首页> 外国专利> Progressive aerofoil trailing edge for aircraft has flap, which can be adjusted both downward and upward by positive and by negative flap deflections respectively whereby aerofoil profile is closed on top side by sealing flap

Progressive aerofoil trailing edge for aircraft has flap, which can be adjusted both downward and upward by positive and by negative flap deflections respectively whereby aerofoil profile is closed on top side by sealing flap

机译:飞机的渐进式翼型后缘具有襟翼,可分别通过正向和负向襟翼偏转向下和向上调节,从而通过密封襟翼在顶部关闭翼型轮廓

摘要

Progressive aerofoil trailing edge has a flap (4), which can be adjusted both downward and upward by a positive and by negative flap deflections respectively. The aerofoil profile is closed on the top side by the sealing flap (7) and on the lower side by the ventilation flap (5) for using the flap as control flap with adjustments of the flap between negative and small positive flap deflections. The ventilating flap releases a flow from the lower side of the aerofoil (1) to the upper side of the flap and the sealing flap is removed from the upper side of the flap at a predetermined gap for releasing a downstream flow for using the flap as lift heightening flap with the adjustment of the flap between small positive and large positive flap deflection of the ventilation flap.
机译:渐进式翼型后缘有一个襟翼(4),可以分别通过正向和负向襟翼偏转向下和向上调节。翼型轮廓在上侧通过密封风门(7)封闭,在下侧通过通气风门(5)封闭,以将风门用作控制风门,并在风门的负向和小正向偏转之间进行调整。通风阀瓣从翼型件(1)的下侧释放到阀瓣的上侧,并且将密封阀瓣从阀瓣的上侧以预定间隙移开,以释放下游流量,以便将阀瓣用作在通风阀的小正向和大正向偏转之间调节风门,从而提升高度。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号