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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
CPC分类号: B64D15/163 , B64C39/028 , B64C2201/028 , B64C2201/104 , B64C2201/165
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。
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公开(公告)号:US20070029440A1
公开(公告)日:2007-02-08
申请号:US10573570
申请日:2004-07-22
CPC分类号: B64D15/163 , B64C39/028 , B64C2201/028 , B64C2201/104 , B64C2201/165
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。
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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
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。
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公开(公告)号:US08186616B2
公开(公告)日:2012-05-29
申请号:US11305345
申请日:2005-12-19
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。
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