首页> 外国专利> Autogyro rotor blade generating lift by rotation

Autogyro rotor blade generating lift by rotation

机译:通过旋转产生升降机的Autogyro转子刀片

摘要

The present invention includes a base-side internal profile region (9) having a first profile (21c) and a distal-side main profile region (21e) different from the first profile (21c) ( 10) and the profile depth curve (22) monotonically decreasing in the longitudinal direction of the auto gyro rotor blade (1) from the region of the blade base (2) in the direction of the blade tip (3) to generate lift. The present invention relates to an auto gyro rotor blade. According to the invention, the autogyro rotor blade (1) has a twist with a twist curve (23) that decreases monotonically from the region of the blade base (2) in the direction of the blade tip (3). 23) has a variable slope in the internal profile region (9) and / or the main profile region (10), the torsion curve (23) is concavely curved in this region (9, 10). [Selection] Figure 2
机译:本发明包括基部侧内部轮廓区域(9),其具有与第一轮廓(21c)(10)和曲线深度曲线不同的第一轮廓(21c)和远端侧主轮廓区域(21e)(22)(22 )在叶片尖端(3)的方向上从叶片底座(2)的区域中单调地减小自动陀螺旋转叶片(1)的纵向,以产生升力。本发明涉及一种自动陀螺转子叶片。根据本发明,自动扬声器转子叶片(1)具有扭曲曲线(23)的扭曲,该扭曲曲线(23)在叶片尖端(3)的方向上从叶片底座(2)的区域单调地减小。图23)23)在内部轮廓区域(9)和/或主轮廓区域(10)中具有可变斜率,扭转曲线(23)在该区域(9,10)中铰接弯曲。 [选择]图2

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