首页> 外国专利> Rotorcraft and a centrifugal compressor equipped with this rotorcraft

Rotorcraft and a centrifugal compressor equipped with this rotorcraft

机译:旋翼飞行器和一个配备此旋翼飞行器的离心式压缩机

摘要

The rotor includes a hub and a plurality of blades provided on the hub, and each of the plurality of blades has a negative pressure surface, a pressure surface, a front edge, a trailing edge, a tip side edge, and a hub side edge. The negative pressure surface is convex toward the trailing edge so as to move the trailing edge toward the pressure plane in the first region, which is a part of the region connected to the trailing edge in the blade height direction. Includes the first curved surface portion curved in a shape.
机译:转子包括毂和设置在轮毂上的多个叶片,并且多个叶片中的每一个具有负压表面,压力表面,前边缘,后缘,尖端侧边缘和轮毂侧边缘。负压表面朝向后缘凸出,以便将后缘朝向第一区域中的压力平面移动,这是连接到叶片高度方向上的后缘的区域的一部分。包括弯曲形状的第一曲面部分。

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