| 发明名称 |
TURBOMACHINE BLADE TIP SHROUD |
| 摘要 |
Embodiments of the present disclosure are directed toward systems including a turbomachine blade tip shroud having a pressure side portion and a suction side portion. The pressure side portion and the suction side portion are divided by a mean camber line of a turbomachine blade, and the pressure side portion has a greater surface area than the suction side portion.
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| 申请公布号 |
US2013189106(A1) |
申请公布日期 |
2013.07.25 |
| 申请号 |
US201213355436 |
申请日期 |
2012.01.20 |
| 申请人 |
CHOUHAN ROHIT;SONI SUMEET;SMITH PAUL KENDALL;JAYANA SRINIVASA GOVARDHAN;PIERRE SYLVAIN;BOMMANAKATTE HARISH;VIJAYAN SANTHOSH KUMAR;KAREFF SPENCER AARON;GENERAL ELECTRIC COMPANY |
发明人 |
CHOUHAN ROHIT;SONI SUMEET;SMITH PAUL KENDALL;JAYANA SRINIVASA GOVARDHAN;PIERRE SYLVAIN;BOMMANAKATTE HARISH;VIJAYAN SANTHOSH KUMAR;KAREFF SPENCER AARON |
| 分类号 |
F01D5/22 |
主分类号 |
F01D5/22 |
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