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SWEPT-WING BOX-TYPE AIRCRAFT WITH HIGH FLIGHT STATIC STABILITY

机译:高度稳定的飞翼箱式飞机

摘要

The box-shaped aircraft for having swept-back wing includes fuselage (1) and jacking system by forming the wings (2,3) of two basic horizontals, one of them has a sweepback angle, and another has a negative sweep angle, is the end extended through two vertical alar parts (4,5) positioned at spaced apart from each other connect perpendicular to principal joint face. The fuselage that wing front wing sweepback (2) bottom extends, wing are negative sweep empennage (3). Extend above empennage (3), which there is continuity (1) and fuselage (1) to be equipped with a pair of of fin (6a, 6b) in its tail portion. The air force (7) of fin empennage and fuselage limits channel, is substantially flat (1a) along these fuselage surfaces.
机译:具有后掠式机翼的箱形飞机包括机身(1)和顶升系统,该系统通过形成两个基本水平翼的机翼(2,3)形成,其中一个具有后掠角,另一个具有负后掠角,该端部延伸穿过彼此间隔开的两个垂直的翼部(4,5),并垂直于主关节面连接。机翼前翼后掠(2)底部延伸的机身,机翼为负后掠尾翼(3)。延伸到尾翼(3)上方,尾翼具有连续性(1)和机身(1),尾翼上将配备一对散热片(6a,6b)。翅片尾翼和机身限制通道的空气力(7)沿着这些机身表面基本上是平坦的(1a)。

著录项

  • 公开/公告号EP1597145A1

    专利类型

  • 公开/公告日2005-11-23

    原文格式PDF

  • 申请/专利权人 FREDIANI ALDO;

    申请/专利号EP20040712662

  • 发明设计人 FREDIANI ALDO;

    申请日2004-02-19

  • 分类号B64C39/06;

  • 国家 EP

  • 入库时间 2022-08-21 21:32:51

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