发明名称 HOLLOW TURBINE BLADE
摘要 A hollow cooled gas turbine blade is made by forming an insert with a hollow airfoil and a hollow root portion and with lateral cooling air passages extending through the wall of the airfoil and positioning the insert in a hollow main blade having an airfoil portion and a notch in the root to receive the root portion of the insert with both root portions having aligned serrations on opposite surfaces for supporting the blade and the insert in a turbine disk.
申请公布号 US3697192(A) 申请公布日期 1972.10.10
申请号 USD3697192 申请日期 1970.05.07
申请人 UNITED AIRCRAFT CORP. 发明人 CHARLES W. HAYES
分类号 B23P15/02;F01D5/18;(IPC1-7):F01D5/08 主分类号 B23P15/02
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