发明名称 |
TURBINE ENGINE AND AERODYNAMIC ELEMENT OF TURBINE ENGINE |
摘要 |
PROBLEM TO BE SOLVED: To provide a turbine engine.SOLUTION: A turbine engine includes an aerodynamic element disposed to aerodynamically interact with a flow of working fluid and contour features disposed on the aerodynamic element in alignment in at least one dimension. The contour features are proximate to one another and configured to encourage counter-rotating vortex flow generation oriented substantially perpendicularly with respect to a main flow direction along the aerodynamic element. |
申请公布号 |
JP2013257137(A) |
申请公布日期 |
2013.12.26 |
申请号 |
JP20130119357 |
申请日期 |
2013.06.06 |
申请人 |
GENERAL ELECTRIC CO <GE> |
发明人 |
SPARKS SCOTT MATTHEW |
分类号 |
F23R3/02;F01D9/02;F01D25/30;F02C3/05;F02C7/00;F02K1/78;F15D1/12 |
主分类号 |
F23R3/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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