| 摘要 |
<p>A turbine engine component (90) has an airfoil portion (110) having a pressure side (116), a suction side (118), a leading edge (112), a trailing edge (114), and a tip (134). The component (90) further has a first cooling microcircuit (100) embedded in a pressure side wall, a second cooling microcircuit (102) embedded in a suction side wall, and a system for cooling the tip comprising a first tip cooling microcircuit receiving cooling fluid from the first cooling microcircuit (100) and a second tip cooling microcircuit receiving cooling fluid from the second cooling microcircuit (102).</p> |
