| 摘要 |
A turbine blade (100) with a cooling arrangement is disclosed. The turbine blade (100) includes at least one supply chamber (202, 202') and at least one impingement cavity (CI, CI'). The supply chamber (202, 202') includes multiple impingement channels (204) configured to direct a cooling fluid from within the supply chamber (202, 202') to the impingement cavity (CI, CI'). The supply chamber (202, 202') also includes one or more collector channels (206) such that the cooling fluid from the impingement cavity (CI, CI') is directed to a collector cavity (CC) within the turbine blade (100). |
