发明申请
US20130104567A1 METHOD AND APPARATUS FOR COOLING GAS TURBINE ROTOR BLADES 审中-公开
用于冷却气体涡轮转子叶片的方法和装置

METHOD AND APPARATUS FOR COOLING GAS TURBINE ROTOR BLADES
摘要:
An airfoil for a gas turbine engine is provided that includes a first sidewall and a second sidewall coupled together at a leading edge and a trailing edge, such that a cavity is defined therebetween. A central plenum and an impingement chamber are defined within the cavity. The central plenum channels cooling fluid to the impingement chamber where cooling fluid impinges on the sidewalls. Cooling fluid is discharged from the impingement chamber via film cooling holes.
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