发明名称 SHAPED RIM CAVITY WING SURFACE
摘要 <p>A shaped rim cavity wing includes an upper surface and a lower surface. The lower surface has a geometric shape to control the separation of airflow as it passes around the lower surface to the top surface. A point of maximum extent defines the boundary between the upper surface and the lower surface, wherein the point of maximum extent defines a corner that that separates airflow from the shaped rim cavity rim and creates a flow re-circulation adjacent to the top surface of the shaped rim cavity wing.</p>
申请公布号 WO2013166284(A1) 申请公布日期 2013.11.07
申请号 WO2013US39261 申请日期 2013.05.02
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 GROVER, ERIC, A.
分类号 F01D5/00;F01D5/12;F01D5/30;F02C3/00;F02C7/00 主分类号 F01D5/00
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