| 摘要 |
<p>The present invention relates to a sealing system (1) for a bearing in a high speed small gas turbine, which system is designed to prevent the air and the oil from passing from a area to another area and to enable directing them to the desired area. The mentioned sealing system (1) comprises a seal ring (2) mounted to the turbine shaft and having holes around the circumference, a ring (3) surrounding seal ring (2) and having holes around the circumference, and a cover ring (4) surrounding seal ring (2) and ring (3) and having holes around the circumference.</p> |
