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
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