首页> 外国专利> movable leading edge flap of an aircraft canopy main wing, and an aircraft canopy main wing

movable leading edge flap of an aircraft canopy main wing, and an aircraft canopy main wing

机译:飞机机盖主翼的可移动前缘襟翼和飞机机盖主翼

摘要

MOBILE FLIGHT ATTACK MOVING FLAP OF AN AIRCRAFT MAIL, AND THE MAIN AIRCRAFT MAIL WING The invention relates to a leading edge movable flap (16) of an aircraft main wing (1), said flap comprising an aerodynamic liner (18) having a bird impact sensitive front zone (24), as well as a backing (28) integral with the aerodynamic liner (18), the flap also comprising a plurality of ribs (34) spaced along a leading leading edge (X ') direction. According to the invention, the flap also comprises, between two directly consecutive ribs, a single rigid avian trajectory wall (42) fixedly fixed to the linings (18,28). On the other hand, in a section taken in a plane orthogonal to the direction (X '), the wall (42) forms with a geometric rope (26) of the flap an angle (244 1) of a value less than 45 198 .
机译:飞机机翼的机动飞行攻击移动襟翼和主飞机机翼本发明涉及飞机主翼(1)的前缘可移动襟翼(16),所述襟翼包括具有鸟类撞击的空气动力学内衬(18)。敏感的前部区域(24)以及与气动衬套(18)一体的背衬(28),襟翼还包括沿前缘(X')方向间隔开的多个肋(34)。根据本发明,襟翼在两个直接连续的肋之间还包括固定地固定到衬里(18,28)上的单个刚性禽弹道壁(42)。另一方面,在垂直于方向(X′)的平面中截取的截面中,壁(42)与襟翼的几何绳索(26)形成的角度(<244> 1)小于45 <198>。

著录项

  • 公开/公告号BRPI0507038A

    专利类型

  • 公开/公告日2007-06-05

    原文格式PDF

  • 申请/专利权人 SONACA S.A;

    申请/专利号BR2005PI07038

  • 发明设计人 CHISTIAN OVERBERGH;MICHEL HAUTECOEUR;

    申请日2005-01-20

  • 分类号B64C9/24;

  • 国家 BR

  • 入库时间 2022-08-21 20:59:21

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