首页> 外国专利> Airfoil trailing edge device for noise reduction

Airfoil trailing edge device for noise reduction

机译:翼型后缘装置,用于降低噪音

摘要

A ridge (28) mounted or defined along a trailing edge (22) of an airfoil (20) for noise reduction. Sides (32, 34) of the ridge converge from respective suction and pressure sides (46, 48) of the trailing edge to a peak (30) of the ridge pointing aft. The sides of the ridge may be concave. The ridge may be hollow (42) or have a core (43) of a sound-absorbing material. The sides of the ridge may be perforated (44A, 44B) for pressure equalization across the ridge. The ridge may be covered with bristles (56) or be defined by the tips (58) of bristles (56A, 56B) of varying length. The peak of the ridge and/or at least one corner (64, 66) of the ridge and/or of the trailing edge (46, 48) may be serrated.
机译:沿机翼(20)的后缘(22)安装或限定的脊(28),用于降低噪声。脊的侧面(32、34)从后缘的相应的吸力和压力侧(46、48)收敛到脊的指向后方的峰(30)。脊的侧面可以是凹的。脊可以是中空的(42)或具有吸音材料的芯(43)。脊的侧面可以被穿孔(44A,44B),以使整个脊上的压力均衡。脊可以被刚毛(56)覆盖,或者由长度不同的刚毛(56A,56B)的尖端(58)限定。脊的峰和/或脊和/或后缘(46、48)的至少一个角(64、66)可以是锯齿状的。

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