| 摘要 |
PROBLEM TO BE SOLVED: To provide a cooling microcircuit for generating a substantially uniform jet of a cooling fluid flowing from the slot of the microcircuit. SOLUTION: This cooling microcircuit is used for turbine engine parts such as a turbine blade having an air foil part. The cooling microcircuit comprises at least one inlet slot for introducing a refrigerant flow into the cooling microcircuit, fluid outlet slots for distributing the film of a refrigerant on the air foil part, and a structure for substantially preventing one jet of the refrigerant flowing through one fluid outlet slot from applying an excessive force to the second jet of the refrigerant flowing out through the one fluid outlet slot. COPYRIGHT: (C)2008,JPO&INPIT
|
