An airfoil cooling circuit includes an impingement cooling circuit and a serpentine cooling circuit. An airfoil for use in a gas turbine engine having a cooling circuit which includes an impingement cooling circuit and a serpentine cooling circuit
申请公布号
WO2013101761(A1)
申请公布日期
2013.07.04
申请号
WO2012US71385
申请日期
2012.12.21
申请人
GENERAL ELECTRIC COMPANY
发明人
BUHLER, JARED, PETER;ALLEN, MARSHALL, SCOTT;DEMERS, DANIEL, EDWARD;MANNING, ROBERT, FRANCIS
