| 摘要 |
The present invention relates to a direct drive type cooling structure for a turbo blower and, more specifically, to a direct drive type cooling structure for a turbo blower, which improves cooling efficiency through multiple holes when a cooling fan is operated by forming multiple holes to cool a stator and multiple holes to cool a coil part, a bearing housing, and a rotor along the outer diameter of a motor casing, thereby providing a thermal balance. |
