发明名称 Vortex generating flow passage design for increased film cooling effectiveness
摘要 It is an object of the invention to provide a film cooling apparatus of increased effectiveness and efficiency. In accordance with the invention, a cooling fluid is injected into a hot flowing gas through a passageway in a wall which contains and is subject to the hot gas. The passageway is slanted in a downstream direction at an acute angle to the wall. A cusp shape is provided in the passageway to generate vortices in the injected cooling fluid thereby reducing the energy extracted from the hot gas for that purpose. The cusp shape increases both film cooling effectiveness and wall area coverage. The cusp may be at either the downstream or upstream side of the passageway, the former substantially eliminating flow separation of the cooling fluid from the wall immediately downstream of the passageway.
申请公布号 US4529358(A) 申请公布日期 1985.07.16
申请号 US19840580419 申请日期 1984.02.15
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 PAPELL, S. STEPHEN
分类号 B64C1/40;B64G1/58;F01D5/18;F02K1/82;F23R3/06;(IPC1-7):F01D5/18 主分类号 B64C1/40
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