    发明授权
    Aircraft configuration for micro and mini UAV 有权
    微型无人机的飞机配置

    公开(公告)号:US08123160B2

    公开(公告)日:2012-02-28

    申请号:US10573570

    申请日:2004-07-22

    IPC分类号: B64C39/12

    摘要: An aircraft arrangement for Mini or Micro UAV comprising a fore wing (14) and an aft wing (12) in tandem closed-coupled arrangement. The aft wing (12) has side panels (18) and control surfaces (19), and tapered planform with positive sweep, while the fore wing (14) has non-positive trailing edge sweep. The fore wing (14) and the aft wing (12) are disposed at different height, and the aircraft arrangement has no other wings or tail arrangements.

    摘要翻译: 一种用于迷你或微型无人机的飞行器装置,其包括串联闭合联接装置的前翼(14)和后翼(12)。 后翼(12)具有侧板(18)和控制表面(19),并且具有正扫掠的锥形平面,而前翼(14)具有非正的后缘扫掠。 前翼(14)和后翼(12)设置在不同的高度,并且飞行器装置没有其他翼或尾翼装置。

    Aircraft configuration for micro and mini uav
    2.
    发明申请
    Aircraft configuration for micro and mini uav 有权
    飞机配置微型和迷你型

    公开(公告)号:US20070029440A1

    公开(公告)日:2007-02-08

    申请号:US10573570

    申请日:2004-07-22

    IPC分类号: B64C1/00 B64C13/20

    摘要: An aircraft arrangement for Mini or Micro UAV comprising a fore wing (14) and an aft wing (12) in tandem closed-coupled arrangement. The aft wing (12) has side panels (18) and control surfaces (19), and tapered planform with positive sweep, while the fore wing (14) has non-positive trailing edge sweep. The fore wing (14) and the aft wing (12) are disposed at different height, and the aircraft arrangement has no other wings or tail arrangements.

    摘要翻译: 一种用于迷你或微型无人机的飞行器装置,其包括串联闭合联接装置的前翼(14)和后翼(12)。 后翼(12)具有侧板(18)和控制表面(19),并且具有正扫掠的锥形平面,而前翼(14)具有非正的后缘扫掠。 前翼(14)和后翼(12)设置在不同的高度,并且飞行器装置没有其他翼或尾翼装置。

    Hybrid transonic-subsonic aerofoils
    3.
    发明申请
    Hybrid transonic-subsonic aerofoils 有权
    混合超音速亚音速翼型

    公开(公告)号:US20060226283A1

    公开(公告)日:2006-10-12

    申请号:US11305345

    申请日:2005-12-19

    IPC分类号: B64C3/14

    CPC分类号: B64C3/14 Y02T50/12

    摘要: A hybrid transonic-subsonic airfoil is provided that combines subsonic and transonic features for achieving simultaneously acceptable aerodynamic characteristics at low subsonic and high transonic Mach numbers.

    摘要翻译: 提供了混合的跨音速亚音速翼型,其组合亚音速和跨音速特征,以在低亚音速和高跨音速马赫数下实现同时可接受的空气动力特性。