Gekühlte Gasturbinenschaufel und deren Herstellungsmethode
摘要
An airfoil (40) for use in a gas turbine engine includes a pressure side (42) and a suction side (44) joined at a trailing edge wall (60) that defines a trailing edge (48). The airfoil (40) includes at least one cooling hole (68) extending through the trailing edge wall (60) so as to pass cooling fluid from the pressure side (42) of the airfoil (40) to the suction side (44). <IMAGE>
申请公布号
DE60027390(D1)
申请公布日期
2006.05.24
申请号
DE2000627390
申请日期
2000.12.08
申请人
GENERAL ELECTRIC CO., SCHENECTADY
发明人
TSAI, GENE CHEN-FU;TUNG, SUNG;FLAHERTY, TERENCE CARROLL;MANNING, ROBERT FRANCIS